Coil winding machine and coil winding method using the same

Abstract: An optical fiber coil winding machine in which first and second spindles (10L, 10R) are axially aligned but spaced apart and a take-up bobbin (B) for winding thereon an optical fiber is held between opposed ends of the first and second spindles. First and second indexes (32L, 32R) are rotatably mounted about the first and second spindles, respectively, and first and second spinners (35L, 35R) are mounted about the first and second indexes in a manner to be movable in their axial direction. First and second sup­ ply bobbins (4L, 4R) having wound thereon an optical fiber are rotatably mounted on the first and second spinners, respectively.

Description: The present invention relates to a coil winding machine for winding a wire or the like onto a take-up bobbin to fabricate a coil. More particularly, the invention pertains to a coil winding machine for fabricating an optical fiber coil and a coil winding method using the winding machine. A sensing coil of a fiber optic gyro is usually formed by a multilayer coil so as to provide for enhanced sensitivity. Conventionally, this multilayer coil has a solenoid-like configuration in which an optical fiber is wound in the opposite direction for each layer as shown in Fig. 1, in which an optical fiber 2 from the one end 2r to the other end 2ℓ thereof is wound onto a take-up bobbin B, with a first layer wound from one end to the other of the bobbin B in its axial direction Z as indicated by the arrow 3a, a second layer in the opposite axial direction as indicated by the arrow 3b... . However, as set forth in N. J. Frigo, SPIE, Vol. 412, pp268-271, 1983, for example, when the sensing coil formed by such a solenoid-like multilayer coil is subjected to a temperature change, its thermic conductivity variations produce an error in the output of the fiber optic gyro which is expressed by Δϑε = nN πΔn₀ 6 (1 + 1/m) where n is the refractive index of the optical fiber, N the number of turns, Δn₀ the product of the temperature coefficient of the refractive index and the temperature changing ratio, and m the number of layers of the coil. With a view to minimizing the output error of the fiber optic gyro, there has been proposed a sensing coil of a type in which the one half and the other half of the length of the optical fiber are --starting from the middle of the optical fibre-- alternately wound onto a single take-up bobbin in such a manner that their individual parts symmetrical with respect to said middle or intermediate point of the fiber are disposed spatially close or adjacent to each other and are subjected to similar temperature changes, thereby reducing the contributing factor to the output error. A variety of coil structures have been proposed to implement such a type of coil. A typical one of them is such a multilayer coil as depicted in Fig. 2, in which two substantially equal halves of the optical fiber, i.e. the one half portion 2R of the optical fiber 2 from its middle or intermediate point 2c to its one end 2r and the other half portion 2L from the intermediate point 2c to its other end 2ℓ, are alternately wound around the take-up bobbin B repeatedly in units of four layers, with the intermediate point 2c held at the innermost position on the bobbin B. A first layer of the coil is formed by winding a part of the one half portion 2R, which is the closest to the intermediate point 2c, around the take-up bobbin B from its one end to its other end in its axial direction Z as indicated by the arrow 3c; a second layer is formed by winding a part of the other half portion 2L, which is the closest to the intermediate point 2c, around the bobbin B in the same direction as in the case of the first layer, as indicated by the arrow 3d; a third layer is formed by winding another part of the other half portion 2L, which is the second closest to the intermediate point 2c, around the bobbin B from the other end to the one end thereof in its axial direction Z as indicated by the arrow 3e; a fourth layer is formed by winding another part of the one half portion 2R, which is the second closest to the intermediate point 2c, around the bobbin B in the same direction as in the case of the third layer, as indicated by the arrow 3f; a fifth layer is formed by winding another part of the one half portion 2R, which is the third closest to the intermediate point 2c, around the bobbin B from the one end to the other in its axial direction Z as indicated by the arrow 3g; and the subsequent layers are also formed in the same manner as described above. With the use of such a type of multilayer coil, the output error of the fiber