INTERFEROMETER STRUCTURE

Abstract: The structure of the invention serves to support mirrors (106) defining a reflective channel (108, 110) which can dynamically be reciprocally widened and narrowed, as in a two-beam interferometer. It is effectively divided, by pivot points (100) on an intermedial axis, into two opposite portions of equal mass, thus affording to the structure immunization against translational forces transmitted through those points. The opposite portions also have their centers of gravity remotely located, so as to generate a counteracting torque in response to moments of rotational inertia transmitted through the pivot points (100). In the structure, integrally formed planar pieces (92, 94, 96) are assembled to provide contiguous elongated elements and an interposed connecting web element (99), a plurality of which web elements (99) produce a flexure joint.

Description: INTERFEROMETER STRUCTURE Two-beam interferometer spectrometers are well known in the art. Most of the modern spectrometer designs, including the Michelson interferometer spectrometer, are described in Griffiths and DeHaseth, Fourier Transform Infrared Spectrometer, John Wiley & Sons, NY, Chapter 4, 121-165 (1986). The Michelson interferometer functions by dividing an inci¬ dent beam of electromagnetic radiation into two separate beams at a beamsplitter, each of which beams is caused to travel along a different optical path; one of the beams is usually directed along a reference path having a fixed optical length, while the other is simultaneously directed along a path of variable length. A retroreflecting element, such as a plane mirror, a cube corner, or a "cats eye" reflector, is placed in the optical path of each beam to return it to the beamsplitter, where the beams recombine to form a single exit beam. The optical path length variation, which is typically achieved by moving one of the retroreflectors, causes the combined exit beam to be ampli¬ tude modulated due to interference between the recombining beams. By converting the interferogra so obtained into an electrical signal, and by then analyzing that signal in a known manner, the spectrum or intensity of the input radiation can, after suitable calibration, be derived as a function of fre¬ quency. More particularly, when such an interferometer is employed in a Fourier transform spectrometer, the exit beam is focused upon a photoconductive detector to produce the electrical inter- ferogram signal. If a sample is so placed that the modulated beam passes through it prior to impinging upon the detector, the analysis performed can determine the absorption spectrum of the sample; other placements of the sample, and other of its charac¬ teristics, can be employed and obtained as well. In those instances in which the optical path length through the interferometer is varied by displacement of a retro- reflecting element along the optical axis of the beam, it will be appreciated that the maximum resolution attainable with the instrument is directly related to the maximum path difference that can be produced; i.e., to the maximum longitudinal dis¬ placement that is attained by moving the retroreflecting ele ent. Because Michelson interferometers rely upon the wave interference that occurs when the two beams recombine at the beamsplitter, an important factor in determining the quality of such a device is the degree to which the optical elements remain aligned during path-length variation. Accordingly, longitudinal displacement of the moving mirror must be effected with extreme accuracy over the entire range of its travel; i.e., the moving mirror must in most cases remain aligned to within a small frac¬ tion of the wavelength of incident light, over a longitudinal displacement of several centimeters. Any irregularity in the mirror guide path, such as might cause even slight tilting of a plane mirror, will lead to significant distortion in the inter- ferogram produced. It is of course well known that substitution of cube-corner and cats-eye retroreflectors for plane mirrors can essentially eliminate such distortion problems; but it is known as well that the use of those elements also entails certain inherent drawbacks. Precision air bearings and the like have been employed in modern interferometers in an effort to satisfy the extreme accuracy requirements to which movable mirror guides are subject. Such systems are however quite expensive, and moreover they require a supply of pressurized gas for operation. Electronic control systems, with feedback to automatic posi¬ tioners, have also been utilized as a means for dynamically maintaining mirror alignment; satisfactory self-aligning systems are however difficult to design, and they tend to be relatively large and expensive. In view of these drawbacks, substantial effort has been devoted to the development of high-quality interferometers that do not rely upon precision bearings or electronic alignment control systems. One approach taken utilizes a tiltable re¬ flector assembly consisting of a pair of parallel, confronting mirrors, rather than a longitudinally displaced retroreflector. As an ostensible improvement thereupon, United States Patent No. 4,915,502, issued on April 10, 1990, teaches a twin-arm interferometer spectrometer having a tiltable reflector assembly by which the optical path lengths of both interferometer beams are varied simultaneously, thereby achieving a desired total path difference by a much smaller rotation of the paired mirrors then would otherwise be required. Such a design affords the advantage of