Patent Publication Number: US-6990867-B2

Title: Force detection device

Description:
BACKGROUND OF THE INVENTION 
   This invention concerns a force detection device, and particularly concerns a force detection device suited for measuring forces and moments independently. 
   Various types of force detection devices are used for controlling motions of robots and industrial machines. Compact force detection devices are also incorporated as man-machine interfaces of input devices for electronic equipment. In order to achieve size and cost reduction, a force detection device used in such an application is required to be as simple in structure as possible and is required to detect forces of the respective coordinate axes in three-dimensional space independently each other. 
   Multi-axis force detection devices that are presently used can be classified into two types, that is, a type, with which specific directional components of a force that acts on a three-dimensional structure are detected as displacements that arise at a specific part, and a type, with which the directional components are detected as mechanical strains that arise at a specific part. A capacitance element type force detection device is a representative device of the former displacement detection type, and with this device, a capacitance element is constituted by a pair of electrodes and the displacement arising at one of the electrodes due to an acting force is detected based on a static capacitance value of the capacitance element. Such a static capacitance type force detection device is disclosed, for example, in Japanese Unexamined Patent Application Publication No. 5-215627/1993. Meanwhile, a strain gauge type force detection device is a representative device of the latter strain detection type, and with this device, a mechanical strain that arises as a result of an acting force is detected as a change of gauge resistance or other form of electrical resistance. Such a strain gauge type force detection device is disclosed, for example, in Japanese Unexamined Patent Application Publication No. 61-292029/1986. 
   In general, the objects of detection by a force detection device are force components in the direction of predetermined coordinate axes and moment components about the predetermined coordinate axes. In the case where an XYZ three-dimensional coordinate system is defined in three-dimensional space, the objects of detection will be the six components of the force components Fx, Fy, and Fz in the directions of the respective coordinate axes and the moment components Mx, My, and Mz about the respective coordinate axes. However priorly, regardless of the displacement detection type or the strain detection type, a force detection device of a considerably complex three-dimensional structure was required to detect the respective components independent of each other. 
   SUMMARY OF THE INVENTION 
   Thus an object of this invention is to provide a force detection device that can detect forces and moments in a distinguished manner by means of a structure that is as simple as possible. 
   (1) The first feature of the invention resides in a force detection device comprising: 
   a base plate, having a top surface parallel to an XY plane in an XYZ three-dimensional coordinate system having an X-axis, a Y-axis and a X-axis; 
   a first displaceable plate, positioned along a plane intersecting a positive part of the X-axis and supported on the base plate in a displaceable manner; 
   a second displaceable plate, positioned along a plane intersecting a negative part of the X-axis and supported on the base plate in a displaceable manner; 
   a first fixed plate, positioned between the Z-axis and the first displaceable plate and fixed onto the base plate; 
   a second fixed plate, positioned between the Z-axis and the second displaceable plate and fixed onto the base plate; 
   a fixed top plate, positioned along a plane spanning across a vicinity of an upper edge of the first fixed plate and a vicinity of an upper edge of the second fixed plate; 
   a displaceable top plate, positioned above the fixed top plate, supported so as to be displaceable with respect to the base plate, and transmitting, to an upper edge of the first displaceable plate and an upper edge of the second displaceable plate, a force in a direction along the XY plane; 
   a force receiving member, positioned on the Z-axis above the displaceable top plate in order to receive a force that is to be detected; 
   a connecting member, positioned along the Z-axis in order to connect the force receiving member and the displaceable top plate; 
   a first X-axis distance sensor, detecting a distance between the first displaceable plate and the first fixed plate; 
   a second X-axis distance sensor, detecting a distance between the second displaceable plate and the second fixed plate; 
   an inclination degree sensor, detecting an inclination degree of the displaceable top plate with respect to the fixed top plate; and 
   a detection processing unit, detecting a force Fx in the X-axis direction, acting on the force receiving member, based on a difference between a detection value of the first X-axis distance sensor and a detection value of the second X-axis distance sensor, and detecting a moment My about the Y-axis, acting on the force receiving member, based on a detection value of an inclination degree in relation to the X-axis direction that is detected by the inclination degree sensor. 
   (2) The second feature of the invention resides in a force detection device according to the first feature, further comprising: 
   a third displaceable plate, positioned along a plane intersecting a positive part of the Y-axis and supported on the base plate in a displaceable manner; 
   a fourth displaceable plate, positioned along a plane intersecting a negative part of the Y-axis and supported on the base plate in a displaceable manner; 
   a third fixed plate, positioned between the Z-axis and the third displaceable plate and fixed onto the base plate; 
   a fourth fixed plate, positioned between the Z-axis and the fourth displaceable plate and fixed onto the base plate; 
   a first Y-axis distance sensor, detecting a distance between the third displaceable plate and the third fixed plate; and 
   a second Y-axis distance sensor, detecting a distance between the fourth displaceable plate and the fourth fixed plate; and 
   wherein the detection processing unit detects a force Fy in the Y-axis direction, acting on the force receiving member, based on a difference between a detection value of the first Y-axis distance sensor and a detection value of the second Y-axis distance sensor, and detects a moment Mx about the X-axis, acting on the force receiving member, based on a detection value of an inclination degree in relation to the Y-axis direction that is detected by the inclination degree sensor. 
   (3) The third feature of the invention resides in a force detection device according to the first or second feature, further comprising: 
   a Z-axis distance sensor, detecting a distance between the displaceable top plate and the fixed top plate; 
   wherein the detection processing unit detects a force Fz in the Z-axis direction, acting on the force receiving member, based on a detection value of the Z-axis distance sensor. 
   (4) The fourth feature of the invention resides in a force detection device according to the first to the third features, further comprising: 
   a rotation angle sensor, detecting a rotation angle about the Z-axis of the displaceable top plate with respect to the fixed top plate; 
   wherein the detection processing unit detects a moment Mz about the Z-axis, acting on the force receiving member, based on a detection value of the rotation angle sensor. 
   (5) The fifth feature of the invention resides in a force detection device according to the first to the third features: 
   wherein fixed electrodes are formed on surfaces of the fixed plates that oppose the displaceable plates, displaceable electrodes are formed on surfaces of the displaceable plates that oppose the fixed plates, and distance sensors for detecting distances between the fixed plates and the displaceable plates are arranged by capacitance elements, each comprising a fixed electrode and a displaceable electrode that oppose each other, to enable detection of distances based on static capacitance values of the capacitance elements. 
   (6) The sixth feature of the invention resides in a force detection device according to the first feature: 
   wherein, when the X-axis and the Y-axis are projected onto a top surface of the fixed top plate, a first fixed electrode is formed on a projected image of a positive part of the X-axis and a second fixed electrode is formed on a projected image of a negative part of the X-axis; 
   wherein, on a bottom surface of the displaceable top plate, a first displaceable electrode is formed at a position opposing the first fixed electrode and a second displaceable electrode is formed at a position opposing the second fixed electrode; and 
   wherein a first capacitance element is constituted of the first fixed electrode and the first displaceable electrode, a second capacitance element is constituted of the second fixed electrode and the second displaceable electrode, and these two capacitance elements are used as an inclination degree sensor arranged to detect an inclination degree in relation to the X-axis direction, based on a difference between a static capacitance value of the first capacitance element and a static capacitance value of the second capacitance element. 
   (7) The seventh feature of the invention resides in a force detection device according to the second feature: 
   wherein, when the X-axis and the Y-axis are projected onto a top surface of the fixed top plate, a first fixed electrode is formed on a projected image of a positive part of the X-axis, a second fixed electrode is formed on a projected image of a negative part of the X-axis, a third fixed electrode is formed on a projected image of a positive part of the Y-axis, and a fourth fixed electrode is formed on a projected image of a negative part of the Y-axis; 
   wherein, on a bottom surface of the displaceable top plate, a first displaceable electrode is formed at a position opposing the first fixed electrode, a second displaceable electrode is formed at a position opposing the second fixed electrode, a third displaceable electrode is formed at a position opposing the third fixed electrode, and a fourth displaceable electrode is formed at a position opposing the fourth fixed electrode; and 
   wherein a first capacitance element is constituted of the first fixed electrode and the first displaceable electrode, a second capacitance element is constituted of the second fixed electrode and the second displaceable electrode, a third capacitance element is constituted of the third fixed electrode and the third displaceable electrode, a fourth capacitance element is constituted of the fourth fixed electrode and the fourth displaceable electrode, and these four capacitance elements are used as an inclination degree sensor arranged to detect an inclination degree in relation to the X-axis direction, based on a difference between a static capacitance value of the first capacitance element and a static capacitance value of the second capacitance element, and to detect an inclination degree in relation to the Y-axis direction, based on a difference between a static capacitance value of the third capacitance element and a static capacitance value of the fourth capacitance element. 
   (8) The eighth feature of the invention resides in a force detection device according to the fifth to the seventh features: 
   wherein, with respect to a fixed electrode and a displaceable electrode that constitute a capacitance element, an area of one electrode is set wider than an area of the other electrode so that a static capacitance value will not change when the displaceable electrode undergoes a displacement within a predetermined range in a planar direction. 
   (9) The ninth feature of the invention resides in a force detection device according to the eighth feature: 
   wherein, the fixed plates and the fixed top plate, or the displaceable plates and the displaceable top plate are formed of a conductive material, and the fixed plates and the fixed top plate, or the displaceable plates and the displaceable top plate are in themselves used as a fixed electrode or a displaceable electrode. 
   (10) The tenth feature of the invention resides in a force detection device according to the eighth feature: 
   wherein a box-like structure is formed by mutually joining the displaceable top plate and the plurality of displaceable plates, formed of a conductive material, and the box-like structure is used as a single, common displaceable electrode. 
   (11) The eleventh feature of the invention resides in a force detection device according to the fourth feature: 
   wherein fixed electrodes are formed on a top surface of the fixed top plate, displaceable electrodes are formed on a bottom surface of the displaceable top plate, and the rotation angle sensor, detecting a rotation angle about the Z-axis of the displaceable top plate with respect to the fixed top plate, is arranged by capacitance elements, each comprising a fixed electrode and a displaceable electrode that oppose each other, to enable a detection of the rotation angle based on static capacitance values of the capacitance elements. 
   (12) The twelfth feature of the invention resides in a force detection device according to the eleventh feature: 
   wherein the displaceable electrodes are positioned at positions that are offset in a predetermined rotation direction with respect to positions that oppose the fixed electrodes to enable detection of a rotation direction along with the rotation angle based on increases or decreases of static capacitance values of the capacitance elements. 
   (13) The thirteenth feature of the invention resides in a force detection device according to the twelfth feature: 
   wherein, when the X-axis and the Y-axis are projected onto a top surface of the fixed top plate, a first fixed electrode is formed on a projected image of a positive part of the X-axis, a second fixed electrode is formed on a projected image of a negative part of the X-axis, a third fixed electrode is formed on a projected image of a positive part of the Y-axis, and a fourth fixed electrode is formed on a projected image of a negative part of the Y-axis; 
   wherein, on a bottom surface of the displaceable top plate, a first displaceable electrode is formed at a position offset in a predetermined rotation direction with respect to a position opposing the first fixed electrode, a second displaceable electrode is formed at a position off set in a rotation direction with respect to a position opposing the second fixed electrode, a third displaceable electrode is formed at a position offset in a rotation direction with respect to a position opposing the third fixed electrode, and a fourth displaceable electrode is formed at a position offset in a rotation direction with respect to a position opposing the fourth fixed electrode; and 
   wherein a first capacitance element is constituted of the first fixed electrode and the first displaceable electrode, a second capacitance element is constituted of the second fixed electrode and the second displaceable electrode, a third capacitance element is constituted of the third fixed electrode and the third displaceable electrode, a fourth capacitance element is constituted of the fourth fixed electrode and the fourth displaceable electrode, and detection of a rotation direction along with a rotation angle is enabled based on an increase or a decrease of a sum of static capacitance values of the four capacitance elements. 
   (14) The fourteenth feature of the invention resides in a force detection device according to the first to the thirteenth features: 
   wherein an outer box-like structure, forming a rectangular parallelepiped that is opened at a bottom surface and undergoing elastic deformation by an action of an external force, is joined so that the bottom surface is set on the base plate, side plates or a part thereof of the outer box-like structure are used as the displaceable plates, and a top plate or a part thereof of the outer box-like structure is used as the displaceable top plate. 
   (15) The fifteenth feature of the invention resides in a force detection device according to the fourteenth feature: 
   wherein U-shaped slits, opening upward, are formed in side plates of the outer box-like structure and respective parts surrounded by the respective slits are used as the displaceable plates. 
   (16) The sixteenth feature of the invention resides in a force detection device according to the fifteenth feature: 
   wherein the U-shaped slit, opening upward, is formed in each of four side plates of the outer box-like structure, edges at which two mutually adjacent side plates intersect are used as columns to arrange a structure, with which a top plate of the outer box-like structure is supported by a total of four pillars, and the outer box-like structure is made to deform by elastic deformation of the four columns. 
   (17) The seventeenth feature of the invention resides in a force detection device according to the fourteenth to the sixteenth features: 
   wherein an inner box-like structure, forming a rectangular parallelepiped that is smaller than the outer box-like structure, is joined onto the base plate in a state in which the inner box-like structure is contained in the outer box-like structure and side plates and a top plate of the inner box-like structure are used as the fixed plates and the fixed top plate. 
   (18) The eighteenth feature of the invention resides in a force detection device according to the first to the thirteenth features: 
   wherein four columns, formed of a material that undergoes elastic deformation due to an action of an external force and joined in an erected manner to the base plate, and a top plate, four corners of which are joined to upper ends of the four columns are provided; and 
   wherein the displaceable plates are positioned between respective pairs of mutually adjacent columns, upper edges of the displaceable plate are joined to and thereby supported by edges of the top plate, and the top plate or a part thereof is used as the displaceable top plate. 
