FIBER OPTIC SENSING COIL

Abstract: A symmetric fiber optic sensing coil for use in a rotation sensing device such as a gyroscope. The coil comprises a plurality of turns of a continuous strand of orthogonally wound fiber optic material. The coil may comprise either dualpole or quadrupole symmetry and may be formed on a spool having at least one aperture in each of its circular flanges. The symmetric sensing coil is minimally affected by environmental factors such as temperature, vibration and magnetic fields that can otherwise produce measurements that are indistinguishable from sensed rotation.

Description: This invention relates to sensing coils for fiber optic rotation sensing devices and tooling therefor. Fibre optic rotation sensing devices, such as gyroscopes, comprise two main components, (1) an interferometer (including a light source, beamsplitter, and detector) and (2) a fibre optic sensing coil, that are mounted to a rotatable platform. Light from the interferometer's light source is split by the beamsplitter into two beams, which are coupled into respective opposed ends of the sensing coil. The interferometer and associated electronics process the phase relationship between the two interfering, counter-propagating, beams of light when they emerge from (opposite ends of) the coil. A phase shift difference between the two beams results from (1) coil rotation and (2) so-called "environmental" factors. Environmental factors include such variables as temperature, vibration (both acoustical and mechanical), and magnetic fields. These factors can induce phase shifts between the counter-rotating beams which are indistinguishable from those that are induced by rotation. Environment-induced phase shifts reflect the effects of such factors upon variations in the optical light path that each beam encounters as it travels through the coil. Environmental factors are both time varying and unevenly distributed throughout the coil. As it takes a finite amount of time for a beam's wave front to pass a particular point, the effects upon the two beams are unequal, producing an undesirable (phase-shift) effect that is not later cancelled out. In the past, particular coil winding arrangements have been utilized in attempts to minimize the effects of environmental interference factors and thereby enhance the accuracy of the sensor. Symmetric windings are arranged so that the center of the fiber forms the central turns of the coil while the ends of the fiber form its outer turns. While the advantages of symmetric windings are recognized, this desirable arrangement has proven difficult to realize. At the present time, fiber optic sensing coils are commonly wound in a helix-type configuration. In a helix winding, turns of the fiber cross the coil axis at ninety degrees plus or minus a so-called "helix angle". In the first layer of such a sensing coil, the turns are generally wound from left to right, forming a left-handed helix. The fiber of the second layer, which rests atop the first layer, runs from right to left to form a right-handed helix. Unfortunately, the reversal of the senses of the windings of adjacent layers tends to destroy the desired symmetry and regularity of the coil. The windings of a layer tend to "follow" the reversely-­ directed "grooves" that are formed between adjacent turns of the underlying layer. As a result, it is quite difficult to maintain the desired reversal of the senses of the windings of adjacent layers. Furthermore, as the turns of a layer alternate between lying atop and following the "grooves" of the preceding layer, the space between turns widens to an extent that turns from overlying layers begin to merge with those of preceding layers. The departure from an ideal, reversely-wound, helical configuration increases as the number of overlying layers increases. At a radial distance of twelve to fourteen layers it is virtually impossible to distinguish the senses of the turns or the turns of adjacent layers. As a consequence, the desired cancellation of the effects of environmental disturbances is limited by the very configuration of the conventional, helically-wound, fiber optic sensing coil. According to one aspect of the present invention there is provided a coil for a fiber optic rotation sensor comprising a continuous fiber of substantially round and uniform cross section arranged into a cylindrical coil comprising a plurality of layers of turns of said fiber whereby grooves are formed by adjacent turns, characterised in that each of said turns includes a first portion orientated perpendicularly to the axis of said coil and a second portion angularly disposed with respect thereto, each of said layers comprising a plurality of turns wherein said first portions are adjacent one another and said second portions are adjacent one another and adjacent layers are arranged so that the first portions of turns of a layer lie in the grooves created between the first portions of the turns of the underlying layer. According to a second aspect of the invention, there is provided a spool for use in orthogonally winding an optical coil according to claim 1 and comprising a cylindrical core having a pair of substantially-circular