inεensitivity to linear movement of the optical element (i.e., only angular displacements will change the path length) ; moreover, rotating bearings are generally easier and less expensive to produce than are longitudinal or linear ones. Also of interest is United States Patent No. 4,383,762, issued May 17, 1983, which provides a two-beam interferometer for Fourier spectroscopy in which a rigid pendulum arm is used to mount moving cube corner retroreflectors. The pendulous movement (arcuate oscillation) enables accurate optical path- length variation to be produced in a smoothly guided motion, and the cube corner retroreflectors render the optical system un¬ affected by the resultant tilt; this avoids the disadvantages for Fourier spectroscopy that are inherent in the deviation from strict linearity that characterizes such pendulous motion. So-called "porch swing" mounting arrangements are also known in the art, in which structural elements, supported at four pivot points, form a parallelogram by which a mirror, mounted at right angles to one side of the parallelogram, can be translated along an axis that is perpendicular to the mirror's plane. While such designs can provide inexpensive systems in which mounted mirrors are constrained to linear motion, due to the relatively large displacement distances that were deemed necessary they have not herefore been considered practical for use in instruments in which high resolutions are to be realized. Pervading all of the foregoing considerations is the need to effectively isolate the mirror-supporting interferometer structure from extraneous forces, which would tend to produce aberrant distortions of the structure, and to thereby introduce inaccuracies into the optical measurements made; such forces will normally arise from environmental vibrational effects, and can of course be of a rotational or translational nature. Con¬ siderations of manufacturing cost and feasibility are, needless to say, also of primary importance. Accordingly, it is a broad object of the present invention to provide a novel structure for the dynamic support of reflec¬ tive elements, in which a high degree of immunization against environmental vibration and other extraneous forces is afforded. A more specific object is to provide such a structure in which immunization may be afforded against rotational as well as translational forces. Other objects of the invention are to provide such struc¬ ture in which a plurality of reflective elements are incorpo- rated, and to provide, more particularly, a two-beam interfero¬ meter utilizing such structure. Yet another object is to provide a novel structure having the foregoing features and advantages, fabricated from a plural¬ ity of unitary planar pieces, each integrally formed to provide, in assembly with the others, contiguous rigid members and inter¬ posed flexible joints. Still further objects of the invention are to provide a novel structure, and an interferometer incorporating the same, having the foregoing features and advantages and which are, in addition, of relatively incomplex design and construction, and hence of relatively facile and inexpensive manufacture. SUMMARY OF THE INVENTION It has now been found that certain of the foregoing and related objects of the invention are attained by the provision of structure comprising a multiplicity of rigid members, includ¬ ing a pair of opposing side members, and a pair of opposing end members, flexibly interconnected so as to permit conjoint dis¬ placement of the side members in opposite directions along parallel axes of shifting, with the end members rotating in the same direction about pivot points located on an intermedial axis lying between, and parallel to, the axes of shifting. The in¬ termedial axis divides the structure into two portions, each portion including one of the side members and having its center of gravity located on a common axis that extends perpendicular to the axes of shifting. The center of gravity of at least a first one of the portions, inclusive of a first one of the side members, is spaced to the side of the intermedial axis that is opposite to the axis of shifting of the "first" side member. The center of gravity of the other portion of the struc- ture, inclusive of the other side member, will preferably be similarly spaced in a remote relationship to the "other" side member, across the intermedial axis. Most desirably, the centers of gravity of the two portions will be equidistantly spaced from the intermedial axis, and the portions will be of substantially equal mass. Lateral marginal portions of the side members of which the structure is comprised will generally be connected directly to the contiguous marginal portions of the end members by flexible joints, to thereby form a frame within which an open space is defined. In more specific embodiments, the structure described will include a plurality of reflective elements so supported by the frame as to define a reflective channel within its open space. The centers of gravity of the two portions of such a structure will most advantageously be of such magnitude and disposition as to cooperatively produce, in reaction to any extraneous force that would tend to rotate the frame about its pivot points, a counteracting torque about the intersection of the above- mentioned intermedial and common axes, the value and direction of which will dynamically substantially counterbalance the extraneous force. Even more specific forms of the structure may additionally include a first internal wall connected to the "first" side member and