   (19) The nineteenth feature of the invention resides in a force detection device according to the fourteenth to the eighteenth features: 
   wherein by forming slits in the top plate, the top plate is partitioned into a displaceable top plate positioned at a center, peripheral parts positioned at a periphery of the displaceable top plate, and beams having flexibility and connecting the displaceable top plate and the peripheral parts, so that the displaceable top plate is displaced with respect to the peripheral parts by a deflection of the beams and the peripheral parts are connected to the base plate via side plates or columns of the outer box-like structure. 
   (20) The twentieth feature of the invention resides in a force detection device according to the nineteenth feature: 
   wherein when the X-axis and the Y-axis are projected onto the top plate, a displaceable top plate having a shape of vanes of a fan is arranged from a first vane-like part, positioned on a projected image of a positive part of the X-axis, a second vane-like part, positioned on a projected image of a negative part of the X-axis, a third vane-like part, positioned on a projected image of a positive part of the Y-axis, a fourth vane-like part, positioned on a projected image of a negative part of the Y-axis, and a central part, positioned on a projected image of an origin O and connected to inner side parts of the first to fourth vane-like parts; 
   wherein a respective beam is positioned between every two mutually adjacent vane-like parts so that the central part is supported by four beams; and 
   wherein the four beams are connected to the central part at their inner ends and connected to the peripheral parts at their outer ends and the connecting member is connected to a top surface of the central part. 
   (21) The twenty-first feature of the invention resides in a force detection device according to the twentieth feature: 
   wherein each beam comprises: a horizontal beam, whose main surface faces a horizontal direction; a vertical beam whose main surface faces a vertical direction; and an intermediate joint, connecting the horizontal beam and the vertical beam; and is thereby made a structure with which both deflection in the horizontal direction and deflection in the vertical direction can occur readily. 
   (22) The twenty-second feature of the invention resides in a force detection device according to the first to the twenty-first features: 
   wherein a control member is provided, which, in order to restrict displacements of the force receiving member with respect to the base plate within predetermined ranges, has control surfaces that contact the force receiving member when the force receiving member is about to become displaced beyond the predetermined range. 
   (23) The twenty-third feature of the invention resides in a force detection device according to the twenty-second feature: 
   wherein at least a part of the force receiving member and a part of the control member that are involved in contact are formed of a conductive material, and a contact detection circuit, detecting a state of contact of the force receiving member and the control member based on a state of electrical conduction, is provided. 
   (24) The twenty-fourth feature of the invention resides in a force detection device according to the twenty-third feature: 
   wherein a hollow part is formed in a vicinity of a control surface of the control member or an opposing surface of the force receiving member that opposes the control surface, a surface layer part at which the hollow part is formed is arranged as a thin part with flexibility, a conductive contact protrusion is formed on a surface of the thin part, and a state of electrical conduction by contacting of the contact protrusion with the opposing surface or the control surface is arranged to be detected prior to contacting of the opposing surface and the control surface. 
   (25) The twenty-fifth feature of the invention resides in a force detection device according to the twenty-fourth feature: 
   wherein a conductive conical protrusion, a tip part of which undergoes plastic deformation, is provided on the control surface of the control member or a surface of the force receiving member that opposes the control surface. 

   
     BRIEF DESCRIPTION OF THE DRAWINGS 
       FIG. 1  is a side view of a force detection device of a basic embodiment of the invention (a detection processing unit  250  is indicated by a block) with the Z-axis passing through a central position. 
       FIG. 2  is a side view in section across the XZ plane of the force detection device shown in  FIG. 1 . 
       FIG. 3  is a top view of the force detection device shown in  FIG. 2 . 
       FIG. 4  is a transverse section along line  4 — 4  of the force detection device shown in  FIG. 2 . 
       FIG. 5  is a transverse section along line  5 — 5  of the force detection device shown in  FIG. 2 . 
       FIG. 6  is a transverse section along line  6 — 6  of the force detection device shown in  FIG. 2 . 
       FIG. 7  is a bottom view of an outer box-like structure  100  which is removed from the force detection device shown in  FIG. 2 . 
       FIGS. 8A to 8C  are schematic diagrams illustrating the principle of detection of a force Fx in the X-axis direction by the force detection device shown in  FIG. 2 . 
       FIGS. 9A to 9C  are schematic diagrams illustrating the principle of detection of a force Fz in the Z-axis direction by the force detection device shown in  FIG. 2 . 
       FIGS. 10A to 10C  are schematic diagrams illustrating the principle of detection of a moment My about the Y-axis by the force detection device shown in  FIG. 2 . 
       FIG. 11  is a table showing the principle of detection of various forces and moments by the force detection device shown in  FIG. 2 . 
       FIG. 12  is a diagram showing the calculation equations for detecting the various forces and moments based on the table shown in  FIG. 11 . 
       FIG. 13  is a top view showing a state in which a positive moment +Mz about the Z-axis is acting on the force detection device shown in  FIG. 2 . 
       FIGS. 14A to 14C  are top projections showing the principle of detection of a moment Mz about the Z-axis by the force detection device shown in  FIG. 2  (the hatching indicates the effective area portions of electrode pairs that form capacitance elements and does not indicate cross sections). 
       FIGS. 15A and 15B  are top projections illustrating the electrode configuration of a modification example for detecting both the direction and magnitude of a moment Mz about the Z-axis by the force detection device shown in  FIG. 2 . 
       FIGS. 16A to 16C  are top projections showing the principle of detection of a moment Mz about the Z-axis by the force detection device with the electrode configuration shown in  FIG. 15  (the hatching indicates the effective area portions of electrode pairs that form capacitance elements and does not indicate cross sections). 
       FIG. 17  is a table showing the principle of detection of various forces and moments by the force detection device with the electrode configuration shown in  FIG. 15 . 
       FIG. 18  is a diagram showing the calculation equations for detecting the various forces and moments based on the table shown in  FIG. 17 . 
       FIG. 19  is a side view in section of a force detection device of an embodiment with which the electrode configuration is simplified. 
       FIG. 20  is a side view in section of a force detection device of another embodiment with which the electrode configuration is simplified. 
       FIG. 21  is a plan view showing an example of an electrode configuration suited for the detection of a moment Mz about the Z-axis. 
       FIG. 22  is a side view of a force detection device of a practical embodiment of this invention. 
       FIG. 23  is a schematic diagram illustrating the principle of detection of a force Fx in the X-axis direction by the force detection device shown in  FIG. 22 . 
       FIG. 24  is a top view of the force detection device shown in  FIG. 22  (a force receiving member  110  and a connecting member  120  are omitted from illustration). 
       FIG. 25  is a top view of a modification example of the force detection device shown in  FIG. 22  (force receiving member  110  and connecting member  120  are omitted from illustration). 
       FIG. 26  is a diagram showing the structure of a top plate  130  of the modification example shown in  FIG. 25 . 
       FIG. 27  is a top view of a modification example, with which the modification example of the force detection device shown in  FIG. 25  is modified further (force receiving member  110  and connecting member  120  are omitted from illustration). 
       FIG. 28  is an enlarged perspective view of a beam used in the modification example shown in  FIG. 27 . 
       FIG. 29  is a sectional side view of a modification example, wherein a control member for controlling displacement is added to the embodiment shown in  FIG. 19 . 
       FIGS. 30A to 30C  are enlarged sectional views showing a structural example and an operation of the control member of the modification example shown in  FIG. 29 . 
       FIGS. 31A to 31C  are enlarged sectional views showing another structural example and an operation of the control member of the modification example shown in  FIG. 29 . 
       FIG. 32  is a top view showing a modification example of control member  400  shown in  FIG. 29 . 
   

   DESCRIPTION OF THE PREFERRED EMBODIMENTS 
   This invention shall now be described based on illustrated embodiments. 
   &lt;&lt;&lt;§1. Structure of a Basic Embodiment &gt;&gt;&gt; 
   The structure of a force detection device of a basic embodiment of this invention shall first be described with reference to  FIGS. 1 to 7 .  FIG. 1  is a side view of this force detection device. The major components in terms of appearance of this force detection device are, as shown in order from the top, a force receiving member  110 , a connecting member  120 , a top plate  130 , side plates  140 , a pedestal  150 , and a base plate  200 . For the sake of convenience, the box-like structure, formed of upper plate  130 , side plates  140 , and pedestal  150 , shall be referred to hereinafter as “outer box-like structure  100 .” Though detection processing unit  250  is drawn as a block in this figure, it is actually arranged from an analog or digital computational circuit for performing detection based on the detection principles to be described later. 
   Here, for the sake of description, an XYZ three-dimensional coordinate system shall be defined with the origin O being set at a central part of force receiving member  110 , the X-axis being set in the right direction of the figure, the Z-axis being set in the upper direction of the figure, and the Y-axis being set in the direction perpendicular to and directed towards the rear side of the paper surface of the figure. The top surface of base plate  200  is a plane parallel to the XY plane. The force detection device shown here can detect the five components of a force Fx in the X-axis direction, a force Fy in the Y-axis direction, a force Fz in the Z-axis direction, a moment Mx about the X-axis, and a moment My about the Y-axis independent of each other. In §3, an embodiment, which can detect six components that furthermore include a moment Mz about the Z-axis, shall be described. 
   In the present application, the term “force” may be used as suitable to refer to a force in the direction of a specific coordinate axis or as a collective force that includes the moment components. For example, whereas in  FIG. 1 , forces Fx, Fy, and Fz refer to the force components in the direction of the respective coordinate axes and not moments, in the case of the expression, “the six forces of Fx, Fy, Fz, Mx, My, and Mz,” the term “force” shall refer to the collective force that includes the force components in the respective coordinate axis directions and the moment components about the respective coordinate axes. Also, a positive moment about a certain coordinate axis shall be defined as being in the direction of rotation of a right-handed screw in the case where the right-handed screw is advanced in the positive direction of the predetermined coordinate axis. 
     FIG. 2  is a side view in section along the XZ plane of this force detection device. Origin O of the coordinate system is indicated at the central position of force receiving member  110 . As illustrated, outer box-like structure  100  is a hollow, rectangular parallelepiped box, which is opened at the bottom. Though in  FIG. 1 , this outer box-like structure  100  is illustrated as comprising the three elements of upper plate  130 , side plates  140 , and pedestal  150 , actually a total of four side plates  140  exist. In the following, when referring to each of these four side plates  140  individually, these shall be called “first side plate  141 ” to “fourth side plate  144 .” Pedestal  150  is provided to support outer box-like structure  100  in a manner enabling displacement on the top surface of base plate  200  and though it does not serve an essential role in the operation of this force detection device, it is preferably provided in terms of practical use. A somewhat smaller inner box-like structure  300  is contained inside outer box-like structure  100 . This inner box-like structure  300  is also a hollow, rectangular parallelepiped box, which is opened at the bottom and is arranged from a single top plate  330  and four side plates  341  to  344 . 
     FIG. 3  is a top view of this force detection device. As illustrated, with this embodiment, force receiving member  110  is a disk-like member and is joined to the cylindrical connecting member  120  as indicated by the broken lines at a central part of its bottom surface. This cylindrical connecting member  120  has the Z-axis passing through its center, has its upper end connected to the central part of the bottom surface of force receiving member  110 , and has its lower end connected to a central part of the top surface of top plate  130 . Top plate  130  is a square plate that forms the top surface of outer box-like structure  100 . Outer box-like structure  100  is positioned with the Z-axis as its center, and as indicated in the figure by the broken lines, first side plate  141  is positioned at a positive region of the X-axis, second side plate  142  is positioned at a negative region of the X-axis, third side plate  143  is positioned at a positive region of the Y-axis, and fourth side plate  144  is positioned at a negative region of the Y-axis. First side plate  141  and second side plate  142  are parallel to the YZ plane and third side plate  143  and fourth side plate  144  are parallel to the XZ plane. Pedestal  150  has a frame structure that surrounds the periphery of the lower edges of the respective side plates  141  to  144  and the bottom surface thereof is joined to the top surface of base plate  200 . 
   As shown in the side view in section of  FIG. 2 , force receiving member  110 , connecting member  120 , and outer box-like structure  100  (upper plate  130 , first side plate  141  to fourth side plate  144 , and pedestal  150 ) form an integral structure of the same material, and in the case of this basic embodiment, the structure is formed of an insulating material. Likewise, upper plate  330  and first side plate  341  to fourth side plate  344 , which form inner box-like structure  300 , also form an integral structure of the same material, and in the case of this basic embodiment, the structure is formed of an insulating material. Base plate  200  is also a base plate formed of an insulating material. For practical use however, force receiving member  110 , connecting member  120 , and outer box-like structure  100  are preferably formed of a metal or other conductive material as shall be described in §4. 
   Force receiving member  110  is a component that is positioned along the Z-axis above top plate  130  in order to receive a force that is to be detected. The present force detection device has a function of detecting an external force that acts on this force receiving member  110 . A force that acts on force receiving member  110  is transmitted by connecting member  120  to top plate  130 , and as a result, outer box-like structure  100  undergoes deformation. With this force detection device, the external force that acts on force receiving member  110  is detected by recognition of this deformation of outer box-like structure  100 . Outer box-like structure  100  must thus be formed of a material with flexibility that can undergo elastic deformation by the action of the external force. Since elastic deformation will occur with various materials as long as the side plates and the top plate are made somewhat thin in thickness, difficulties will not arise in the selection of material. 