optic gyro is markedly reduced as compared with the output error suffered in the case of employing the solenoid-like multi-layer coil shown in Fig. 1, as expressed by Δϑε = nN πΔn₀ 6 1 4m(m - 1) Incidentally, the conventional winding machine is designed exclusively for fabricating the solenoid-like multilayer as depicted in Fig. 1, and hence it cannot be utilized for producing the multilayer coil such as shown in Fig. 2. According to a conventional method for the manufacture of the multilayer coil depicted in Fig. 2, the one half 2R of the optical fiber 2 from its one end 2r to its middle or intermediate point 2c thereof and the other half 2L from its other end 2ℓ to its middle point 2c are wound onto a pair of supply bobbins 4R and 4L through use of a winding machine as shown in Fig. 3, then the middle point 2c of the optical fiber 2 is disposed at the innermost position in the take-up bobbin B, and as shown in Fig. 4, the one half 2R and the other half 2L of the optical fiber 2 are manually wound onto the take-up bobbin B from the supply bobbins 4R and 4L in the sequence and manner described previously with respect to Fig. 2. Another conventional method for the manufacture of the multilayer coil depicted in Fig. 2 is disclosed in the document EP-A-0 221 264. First, in the same way as shown in Fig. 3, two supply bobbins are prepared, each carrying one half of the optical fiber. Then, the two supply bobbins are alternately fixed to the take-up bobbin to be rotated with the latter. By rotating the take-up bobbin, a first layer is formed from the optical fiber drawn from the non-fixed supply bobbin. Before forming the next layer, the supply bobbins are exchanged and then the process is repeated. However, this prior art method involves handwork as mentioned above, and hence is very time- and labor-consuming. In addition, since the manual winding of the optical fiber 2 onto the take-up bobbin B is subject to each worker's individual difference in skill and concentration on the work, it is difficult to obtain multilayer coils in uniform quality. The document DE-A-1 614 559 discloses a coil winding machine for winding two wires in parallel layer by layer onto a take-up bobbin. This known machine comprises a spindle to one end of which a take-up bobbin holder is rotatably mounted by means of a bearing. A first tubular assembly is disposed on the spindle and rotatably supported by a frame. Opposite to the take-up bobbin a second tubular assembly is rotatably mounted to the frame. Both of the first and second tubular assemblies have guide arms for guiding the wires to be wound on the take-up bobbin. Adjacent to the end of the first tubular assembly on the side opposite to the take-up bobbin, a first supply bobbin is arranged coaxially with the first tubular assembly. A second supply bobbin is disposed adjacent to the end of the second tubular assembly facing away from its guide arms, the second supply bobbin being arranged coaxially to the common axial line of the first and second tubular assemblies. The wire from the first supply bobbin passes through the hollow inside of the spindle into a guide arm of the first tubular assembly to be guided radially outwardly and towards the second tubular assembly in the axial direction, leaves the guide arm and passes through guide holes in a guide arm of the second tubular assembly to be guided to the take-up bobbin by the latter. The wire from the second supply bobbin passes through the hollow shaft of the second tubular assembly and is guided by a guide arm of the second tubular assembly to the take-up bobbin. The spindle is axially movable such as to align guide holes in the guide arms of the second tubular assembly with the take-up space of the take-up bobbin. The document DE-A-33 28 403 discloses an apparatus for simultaneously winding a respective coil in two nuts of a stator or rotor of an electric rotating machine. The known apparatus comprises first and second spindles axially aligned but spaced apart from each other for holding the stator or rotor therebetween via respective chuck means. First and second tubular assemblies are rotatably and translatably mounted around said first and second spindles, respectively, and have first and second guide arms externally secured to them for guiding wires from a first and a second supply bobbin transversely up to the stator or rotor. The two tubular assemblies are simultaneously and synchronously rotated around said spindle by a common motor. It is an object of the present invention to provide an optical fiber coil winding machine and method for operating such machine by which one or more optical fibers prestored on two supply bobbins