projecting therefrom toward the "other" side member, and a second internal wall connected to the other side member and projecting therefrom toward the "first" side member. Both of the internal walls will traverse the intermedial axis of the structure, and will have mutually confronting faces on which are mounted the reflective, channel-defining elements, disposed in laterally spaced, substantially parallel planes. The end members of the structure will normally have pivot elements dis¬ posed on its intermedial axis, so that conjoint shifting of the side members will cause reciprocal widening and narrowing of the reflective channel. Other objects of the invention are attained by the provi¬ sion of a structure comprised of a plurality of reflective chan¬ nel-defining elements, as herein described, in which the two op¬ posite structure portions are of such mass and configuration as to statically balance one another irrespective of the orienta- tion of the intermedial axis. Further objects are attained by the provision of a two-beam interferometer comprising, in addi¬ tion to the support structure described, mounting means, a beam¬ splitter for directing electromagnetic radiation into the re¬ flective channel of the structure, and reflecting means for returning to the beamsplitter electromagnetic radiation that has traversed the channel. And yet additional objects are attained by the provision of support structure having at least some of the features set forth, but comprised of an assembly of at least two similar planar pieces secured in substantially coextensive, superposed relationship and providing at least one contiguous pair of rigid members, consisting of a side member and an end member, and an interposed flexible joint. Each planar piece is of integrally formed, unitary construction, and includes first and second elongate elements, and a flexible web element joining their contiguous end portions. The web element extends on an oblique axis to the longitudinal axes of both of the elongate elements when they are mutually perpendicular; normally the oblique axis will lie at an angle of 45° to the longitudinal axes. In as¬ sembly, the "first" elements of the two planar pieces together provide the side member of the contiguous pair, the "second" elements together provide the end member, and the web elements together provide the flexible joint therebetween. By so con- structing and arranging the pieces as to cause the oblique axes of the web members to cross one another, the contiguous members will be constrained to relative movement about a single axis of flexure, at the point of intersection of the oblique axes. Each of the web elements of the planar pieces may desirably be defined by opposing concave edges of equal radius, with center points disposed on an axis perpendicular to its oblique axis. A central zone will thereby be defined at the axis of flexure, which constitutes the thinnest point along the length of the web element. Generally, each of the planar pieces will consist of four elongate elements, and four interposed web elements, thus providing a closed, frame-like piece. BRIEF DESCRIPTION OF THE DRAWINGS Figure 1 is a schematic block diagram of a Fourier trans¬ form infrared (FT-IR) spectrometer incorporating an interfero- meter embodying the present invention; Figure 2 is a schematic plan view of one form of a channel- defining support structure suitable for use in the interfero¬ meter of the invention, with an alternate position of an inter¬ mediate wall shown in phantom line; Figure 3 is a schematic, end elevational view of the struc¬ ture shown in Figure 2; Figure 4 is a schematic plan view of an interferometer incorporating the structure shown in Figures 2 and 3, including a beamsplitter and retroreflecting mirrors, in which is diagram- matically illustrated the paths of the beam components through the two reflective channels defined; Figure 5 is a plan view similar to that of Figure 2, show¬ ing a balanced support structure providing interferometer walls. Figure 6 is a plan view of a more specific form of support structure of the kind shown in Figure 5; Figure 7 is an elevational view of the structure of Figure 6, taken in partial section along line 7-7 thereof. Figure 8 is a diagrammatic representation of idealized support structure embodying the present invention, in assembly with mounting means; Figure 9 is a plan view of an assembly suitable for use in providing a preferred form of support structure embodying the present invention; Figure 10 is a side elevational view of the assembly of Figure 9; and Figure 11 is a fragmentary plan view showing two of the planar pieces from which the assembly of Figures 9 and 10 is constructed, drawn to a somewhat enlarged scale. DETAILED DESCRIPTION OF THE PREFERRED AND ILLUSTRATED EMBODIMENTS Turning initially to Figure 1 of the drawings, therein schematically illustrated is an FT-IR spectrometer, generally designated by the numeral 10. The spectrometer includes a radiation source 12 capable of producing a collimated beam of infrared radiation, which is directed (by suitable transfer optics, not shown) into the interferometer, generally designated by the numeral 14, by which it is amplitude modulated as a func¬ tion of frequency. After passing through the sample compartment 16, the interferogram beam is caused to impinge upon a photocon- ductive detector 18, the output electrical signal from which is then subjected to analysis in the computer 20 to provide desired analytic data. A specific form of support structure, utilized for defining reflective paths