   Top plate  130  and the respective side plates  141  to  144  that form outer box-like structure  100  thus undergo displacement due to an external force that is transmitted from force receiving member  110 . In view of such functions, the respective side plates  141  to  144  shall be referred to hereinafter as “displaceable plates  141  to  144 ” and top plate  130  shall be referred to hereinafter as “displaceable top plate  130 .” On the other hand, since the external force from force receiving member  110  does not act on top plate  330  and the respective side plates  341  to  344  that form inner box-like structure  300 , these remain fixed to base plate  200 . Thus the respective side plates  341  to  344  shall be referred to hereinafter as “fixed plates  341  to  344 ” and top plate  330  shall be referred to hereinafter as “fixed top plate  330 .” 
   As shown in part in the side view in section of  FIG. 2 , a plurality of electrodes E 1  to E 9  and F 1  to F 9  are formed on the outer side surfaces of inner box-like structure  300  and the inner side surfaces of outer box-like structure  100 . Here, electrodes E 1  to E 9 , which are formed on the outer side surfaces of inner box-like structure  300 , shall be referred to as “fixed electrodes” and electrodes F 1  to F 9 , which are formed on the inner side surfaces of outer box-like structure  100  shall be referred to as “displaceable electrodes.” As indicated by these names, whereas fixed electrodes E 1  to E 9  are electrodes that are fixed onto base plate  200  via inner box-like structure  300 , displaceable electrodes F 1  to F 9  are electrodes that undergo displacement in accompaniment with the deformation of outer box-like structure  100 . Displaceable electrodes F 1  to F 9  are positioned at positions that oppose fixed electrodes E 1  to E 9 , respectively. 
   The shapes and positions of the respective electrodes are shown clearly in  FIGS. 4 to 7 .  FIG. 4  is a transverse section along line  4 — 4  of the force detection device shown in  FIG. 2 , and shows, in a sectioned state, the interior of outer box-like structure  100  surrounded by first displaceable plate  141  to fourth displaceable plate  144 . In particular, the shapes and positions of the five fixed electrodes E 1  to E 5 , formed on fixed top plate  330 , which forms the top surface of inner box-like structure  300 , are shown clearly. That is, when the X-axis and the Y-axis are projected onto the top surface of fixed top plate  330 , first fixed electrode E 1  is formed on the projected image of a positive part of the X-axis, second fixed electrode E 2  is formed on the projected image of a negative part of the X-axis, third fixed electrode E 3  is formed on the projected image of a positive part of the Y-axis, fourth fixed electrode E 4  is formed on the projected image of a negative part of the Y-axis, and fifth fixed electrode E 5  is formed on the projected image of the origin O. Here, first fixed electrode E 1  to fourth fixed electrode E 4  are electrodes of the same size and same shape and are positioned at positions that are symmetrical with respect to the XZ plane or the YZ plane. Meanwhile, fifth fixed electrode E 5  is a circular electrode having the Z-axis as the central axis. 
   Meanwhile, fixed electrodes E 6  to E 9  are positioned respectively at the four side surfaces of inner box-like structure  300 , and opposite these positions are disposed displaceable electrodes F 6  to F 9 . The positions of these electrodes are shown clearly in  FIG. 5 .  FIG. 5  is a transverse section along line  5 — 5  of the force detection device shown in  FIG. 2 . First displaceable plate  141  to fourth displaceable plate  144 , which form the respective side surfaces of outer box-like structure  100 , and first fixed plate  341  to fourth fixed plate  344 , which form the respective side surfaces of inner box-like structure  300 , are respectively shown in section, and displaceable electrodes F 6  to F 9 , formed on the inner side surfaces of the respective displaceable plates  141  to  144 , and fixed electrode E 6  to E 9 , formed on the outer side surfaces of the respective fixed plates  341  to  344 , are also shown in section. 
     FIG. 6  is a transverse section along line  6 — 6  of the force detection device shown in  FIG. 2 , and the state as viewed from the right direction of  FIG. 2  is shown. As shown here, sixth fixed electrode E 6 , which is formed on first fixed plate  341 , is a rectangular, plate-shaped electrode. Though here for the sake of convenience, the four fixed electrodes E 6  to E 9  and the four displaceable electrode F 6  to F 9  are described as being plate-shaped electrodes of the same shape and same size, for practical use, a pair of mutually opposing electrodes are preferably differed slightly in size with respect to each other as shall be described later. Here, the conditions in which electrodes E 1 /F 1 , electrodes E 8 /F 8 , and electrodes E 9 /F 9  oppose each other across a predetermined interval are also shown. 
     FIG. 7  is a bottom view of outer box-like structure  100  which is removed from the force detection device shown in FIG.  2 . The state of the interior of this outer box-like structure  100  is shown in the space surrounded by the frame-like pedestal  150 . As shown here, five displaceable electrodes F 1  to F 5  are disposed at the bottom face of displaceable top plate  130 , which is positioned at the inner side of the figure, and these electrodes respectively oppose the five fixed electrodes E 1  to E 5 , shown in  FIG. 4 . Though here for the sake of convenience, the five displaceable electrodes F 1  to F 5  are described as being the same in shape and size as the five fixed electrode E 1  to E 5 , for practical use, the sizes are preferably differed slightly as shall be described later.  FIG. 7  also shows the conditions in which displaceable electrodes F 6  to F 9  are formed at the respective inner side surfaces of displaceable plates  141  to  144 . 
   A space is thus formed between outer box-like structure  100  and inner box-like structure  300  as shown in the side view in section of  FIG. 2 , and this space is used to form the nine pairs E 1 /F 1  to E 9 /F 9  of mutually opposing electrodes. Here, whereas electrodes E 1  to E 9 , which are formed on the outer side surfaces of inner box-like structure  300 , are all fixed electrodes that are fixed via inner box-like structure  300  to base plate  200 , electrodes F 1  to F 9 , which are formed on the inner side surfaces of outer box-like structure  100 , are all displaceable electrodes, which undergo displacement in accompaniment with the deformation of outer box-like structure  100 . Here, for the sake of description, the nine sets of static capacitance elements constituted of the nine electrode pairs E 1 /F 1  to E 9 /F 9  shall respectively be referred to as “capacitance elements C 1  to C 9 .” The same symbols C 1  to C 9  shall also be used to express the respective static capacitance values of capacitance elements C 1  to C 9  as well. 
   Capacitance elements C 6  to C 9  have the role of detecting the displacements of first displaceable plate  141  to fourth displaceable plate  144 . For example, in the transverse section of  FIG. 5 , when first displaceable plate  141  is displaced in the positive X-axis direction (the right direction in the figure), sixth displaceable electrode F 6  also moves in the same direction, that is, in the direction of moving away from sixth fixed electrode E 6 , causing the distance between electrodes of capacitance element C 6 , constituted of the electrode pair E 6 /F 6 , to spread and the static capacitance value C 6  to decrease. Oppositely, when first displaceable plate  141  is displaced in the negative X-axis direction (left direction in the figure), the distance between electrodes of capacitance element C 6  is narrowed and the static capacitance value C 6  increases. 
   The static capacitance value C 6  of capacitance element C 6  is thus a parameter that indicates the distance between first displaceable plate  141  and first fixed plate  341 . Likewise, the static capacitance value C 7  of capacitance element C 7 , constituted of the electrode pair E 7 /F 7 , is a parameter that indicates the distance between second displaceable plate  142  and second fixed plate  342 , the static capacitance value C 8  of capacitance element C 8 , constituted of the electrode pair E 8 /F 8 , is a parameter that indicates the distance between third displaceable plate  143  and third fixed plate  343 , and the static capacitance value C 9  of capacitance element C 9 , constituted of the electrode pair E 9 /F 9 , is a parameter that indicates the distance between fourth displaceable plate  144  and fourth fixed plate  344 . 
   The role of capacitance element C 5  is to detect the displacement of displaceable top plate  130  in relation to the Z-axis direction. For example, when in the side view in section of  FIG. 2 , displaceable top plate  130  is displaced in the positive direction along the Z-axis (upward direction in the figure), fifth displaceable electrode F 5  also moves in the same direction, that is, in the direction of moving away from fifth fixed electrode E 5 , causing the distance between electrodes of capacitance element C 5 , constituted of the electrode pair E 5 /F 5 , to spread and the static capacitance value C 5  to decrease. Oppositely, when displaceable top plate  130  is displaced in the negative Z-axis direction (downward direction in the figure), the distance between electrodes of capacitance element C 5  is narrowed and the static capacitance value C 5  increases. The static capacitance value C 5  of capacitance element C 5  is thus a parameter that indicates the distance between displaceable top plate  130  and fixed top plate  330 . 
   Meanwhile, capacitance elements C 1  to C 4  have the role of detecting the inclination degree of displaceable top plate  130  with respect to fixed top plate  330 . For example, consider the case where a positive moment +My about the Y-axis (a clockwise moment about the axis perpendicular to the paper surface) acts on force receiving member  110  in the side view in section of  FIG. 2 . In this case, the moment that acts on force receiving member  110  is transmitted via connecting member  120  to displaceable top plate  130 . The moment thus transmitted applies to displaceable top plate  130  a force that displaces the right half in the figure downwards and displaces the left half in the figure upwards. As a result, displaceable top plate  130  becomes inclined with respect to the original level state in a manner such that its right side in  FIG. 2  is lowered and its left side is raised. In the present Specification, such an inclination degree related to direction shall be referred to as “an inclination degree in relation to the X-axis direction.” 
   This “inclination degree in relation to the X-axis direction” can be detected as a difference in the static capacitance values of capacitance elements C 1  and C 2 . That is, when displaceable top plate  130  is put in an inclined state such as that described above, the distance between electrodes of capacitance element C 1 , which is constituted of the electrode pair E 1 /F 1  decreases, and the static capacitance value C 1  increases. Meanwhile, the distance between electrodes of capacitance element C 2 , which is constituted of the electrode pair E 2 /F 2  increases, and the static capacitance value C 2  decreases. The difference between the two, (C 1 −C 2 ), is thus a value that indicates the inclination degree in relation to the X-axis direction of displaceable top plate  130 . Also, when top plate becomes inclined in a direction such that, with respect to the original level state, the right side in  FIG. 2  is raised and the left side is lowered, the distance between electrodes of capacitance element C 1  increases so that the static capacitance value C 1  decreases and the distance between electrodes of capacitance element C 2  decreases so that the static capacitance value C 2  increases. The inclination degree in this case can thus be determined as the “inclination degree in relation to the X-axis direction” from the difference between the two capacitance values, (C 1 −C 2 ) (in this case, the difference, (C 1 −C 2 ), becomes a negative value). The direction and magnitude of the inclination degree in relation to the X-axis direction can thus be detected as the difference in the static capacitance values of capacitance elements C 1  and C 2 . 
   By exactly the same principle as the above, the direction and magnitude of the inclination degree in relation to the Y-axis can be detected as the difference, (C 3 −C 4 ), of the static capacitance values of capacitance elements C 3  and C 4 . That is, if the inclination degree, concerning the inclination direction such that, with respect to the original level state, the right side of displaceable top plate  130  in  FIG. 6  (in which the Y-axis direction is the horizontal direction) is lowered and the left side is raised or the opposite inclination degree such that the right side is raised and the left side is lowered, is to be referred to as the “inclination degree in relation to the Y-axis direction,” this “inclination degree in relation to the Y-axis direction” can be detected as the difference in the static capacitance values of capacitance elements C 3  and C 4  and the sign thereof indicates the inclination direction. Capacitance elements C 1  to C 4  thus have the function of detecting the “inclination degree in relation to the X-axis direction” and the “inclination degree in relation to the Y-axis direction” of displaceable top plate  130  with respect to fixed top plate  330 . 
   &lt;&lt;&lt;§2. Detection Operations of the Basic Embodiment &gt;&gt;&gt; 
   The detection operations by the force detection device of the above-described basic embodiment shall now be described. As mentioned above, this force detection device can detect the five components of a force Fx in the X-axis direction, a force Fy in the Y-axis direction, a force Fz in the Z-axis direction, a moment Mx about the X-axis, and a moment My about the Y-axis that are applied to force receiving member  110 . 
   The principle of detection of a force Fx in the X-axis direction shall first be described with reference to the schematic diagrams of  FIGS. 8A to 8C .  FIG. 8A  is an XZ elevation view that schematically shows the components involved in the detection of a force Fx in the X-axis direction and a moment My about the Y-axis by the present force detection device and shows the state in which no external force is acting. As described in §1, base plate  200  is a base plate having a top surface that is parallel to the XY plane in the XYZ three-dimensional coordinate system, and on this base plate  200  are positioned first displaceable plate  141 , second displaceable plate  142 , first fixed plate  341 , and second fixed plate  342 . Also, displaceable top plate  130  is positioned so as to be suspended across the upper end of first displaceable plate  141  and the upper end of second displaceable plate  142  and fixed top plate  330  is positioned so as to be suspended across the upper end of first fixed plate  341  and the upper end of second fixed plate  342 . 
   Also, force receiving member  110  is a component that is positioned on the Z-axis above displaceable top plate  130  in order to receive the force that is to be detected, and connecting member  120  is a component that is positioned along the Z-axis in order to connect force receiving member  110  and displaceable top plate  130 . In the present example, connecting member  120  is connected to the central part of the top surface of displaceable top plate  130  and an external force that acts on force receiving member  110  is transmitted via connecting member  120  to displaceable top plate  130 . 
     FIG. 8B  is a diagram showing the displacement state of the respective parts when a force +Fx in the positive X-axis direction acts on force receiving member  110 . As illustrated, the external force +Fx that acts on force receiving member  110  is transmitted via connecting member  120  to displaceable top plate  130  and applies to displaceable top plate  130  a force that makes it move in the right direction in the figure. This force is also transmitted to first displaceable plate  141  and second displaceable plate  142  and the force +Fx in the positive X-axis direction thus acts on the upper edge of first displaceable plate  141  and the upper edge of second displaceable plate  142 . As a result, first displaceable plate  141  and second displaceable plate  142  become inclined by just an angle θ towards the positive X-axis direction as illustrated. Since with the structure described in §1, first displaceable plate  141 , second displaceable plate  142 , and displaceable top plate  130  are arranged as parts of outer box-like structure  100 , a side surface of this outer box-like structure  100  becomes deformed to a parallelogram, such as that illustrated. 