flanges positioned at opposed ends of said core, characterised in that each of said flanges has at least one aperture that is outwardly directed from said core to the flange periphery, said apertures having rounded interior edges, and said flanges tapering to said rounded interior edges. For a better understanding of the invention and to show how the same may be carried into effect, reference will now be made, by way of example, to the accompanying drawings, in which: Figure 1 is a perspective view of a fiber optic sensing coil in accordance with a first embodiment; Figure 2 is a perspective view of a spool for use in forming a coil in accordance with the embodiment of Figure 1; Figure 3 is a partially broken front elevation view of a fiber optic sensing coil as it is wound up on a spool; Figure 4 is a greatly enlarged, broken view taken along the section line 4-4 of the coil and spool of Figure 3 that illustrates the so-called "climbing" of the fiber of an orthogonally-wound fiber optic sensing coil of the quadruple type; Figure 5 is a partial side view, corresponding generally to that of Figure 4, that illustrates the contrasting mode of fiber climbing in an orthogonally wound sensing coil of the dualpole; and Figure 6 is a perspective view of a spool for use in forming a sensing coil in accordance with the embodiment of Figure 5. Turning now the drawings, Figure 1 is a perspective view of a sensing coil 10 for incorporation into a fiber optic gyroscope. Such a gyroscope is disclosed, for example, in United States Patent Number 4,410,275 of Shaw for "Fiber Optic Rotation Sensor" issued October 18, 1983. The self-supporting coil 10 comprise a continuous strand of optical fiber 12 (shown somewhat enlarged in diameter for clarity) that was previously formed upon a spool or like support (not shown) to comprise a plurality of concentric coil turns about a central axis 14. The coil 10 forms an optical cavity for counter-rotating beams of optical energy which are coupled into respective opposed ends 16, 18 of the single continuous coil fiber 12. An operational embodiment of a coil 10 has been formed of a total of 1056 turns (22 layers, each of 48 turns) of average turn radius approximately 7.5 centi­ meters. The fiber 12 has representative dimensions of, for example, 250 microns (outer diameter), by 75 microns (cladding diameter) for use with a 0.825 micron wavelength laser. Such dimensions and quantifying numbers are given solely as representative of a known application of the invention and by no means do they represent or imply any limitation upon the scope of this invention. The fiber that forms the coil 10 is wound symmetrically about the axis 14. As will become further apparent, the winding is accomplished in such a way that the fiber's turns are symmetrical about its center or midpoint 20 with the ends 16, 18 of the fiber 12 radiating therefrom in a symmetrical configuration of the orthogonal (quadrupole embodiment) type. To achieve an orthogonal configuration, the continuous optical fiber 12 is trans­ ferred in equal amounts according to a selected protocol, from two different supply reels to a single take-up reel or spool (discussed below) of preselected configuration so that two equal "supply" segments 22, 24 of the fiber 12 extend, in opposite directions, from its center 20. Each layer of the coil 10 comprises a plurality of turns of only one of the oppositely-directed segments 22 or 24. The coil 10 may be either self-supporting (as shown in Figure 1) or may remain wound about a spool when in use as an element of a sensor. In a self-supporting coil 10, the contiguous coil turns are fixed by appropri­ ate adhesive prior to removal from a winding spool. Removal is normally accomplished by application of a thermoplastic coating to the fiber (prior to winding) followed by heating the wound coil to fuse and bond the coatings of contiguous turns. Figure 2 is a perspective view of a support or take-up spool 26 for use in forming the sensing coil 10. The spool 26 includes a pair of generally-circular flanges 28 and 30 mounted to opposed ends of a cylindrical hollow core 32 to form boundaries for retaining turns of the optical fiber as the sensing coil 10 is wound thereon. An orthogonally wound layer 34 of nylon fiber, of uniform diameter and roundness, may be fixed (by gluing or like means) to the surface of the core 32. The diameter of such fiber is preferably at least as great as that of the optical fiber of the coil and should not exceed it by more than three (3) per cent to assure that an identical number of turns per layer is achieved in the winding of the coil upon the spool. Alternatively, the equivalent pattern may be formed by machining, molding or the like, at the surface of the core 32. It will become apparent from the discussion that follows that such texturing of the surface of the core promotes the winding of orthogonal layers onto the spool. The flanges 28, 30 may be either permanently or removably fixed to the core 32. In a detachable assembly, the flanges 28, 30 may be fixed by means of conventional spring-like metal fingers or the like that are arranged to engage the inner surface of the core 32. An exemplary embodiment of the spool 