through an interferometer embodying the inven¬ tion, is illustrated in Figures 2 and 3. The assembly consists of two stationary outer walls 22, 24 (supported by means not specifically suggested) , and a movable inner wall 26, the con— fronting surfaces of which walls 22, 24, 26 mount planar mirrors 28. The inner wall 26 is attached at the top and bottom to the stationary wall 24 by linking elements 30, which are of equal length and are connected at their opposite ends by flexible means; this parallelogrammic assembly serves of course to con- strain the wall 26 to movement in parallel planes, and to main¬ tain at least substantial parallelism with respect to the planes of walls 22 and 24. A drive mechanism 34 (which may be of a piezoelectric, magnetic or mechanical nature) is operatively connected to the inner wall 26 and serves to reciprocate it between alternative positions, constantly and at a controlled rate of speed. As wall 26 is caused to oscillate vertically (in the orien¬ tation depicted) , the linking elements 30, 32 constrain it to lateral movement in parallel planes, narrowing one of the channels while simultaneously widening the other, with the plane mirrors 28 in turn always being maintained substantially parallel to one another. Needless to say, the phantom line representation of Figures 1 and 2 show the wall 26 displaced (from the full-line, centralized position) to a position closer to the wall 24 and further from the wall 22. This will of course cause a beam directed into the channel between walls 24 and 26 (in the phantom line relationship depicted) to follow a shorter traversal path distance than a beam directed into the channel between the walls 22 and 26, which will be commensur- ately lengthened. Turning now to Figure 4 (wherein the same reference numbers are used to designate parts common to the preceding Figures) , collimated electromagnetic radiation 46 is directed upon a par¬ tially reflecting beamsplitter 36, by which the input beam is divided into two separate component beams, a reflected component 50 and a transmitted component 52. Both beam components impinge upon the mirrors 28 defining the paths through their respective channels; as will be noted, the beamsplitter 36 is generally parallel to the planes of the mirrors 28, and the beams make four reflections in traversing the channels in each direction. Upon exiting the opposite ends of the channels, the components 50, 52 strike the planar reflective surfaces 42, 44 of retro- reflector 40, respectively, which surfaces are oriented with strict perpendicularity to the emerging beams so as to cause the beam components to precisely retrace their original paths re¬ versely through the channels, reco bining at the beamsplitter 36 and forming exit beam 54. That beam is directed toward a focusing element (not shown) , through a sample in the compart- ment 16 (in the embodiment depicted by Figure 1) , and finally onto a photoconductive detector 18. Figure 5 illustrates support structure for an interfer¬ ometer embodying the invention, which is mechanically balanced about its pivot points and hence affords optimal levels of mechanical stability. The system comprises a frame of four rigid plates 70, 72, 74 and 76, flexibly joined to one another at the corners. Wall 78 is rigidly mounted on the upper plate 74, with its plane normal to that of the plate, and walls 80 and 82 are similarly mounted on the lower plate 76; end plates 70 and 72 are pivotably supported midway along their lengths at 84 and 86, and a beamsplitter (not shown) is so disposed as to project radiation from an incident beam into the two channels so defined (i.e., it will lie in a generally parallel to the planes of the mirrors 28 on the walls 78-82, and in registry there- with) . Consequently, when force is applied to plate 72, through activation of an operatively connected drive mechanism 88, a distortion of the original rectangular geometry is produced, by which the frame plates and the attached walls are brought to the parallelogrammic relationship shown in phantom line. This re¬ configuration of the frame moves the confronting mirrors 28 on the walls 78 and 82 closer to one another while simultaneously increasing the distance between the mirrors 28 on the walls 78 and 80; the parallel orientation of the mirror planes will of course be maintained in all positions. It will be appreciated that an arrangement similar to that of Figure 5 could be used in which one of the plates 74 or 76 is fixedly mounted while the other is free to move; doing so would however tend to compromise somewhat the stability provided by the illustrated system. It will also be apparent to those skilled in the art that, in accordance with certain embodiments of the invention, alternative systems may be substituted for those described. Designs for mounts, by which relatively dis- placeable parallel mirrors can be kept aligned to within a few arc-seconds, have been disclosed for example by Jones, R.V. 1962 "Some Uses of Elasticity in Instrument Design" J. Sci. Instrum. , 39, 193-203 (note in particular the parallel spring movement illustrated on page 196) ; Jones, R.V. and Young, I.R. 1956 "Some Parasitic Deflexions in Parallel Spring Movements" J. Sci. Instrum., 33, 11-15; Bradley, D.J. 1962 "Parallel Movement for High Finesse Interferometric Scanning" J. Sci. Instrum. , 39, 41-45; and Smith, S.T. et al 1987 "Design and Assessment of Monolithic High Precision Translation Mechanisms" J. of Physics E. 20, 977-983 (note in particular the simple compound recti¬ linear spring arrangement illustrated on page 