   Due to such deformation, the distance between first displaceable plate  141  and first fixed plate  341  increases and the distance between second displaceable plate  142  and second fixed plate  342  decreases. Oppositely when a force −Fx in the negative X-axis direction acts, the displacement state of the respective parts will be as shown  FIG. 8C . That is, first displaceable plate  141  and second displaceable plate  142  become inclined by just an angle θ towards the negative X-axis direction as illustrated (here, the inclination direction is provided with a sign and the inclination angle in this case is expressed as −θ). Due to such deformation, the distance between first displaceable plate  141  and first fixed plate  341  decreases and the distance between second displaceable plate  142  and second fixed plate  342  increases. 
   Thus when a first X-axis distance sensor, which detects the distance between first displaceable plate  141  and first fixed plate  341 , and a second X-axis distance sensor, which detects the distance between second displaceable plate  142  and second fixed plate  342 , are provided, the difference in the distance values detected by these sensors will indicate the force Fx in the X-axis direction that acts on force receiving member  110 . That is, the magnitude of this difference of detection values indicates the absolute value of the force Fx and the sign of this difference of detection values indicates the direction of the force Fx. 
   As shown in the side view in section of  FIG. 2 , with the force detection device described in §1, sixth capacitance element C 6 , constituted of the electrode pair E 6 /F 6 , functions as the first X-axis distance sensor, and seventh capacitance element C 7 , constituted of the electrode pair E 7 /F 7 , functions as the second X-axis distance sensor. The difference (C 7 −C 6 ) of the static capacitance values of these capacitance elements C 6  and C 7  can thus be output as the detection value of the force Fx in the X-axis direction. (C 7 −C 6 ) is used instead of (C 6 −C 7 ) in the equation for determining the difference so as to provide an Fx having a correct sign in consideration that the magnitude of the distance between electrodes of the electrode pair that constitute a capacitance element is in a reverse relationship with the magnitude of the static capacitance value. 
   Though the principle of detection of a force Fx in the X-axis direction were described above, the principle of detection of a force Fy in the Y-axis direction is all the same. That is, when a force Fy in the Y-axis direction acts on force receiving member  110 , third displaceable plate  143  and fourth displaceable plate  144  become inclined in the Y-axis direction. Thus when a first Y-axis distance sensor, which detects the distance between third displaceable plate  143  and third fixed plate  343 , and a second Y-axis distance sensor, which detects the distance between fourth displaceable plate  144  and fourth fixed plate  344 , are provided, the difference in the distance values detected by these sensors will indicate the force Fy in the Y-axis direction that acts on force receiving member  110 . The magnitude of the difference of the detection values indicates the absolute value of the force Fy and the sign of the difference of the detection values indicates the direction of the force Fy in this case as well. 
   As shown in the sectional view of  FIG. 6 , with the force detection device described in §1, eighth capacitance element C 8 , constituted of the electrode pair E 8 /F 8 , functions as the first Y-axis distance sensor, and ninth capacitance element C 9 , constituted of the electrode pair E 9 /F 9 , functions as the second Y-axis distance sensor. The difference (C 9 −C 8 ) of the static capacitance values of these capacitance elements C 8  and C 9  can thus be output as the detection value of the force Fy in the Y-axis direction. Here, (C 9 −C 8 ) is used in the equation for determining the difference in consideration of providing an Fy having a correct sign. 
   Next, the principle of detection of a force Fz in the Z-axis direction shall be described with reference to the schematic diagrams of  FIGS. 9A to 9C . First, let the state shown in  FIG. 9A  be that in which no external force is acting. When from this state, a force +Fz in the positive Z-axis direction acts, the displacement state of the respective parts will be as shown in  FIG. 9B , and when a force −Fz in the negative Z-axis direction acts, the displacement state of the respective parts will be as shown in  FIG. 9C . Though for the sake of illustration, states, in which the position of displaceable top plate  130  changes vertically by the extension or shrinkage of first displaceable plate  141  and second displaceable plate  142  in the Z-axis direction, are shown in schematic diagrams  9 B and  9 C, in actuality, the structure as a whole undergoes a predetermined form of deformation with the respective parts being in mutual relationships. That is, in actuality, when a force Fz in the Z-axis direction acts, first displaceable plate  141  and second displaceable plate  142  extend or shrink in the Z-axis direction and also become somewhat inclined with respect to base plate  200 , and displaceable top plate  130  itself undergoes a deformation in which it extends in the planar direction and becomes convex in the upward or downward direction. 
   Regardless of the actual form of deformation, when a force +Fz of the positive Z-axis direction acts on force receiving member  110 , the distance between displaceable top plate  130  and fixed top plate  330  expands and when a force −Fz in the negative Z-axis direction acts, the distance between displaceable top plate  130  and fixed top plate  330  shrinks. Thus if a Z-axis distance sensor that detects the distance between the two top plates is provided, the distance value that is detected by this sensor will indicate the force Fz in the Z-axis direction that acts on force receiving member  110 . That is, if the detection value of this Z-axis distance sensor in the state shown in  FIG. 9A  is set as a reference value, an increase of the detected distance value with respect to the reference value will mean that a force +Fz in the positive Z-axis direction is detected and the amount of increase will indicate the magnitude of the acting force. Oppositely, when the detected distance value decreases with respect to the reference value, this will mean that a force −Fz in the negative Z-axis direction is detected and the amount of decrease will indicate the magnitude of the acting force. 
   As shown in the side view in section of  FIG. 2 , with the force detection device described in §1, fifth capacitance element C 5 , constituted of the electrode pair E 5 /F 5 , functions as the Z-axis sensor. Capacitance element C 5  can thus be used for detecting the value of the force Fz in the Z-axis direction. However, since the magnitude of the distance between electrode pairs that constitute the capacitance element is in a reverse relationship with respect to the magnitude of the static capacitance value, when the static capacitance value C 5  increases with respect to the reference value, this will mean that a force −Fz in the negative Z-axis direction is detected (state of  FIG. 9C ), and when the static capacitance value C 5  decreases with respect to the reference value, this will mean that a force +Fz in the positive Z-axis direction is detected (state of  FIG. 9B ). 
   Next, the principle of detection of a moment My about the Y-axis shall be described with reference to the schematic diagrams of  FIGS. 10A to 10C . First, let the state shown in  FIG. 10A  be that in which no external force is acting. Then from this state, let a positive moment +My about the Y-axis act on force receiving member  110 . Such a moment +My acts, on force receiving member  110  shown in  FIG. 3 , as a force that pushes an action point P 1  downwards perpendicularly with respect to the paper surface and pushes an action point P 2  upwards perpendicularly with respect to the paper surface. The respective parts of this force detection device will thus be displaced from the state shown in  FIG. 10A  to the state shown in  FIG. 10B . On the other hand, if oppositely a negative moment −My about the Y-axis acts, the displacement states of the respective parts will be as shown in  FIG. 10C . Though for the sake of illustration, states, in which the position of displaceable top plate  130  changes vertically due to the extension or shrinkage of first displaceable plate  141  and second displaceable plate  142  in the Z-axis direction, are illustrated in these schematic diagrams  10 B and  10 C as well, in actuality, the structure as a whole undergoes a predetermined form of deformation with the respective parts being in mutual relationships. Thus in actuality, first displaceable plate  141  and second displaceable plate  142  extend or shrink in the Z-axis direction and also become somewhat inclined with respect to base plate  200 , and displaceable top plate  130  itself becomes deflected as well. 
   Regardless of the actual form of deformation, when a moment My about the Y-axis acts on force receiving member  110 , displaceable top plate  130  becomes inclined in relation to the X-axis direction with respect to fixed top plate  330 . Thus if an inclination degree sensor is provided that detects the inclination degree in relation to the X-axis direction of displaceable top plate  130  with respect to fixed top plate  330 , the inclination degree value that is detected by this sensor will indicate the moment My about the Y-axis that acts on force receiving member  110 . Let assume that an inclination degree sensor is prepared, which can indicate the inclination degree of displaceable top plate  130  in the state shown in  FIG. 10A  as zero. This sensor outputs the inclination degree upon inclination in the direction shown in  FIG. 10B  as a positive detection value, and outputs the inclination degree upon inclination in the direction shown in  FIG. 10C  as a negative detection value. In this case, the output of this inclination degree sensor will indicate the moment My about the Y-axis that acts on force receiving member  110 . 
   As mentioned above, with the force detection device described in §1, the four capacitance elements C 1  to C 4 , constituted of the four fixed electrodes E 1  to E 4 , shown in  FIG. 4 , and the four displaceable electrodes F 1  to F 4 , shown in  FIG. 7 , function as inclination degree sensors that detect the inclination degree of displaceable top plate  130  with respect to fixed top plate  330 . Since this inclination degree sensor can detect an inclination degree in relation to the X-axis direction as a difference, (C 1 −C 2 ), between the static capacitance value of first capacitance element C 1  and the static capacitance value of second capacitance element C 2 , a moment My about the Y-axis is consequently detected as the value of (C 1 −C 2 ). 
   The detection of a moment Mx about the X-axis that acts on force receiving member  110  can also be detected based on exactly the same principle. A moment Mx about the X-axis acts on force receiving member  110  in  FIG. 3  as a force that pushes an action point P 4  downwards perpendicularly with respect to the paper surface and pushes an action point P 3  upwards perpendicularly with respect to the paper surface. Displaceable top plate  130  thus undergoes an inclination in relation to the Y-axis direction with respect to fixed top plate  330 . Since with the force detection device described in §1, the inclination degree in relation to the Y-axis direction can be detected as the difference, (C 4 −C 3 ), between the static capacitance value of third capacitance element C 3  and the static capacitance value of fourth capacitance element C 4 , a moment Mx about the X-axis is consequently detected as the value of (C 4 −C 3 ). Here, (C 4 −C 3 ) is used in consideration of obtaining an Mx with the correct sign. 
   Thus by using the force detection device of the basic embodiment described in §1, the five components of a force Fx in the X-axis direction, a force Fy in the Y-axis direction, a force Fz in the Z-axis direction, a moment Mx about the X-axis, and a moment My about the Y-axis that act on force receiving member  110  can be detected in consideration of their respective signs.  FIG. 11  shows a table that indicates, in consideration of the signs of the acting forces, the modes of variation of the static capacitance values of the respective capacitance elements C 1  to C 9  when forces of these five components act, and here “0” indicates no change, “+” indicates an increase, and “−” indicates a decrease. 
   In consideration that the results such as those shown in the table of  FIG. 11  are obtained, by preparing, as detection processing unit  250  shown as a block in  FIG. 1 , a circuit that measures the static capacitance values of the nine capacitance elements C 1  to C 9  and a processing device that performs operations based on the equations shown in  FIG. 12 , it becomes possible to obtain the five components of Fx, Fy, Fz, Mx, and My. 
   The equations shown in  FIG. 12  are equations in which the sign of the force that is obtained is considered. For example, a force Fx in the X-axis direction is determined by the difference, (C 7 −C 6 ), a force Fy in the Y-axis direction is determined by the difference, (C 9 −C 8 ), and the sign of each of these differences indicates whether the force is directed in the positive direction or the negative direction of the respective coordinate axis. Likewise, the moment Mx about the X-axis is determined by the difference (C 4 −C 3 ), the moment My about the Y-axis is determined by the difference (C 1 −C 2 ), and the sign of each of these differences indicates whether the moment is a positive direction moment (with a direction of rotation by which a right-handed screw is made to progress in the positive direction of the corresponding axis) about the respective coordinate axis or a negative direction moment (with a direction of rotation by which a right-handed screw is made to progress in the negative direction of the corresponding coordinate axis) about the respective axis. With regard to a force Fz in the Z-axis direction, since this is determined not as a difference of the static capacitance values of two capacitance elements but is determined by the static capacitance value C 5  of fifth capacitance element C 5  alone, the amount of increase or decrease of this capacitance value C 5  with respect to a predetermined reference value indicates the magnitude of the force Fz that acts in the Z-axis direction as described above. Though in the equation of  FIG. 12 , Fz=−C 5  and a minus sign is added to the front, this indicates that the increase/decrease relationship of the capacitance value C 5  is opposite in sign to the force Fz (that is, an amount of increase of C 5  indicates a force −Fz in the negative Z-axis direction and an amount of decrease of C 5  indicates a force +Fz in the positive Z-axis direction). Also, as can be understood from the table of  FIG. 11 , a force Fz in the Z-axis direction can be determined by the equation, Fz=−(C 1 +C 2 +C 3 +C 4 +C 5 ) or Fz=−(C 1 +C 2 +C 3 +C 4 ). 
   As mentioned above, in the table of  FIG. 11 , a cell in which “+” is indicated signifies that when the corresponding force acts, the static capacitance value of the corresponding capacitance element increases and a cell in which “−” is indicated signifies that when the corresponding force acts, the static capacitance value of the corresponding capacitance element decreases. The reasons why such increases and decreases of static capacitance values occur have been described above using the schematic diagrams of  FIGS. 8A to 10C . On the other hand, though a cell in which “0” is indicated signifies that even when the corresponding force acts, the static capacitance value of the corresponding capacitance element does not change, in actuality, the change of static capacitance will not necessarily be completely zero in all such cases. The validity of the contents of the respective cells of the table of  FIG. 11  in which “0” is indicated shall now be examined. 