26 includes flanges of 15 centimeter diameters and 2.5 millimeter thickness with an outer core diameter of 14 centimeters and core thickness of 2.5 millimeters. The spool 26 is preferably of relatively high thermal conductivity and low thermal expansion coefficient material. Elongated apertures 36 and 38 are located in flanges 28 and 30 respectively. As will be shown below, such apertures provide a means for displacing the fiber supply segments beyond the flanges during the coil winding process to prevent undesired interferences with the coil formation process. The apertures 36, 38 extend from the surface of the core 32 to the flange's outer edges and are laterally displaced by a distance x. The significance of the relative displacements of the apertures 36, 38 will become apparent below. The apertures are not radial but rather separated by x throughout their lengths so that the size of a crossover region (discussed below) remains constant throughout the coil. Figure 3 is an partial broken front elevation view of a fiber optic sensing coil 10 wound upon a spool as illustrated in Figure 2. As indicated in this view, fiber of the supply segment 24 is displaced outside the flange 28 through the aperture 36. Fiber from supply segment 22, having "climbed" or risen from a preceding layer is wound orthogonally into the first turn of the next coil layer. For purposes of illustration, the fiber material 12 is shown in exaggerated proportion with respect to flange thickness, the ratio of flange thickness to fiber diameter in an actual embodiment being approxi­ mately 10 to 1. In an orthogonally wound coil, unlike a helical coil, the greater portion of each coil turn is oriented substantially perpendicular to the coil axis. Thus a right angle 40 exists between the major portion 42 of each turn forming a layer and the coil axis 14. This alignment utilizes the grooves formed between adjacent turns (or an end turn and the adjacent flange) of adjacent coil layers to secure or anchor a substantial percentage of the length of each turn. Such grooves provide inter­ locking channels for guiding the turns of overlying layers. Such an interlocking effect can be seen quite clearly at the lower sectional portion of the coil of Figure 3. The substantially round fibers of adjacent layers are seen to fit neatly into the grooves that exist between the round fibers of the preceding layer. The number of turns of the optical fiber (per layer) determines the distance d between the opposed interior surfaces of the flanges 28 and 30. The distance d is calculated as: d = ( n + 1/2 )*d Fiber where n = number of turns per layer d Fiber = diameter of optical fiber. As discussed above, the greater portion of each coil turn is orthogonal to the coil axis 14. A "cross-over" region of turn segments that are angularly-­ inclined with respect to the major orthogonal turn segments is formed in each layer. The angularly-inclined segments (each of which comprises between five to ten per cent of a coil turn depending on coil diameter) of overlying coil layers do not interlock as do the orthog­ onal turn segments. Rather, the design of the coil is effectively "anchored" throughout ninety (90) to ninety-­ five (95) percent of the windings so that both the beginning and the end of each angularly-inclined turn section is reliably secured. As a result, inconsistencies (in terms of angular orientations) between the crossover regions of overlying coil layers do not degrade the structure. As shown at 44, a cutaway section for exposing a portion of the cross-over region of the underlying fiber layer, the fibers of this region are oppositely directed. As mentioned above, such a reversal can be sustained in Applicant's coil unlike a helically-­ wound coil wherein an anchoring orthogonal turn section is not provided. In forming a quadrupole coil by utilizing the tooling of the spool 26 of Figure 2, a cross-over region of the fiber layer is formed between taper point 46 and taper point 48 of the interior surfaces of the flanges 28 and 30 respectively that define the beginnings of tapers in the flanges towards the apertures 36 and 38. The tapers and the apertures provide room for the fiber to "climb" up and around the end turns of preceding layers without disturbing the layer. A bend 50 of the fiber occurs as the fiber of a supply segment climbs from the underlying layer formed from that supply segment. The geometry of the flange 30 is arranged so that its interior surfaces begin to taper at 48, 52 while the exterior surfaces of the flange 30 begin to taper at 54, 56 toward the rounded apexes 58, 60 that define the sides of the aperture 38. A like arrangement is provided with respect to the region of the aperture 36 of the flange 28. The exterior tapers of the flanges provide a measure of protection when the supply segments are displaced outside or within an aperture preventing undesirable "pinching" of the optical fiber. The rounded apexes provide further protection against damage to the fiber during the winding of the coil. The climbing or ascent of a supply segment from layer to layer is shown in Figure 4, a partially broken side elevation view taken at 4-4 of Figure 3. In this view "end" turns (each