978) . Turning now to Figures 6 and 7, the system shown therein is comprised essentially of a unitary support body, generally designated by the numeral 90, which may be machined or otherwise formed from a single, rectangular block of metal or the like. It consists of front and rear walls 92, 94, respectively, and end walls 96, the four walls being joined at the corners by flexible hinge elements or joints 98, formed by cutting grooves 99 of semicircular cross section, producing right cylindrical channels therealong. Pivot edges 100 project inwardly from along the internal surfaces of the end walls 96, midway along their lengths and into registry with the flexural plane of the adjacent hinge elements 98, which edges 100 serve to mount the body 90 on suitable support structure (not shown) . A central interior wall 102 projects rearwardly from the front wall 92 to a point short of the rear wall 94, and two lateral walls 104 project forwardly from the rear wall 94 to points short of the front wall 92 and with equidistant spacing from the central wall 102. Plane mirrors 106 are secured against the four confronting faces of the walls 102 and 104, to define reflective channels 108 and 110 therebetween. As will be appreciated, the applica¬ tion of force (by means not shown) to one of the exterior walls of the body 10 will serve to produce the necessary and desirable displacement of the reflective surfaces defining the channels 108, 110, in accordance with the disclosure hereinabove pro¬ vided. The body 90, used in the assembly of Figures 6 and 7, is (like that of Figure 5) advantageous in providing a structure that is mechanically balanced about pivot edges 100, which lie on an intermedial plane that demarcates two statically balanced portions of the frame. Such structure may include means by which the center of gravity can be located precisely on the axis of pivoting; removal of material from holes, such as those shown at 112 in Figure 7, could serve that purpose (in addition to reducing the overall mass of the body) . In accordance with certain of the preferred embodiments of the invention, however, several of the holes 112 carry weighting plugs 114, which increase the mass of the outer end portions of the walls 102, 104. This serves to displace to remote positions the centers of gravity of the two portions of which the body 90 consists; i.e., the center of gravity of the portion of the structure above the intermedial axis (on which lies substan¬ tially the upper horizontal part of line 7-7) , as depicted in Figure 6, is below that axis (or plane) , and the center of gravity of the lower portion of the structure is above the axis. This in turn serves to immunize the structure against distortion due to moments of rotational inertia acting at the pivot edges 100. The diagrammatic representation constituting Figure 8 of the drawings shows the mass and spatial relationships of an idealized system for producing such isolation, consisting of support structure and mounting means, generally designated re¬ spectively by the numerals 116 and 118. The support structure includes opposite side members 120, 122, opposite end members 124, 126, and interposed flexible joints 128 connecting con¬ tiguous end portions of the rigid members. In this form, the two side members 120, 122 have the same mass, as do the two end members 124, 126; the side members 120, 122 are equidistantly spaced from the axis x-x through the elements 130, which thereby serves to effectively divide the structure 116 into two por¬ tions, the overall mass and configurations of which are equal. Figure 8 also shows that the centers of gravity, CG A and CG- β , respectively, of the side members 120, 122 (and hence, of the opposite structure portions defined) are disposed on an axis y-y which is perpendicular to the axis x-x and effectively divides the structure 116 into two equal lateral portions. Although not indicated by any structural feature illustrated, it will be noted that the center of gravity CG A of the upper half portion of the structure (as depicted) is spaced to the side of the intermedial axis x-x opposite to that on which the included member 120 is disposed, and that the corresponding center of gravity CG-*-* of the lower half portion of the structure is dis- placed from the included member 122 to the upper side of the axis; moreover, the centers of gravity CG A and CG B are equi- distantly spaced from the intermedial axis. In addition, because the end members 124, 126 are of uniform cross section along their entire length, and the pivot elements 130 are located at their mid-points, their centers of gravity CG C and CG D are disposed at those points. As a result, the portions of the structure 116 disposed to the opposite sides of the intermedial axis x-x will be of the same mass, and will balance one another irrespective of the orientation of that axis. Because of the remote, opposite-side displacement of the centers of gravity CG A and CGg, moreover, they will coact to produce a torque that is directed oppositely to any external force that would tend to produce rotation of the members 124, 126 about the pivot elements 130. If, for example, one were to set the structure in rotation about its pivot points, and thereafter arrest rotation thereat, there would be no tendency for continued flexure to occur. Thus, the moment of inertia produced by CG A and CG- 3 , **- n response to torques applied at points 130, can precisely balance, and thereby effectively neutralize, aberrant distortion effects and, in turn, immunize the structure against extraneous