   In the rows of ±Fx and rows of ±Fy in the table of  FIG. 11 , the contents of all of the cells for capacitance elements C 1  to C 5  are “0,” and this is based on the premise that when a deformation such as that shown in  FIG. 8B  or  8 C occurs, the distance between displaceable top plate  130  and fixed top plate  330  does not change at all. However in actuality, since when side surfaces deform to a parallelogram as shown in  FIG. 8B  or  8 C, the distance between displaceable top plate  130  and fixed top plate  330  is slightly shortened, the contents of the respective cells mentioned above should not be “0” but should be “+.” Also, even when just a force Fx in the X-axis direction acts on force receiving member  110 , since the force is transmitted to displaceable top plate  130  via connecting member  120 , the force will not necessarily be transmitted as a force that moves displaceable top plate  130  in parallel in the right direction of the figure but may cause displaceable top plate  130  to become slightly inclined from the level state as well. However when a force ±Fx actually acts, the changes of the static capacitance values of capacitance elements C 1  to C 5  will be small in comparison to the changes of the static capacitance values of capacitance elements C 6  and C 7 , and when a force ±Fy acts, the changes of the static capacitance values of capacitance elements C 1  to C 5  will be small in comparison to the changes of the static capacitance values of capacitance elements C 8  and C 9 . Thus within the range of measurement precision in which the changes of the static capacitance values of capacitance elements C 1  to C 5  when a force Fx or Fy acts can be ignored, the contents of the abovementioned cells can be considered as being practically “0.” 
   Also in the rows of ±Fx in the table of  FIG. 11 , the contents of the cells for capacitance elements C 8  and C 9  are “0,” and this is based on the premise that when a deformation such as shown in  FIG. 8B  or  8 C occurs, third displaceable plate  143  and fourth displaceable plate  144  will be kept in vertical states and will not become inclined. This premise is also not necessarily satisfied in actuality. In particular, with the basic embodiment described in §1, since outer box-like structure  100  deforms in an overall manner, it can be considered that the abovementioned premise will not be satisfied completely. However, even in this case, the changes will normally be within a range that can be ignored in comparison to the changes of the static capacitance values of the cells in which “+” or “−” is indicated and can thus be considered to be “0.” The same applies likewise to the cells for capacitance elements C 6  and C 7  in the rows of ±Fy. 
   The same reason applies furthermore as to why the contents of the cells for capacitance elements C 6  to C 9  in the rows of ±Fz in the table of  FIG. 11  are “0.” That is, when a deformation such as shown in  FIG. 9B  or  9 C occurs, though first displaceable plate  141  to fourth displaceable plate  144  will not necessarily be kept in the vertical states and thus slight changes may occur in the static capacitance values of capacitance elements C 6  to C 9 , it can be considered that such changes will normally be within a range that can be ignored. 
   Next, in the table of  FIG. 11 , the contents of the cells for capacitance element C 5  in the rows of ±Mx and the rows of ±My are “0.” The contents of these cells for capacitance element C 5  are “0” based on the reasoning that fifth fixed electrode E 5 , shown in  FIG. 4 , and fifth displaceable electrode F 5 , shown in  FIG. 7 , have shapes that are symmetrical with respect to the X-axis and Y-axis and thus even when a deformation such as that shown in  FIG. 10B  or  10 C occurs, the electrode interval of capacitance element C 5  will increase at a part but decrease at another part so that in total, the static capacitance value C 5  will not change. Thus though the contents of the cells for capacitance element C 5  may not actually be completely zero, there will not be a problem normally even if these are handled as being zero. The reason why the contents of the cells for capacitance elements C 1  and C 2  in the rows of ±Mx are “0” and why the contents of the cells for capacitance elements C 3  and C 4  in the rows of ±My are “0” is the same, and with these cases, it can be considered that though the electrode interval will increase at a part, it will decrease at another part so that the electrode interval will not change in total. 
   Also, the reason why the contents of the cells for capacitance elements C 6  to C 9  in the rows of ±Mx and ±My in the table of  FIG. 11  are “0” is because, even though when a deformation such as that shown in  FIG. 10B  or  10 C occurs, first displaceable plate  141  to fourth displaceable plate  144  may not necessarily be kept in the vertical states and thus slight changes may occur in the static capacitance values of capacitance elements C 6  to C 9 , it can be considered that such changes will normally be within a range that can be ignored. 
   As another factor by which a “0” in the table shown in  FIG. 11  may not be strictly “0,” the effective areas of the electrodes must be considered. The parameters that determine the static capacitance value of a capacitance element are the dielectric constant between the electrodes, the electrode interval, and the electrode area. Though in the description up until now, only the electrode interval of a capacitance element was noted in considering changes of the static capacitance value, the electrode area of a capacitance element is also a parameter that changes the static capacitance value. Thus when a planar deviation occurs in the pair of opposing electrodes that constitute a capacitance element, the effective area in terms of the electrodes that constitute the capacitance element decreases and the static capacitance value thus changes. 
   In consideration of this point, the contents of the cells for capacitance elements C 8  and C 9  in the rows of ±Fx in the table of  FIG. 11  are also affected by changes in the effective area of the electrodes and will not be strictly “0” due to this factor as well. For example, with the structure shown in  FIG. 5 , if due to an external force +Fx, first displaceable plate  141  and second displaceable plate  142  become inclined in the right direction of the figure and, as a result, the positions of third displaceable plate  143  and fourth displaceable plate  144  become shifted even slightly in the right direction of the figure, the effective areas in terms of the electrodes that constitute the capacitance elements decrease and changes of the static capacitance values of C 8  and C 9  cannot be avoided even if there are no changes in the electrode intervals of the electrode pair E 8 /F 8  and electrode pair E 9 /F 9 . However, as long as the change of static capacitance value that is caused by such a change of effective area is within a range that can be ignored in comparison to a change of static capacitance value in a cell in which “+” or “−” is indicated, there will be no problem in setting the contents of the respective cells mentioned above to “0.” 
   Thus in the table shown in  FIG. 11 , though with the cells in which “0” is indicated, the change of static capacitance value may not be strictly zero, if the degrees of change in the cells in which “+” or “−” is indicated are adequately significant in comparison to the degrees of change in the cells in which “0” is indicated, the five force components can be detected independent of each other by the detection principles based on this table. Designs, for making the actual capacitance value changes, which are related to the cells in which “0” is indicated, close to zero, shall be described in detail in §4 and §5. 
   Though with the force detection device described in §1, first displaceable plate  141  to fourth displaceable plate  144  and displaceable top plate  130  are prepared as side surfaces and the top surface of outer box-like structure  100  and first fixed plate  341  to fourth fixed plate  344  and fixed top plate  330  are prepared as side surfaces and the top surface of inner box-like structure  300 , such box structures do not have to be used necessarily in putting this invention to practice. For example, for detection of a force Fx in the X-axis direction and a moment My about the Y-axis, it is adequate to prepare just the structure shown in  FIG. 8A . 
   Also, though with the force detection device described in §1, first displaceable plate  141  to fourth displaceable plate  144  and first fixed plate  341  to fourth fixed plate  344  are positioned so as to be perpendicular to base plate  200  (and parallel to the YZ plane or the XZ plane), in principle, these do not necessarily have to be positioned perpendicular to base plate  200 . 
   That is, it is sufficient that first displaceable plate  141  be positioned along a plane that intersects with a positive part of the X-axis and be supported directly on or indirectly via a member that undergoes elastic deformation on base plate  200  so as to be displaceable, second displaceable plate  142  be positioned along a plane that intersects with a negative part of the X-axis and be supported directly on or indirectly via a member that undergoes elastic deformation on base plate  200  so as to be displaceable, third displaceable plate  143  be positioned along a plane that intersects with a positive part of the Y-axis and be supported directly on or indirectly via a member that undergoes elastic deformation on base plate  200  so as to be displaceable, and fourth displaceable plate  144  be positioned along a plane that intersects with a negative part of the Y-axis and be supported directly on or indirectly via a member that undergoes elastic deformation on base plate  200  so as to be displaceable. 
   Also, it is sufficient that first fixed plate  341  be positioned between the Z-axis and first displaceable plate  141  and be fixed in some form onto base plate  200 , second fixed plate  342  be positioned between the Z-axis and the second displaceable plate  142  and be fixed in some form onto base plate  200 , third fixed plate  343  be positioned between the Z-axis and third displaceable plate  143  and be fixed in some form onto base plate  200 , and fourth fixed plate  344  be positioned between the Z-axis and fourth displaceable plate  144  and be fixed in some form onto base plate  200 . 
   Furthermore, it is sufficient that fixed top plate  330  be positioned along a plane spanning the vicinity of the upper edge of first fixed plate  341  and the vicinity of the upper edge of second fixed plate  342  and be fixed in some form to base plate  200  and displaceable top plate  130  be positioned above fixed top plate  330 , be supported via a member that undergoes elastic deformation so as to be displaceable with respect to substrate  200 , and be able to transmit forces along the XY plane onto the upper edge of first displaceable plate  141  and the upper edge of second displaceable plate  142 . 
   &lt;&lt;&lt;§3. Detection of a Moment Mz about the Z-axis &gt;&gt;&gt; 
   With respect to the force detection device of the basic embodiment described in §1, the detection operations were explained in §2 so that the five force components of Fx, Fy, Fz, Mx, and My can be detected separately and independent of each other by carrying out calculations based on the equations shown in  FIG. 12 . Here, designs for detecting a sixth forth component, in other words, a moment Mz about the Z-axis shall be described. 
     FIG. 13  is a top view showing the state in which a positive moment +Mz about the Z-axis is acting on force receiving member  110  of this force detection device. As illustrated, the moment +Mz is a force that rotates force receiving member  110  counterclockwise and is a force that moves action points P 1  to P 4  on force receiving member  110  counterclockwise about the Z-axis. Since such a force is transmitted via connecting member  120  to displaceable top plate  130  as a twisting force, first displaceable plate  141  to fourth displaceable plate  144  become deflected as illustrated and displaceable top plate  130  also rotates counterclockwise. Needless to say, the rotation angle here will be in accordance with the magnitude of the acting moment Mz about the Z-axis. Thus by providing a rotation angle sensor for detecting a rotation angle about the Z-axis of displaceable top plate  130  with respect to fixed top plate  330 , a moment Mz about the Z-axis that acts on force receiving member  110  can be detected based on the detection value of this rotation angle sensor. 
   Actually, the magnitude of this rotation angle can be detected using first capacitance element C 1  to fourth capacitance element C 4 . The principle shall now be described with reference to the top projections of  FIGS. 14A to 14C .  FIG. 14A  is a top projection showing the positional relationships of the five fixed electrodes E 1  to E 5  formed on the top surface of fixed top plate  330  and the five displaceable electrodes F 1  to F 5  formed on the bottom surface of displaceable top plate  130  in the state in which no external force is acting on the force detection device of the basic embodiment described in §1. Here, the hatching indicates the effective areas of the electrode pairs that constitute a capacitance element and does not indicate cross sections. As illustrated, in this state, the five displaceable electrodes F 1  to F 5  completely overlap with the five fixed electrodes E 1  to E 5  and the region corresponding to the total area (hatched part) of the actual electrodes contributes as a capacitance element. 
   However, when as shown in  FIG. 13 , a positive moment +Mz about the Z-axis acts and displaceable top plate  130  rotates counterclockwise, the positional relationships of the respective electrodes change as shown in  FIG. 14B . That is, though the positional relationship of the circular fixed electrode E 5  and displaceable electrode F 5 , which are disposed at the center, do not change, since the four displaceable electrodes F 1  to F 4  (indicated by the broken lines) move counterclockwise, the effective area indicated by the hatching decreases. The static capacitance values of all four capacitance elements C 1  to C 4  thus decrease. Here, since the static capacitance value of capacitance element C 5 , formed by the electrode pair E 5 /F 5 , does not change, in the case where changes occur in C 1  to C 4  even though there is no change in C 5 , it can be judged a moment Mz about the Z-axis is acting. 
   By making use of such principle, the magnitude of a moment Mz about the Z-axis can be detected even with the force detection device of the basic embodiment described in §1. However, the direction of moment Mz cannot be detected. That is, even in the case where a negative moment −Mz about the Z-axis acts and displaceable top plate  130  rotates clockwise, though the positional relationships of the respective electrodes will change as shown in  FIG. 14C , the values of the static capacitance value C 1  to C 4  will still decrease. Thus though in the case where changes occur in C 1  to C 4  and there is no change in C 5 , the degree of change indicates the magnitude of the moment Mz about the Z-axis, the direction in which the moment is acting (that is, the sign of Mz) cannot be specified. 
   To perform detection that considers the direction (sign) of a moment Mz about the Z-axis, displaceable electrodes F 1  to F 4  are positioned at positions that are offset in a predetermined rotation direction with respect to the positions at which they oppose fixed electrodes E 1  to E 4 . By doing so, it becomes possible to detect the rotation direction along with the rotation angle based on increases or decreases of the static capacitance values of capacitance elements C 1  to C 4 . 
   For example, five fixed electrodes EE 1  to EE 5  are formed on the top surface of fixed top plate  330  as shown in  FIG. 15A . That is, when the X-axis and the Y-axis are projected onto the top surface of fixed top plate  330 , first fixed electrode EE 1  is formed on the projected image of a positive part of the X-axis, second fixed electrode EE 2  is formed on the projected image of a negative part of the X-axis, third fixed electrode EE 3  is formed on the projected image of a positive part of the Y-axis, fourth fixed electrode EE 4  is formed on the projected image of a negative part of the Y-axis, and fifth fixed electrode EE 5  is formed on the projected image of the origin O. Though in this example, fixed electrodes EE 1  to EE 4  have vane-like shapes, these do not have to be vane-like in shape. Also, fifth fixed electrode EE 5  is used for the detection of a force Fz in the Z-axis direction and is not used in the detection of a moment about the Z-axis. 