from a different coil layer) adjacent the flange 30 are numbered sequentially from 62 to 78. In practice, of course, a wide range of numbers of layers may be employed. The order of the supply segments, and the resultant climbing sequence is determined by the specific type (quadrupole, dualpole or variations thereof) of orthogonal coil configuration employed. Figure 4 relates to a coil of quadrupole symmetry wherein the end turns 62, 68, 70, 76, and 78 (i.e. every fourth layer, beginning with the layer adjacent the core of the spool) are wound from one supply segment while the layers of the turns 64, 66, 72, and 74 are wound from the other supply segment. The inclined section 80 of fiber of the first supply segments climbs around the edge turns (and layers aligned therewith) to reach and thereby initiate the formation of an overlying layer indicated by the end turn 68. Similarly, an inclined section 82 begins with the end turn 70 that is shown to lie atop the layer 68 and climbs above the two layers of end turns 72 and 74 to begin the end turn 76 that initiates the corresponding overlying layer. The identical climbing process occurs at the opposed edge or "cheek" of the coil. The two sequences are staggered as a result of the occurrence of an initial one-layer step from the innermost layer to an overlying layer. Thereafter, the climbing or winding proceeds by the illustrated "jumping" of two overlying layers. Thus at the opposed cheek, the second supply segment climbs from layer 62 to layer 64, then from layer 66 to layer 72, etc.. Figure 5 corresponds generally to the preceding figure for illustrating an orthogonally wound optical fiber having alternative dualpole symmetry. In such a symmetry each adjacent layer is wound from a different supply segment alternating with every layer rather than with every other layer as in the coil of the quadrupole symmetry described above. As will be shown below, this variation of the winding process is enhanced by the spool design that differs from the spool utilized for forming a quadrupole wound coil. As each layer climbs, inclined segments, originating with each supply segment, extend from each end turn at each of the opposed cheeks of the coil. Thus inclined segments 84 from the first supply climb from layers 86 to 90, 94 to 98, and 102 to 106 respectively while the oppositely inclined fiber segments 110 of the second supply climb from layers 88 to 92, 96 to 100 and 104 to 108 respectively. The turns of both quadrupole and dualpole wound coils are characterized by substantially larger orthogonal portions than the angular portions that comprise the cross-over regions of each layer. As a result, in each of such embodiments, the major portion of each turn interlocks with those of underlying layers so that the beginnings and ends of crossover region segments are secured and their preferred orientations preserved. Thus, both embodiments avoid the harmful distortion of turns that occurs in the formation of a helically wound coil. Figure 6 is a perspective view of a spool 112 adapted for use in forming a dualpole wound coil. As in the spool 26 of Figure 2, flanges 114, 116 include elongated apertures separated by an identical distance x for permitting and assisting the above described fiber climbing process. However, a pair of apertures 118, 120 are formed in each of the flanges 114, 116 rather than a single opening. The additional aperture is provided to prevent interference between the oppositely-directed supplies during the winding process. Further, by providing a pair of apertures in each flange the positions of the oppositely-inclined "climbing" portions of turns are separated preventing undesirable crossing of the inclined segments 84 and 110 of Figure 5. Thus it is seen that there has been brought to the art an improved fiber optic sensing coil and tooling for use in fabricating such a coil. By utilizing such a coil, one may measure rotation with greater accuracy as the effects of environmental factors are minimized. It has been mentioned that the fiber is wound from two supplies onto the spool. In one scheme, one supply is clamped coaxially to the spool and rotated therewith to wind one or more layers from the other supply. A shuttle is used to guide the fiber on the desired path. Then, the one supply is released and the other clamped coaxially to the spool so that one or more layers can be wound from the one supply. This process is repeated, alternating between the supplies, until all the layers are complete and an orthocyclic winding is achieved. When the condition shown in Figure 1 is attained, the center of the fiber will lie at the centre of the innermost layer. It thus follows that the supply used to form the innermost layer will have supplied one half a layer more than the other supply. It is also a result that, commencing from the center of the fiber, the two paths to the free ends are substantially symmetrical, this resulting from the use of two supplies for the one fiber. While this invention has been described in its preferred embodiments, its scope is not limited thereto. Rather it is only limited insofar as defined in the following set of claims and such scope includes all equivalents thereof.