forces transmitted from the environment; i.e., in this structure the CG^/CGg moment of in¬ ertia will be of equal magnitude, but of opposite direction, to the combined moments of inertia of the end members 124, 126 about CG C and CG-**-. Because of the statically balanced relation¬ ship that exists between the same two portions of the structure, moreover, translational forces imparted thereto through the points 130 will be negated as well. It should be appreciated that these principles of static and dynamic balance apply alone and together, and thus enable the provision of a structure that is immunized either rotationally or translationally, or both. The mounting structure diagrammatically illustrated in Figure 8 includes pivot members 132, which cooperate with the pivot elements 130 of the support frame 116 to mount it in the manner described. The system additionally includes a drive unit 134, which is provided to impart controlled distortional motion to the structure 116 so as to adapt it for use in interfero- metric applications. Turning finally to Figures 9-11 of the drawings, therein illustrated is an assembly suitable for use in providing the support structure of the invention. The assembly consists of six planar pieces of frame-like configuration, generally desig¬ nated by the numerals 138 and 140, stacked in an alternating arrangement, as seen in Figure 10. Each of the pieces 138, 140 consists of opposite side elements 142 and 143, and opposite end elements 144 and 145, the contiguous portions of which are joined by a web elements 146, 146"; the different designations 146, 146' are indicative of the opposite orientations of the 45° oblique axes on which the web elements extend. As best seen in Figure 11, each element 146, 146* is defined by opposing concave edges, which closely approach one another at the mid-point of the element to define a flexure zone 147 thereat of very thin cross section. The elongate elements 142-145 are formed with holes 150, which register with one another in the stacked ar¬ rangement and serve to receive fasteners 152 by which the pieces 138, 140 are secured in assembly. Figure 9 best shows that the web elements 146, 146' cross one another in the assembly, with the flexure zones 147 thereof aligned at the intersection. The web elements thus function in the manner of a so-called "cross-spring pivot," a flexure con¬ struction that is broadly known in the art and that constrains the attached members to relative movement about a single axis; in the present assembly, the web element constrains the frame- defining members, constituted by the stacked elongate elements 142-145, to relative movement solely on the axes through the aligned flexure zones 147. Although the double concave form of the web elements illustrated may be preferred in certain instances, it is not necessary that they have that shape in order to function in the intended manner. Elements that are uniform along their length may for example be substituted, albeit that the illustrated form of web elements provides smooth transitions from the connected elements to the pivot points, and minimizes stress concentra¬ tions that might otherwise be presented at locations of attach¬ ment. Moreover, it will be appreciated that the assembly illu¬ strated in Figures 9 and 10 would be so modified as to provide suitable members for supporting reflective elements, in those instances in which the assembly is to be employed in an inter¬ ferometer or a like optical instrument. Many other modifications may of course be made to the structures and assembly described, without departure from the novel concepts of the invention. For instance, it will often be advantageous to provide means for variably adjusting the mass and mass distribution of a structure, or of a portion thereof, so as to enable most convenient repositioning of centers of gravity. Similarly, it will be appreciated that an assembly of integrally formed stacked pieces, of the character shown in Figures 9-11, may be employed to provide a flexible structure for virtually any purpose, and of virtually any configuration, and that the number and arrangement of such pieces employed therein can of course vary; for example, an optimal arrangement may constitute four pieces, stacked in the sequence 138, 140, 140, 138, with a spacer (i.e., a piece devoid of web elements 147) centrally interposed between the pieces 140. Materials of construction will be obvious to those skilled in the art, taking into account the purpose for which the article is intended. Finally, it should perhaps be pointed out that references herein to "extraneous" forces is intended to encompass all such forces as may introduce uncontrolled, and undesirable distortion into a structure, but will generally refer to vibration that is trans¬ mitted from an external source through a mounting system. Thus, it can be seen that the present invention provides a novel structure for the dynamic support of reflective elements, in which a high degree of immunization against vibration and other extraneous forces is afforded, and in particular immuniza¬ tion against both translational and rotational effects. The structure may comprise a two-beam interferometer, and may most desirably be fabricated from a plurality of unitary planar pieces, integrally formed to provide, in assembly, contiguous rigid members and interposed flexible joints. The novel struc¬ ture, interferometer, and assembly of the invention are, in addition, of relatively incomplex design and construction, and hence of relatively facile and inexpensive manufacture.