   Meanwhile, on the bottom surface of displaceable top plate  130 , five displaceable electrodes FF 1  to FF 5  are formed as shown in  FIG. 15B .  FIG. 15B  does not show the bottom surface of displaceable top plate  130  but shows the positions of five displaceable electrodes FF 1  to FF 5  with respect to fixed top plate  330 , in other words, shows the projected images when the five displaceable electrodes FF 1  to FF 5 , formed on the bottom surface of displaceable top plate  130 , are projected onto the top surface of fixed top plate  330 . Thus in  FIG. 15B , fixed top plate  330  and the five displaceable electrodes FF 1  to FF 5  are shown by broken lines. 
   In both  FIGS. 15A and 15B , reference axes W 1  and W 2  are indicated by broken lines. These reference axes W 1  and W 2  correspond to the diagonals of a square that forms the top surface of fixed top plate  330 . A comparison of the positional relationships of the respective reference axes W 1  and W 2  and the respective fixed electrodes EE 1  to EE 4  shown in  FIG. 15A  and the positional relationships of the respective reference axes W 1  and W 2  and the respective displaceable electrodes FF 1  to FF 4  shown in  FIG. 15B  shows that displaceable electrodes FF 1  to FF 4  are positioned at positions that are offset by just a predetermined rotation angle in the clockwise direction. For example, first displaceable electrode FF 1  is positioned at a position that is offset by just a predetermined rotation angle in the clockwise direction with respect to the position that opposes first fixed electrode EE 1 . 
     FIGS. 16A to 16C  show top projections for illustrating the changes of the effective areas of the electrodes in the force detection device with such an offset electrode configuration. The hatching does not indicate cross sections but indicates the effective areas of electrode pairs that constitute capacitance elements in this figure as well. First,  FIG. 16A  shows the positional relationships of the five fixed electrodes EE 1  to EE 5  (indicated by solid lines), formed on the top surface of fixed top plate  330 , and the five displaceable electrodes FF 1  to FF 5  (indicated by broken lines), formed on the bottom surface of displaceable top plate  130 , in the state in which no external force is acting. As illustrated, in this state, the four displaceable electrodes FF 1  to FF 4  are shifted by just an offset angle δ  0  with respect to the four fixed electrodes EE 1  to EE 4 . In this state, the effective areas in terms of the electrodes constituting the capacitance elements are the areas of the regions indicated by the hatching in the figure. 
   Here, when a positive moment +Mz about the Z-axis acts and displaceable top plate  130  rotates counterclockwise, the positional relationships of the respective electrodes change as shown in  FIG. 16B . That is, the offset angle decreases to δ  1  and the effective areas of the electrodes increase. This means that the static capacitance values of the four capacitance elements C 1  to C 4  increase. Oppositely, when a negative moment −Mz about the Z-axis acts and displaceable top plate  130  rotates clockwise, the positional relationships of the respective electrodes change as shown in  FIG. 16C . That is, the offset angle increases to δ  2  and the effective areas of the electrodes decrease. This means that the static capacitance values of the four capacitance elements C 1  to C 4  decrease. Thus by determining the sum of the static capacitance values of the four capacitance elements C 1  to C 4 , the rotation angle and the rotation direction can be determined based on the increase or decrease of this sum. 
   The table shown in  FIG. 17  has the rows for moments ±Mz about the Z-axis added to the table of  FIG. 11 , and with the equations shown in  FIG. 18 , an equation concerning Mz is added to the equations shown in  FIG. 12 . Thus by using fixed electrodes EE 1  to EE 5 , shown in  FIG.15A , and displaceable electrodes FF 1  to FF 5 , shown in  FIG. 15B , in place of the fixed electrodes E 1  to E 5  and displaceable electrodes F 1  to F 5  of the force detection device described in §1, detection by the principles illustrated in the table of  FIG. 17  becomes possible and the six components of Fx, Fy, Fz, Mx, My, and Mz can be detected independent of each other as indicated by the equations of  FIG. 18 . 
   As is clear from the table of  FIG. 17 , even if all of the static capacitance values of capacitance elements C 1  to C 4  increase or decrease, the cause of such increase or decrease is not necessarily based on the actions of a moment Mz about the Z-axis in all cases. This is because increases or decreases of the static capacitance values of capacitance elements C 1  to C 4  can also occur due to the action of a force Fz in the Z-axis direction. Meanwhile, an increase or decrease of the static capacitance value of capacitance element C 5  will mostly be due to the action of a force Fz in the Z-axis direction. Thus under an environment in which a force Fz in Z-axis direction acts, a correction of eliminating the amount due to the action of a Z-axis direction force Fz must be performed on the sum of the static capacitance values of the four capacitance elements C 1  to C 4  and the corrected value must be used as that of the moment Mz about the Z-axis. The correction term f (Fz) indicated in the equation for Mz in  FIG. 18  is a term for performing such a correction. 
   &lt;&lt;&lt;§4. Embodiment with a Simplified Electrode Configuration &gt;&gt;&gt; 
   With the embodiment described in §1, nine fixed electrodes E 1  to E 9  are formed on the inner box-like structure  300  and nine displaceable electrodes F 1  to F 9  are formed on the outer box-like structure  100 , that is, a total of 18 electrodes are used to arrange a total of nine capacitance elements C 1  to C 9 . However, 18 electrodes are not necessarily required to arrange the nine capacitance elements. For example, the nine fixed electrodes E 1  to E 9  may be arranged as a single common fixed electrode or the nine displaceable electrodes F 1  to F 9  can be arranged as single common displaceable electrodes. The embodiment described here is an example of the latter. According to this embodiment, though nine fixed electrodes E 1  to E 9  must be formed on the inner box-like structure  300 , a single common displaceable electrode is arranged on the outer box-like structure  100  to simplify the electrode configuration. 
   Moreover with the embodiment described here, since outer box-like structure  100  is formed of a conductive material and first displaceable plate  141  to fourth displaceable plate  144  and displaceable top plate  130  are themselves used as displaceable electrodes, the electrode configuration can be practically realized by simply preparing nine fixed electrodes E 1  to E 9  on the inner box-like structure  300 . 
     FIG. 19  is a side view in section (section along the XZ plane) showing the basic arrangement of a force detection device of an embodiment to be described in this §4 and corresponds to  FIG. 2  for the embodiment described in §1. The differences with respect to the force detection device shown in  FIG. 2  are that force receiving member  110 , connecting member  120 , and outer box-like structure  100  (displaceable top plate  130 , first displaceable plate  141  to fourth displaceable plate  144 , and pedestal  150 ) are formed of a conductive material and displaceable electrodes F 1  to F 9  are all omitted. Since the entirety of outer box-like structure  100  is formed of a conductive material, the parts of outer box-like structure  100  that oppose the respective fixed electrodes E 1  to E 9  serve the functions of displaceable electrodes F 1  to F 9 , respectively. In other words, outer box-like structure  100  itself functions as a single common displaceable electrode. The detection operations of the force detection device shown in  FIG. 19  are exactly the same as the detection operations of the force detection device shown in  FIG. 2  and are as has been described in §2. 
   Though the force detection device shown in  FIG. 19  thus has the merit of being simple in mechanical structure in comparison to the force detection device shown in  FIG. 2 , this is not the only merit. In §2, a change of the effective area of an electrode was described as a cause as to why “0” is not realized strictly even when “0” is indicated in the table shown in  FIG. 11 . For example, as has been described above, with the force detection device shown in  FIG. 2 , when for the structure shown in  FIG. 5 , first displaceable plate  141  and second displaceable plate  142  become inclined in the right direction of the figure due to the action of an external force +Fx and consequently the positions of third displaceable plate  143  and fourth displaceable plate  144  becomes shifted even slightly in the right direction in the figure, the effective areas of the electrode pair E 8 /F 8  and the electrode pair E 9 /F 9  decrease and cause changes in the static capacitance values C 8  and C 9 . However, with the force detection device shown in  FIG. 19 , changes in the static capacitance values due to such a cause will not occur. 
   To be specific, with the force detection device shown in  FIG. 19 , capacitance element C 6  is constituted of fixed electrode E 6  and a displaceable electrode formed by a part (the region that opposes fixed electrode E 6 ) of displaceable plate  141 , and here, no matter how displaceable plate  141  becomes displaced, the effective electrode area that constitutes capacitance element C 6  is fixed. That is, by setting the area of either one of the fixed electrode and displaceable electrode, which constitute a capacitance element as a pair, wider than the area of the other, the static capacitance value can be prevented from changing even if the displaceable electrode undergoes a displacement within a predetermined range in a planar direction. With the force detection device shown in  FIG. 19 , since outer box-like structure  100  is a single common displaceable electrode, the area of a displaceable electrode will always be set wider than the area of a fixed electrode and a change in the static capacitance value will not occur even if the displaceable electrode is displaced in a planar direction. 
   A metal is most suited as the conductive material for forming outer box-like structure  100 . Due to the principles of detection by this force detection device, outer box-like structure  100  must be able to undergo elastic deformation with some degree of freedom. A metal has the property of being able to undergo some degree of elastic deformation, is conductive, and moreover has integrity. With the force detection device shown in  FIG. 19 , for example, force receiving member  110 , connecting member  120 , and outer box-like structure  100  may be formed of a metal, such as aluminum. Base plate  200  and inner box-like structure  300  may be formed of an insulating material, such as a ceramic. However, in order to avoid the occurrence of changes in the electrode intervals of the capacitance elements due to thermal expansion of the respective parts caused by changes of the temperature environment, all parts are preferably formed of the same metal, such as aluminum. When all parts are formed of the same metal, since fixed electrodes E 1  to E 9  must be in electrically separated states, for example, ceramic substrates may be adhered onto the outer surfaces of inner box-like structure  300  and the respective fixed electrodes E 1  to E 9  may be formed on top of these ceramic substrates. Ceramic substrates are excellent in insulating property, small in the thermal expansion coefficient, and are thus optimal for the above use. Needless to say, in putting the present invention into practice, the materials of the respective parts are not restricted to specific materials 
   With the arrangement shown in  FIG. 19 , a force detection device with the function of detecting a moment Mz about the Z-axis cannot be realized as described in §3. This is because displaceable top plate  130 , which is conductive, acts in itself as a single common displaceable electrode with respect to fixed electrodes E 1  to E 4  and even when a rotational displacement about the Z-axis occurs with displaceable top plate  130 , a change in effective area will not occur in terms of the electrodes constituting capacitance elements C 1  to C 4 . 
   In order to realize a force detection device with the function detecting a moment Mz about the Z-axis, an arrangement such as shown in the side view in section of  FIG. 20  may be used. Though this force detection device is the same as the force detection device shown in  FIG. 19  in that the entirety of outer box-like structure  100  is formed of a conductive material, here, five displaceable electrodes FF 1  to FF 5  are formed on an insulating layer  160  on the bottom surface of displaceable top plate  130  and five fixed electrodes EE 1  to EE 5  are formed on the top surface of fixed top plate  330  so as to oppose the displaceable electrodes. Here, displaceable electrodes FF 1  to FF 4  and fixed electrodes EE 1  to EE 4  are positioned as shown in  FIGS. 15A and 15B  and arranged so that there is an offset in a predetermined rotation direction. 
     FIG. 21  is a plan view showing an example of an electrode configuration of fixed electrodes and displaceable electrodes that is considered to be most preferable in realizing a force detection device having the function of detecting a moment Mz about the Z-axis. The five electrodes EE 1 ′ to EE 5 ′ shown in the figure are fixed electrodes positioned on the top surface of fixed top plate  330 , and the opposing electrodes FF 1 ′ to FF 5 ′ are displaceable electrodes positioned on the bottom surface of displaceable top plate  130 .  FIG. 21  is a plan view showing the state in which displaceable electrodes FF 1 ′ to FF 5 ′ are positioned above fixed electrodes EE 1 ′ to EE 5 ′, and the parts of fixed electrodes EE 1 ′ to EE 5 ′ that are indicated by broken lines are the parts that are hidden below displaceable electrodes FF 1 ′ to FF 5 ′. As illustrated there is an offset in a predetermined rotation direction between displaceable electrodes FF 1 ′ to FF 4 ′ and fixed electrodes EE 1 ′ to EE 4 ′. 
   Also as illustrated, whereas the five electrodes EE 1 ′ to EE 5 ′ are electrodes that are physically independent of each other, displaceable electrodes FF 1 ′ to FF 5 ′ are fused mutually and form a single common displaceable electrode. Even when displaceable electrodes FF 1 ′ to FF 5 ′ are thus arranged as a single common displaceable electrode, five capacitance elements C 1  to C 5  are still constituted and the six force components can be detected based on the principles shown by the table of  FIG. 17 . 
   With the electrode configuration shown in  FIG. 21 , displaceable electrodes FF 1 ′ to FF 5 ′ are arranged as a single common displaceable electrode and the area of each individual displaceable electrode is set to be always wider than the area of a fixed electrode. Thus even if a displaceable electrode is displaced in a planar direction (a direction parallel to the XY plane), erroneous detection of this displacement as a moment Mz about the Z-axis can be prevented. For example, even if the entirety of displaceable electrodes FF 1 ′ to FF 5 ′ moves slightly parallel in the right direction of the figure from the state shown in  FIG. 21 , (such a parallel movement will occur if a force +Fx is applied), the effective area related to the electrode pair EE 1 ′/FF 1 ′ and the effective area related to the electrode pair EE 2 ′/FF 2 ′ will not change. Though in this case, the effective area related to the electrode pair EE 3 ′/FF 3 ′ will increase, since the effective area related to the electrode pair EE 4 ′/FF 4 ′ will oppositely decrease, the total of the static capacitance values of the four capacitance elements will not change. In the equation shown in  FIG. 18 , a moment Mz about the Z-axis is detected by the total of the static capacitance values of the four capacitance elements C 1  to C 4  in consideration of this merit. With the electrode configuration shown in  FIG. 21 , when a force +Fx is applied, since the static capacitance value C 3  increases and C 4  decreases, the same capacitance value changes as those of the cells of ±Mx in the table of  FIG. 17  occur. However, since the capacitance change due to an increase or decrease of the effective area of an electrode is adequately small in comparison to a capacitance change caused by an increase or decrease of an electrode interval, a force Fx in the X-axis direction will not be detected significantly as a moment Mx about the X-axis. Likewise, a force Fy in the Y-axis direction will not be detected significantly as a moment My about the Y-axis. 