are wound onto a single take-up bobbin in a desired sequence and manner so that a multilayer coil of a desired structure can be obtained in uniform quality without involving large amounts of time and labor. This object is achieved with a coil winding machine and a method of operating it as claimed. The optical fiber coil winding machine of the present invention includes a pair of spindles holding therebetween a take-up bobbin and two rotary mechanisms which individually support one supply bobbin each having prestored thereon a part of or whole optical fiber. The rotary mechanisms can be mounted on the spindles concentrically therewith. The coil winding operation by the machine of the present invention starts with installing the take-up bobbin between the spindles and then mounting the supply bobbins on the corresponding rotary machanisms, followed by driving the spindles and the rotary mechanisms in accordance with a preset procedure, whereby one or more optical fibers stored on the supply bobbins can be wound onto the single take-up bobbin in a predetermined sequence and manner. Fig. 1 is a sectional view showing a usual solenoid-like multilayer coil; Fig. 2 is a sectional view showing, by way of example, a known optical fiber coil which is intended to be fabricated by the coil winding machine of the present invention; Fig. 3 is a diagram showing the state in which two substantially equal halves of an optical fiber are wound onto a pair of supply bobbins; Fig. 4 is a diagram showing a conventional method for manufacturing the known multilayer coil of the structure shown in Fig. 2; Fig. 5 is a sectional view illustrating an embodiment of the coil winding machine of the present invention; and Fig. 6 is a front view illustrating its principal parts. Figs. 5 and 6 illustrate an embodiment of the coil winding machine of the present invention, in which a pair of rotary mechanisms 30L and 30R, which individually support a pair of supply bobbins 4L and 4R, are rotatably mounted on a pair of rotatable spindles 10L and 10R concentrically therewith, the spindles holding therebetween a take-up bobbin B. As shown in Figs. 5 and 6, a bobbin adapter 20 loaded with the take-up bobbin B is held between the pair of axially aligned spindles 10L and 10R with their inner end portions 11L and 11R spaced a predetermined distance apart. The bobbin adapter 20 has a construction in which an inner tubular center 22 having fixed thereto one end of a spring 21 is housed in an outer tubular center 23; the spring 21 is fixed at the other end to the outer tubular center 23; a screw 24 is secured to the inner tubular center 22 for preventing it from coming off; a flange 25 is attached to one end of the outer tubular center 23 by means of a screw 26; the take-up bobbin B is mounted about the outer tubular center 23; and a flange 27 is attached to the other end of the outer tubular center 23 by screws 28. The bobbin adapter 20 is inserted between the inner end portions 11L and 11R of the spindles 10L and 10R, with the inner tubular center 22 pressed into the outer one 23 against the force of the spring 21, and then the pressing force applied to the inner tubular center 22 is removed. In consequence, the inner tubular center 22 partly projects out of the outer one 23 by the force of the spring 21 and the bobbin adapter 20 is resiliently held by the spindles 10L and 10R between their inner end portions 11L and 11R applying constant pressures to the adapter 20. Pulleys 12L and 12R are installed on the spindles 10L and 10R at the other ends thereof respectively. By driving the pulleys 12L and 12R at the same speed in the same direction. the spindles 10L and 10R and the bobbin adapter 20 loaded with the take-up bobbin B are rotated as one body. The rotary mechanism 30L on the spindle 10L, which carries the one supply bobbin 4L, includes: an index 32L having a flange 31L and rotatably mounted on the spindle 10L; a spinner 35L having a flange 33L and an arm 34L and mounted on the index 32L, the flange 33L being slidably coupled with the flange 31L by a guide 36L; a guide pulley 37L attached to the tip of the arm 34L; and a pulley 38L installed on the index 32L at its one end near the other end of the spindle 10L. The supply bobbin 4L is put on the spinner 35L from the side of the one end portion 11L of the spindle 10L prior to the loading of the bobbin adapter 20 between the spindles 10L and 10R. By driving the pulley 38L the index 32L and the spinner 35L are rotated as one piece. In that portion of the spinner 35L where the supply bobbin 4L is mounted there are provided bearings 39L which permit the bobbin 4L to freely rotate relative to the index 