Claims: THE CLAIMS Having thus described the invention, what is CLAIMED is: 1. Structure for the dynamic support of reflective ele¬ ments, immunized against extraneous forces, comprising a multi- plicity of rigid members including a pair of opposing side members and a pair of opposing end members, said members being flexibly interconnected so as to permit conjoint displacement of said side members in opposite directions along parallel axes of shifting, with said end members rotating in the same direction about pivot points located on an intermedial axis lying between and parallel to said axes of shifting, said intermedial axis effectively dividing said structure into two portions, each of said portions including one of said side members and having its center of gravity located on a common axis that extends perpen- dicular to the aforesaid axes, said center of gravity of at least a first one of said portions, inclusive of a first one of said side members, being spaced to the side of said intermedial axis opposite to said axis of shifting of said first side member. 2. The structure of Claim 1 wherein said center of gravity of the other of said portions, inclusive of the other of said side members, is spaced to the side of said intermedial axis opposite to said axis of shifting of said other side member. 3. The structure of Claim 2 wherein said centers of gravity of said portions are equidistantly spaced from said intermedial axis, and wherein said portions are of substantially equal mass. 4. The structure of Claim 1 wherein each of said rigid members has lateral marginal portions, said marginal portions of said side members being connected directly to the contiguous marginal portions of said end members by flexible joints, and said members forming a frame within which an open space is de¬ fined. 5. The structure of Claim 4 additionally including a first internal wall connected to said first side member and projecting therefrom into said space toward the other side member, and a second internal wall connected to said other side member and projecting therefrom into said space toward said first side member, said internal walls having mutually confronting faces and both traversing said intermedial axis. 6. The structure of Claim 5 wherein at least said first internal wall is so constructed as to have a major proportion of its mass located to the side of said intermedial axis that is remote from said axis of shifting of said first side member, to so space said center of gravity of said first one of said por¬ tions. 7. The structure of Claim 5 wherein said structure in¬ cludes a third internal wall connected to said other side member and projecting therefrom into said space toward said first side member, traversing said intermedial axis and laterally spaced from said first internal wall to the opposite side from said second wall, said first and third walls having mutually con¬ fronting faces. 8. The structure of Claim 7 wherein each of said internal walls is so constructed as to have a major proportion of its mass located to the side of said intermedial axis that is re¬ motely spaced, across said intermedial axis, from said axis of shifting of the one of said side members to which said internal wall is connected, said center of gravity of each of said por¬ tions thereby being spaced to the side of said intermedial axis opposite to said axis of shifting of said connected side member. 9. The structure of Claim 1 wherein said rigid members form a frame within which an open space is defined, wherein said structure includes a plurality of reflective elements supported by said frame so as to define a reflective channel therebetween within said open space, and wherein said centers of gravity of said two portions are of such magnitude and disposition as to cooperatively produce, in reaction to any extraneous force that produces an applied torque tending to rotate said frame about said pivot points, a counteracting torque about the intersection of said intermedial and common axes, said counteracting torque being of such value and direction as to dynamically substan¬ tially balance such applied torque. 10. The structure of Claim 9 wherein said center of gravity of the other of said portions, inclusive of the other of said side members, is spaced to the side of said intermedial axis opposite to said axis of shifting of said other side member. 11. The structure of Claim 9 wherein said portions of said structure are of such mass and configuration as to statically balance one another irrespective of the orientation of said intermedial axis. 12. The structure of Claim 9 additionally including a first internal wall connected to said first side member and pro¬ jecting therefrom into said space toward the other side member, and a second internal wall connected to said other side member and projecting therefrom into said space toward said first side member, said internal walls having mutually confronting faces and both traversing said intermedial axis, said reflective elements being disposed on said confronting faces and in laterally spaced planes, substantially parallel to one another, to define said reflective channel therebetween extending through said structure. 