Claims: 1. A coil for a fiber optic rotation sensor comprising a continuous fiber (12) of substantially round and uniform cross section arranged into a cylindrical coil (10) comprising a plurality of layers of turns of said fiber whereby grooves are formed by adjacent turns, characterised in that each of said turns includes a first portion (42) orientated perpendicularly to the axis of said coil (10) and a second portion (44) angularly disposed with respect thereto, each of said layers comprising a plurality of turns wherein said first portions are adjacent one another and said second portions are adjacent one another and adjacent layers are arranged so that the first portions of turns of a layer lie in the grooves created between the first portions of the turns of the underlying layer. 2. A coil as defined in claim 1, wherein said first portions (42) comprises between ninety to ninety-­ five percent of the length of each turn. 3. A coil as defined in claim 1 or 2 wherein said coil has been wound form two supplies, each of said supplies providing substantially one half of said fiber, said layers having been wound in opposite directions from said supplies, and said coil is formed by alternating windings from said supplies. 4. A coil as defined in claim 1, 2 or 3, wherein said fiber additionally includes a plurality of inclined turn segments for connecting layers. 5. A coil as defined in claim 4 wherein said inclined turn segments are located at an edge of a layer. 6. A coil as defined, in claim 3, or claim 4 or 5 when appended to claim 3, wherein two layers are wound consecutively from one supply. 7. A coil as defined in claim 3, or claim 4 or 5 when appended to claim 3, wherein adjacent layers are wound from different supplies. 8. A spool for use in orthogonally winding an optical coil according to claim 1 and comprising a cylindrical core (34) having a pair of substantially-­ circular flanges (28,30) positioned at opposed ends of said core (34), characterised in that each of said flanges has at least one aperture (36, 38) that is outwardly directed from said core to the flange periphery, said apertures having rounded interior edges (58), and said flanges tapering to said rounded interior edges. 9. A spool as defined in claim 8, wherein a single layer of orthogonally-wound fiber is fixed to the surface of said core. 10. A spool as defined in claim 8 wherein an orthogonal winding pattern in formed in the surface of said core. 11. A spool as defined in claim 8, 9 or 10, wherein a single aperture is formed in each flange and said apertures are laterally offset by a predetermined amount. 12. A spool as defined in claim 11 wherein said apertures are parallel throughout their lengths. 13. A spool as defined in claim 9 or 10, wherein a pair of apertures is formed in each flange and the apertures of said flanges are aligned. 14. A spool as defined in any one of claims 8 to 13, wherein said apertures further include rounded exterior edges and said flanges taper to said rounded exterior edges. 15. A spool for use in orthogonally winding an optical coil according to claim 1 and comprising a cylindrical core (34) having a pair of substantially-­ circular flanges (28,30) positioned at opposed ends of said core (34), characterised in that each of said flanges has at least one aperture (36, 38) that is outwardly directed from said core to the flange periphery, and an aperture in one flange being laterally offset from an aperture on the other flange. 16. A fiber optic rotation sensing device including a coil according to any one of claims 1 to 7.

Inventors: BEDNARZ, BRONEK
Applicants: LITTON SYSTEMS CANADA LIMITED
Application year: 1988
Main classification: G01C19
IPC codes: G02B6, G01C19