   &lt;&lt;&lt;§5. Embodiment with a Practical Structure &gt;&gt;&gt; 
   With the force detection device of the basic embodiment described in §1, outer box-like structure  100 , having a rectangular parallelepiped shape with an open bottom surface and formed of a material that undergoes elastic deformation due to the action of an external force, has its bottom surface joined to base plate  200  so as to be set on the base plate, the four side plates  141  to  144  of this outer box-like structure  100  are used as the displaceable plates, and top plate  130  of this outer box-like structure  100  is used as the displaceable top plate. Also, inner box-like structure  300 , having a rectangular parallelepiped shape that is smaller than outer box-like structure  100 , is joined to base plate  200  in the state in which it is contained in outer box-like structure  100 , and the four side plates  341  to  344  and top plate  330  of this inner box-like structure  300  are used as the fixed plates and the fixed top plate. 
   Such use of outer box-like structure  100  and inner box-like structure  300  is useful in that the components necessary for carrying out the present invention can be positioned at the required position by comparatively simple structures. However, the structure of the basic embodiment described in §1 may not always carry out measurements at adequate precision. The reason is that, as was described in §2, though in the table of  FIG. 11  or  17 , the cells in which “0” is indicated signifies that even when a corresponding force acts, changes will not occur in the static capacitance values of the corresponding capacitance elements, in actuality, the changes of the static capacitance values will not be completely zero in all of these cases. If a significant change in static capacitance value is detected in relation to a cell in which “0” is indicated in an abovementioned table, the detection result of each individual force component will be interfered by the other force components and it will not be possible to detect the respective force components independent of each other. 
   In order to eliminate the interference of other force components as much as possible and obtain detection values of high precision, a structure satisfying the following conditions must be realized. A first condition is that when a force Fx in the X-axis direction or a force Fy in the Y-axis direction acts on force receiving member  110 , though displacements will occur with displaceable electrodes F 6  to F 9 , which are formed at the displaceable plates  141  to  144 , no displacement will occur with displaceable electrodes F 1  to F 5 , which are formed on the displaceable top plate  130  or even if displacements occur, such displacements will be extremely small in comparison to the displacements that occur with displaceable electrodes F 6  to F 9 . A second condition is that when a force Fz in the Z-axis direction, a moment Mx about the X-axis, or a moment My about the Y-axis acts on force receiving member  110 , though displacements will occur with displaceable electrodes F 1  to F 5 , which are formed on the displaceable top plate  130 , no displacement will occur with displaceable electrodes F 6  to F 9 , which are formed on displaceable plates  141  to  144 , or even if displacements occur, such displacements will be extremely small in comparison to the displacements that occur with displaceable electrodes F 1  to F 5 . 
   Here, modification examples with structural designs that are effective for satisfying the above two conditions shall be described. First, with the modification example shown in  FIG. 22 , a U-shaped slit S, which opens upward, is formed in a side plate  140  of the force detection device of the basic embodiment shown in  FIG. 1  and a part  140 A that is surrounded by this slit S is used as a displaceable plate. As illustrated, due to U-shaped slit S, side plate  140  is divided into a part  140 A, which is surrounded by slit S, and a margin plate  140 B at the outer side of slit S. Here, the part  140 A, which is surrounded by slit S, is used as a displaceable plate. Since outer box-like structure  100  actually has first side plate  141  to fourth side plate  144 , U-shaped slits S 1  to S 4 , which open upward, are formed respectively in the four side plates to form first displaceable plate  141 A to fourth displaceable plate  144 A and margin plates  141 B to  144 B. 
   When a force Fx in the X-axis direction acts on outer box-like structure  100  in which slits S are formed in such a manner in the respective side plates, the overall frame structure of outer box-like structure  100  deform to a parallelepiped as shown in  FIG. 23 . However, since the parts forming this frame structure are parts, such as margin plates  141 B and  142 B that are at the outer sides of slits S, displaceable plates  141 A and  142 A, which are parts at the inner sides of slits S, move in parallel in the positive X-axis direction along with displaceable top plate  130 . It can be understood from a comparison of  FIG. 23  with  FIG. 8B  that by the forming of these slits S, the effect of increasing the displacements of displaceable plates  141 A and  142 A is provided. 
     FIG. 24  is a top view showing a state in which slits S 1  to S 4  are formed respectively in the four side plates  141  to  144  that form outer box-like structure  100  to thereby form first displaceable plate  141 A to fourth displaceable plate  144 A and margin plates  141 B to  144 B (force receiving member  110  and connecting member  120  are omitted from illustration). Here, if the edges parallel to the Z-axis at the intersections of two mutually adjacent side plates are considered as being columns, a total of four columns L 1  to L 4  are formed by margin plates  141 B to  144 B, which exist at the positions of the four corners of displaceable top plate  130  as illustrated. The structure is thus one in which displaceable top plate  130  is supported by these four columns L 1  to L 4  and outer box-like structure  100  deforms by the elastic deformation of these four columns L 1  to L 4 . 
   In other words, outer box-like structure  100 , which is shown in  FIGS. 22 and 24 , has a structure wherein four columns L 1  to L 4 , formed of a material that undergoes elastic deformation due to the action of an external force, are joined in a perpendicularly erected state to base plate  200  and the four corners of top plate  130 , which functions as a displaceable top plate, are joined to the upper ends of the four columns L 1  to L 4 . Moreover, each of displaceable plates  141 A to  144 A is positioned between a pair of mutually adjacent columns and the upper edge of each of displaceable plates  141 A to  144 A is joined to one edge of top plate  130 . Each of displaceable plates  141 A to  144 A is thus supported on base plate  200  by its upper edge being joined to one edge of top plate  130 . 
   With such a structure with slits S, when a force Fx in the X-axis direction or a force Fy in the Y-axis direction acts on force receiving member  110 , the displacements that occur in regard to displaceable electrodes F 1  to F 5 , formed on the displaceable top plate  130 , can be made extremely small in comparison to the displacements that occur in regard to displaceable electrodes F 6  to F 9 . The abovementioned first condition is thus satisfied. 
     FIG. 25  shows a top view of modification example with which a further improvement is added to the modification example of  FIG. 24  (force receiving member  110  and connecting member  120  are omitted from illustration). The difference with respect to the modification example shown in  FIG. 24  is that four “C”-shaped slits SS 1  to SS 4  are formed on top plate  130  as well. Each of these four “C”-shaped slits SS 1  to SS 4  is formed so that the open part of the letter “C” faces the center. Since  FIG. 25  is somewhat complicated, a plan view, with which just top plate  130  is extracted, is shown in  FIG. 26 . The parts drawn in gray in this figure are the parts that are partitioned by slits SS 1  to SS 4 . 
   That is, as illustrated, top plate  130  is partitioned into displaceable top plates  131  to  135 , which are positioned at the center, peripheral parts  136  to  139 , which are positioned at the periphery of the top plates, and four beams B 1  to B 4 , which has flexibility and connects the top plates and peripheral parts to each other. Displaceable top plates  131  to  135 , which are positioned at the center, are, as a whole, like the vanes of a fan, and are arranged so that when the X-axis and the Y-axis are projected onto this top plate  130 , a first vane-like part  131  is positioned at the projected image of a positive part of the X-axis, a second vane-like part  132  is positioned at the projected image of a negative part of the X-axis, a third vane-like part  133  is positioned at the projected image of a positive part of the Y-axis, a fourth vane-like part  134  is positioned at the projected image of a negative part of the Y-axis, and a central part  135 , which is connected to the inner side parts of the respective vane-like parts  131  to  134 , is positioned at the projected image of the origin O. The displaceable top plates are thus formed of parts (that is, vane-like parts  131  to  134  and central part  135 ) of top plate  130 . 
   Also, by the positioning of a beam between every two adjacent vane parts, central part  135  is structurally supported by the four beams B 1  to B 4 . That is, the inner ends of the four beams B 1  to B 4  are connected to central part  135  and the outer ends are connected to peripheral parts  136  to  139 . A force in a direction along the XY plane that acts on central part  135  is thus transmitted by the four beams B 1  to B 4  to peripheral parts  136  to  139  and furthermore to displaceable plates  141 A to  144 A. Connecting member  120  is connected to an action point Q on the top surface of central part  135  and an external force acting on force receiving member  110  is thereby transmitted to this action point. Meanwhile, action points Q 1  to Q 4 , to which the outer ends of the four beams B 1  to B 4  are connected, are respectively supported by columns L 1  to L 4 . Thus by the deflection of the four beams B 1  to B 4 , the entirety of the displaceable top plate, having the shape of the vanes of a fan, becomes displaced with respect to peripheral parts  136  to  139 . Moreover, at the positions of action points Q 1  to Q 4 , peripheral parts  136  to  139  are connected via columns L 1  to L 4  to base plate  200 . 
   By providing top plate  130  with such a structure, it becomes possible to cause large displacements to occur in regard to displaceable top plates  131  to  135 , which are like the vanes of a fan, when a force Fz in the Z-axis direction, a moment Mx about the X-axis, or a moment My about the Y-axis acts on force receiving member  110 . In particular, since the outer peripheral parts of vane-like parts  131  to  134  are arranged as free ends that are separated from peripheral parts  136  to  139  due to slits SS 1  to SS 4 , comparatively large displacements can be made to occur. Moreover, the displacements of these vane-like parts  131  to  134  will not be transmitted directly to peripheral parts  136  to  139 . Since forces Fz, Mx, and My, which are transmitted from connecting member  120  to action point Q, will be transmitted directly to vane-like parts  131  to  134 , vane-like parts  131  to  134  will be displaced effectively based on the forces Fz, Mx, and My and these forces are thus detected effectively based on the above-described principles. Meanwhile, since the forces Fz, Mx, and My are transmitted to peripheral parts  136  to  139  only via the four beams B 1  to B 4 , these will hardly be transmitted to displaceable plates  141  to  144  connected to peripheral parts  136  to  139 . This thus satisfies the abovementioned second condition, that is, the condition that when a force Fz, Mx, or My acts on force receiving member  110 , though displacements will occur with displaceable electrodes F 1  to F 5 , which are formed at the displaceable top plate side, the displacements that occur with displaceable electrodes F 6  to F 9 , which are formed on displaceable plates  141  to  144 , will be extremely small. 
     FIG. 27  is a top view of a modification example, with which further improvements are made on the modification example shown in  FIG. 25  (force receiving member  110  and connecting member  120  are omitted from illustration). This modification example provides the merit of improving the detection sensitivity of the force detection device with the function of detecting a moment Mz about the Z-axis, which was described in §3. As was shown in  FIG. 13 , in order to detect a moment Mz about the Z-axis, the entirety of outer box-like structure  100  must undergo a deformation of twisting about the Z-axis. When a structure, in which central part  135  is supported by four beams B 1  to B 4 , is employed as in the example shown in  FIG. 25 , since all four beams B 1  to B 4  are made flexible, a deformation of twisting about the Z-axis is much more likely to occur in comparison to a structure without slits, such as that shown in  FIG. 13 . With the modification example shown in  FIG. 27 , the structure of the four beams is designed so that this deformation of twisting about the Z-axis occurs even more readily. 
   That is, as illustrated, the four beams making the connection between columns L 1  to L 4  and central part  135  are respectively formed of horizontal beams B 11 , B 21 , B 31 , and B 41 , which are positioned at the outer side, intermediate joints B 12 , B 22 , B 32 , and B 42 , which are positioned in the middle, and vertical beams B 13 , B 23 , B 33 , and B 43 , which are positioned at the inner side.  FIG. 28  shows an enlarged perspective view of the third beam that is shown at the lower left of  FIG. 27 . As illustrated, horizontal beam B 31  is a beam with which its main surface faces the horizontal direction and has the property of deflecting readily in the vertical direction. On the other hand, beam B 33  is a beam with which its main surface faces the vertical direction and has the property of deflecting readily in the horizontal direction. Intermediate joint B 32  is a member that connects the two types of beams at the middle. By using such a beam, a structure with which both deflection in the vertical direction and deflection in the horizontal direction occur readily can be realized and a deformation of twisting about the Z-axis can be made to occur readily, thus making it possible to detect a moment Mz about the Z-axis readily. 
   The modification example shown in  FIG. 27  also differs from the example shown in  FIG. 25  in the shape of the displaceable top plate. That is, with the example shown in  FIG. 25 , a displaceable top plate with the shape of the vanes of a fan is provided by four vane-like parts  131  to  134 , each with the shape of an isosceles triangle, and circular central part  135 , positioned at the center. On the other hand, with the modification example shown in  FIG. 27 , though the circular central part  135  is the same, each of the four vane-like parts  131 A to  134 A are changed to the shapes illustrated. These shapes correspond to displaceable electrodes FF 1 ′ to FF 5 ′, shown in  FIG. 21 . That is, with the modification example shown here in  FIG. 27 , the entirety of top plate  130  is formed of a metal or other conductive material, and the displaceable top plate with the illustrated shape functions in itself as a single common displaceable electrode. Though in order to avoid the figure from becoming too complicated, the illustration of inner box-like structure  300  is omitted from  FIG. 27 , in actuality, fixed electrodes EE 1 ′ to EE 5 ′ are positioned at positions of the top surface of fixed top plate  330  that are offset as shown in  FIG. 21 . 