13. The structure of Claim 12 wherein each of said reflec¬ tive elements is a plane mirror. 14. The structure of Claim 12 wherein said structure addi¬ tionally includes pivot elements disposed on said end members and said intermedial axis, such conjoint shifting of said side members causing said channel defined between said reflective elements to reciprocally widen and narrow. 15. Structure for the dynamic support of reflective ele¬ ments, immunized against extraneous forces, comprising a multi- plicity of rigid members including a pair of opposing side members and a pair of opposing end members, said members being flexibly interconnected so as to provide a frame and to permit conjoint displacement of said side members in opposite direc¬ tions along parallel axes of shifting, with said end members rotating in the same direction about pivot points located on an intermedial axis lying between and parallel to said axes of shifting; and a plurality of reflective elements supported by said frame and defining a reflective channel therebetween, said intermedial axis effectively dividing said structure into two portions that are of such mass and configuration as to statically balance one another irrespective of the orientation of said intermedial axis. 16. The structure of Claim 15 wherein said portions are of equal mass and have their centers of gravity equidistantly spaced from said intermedial axis. 17. A two-beam interferometer comprising: mounting means including pivot elements for providing pivotal support; said structure of Claim 9, said pivot elements of said mounting means engaging said end members of said structure at said pivot points, and permitting such conjoint displacement of said side members; a beamsplitter for directing electromagnetic radiation into said channel of said structure; and reflecting means for returning to said beamsplitter electromagnetic radiation traversing said channel. 18. A two-beam interferometer comprising: mounting means including pivot elements for providing pivotal support; said structure of Claim 15, said pivot elements of said mounting means engaging said end members of said structure at said pivot points, and permitting such conjoint displacement of said side members; a beamsplitter for directing electromagnetic radiation into said channel of said structure; and reflecting means for returning to said beamsplitter electromagnetic radiation traversing said channel. 19. The structure of Claim 15 wherein said structure com- prises at least two planar pieces of similar configuration affixed in substantially coextensive, superposed relationship and cooperatively providing at least one contiguous pair of said members consisting of a side member and an end member, and pro¬ viding a flexible joint between said members of said contiguous pair, each of said planar pieces being of integrally formed, unitary construction and including first and second elongate elements having longitudinal axes and contiguous end portions, and a flexible web element joining said contiguous end portions and extending therebetween on an oblique axis to both of said longitudinal axes when said longitudinal axes are mutually per¬ pendicular, said first elements of said two pieces together providing said side member of said contiguous pair, said second elements of said two pieces together providing said end member of said contiguous pair, and said web elements of said two pieceε together providing said flexible joint therebetween, said oblique axes crossing one another and thereby causing said web elements to constrain said members of said contiguous pair to relative movement about a single axis of flexure, disposed at the intersection of said oblique axes. 20. The structure of Claim 19 wherein said oblique axis is disposed at 45° to said mutually perpendicular longitudinal axes. 21. The structure of Claim 19 wherein each of said web elements of said planar pieces is defined by opposing, concave edges having the same radius, and a center point on an axis per¬ pendicular to said oblique axis, said concave edges defining, at the mid-point of said element, a zone of minimum cross section at said axis of flexure. 22. The structure of Claim 19 wherein each of said planar pieces is of closed, frame-like form, and consists of four of said elongate elements interconnected by four of said web elements.

Inventors: SOLOMON PETER R, SOLOMON, PETER, R.
Applicants: ADVANCED FUEL RES INC, ADVANCED FUEL RESEARCH, INC.
Application year: 1993
Main classification: G01B9
IPC codes: G01B9, G01J9