32L and the spinner 35L. The spinner 35L is coupled to the index 32L through the guide 36L and the supply bobbin 4L is mounted on the spinner 35L, so that the spinner 35L and the bobbin 4L are axially movable relative to the index 32L and the spindle 10L, within a predetermined range in their axial directions, respectively. A translation mechanism 40L is to translate the spinner 35L and the supply bobbin 4L, without impeding their rotation, relative to the index 32L and the spindle 10L in their axial directions, respectively. The translation mechanism 40L comprises a traverser 41L secured to the flange 33L of the spinner 35L, a feed screw 42L coupled to the traverser 41L, and a pulley 43L installed on the feed screw 42L. With the rotation of the pulley 43L in one direction, the traverser 41L, the spinner 35L and the supply bobbin 4L move as one body toward the take-up bobbin B, whereas when the pulley 43L is driven in the other direction, the traverser 41L, the spinner 35L and the bobbin 4L move away from the bobbin B. For the convenience of illustration, let it be assumed that the pulleys 12L, 12R, 38L, 38R, 43L and 43R include drive means therefor. A rotary mechanism 30R on the spindle 10R, which supports the other supply bobbin 4R, is symmetrical in configuration with the rotary mechanism 30L on the spindle 10L. A translation mechanism 40R for the supply bobbin 4R is also symmetrical in configuration with the translation mechanism 40L for the supply bobbin 4L. Accordingly, the parts of the rotary mechanism 30R and the translation mechanism 40R which correspond to the respective parts of the rotary and translation mechanisms 30L and 40L are identified by the same reference numerals with Rs in place of Ls. The illustrated example is intended for fabricating the multilayer coil of the structure depicted in Fig. 2. In this case, the one half 2L of the optical fiber 2 from its one end 2ℓ to the vicinity of its intermediate point 2c and the other half 2R from its other end 2ℓ to the vicinity of its intermediate point 2c are previously wound in a solenoid form on the supply bobbins 4L and 4R, respectively, by use of a conventional winding machine, as shown in Fig. 3. Then the intermediate portion of the optical fiber 2 in the vicinity of its intermediate point 2c is wound several turns around the take-up bobbin B mounted on the bobbin adapter 20 (see Fig. 6). Thereafter the supply bobbin 4L is put on the spinner 35L and the portion of the optical fiber 2 between the supply bobbin 4L and the take-up bobbin B is drawn across the guide pulley 37L. At the same time, the supply bobbin 4R is put on the spinner 35R and the portion of the optical fiber 2 between the supply bobbin 4R and the take-up bobbin B is drawn across the guide pulley 37R. Finally, the bobbin adapter 20 loaded with the take-up bobbin B is installed between the spindles 10L and 10R. At this time, the portion of the optical fiber 2 in the neighborhood of its intermediate point 2c is wound around the take-up bobbin B at one end thereof near the supply bobbin 4L, the spinner 35L and the supply bobbin 4L are placed at their outermost position or fartherest from the take-up bobbin B, and the spinner 35R and the supply bobbin 4R are placed at their innermost position or closest to the take-up bobbin B. The pulleys 12L, 12R, 38L, 38R and 43L, 43R are driven by a drive means (not shown) following the steps described below for driving the spindles 10L, 10R, the indexes 32L, 32R, and the feed screws 42L, 42R to rotate the take-up bobbin B and the spinners 35L, 35R by which the optical fiber 2 is wound onto the take-up bobbin B from the supply bobbins 4L and 4R. Step 1: The index 32R and the spinner 35R are not rotated but the spindles 10L and 10R, the take-up bobbin B, the index 32L, and the spinner 35L are rotated at the same speed in the counterclockwise direction as viewed from the right-hand side in Figs. 5 and 6, as indicated by the arrow CCW in Fig. 6. Since the spinner 35R remains stationary during the counterclockwise rotation of the take-up bobbin B and the spinner 35L at the same speed, the spinner 35R rotates relative to the take-up bobbin B in the clockwise direction as viewed from the right-hand side in Figs. 5 and 6, as indicated by the arrow CW in Fig. 6, while the spinner 35L is at a standstill relative to the take-up bobbin B. Consequently, the portion of the half 2R of the optical fiber 2 in the vicinity of the intermediate point 2c is wound onto the take-up bobbin B from the supply bobbin 4R. At this time, the supply bobbin 4R rotates relative to the spinner 35R in a manner to let out the portion 2R of the optical fiber 2 to the take-up bobbin