   &lt;&lt;&lt;§6. Embodiment Using a Control Member &gt;&gt;&gt; 
     FIG. 29  is a side view in section showing the structure of a modification example with which a control member  400  is added to the force detection device of the embodiment shown in  FIG. 19 . As mentioned above, with the force detection device of the embodiment of  FIG. 19 , an external force that acts on force receiving member  110  is transmitted to outer box-like structure  100 , and the acting external force is detected by recognition of the form of deformation that arises in outer box-like structure  100 . Outer box-like structure  100  thus has a structure that is provided with some degree of flexibility and undergoes elastic deformation by the action of an external force. However, when an excessive external force acts on force receiving member  110 , a force that exceeds the range of elastic deformation may be applied to outer box-like structure  100  and mechanical damage, such as the inability to return to the original shape even after the external force is eliminated or the forming of cracks in structural parts, etc. may be sustained. 
   The modification example shown in  FIG. 29  is an example wherein a control member  400 , for restricting the displacement of force receiving member  110  with respect to base plate  200  within a predetermined range, is provided in order to prevent mechanical damage due to the transmission of an excessive force to outer box-like structure  100  in the above-described manner. As illustrated, with this example, a control member  400 , which is erected from outer peripheral parts of base plate  200 , is provided. As illustrated, control surfaces  411 ,  412 , and  413  are formed on the control member  400 , and by the contacting of control surfaces  411 ,  412 , and  413  with a force receiving member  110 A, when force receiving member  110 A is about to be displaced beyond a predetermined range, such excessive displacements can be prevented. Force receiving member  110 A of this modification example shown in  FIG. 29  is formed of a disk that is larger in diameter than force receiving member  110  shown in  FIG. 19  and its circumferential parts are the surfaces opposing control surfaces  411 ,  412 , and  413 . 
   For example, displacement of this force receiving member  110 A downward (in the −Z direction) is restricted to be within the illustrated dimension d 1  by control surface  411 . Even if a large downward force acts on force receiving member  110 A, the bottom surface of force receiving member  110 A contacts control surface  411  at the point at which the downward displacement of force receiving member  110 A reaches the dimension d 1  and further displacement is thus prevented. 
   Also, displacement of force receiving member  110 A upward (in the +Z direction) is restricted to be within the illustrated dimension d 2  by control surface  412 . Even if a large upward force acts on force receiving member  110 A, the top surface of force receiving member  110 A contacts control surface  412  at the point at which the upward displacement of force receiving member  110 A reaches the dimension d 2  and further displacement is thus prevented. 
   Furthermore, displacement of force receiving member  110 A in a lateral direction (in the ±X direction or ±Y direction) is restricted to be within the illustrated dimension d 3  by control surface  413 . Even if a large force in a lateral direction acts on force receiving member  110 A, a side surface of force receiving member  110 A contacts control surface  413  at the point at which the displacement of force receiving member  110 A in the lateral direction reaches the dimension d 3  and further displacement is thus prevented. 
   The force detection device shown in  FIG. 29  is equipped with a function of enabling electrical detection of an anomaly when the anomalous situation of force receiving member  110  contacting any of control surfaces  411 ,  412 , and  413  occurs. That is, with this force detection device, force receiving member  110 A, connecting member  120 , displaceable top plate  130 , displaceable plate  140 , and pedestal  150  are arranged as an integral structure formed of a metal or other conductive material, and control member  400  is also formed of a metal or other conductive material. An insulating layer  420  is inserted between pedestal  150  and control member  400  so that in the illustrated state, pedestal  150  and control member  400  are electrically insulated from each other. Also, pedestal  150  is wired to a terminal T 1  and control member  400  is wired to a terminal T 2 . 
   Here, if a circuit that detects the state of electrical conduction across terminals T 1  and T 2  is provided, this circuit will function as a contact detection circuit that detects the state of contact of force receiving member  110 A and control member  400  based on the state of electrical conduction. That is, when force receiving member  11 A and control member  400  come in contact at any of the control surfaces  411 ,  412 , and  413 , since a state of electrical conduction across terminals T 1  and T 2  will be realized via this contacting part, the contact can be detected electrically. 
   By using such a function, it becomes possible, when an external force that exceeds a predetermined tolerable range is applied to the force detection device, to electrically detect this fact and issue an alarm, to record the occurrence of this fact, and take appropriate measures. 
     FIGS. 30A to 30C  show diagrams concerning a design related to control surface  411  of the above-described force detection device shown in  FIG. 29 , that is, shows enlarged sectional views of an example of the structure of control surface  411  at the control member  400  side. As shown in  FIG. 30A , a hollow part V is formed in the vicinity of control surface  411  of control member  400 , and a thin part  430  with flexibility is formed by the surface layer part at which hollow part V is formed. Moreover, a conductive contact protrusion  431  is disposed on the top surface of this thin part  430 . 
     FIG. 30A  shows a state in which the predetermined interval d 1  is maintained between control surface  411 , having such a structure, and the opposing surface at the force receiving member  110 A side. Here, when an external force −Fz, directed in the negative Z-axis direction (downward direction in the figure), acts on force receiving member  110 A, force receiving member  110 A moves downward and its bottom surface comes in contact with contact protrusion  431  as shown in  FIG. 30B . When the state shown in  FIG. 30B  is entered, since the contacting of the components can be detected electrically as described above, measures, such as the issuing of an alarm, can be taken. When the external force −Fz increases further, thin part  430  deflects as shown in  FIG. 30C  and contact protrusion  431  becomes pushed in towards hollow part V. As a result, a state in which the bottom surface (the surface opposing control surface  411 ) of force receiving member  110  is in complete contact with control surface  411  is entered. 
   A merit of such an arrangement is that, electrical contact can be detected and measures, such as the issuing of an alarm, can be taken at a stage immediately prior to force receiving member  110 A coming in contact with control surface  411  (that is, the stage at which contact protrusion  431  contacts force receiving member  110 A as shown in  FIG. 30B ). In other words, whereas when the state shown in  FIG. 30C  is reached, since force receiving member  110 A will actually collide with control surface  411  and it will be too late to take measures, such as the issuing of an alarm, etc., if measures, such as the issuing of an alarm, etc., can be taken at the stage of  FIG. 30B , there is a possibility for prevention of the reaching of the state of  FIG. 30C . Moreover, even when the state of  FIG. 30C  is reached, since contact protrusion  431  will be in a state in which it is pushed into hollow part V and will be protected, it will not break. 
   Though in the example illustrated in  FIGS. 30A to 30C , hollow part V, thin part  430 , and contact protrusion  431  are formed in the vicinity of control surface  411  at the control member  400  side, these may be formed instead in the vicinity of the opposing surface at the force receiving member  110 A side. 
     FIGS. 31A to 31C  show enlarged sectional views of another design concerning control surface  411 . In this example, a conductive, conical protrusion  441 , the tip part of which undergoes plastic deformation, is formed on control surface  411  as shown in  FIG. 31A . The material of conical protrusion  441  does not need to be made different from the material of control member  400  in order to make the tip part undergo plastic deformation. For example, by using aluminum or other general metal for control member  400  and forming conical protrusion  441  out of the same metal material, a sharp tip part will undergo some degree of plastic deformation. 
     FIG. 31A  shows the state in which the predetermined interval d 1  is maintained between control surface  411  with such a structure and the opposing surface at the force receiving member  110 A side. Here, when an external force −Fz, directed in the negative Z-axis direction (downward direction in the figure) is made to act on force receiving member  110 A, force receiving member  110 A moves downward and its bottom surface comes in contact with the tip part of conical protrusion  441  as shown in  FIG. 31B . As a result, the tip part of conical protrusion  441  becomes squashed as illustrated and conical protrusion  441  deforms to a conical protrusion  441 A with a squashed tip. Since this deformation is a plastic deformation, even after the external force −Fz is removed and the interval between force receiving member  110 A and control surface  411  returns to the original interval as shown in  FIG. 31C , the tip of conical protrusion  441 A will remain in the squashed state. 
   In view of such a phenomenon, it can be understood that control surface  411 , provided with conical protrusion  441 , is useful for realizing an accurate alarm function. This shall now be described by way of a specific example. For example, suppose that there is a need to use a force detection device that can issue some form of anomaly alarm when a load of 1 kg or more is applied to force receiving member  110 A. To manufacture a force detection device that can answer this need, the dimension between force receiving member  110 A and control surface  411  must be controlled accurately. However, if an actual mass production process is considered, the smaller the dimension d 1  that is illustrated, the more difficult it will be to achieve accurate dimensional control and scattering of the dimensional values will occur among lots. There will thus arise a case, for example, where with one lot, an alarm is issued when a load of 0.9 kg is applied while with another lot, an alarm is not issued until a load of 1.1 kg is applied. It is thus difficult to mass produce the desired force detection device that can accurately issue an alarm when a load of 1 kg is applied. 
   However, by using the force detection device with control surface  411  (control surface with conical protrusion  441  formed thereon) such as shown in  FIG. 31A , a device, which can accurately issue an alarm when a load of 1 kg is applied as desired, can be mass produced even if the dimensional precision according to each individual lot is not high. That is, upon mass producing a device with the structure shown in  FIG. 31A , a process of accurately applying a load of 1 kg to force receiving member  110  of each device is performed. By this process, conical protrusion  441  of each lot will become a conical protrusion  441 A with a squashed tip as shown in  FIG. 31B , and this deformation will be maintained as a plastic deformation even after the load of 1 kg is removed as shown in  FIG. 31C . Here, if the original dimensional precision of lots is not high, the form of plastic deformation will vary according to lot. However, all lots share the property that when a load of 1 kg is applied again to force receiving member  110 A, the state of  FIG. 31B  will be entered and the squashed tip of conical protrusion  441 A will contact the opposing surface of force receiving member  110 A to enable an alarm to be issued. The lots will thus satisfy the desired specifications. 
   Needless to say, when a load, for example, of 1.2 kg is applied when such a lot is used, conical protrusion  441 A will become deformed further and the lot will no longer be one that satisfies the desired specifications. However, since at least an alarm will definitely be issued at the point at which the load of 1.2 kg is applied, the lot can be handled at that point as a damaged lot. Conical protrusion  441  does not necessarily have to be disposed on control surface  411  at the control member  400  side and may instead be disposed on the opposing surface at the force receiving member  110 A side (surface opposing control surface  411 ). 
   By forming, below control surface  411  on which conical protrusion  441 A is formed, a hollow part V and a thin part, with flexibility, at the surface layer part (as in a structure with which conical protrusion  441 A is formed in place of contact protrusion  431  in  FIG. 30A ), since conical protrusion  441 A will become pushed into hollow part V when a large load is applied, the state of the squashed tip part of conical protrusion  441 A can be maintained. In this case, since hollow part V must be formed below conical protrusion  441  from the stage illustrated in  FIG. 31A , at the stage shown in  FIG. 31B , that is, at the stage at which a specific load is applied to squash the tip of conical protrusion  441  and make it into conical protrusion  441 A, hollow part V is temporarily filled with some form of filler so that the force will not escape to hollow part V. 
   &lt;&lt;&lt;§7. Other Modification Examples &gt;&gt;&gt; 
   Though this invention has been described based on the illustrated embodiments, this invention is not limited to these embodiments and can be carried out in various other modes. 
   For example, though with the above-described embodiments, static capacitance type force sensors are used as the X-axis distance sensor, the Y-axis distance sensor, the Z-axis distance sensor, and the inclination degree sensor, these respective sensors do not necessarily have to be static capacitance type force sensors in realizing force detection devices according to the present invention, and piezoresistance force sensors, force sensors using piezoelectric elements, etc. may be used instead. However, in terms of simplifying the structure, the use of static capacitance type force sensors as in the above-described embodiment is most preferable. 
   Also, detection processing unit  250 , which serves the function of determining the final detection values of forces and moments, can actually be realized in various arrangements. For example, a method may be employed wherein the static capacitance values of the individual capacitance elements are measured as analog voltage values, and after conversion of these measured values into digital signals, the operations indicated by the equations in  FIG. 12  or  FIG. 18  are executed using a CPU or other computing device, or a method may be employed wherein the measured values of the static capacitance values of the individual capacitance elements are handled as they are in the form of analog voltage values and the final detection values are output as analog signals. In a case where the latter method is employed, the electrodes of the respective capacitance elements are connected as necessary to an analog operation circuit, comprising an analog adder or an analog subtracter. 
   Also, though with the embodiment shown in  FIG. 24 , a structure with which top plate  130  is supported by four columns L 1  to L 4  was described, in consideration of making top plate  130  be displaced smoothly along the XY plane, the four columns L 1  to L 4  are preferably formed of cylindrical columns with flexibility. Also, there is no need for the interior of inner box-like structure  300  to be hollow and the interior may instead be filled with some form of material. 
   Lastly, a modification example of control member  400 , shown in  FIG. 29 , shall be described.  FIG. 32  is a top view of a control member  400  and a disk-like force receiving member  110 A of this embodiment. As illustrated, with this example, groove parts  415  are formed at positions along the respective coordinate axes of control surface  413  and protruding parts  111  are formed at the same positions of force receiving member  110 A. A certain gap is formed between each protruding part  111  and groove part  415 , when an excessive moment Mz about the Z-axis acts on force receiving member  110 A, protruding parts  111  contact groove parts  415  and further rotation is restricted. This modification example shown in  FIG. 32  thus has, in addition to the functions of the example shown in  FIG. 29 , the function of restricting displacements due to a moment Mz about the Z-axis. 
   As described above, in a force detection device according to the present invention, forces and moments can be detected in a distinguished manner by means of a structure that is as simple as possible.