B, whereas the supply bobbin 4L rotates together with the spinner 35L while remaining at a standstill relative to the take-up bobbin B. At the same time, the feed screw 42R is rotated in a direction in which to move the spinner 35R and the supply bobbin 4R away from the take-up bobbin B at a speed at which they are fed by a distance corresponding to the diameter of the optical fiber 2 for each rotation of the take-up bobbin B. By such feeding of the spinner 35R and the supply bobbin 4R, the portion 2R of the optical fiber 2 is wound side by side onto the take-up bobbin B in its axial direction Z. While the spinner 35R and the supply bobbin B are fed to their outermost position fartherest from the take-up bobbin B, that part of the half 2R of the optical fiber 2 which is the closest to the intermediate point 2c is wound, as the first layer, onto the take-up bobbin B from its one end to the other in its axial direction Z as indicated by the arrow 3c in Fig. 2. Step 2: The index 32L and the spinner 35L are not rotated but the spindles 10L and 10R, the take-up bobbin B, the index 32R and the spinner 35R are driven at the same speed in the clockwise direction as viewed from the right-hand side in Figs. 5 and 6. Since the spinner 35L remains stationary during the clockwise rotation of the take-up bobbin B and the spinner 35R at the same speed, the spinner 35L rotates relative to the take-up bobbin B in the counterclockwise direction as viewed from the right-hand side in Figs. 5 and 6, while the spinner 35R is at a standstill relative to the take-up bobbin B. Consequently, the portion 2L of the optical fiber 2 in the neighborhood of the intermediate point 2c is wound onto the take-up bobbin B from the supply bobbin 4L. At this time, the supply bobbin 4L rotates relative to the spinner 35L in a manner to let out the portion 2L of the optical fiber 2 to the take-up bobbin B, whereas the supply bobbin 4R rotates together with the spinner 35R while remaining at a standstill relative to the take-up bobbin B. At the same time, the feed screw 42L is rotated in a direction in which to move the spinner 35L and the supply bobbin 4L toward the take-up bobbin B at a speed at which they are fed by a distance corresponding to the diameter of the optical fiber 2 for each rotation of the take-up bobbin B. By such feeding of the spinner 35L and the supply bobbin 4L, the portion 2L of the optical fiber 2 is wound side by side onto the take-up bobbin B in its axial direction Z. While the spinner 35R and the supply bobbin 4L are fed to their innermost position closest to the take-up bobbin B, that part of the half 2L of the optical fiber 2 which is the closest to the intermediate point 2c is wound, as the second layer, onto the take-up bobbin B from its one end to the other in its axial direction Z as indicated by the arrow 3d in Fig. 2. Step 3: As in Step 2, the index 32L and the spinner 35L are not rotated but the spindles 10L and 10R, the take-up bobbin B. the index 35R and the spinner 35R are rotated at the same speed in the clockwise direction as viewed from the right-hand side in Figs. 5 and 6. Consequently, the portion 2L of the optical fiber 2 is wound onto the take-up bobbin B from the supply bobbin 4L. At the same time, the feed screw 42L is rotated in the direction opposite from that in Step 2, by which the spinner 35L and the supply bobbin 4L are moved away from the take-up bobbin B at the afore-mentioned speed. In consequence, while the spinner 35L and the supply bobbin B move to the outermost position fartherest from the take-up bobbin B, that part of the half 2L of the optical fiber 2 which is the second closest to the intermediate point 2c is wound, as the third layer, side by side onto the take-up bobbin B from the other end to the one end thereof in its axial direction Z as indicated by the arrow 3e in Fig. 2. Step 4: As in Step 1, the index 32R and the spinner 35R are not rotated but the spindles 10L and 10R, the take-up bobbin B, the index 32L and the spinner 35L are rotated at the same speed in the counterclockwise direction as viewed from the right-hand side in Figs. 5 and 6. Consequently, the portion 2R of the optical fiber 2 is wound onto the take-up bobbin B from the supply bobbin 4R. At the same time, the feed screw 42R is rotated in the direction opposite from that in Step 1, by which the spinner 35R and the supply bobbin 4R are moved toward the take-up bobbin B at the afore-mentioned speed. As a result of this, while the spinner 35R and the supply bobbin 4R move to their innermost position closest to the take-up bobbin B, that part of the half 2R of the optical fiber 2 which is the second closest to the intermediate point 2c is wound side by side, as the fourth layer, onto the take-up bobbin B from the other end to the one end thereof in its axial direction Z as indicated by the arrow 3f in Fig. 2. In the subsequent steps, Steps 1 to 4 described above are repeated. Thus the multilayer coil of the structure shown in Fig. 2 is obtained. After winding of the multilayer coil, the bobbin adapter 20 is dismounted from between the spindles 10L and 10R, the flange 27 is detached from the tubular center 23, and then the take-up bobbin B carrying the multilayer coil is removed from the tubular center 23. The embodiment depicted in Figs. 5 and 6 has been described in connection with the case where the spinner 35R (or 35L) from which a part of the optical fiber 2 is currently wound onto the take-up bobbin B is not rotated but instead the spinner 35L (or 35R) from which the optical fiber 2 is not currently wound onto the take-up bobbin B and the take-up bobbin B are driven at the same speed in the same direction. According to this winding method, the guide pulley 37R (or 37L) which currently guides the optical fiber 2 being wound onto the take-up bobbin B is held at a standstill. Lettig the axis of rotation of the bobbin B be represented by Z and mutually orthogonal axes perpendicular to the Z axis be represented by X and Y, respectively, the spatial coordinate position (x, y, z) where the optical fiber 2 being wound onto the take-up bobbin B is tangent thereto shifts in the Z-axis direction but remains substantially stationary in the X- and the Y-axis direction. This facilitates the operator's monitoring of the state of the optical fiber 2 being wound onto the take-up bobbin B. When there is no need of monitoring the state of the optical fiber 2 being wound onto the take-up bobbin B as in the case where the coil winding machine is so designed as to permit automatic control of the number of turns of the optical fiber 2, only the spinner 35R (or 35L) from which a part of the optical fiber 2 is currently wound onto the take-up bobbin B needs to be driven, with the bobbin B held stationary at all times. In such a case, the pulleys 12L and 12R and the drive means (not shown) therefor can be left out. Alternatively, it is possible to employ an arrangement in which when either one of the left-and right-hand portions 2L and 2R of the optical fiber 2 is wound onto the take-up bobbn B, the bobbin B is rotated, whereas when the other is wound onto the take-up bobbin B, the bobbin B is held stationary and the corresponding spinner 35L or 35R is driven. In the case where the rotary mechanisms 30L and 30R, which individually carry the supply bobbins 4L and 4R, are mounted on the spindles 10L and 10R concentrically therewith as in the embodiment shown in Figs. 5 and 6, the coil winding machine can be formed simple and small. Yet, rotary shafts of the pair of rotary mechanisms may also be provided in parallel or at right angles to the spindles carrying the take-up bobbin. It is also possible to adopt an arrangement in which one different optical fiber is wound in the solenoid form onto each of a pair of supply bobbins in advance, the two fibers are wound onto the take-up bobbin in the same manner as that used for winding the portions 2L and 2R of the optical fiber 2 in the above-described embodiment, and then the two optical fibers thus wound onto the take-up bobbin are connected together, obtaining the multilayer coil of the structure depicted in Fig. 2. The present invention is applicable as well to the case where a part of an optical fiber or one optical fiber is prestored on each of three or more supply bobbins, the respective parts or the respective optical fibers are wound onto a take-up bobbin in a predetermined sequence and manner, and they are connected as required, thereby obtaining a multilayer coil of a predetermined structure. As described above, according to the present invention, two spindles for holding therebetween a take-up bobbin and two rotary mechanisms for individually carrying a respective one of two supply bobbins, each having prestored thereon a part of an optical fiber or one optical fiber, are provided, by which the respective parts of the optical fiber or the respective optical fibers can be wound onto the take-up bobbin in a predetermined sequence and manner, providing a multilayer coil of a desired structure in uniform quality without involving large amounts of time and labor. Furthermore, the entire structure of the coil winding machine can be made simple and small in the case where the two rotary mechanisms each carrying one of the supply bobbins are mounted respectively on the two spindles concentrically therewith.

Claims: A coil winding machine for winding an optical fiber coil onto a take-up bobbin (B), said machine comprising: first (10R) and second (10L) spindles axially aligned but spaced apart from each other, for holding the take-up bobbin (B) therebetween, by its opposite axial ends; first (32R, 35R) and second (32L, 35L) tubular assemblies rotatably and translatably mounted around said first and second spindles, respectively; first (4R) and second (4L) supply bobbins each having an optical fiber (2R, 2L) prestored thereon, rotatably mounted around said first and second tubular assemblies, respectively; first (34R) and second (34L) guide arms externally secured to said first and second tubular assemblies, respectively, for guiding the optical fiber supplied from said first and second supply bobbins transversally up to the take-up bobbin; first (38R) and second (38L) independent driving means for selectively rotating either said first or said second tubular assembly relative to both of said first and second spindles; and first (40R) and second (40L) means for selectively moving either the first or the second tubular assembly axially along its corresponding spindle. The coil winding machine of claim 1, wherein: said first (32R, 35R) and second (32L, 35L) rotatable and translatable tubular assemblies include first (32R) and second (32L) index tubular members rotatably mounted on, and fixed axially to, said first and second spindles, respectively; and first (35R) and second (35L) spinner tubular members mounted around said first and second index tubular members, respectively, in a manner such as to be rotatably secured therewith and axially translatably therealong; and said first (4R) and second (4L) supply bobbins and said first (34R) and second (34L) guide arms are mounted on said first (35R) and second (35L) spinner tubular members, respectively; said first (38R) and second (38L) driving means for rotating are engaged with said first (32R) and second (32L) induex tubular members, respectively; and said first (40R) and second (40L) driving means for translating are engaged with said first (35R) and second (35L) spinner tubular members, respectively. The coil winding machine of claim 2, wherein said first (10R) and second (10L) spindles are arranged so as to be rotatable, the machine further including spindle driving means (12R, 12L) for simultaneously rotating both of said first and second spindles. A method of operating the coil winding machine of claim 3 which comprises the following different steps: Step 1: wherein said first spinner tubular member (35R) is driven to move away from said second spinner tubular member (35L), with said first index tubular member (32R) held stationary, and at the same time, said first and second spindles (10R, 10L) and said second index tubular member (32L) are rotated clockwise at the same speed by a first predetermined number of times so that said take-up bobbin (B) is rotated by said first predetermined number of times while being held stationary relative to said second supply bobbin (4L), whereby said optical fiber (2R) supplied from said first supply bobbin (4R) is wound onto said take-up bobbin (B) by said first predetermined number of times; Step 2: wherein said second spinner tubular member (35L) is driven to approach said first spinner tubular member (35R), with said second index tubular member (32L) held stationary, and at the same time, said first and second spindles (10R, 10L) and said first index tubular member (32R) are rotated counterclockwise at the same speed by a second predetermined number of times so that said take-up bobbin (B) is rotated by said second predetermined number of times while being held stationary relative to said first supply bobbin (4R), whereby said optical fiber (2L) supplied from said second supply bobbin (4L) is wound onto said take-up bobbin (B) by said second predetermined number of times; Step 3: wherein said second spinner tubular member (35L) is driven to move away from said first spinner tubular member (35R), with said second index tubular member (32L) held stationary, and at the same time, said first and second spindles (10R, 10L) and first index tubular member (32R) are rotated counterclockwise at the same speed by a third predetermined number of times so that said take-up bobbin (B) is rotated by said third predetermined number of times while being held stationary relative to said first supply bobbin (4R), whereby said optical fiber (2L) supplied from said second supply bobbin (4L) is wound onto said take-up bobbin (B) by said third predetermined number of times; Step 4: wherein said first spinner tubular member (35R) is driven to approach said second spinner tubular member (35L), with said first index tubular member (32R) held stationary, and at the same time, said first and second spindles (10R, 10L) and said second index tubular member (32L) rotated clockwise at the same speed by a fourth predetermined number of times so that said take-up bobbin (B) is rotated by said fourth predetermined number of times while being held stationary relative to said second supply bobbin (4L), whereby said optical fiber (2R) supplied from said first supply bobbin (4R) is wound onto said take-up bobbin (B) by said fourth predetermined number of times; and Step 5: wherein said Steps 1 through 4 are repeated a plurality of times.

Inventors: HARASHIMA MASAKAZU C O JAPAN A, OHNO ARITAKA C O JAPAN AVIATIO, SHITARA KANJI C O JAPAN AVIATI, HARASHIMA, MASAKAZU C/O JAPAN AVIATION, OHNO, ARITAKA C/O JAPAN AVIATION, SHITARA, KANJI C/O JAPAN AVIATION
Applicants: JAPAN AVIATION ELECTRON, JAPAN AVIATION ELECTRONICS INDUSTRY, LIMITED
Application year: 1989
Main classification: G02B6
IPC codes: G02B6, B65H55, H01F41, B65H54