WO1989008237A1 - Torsional vibration drive - Google Patents
Torsional vibration drive Download PDFInfo
- Publication number
- WO1989008237A1 WO1989008237A1 PCT/EP1988/001152 EP8801152W WO8908237A1 WO 1989008237 A1 WO1989008237 A1 WO 1989008237A1 EP 8801152 W EP8801152 W EP 8801152W WO 8908237 A1 WO8908237 A1 WO 8908237A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- torsional vibration
- wheel rim
- spokes
- vibration drive
- axis
- Prior art date
Links
- 238000005452 bending Methods 0.000 claims abstract description 24
- 230000010355 oscillation Effects 0.000 claims description 3
- 230000005484 gravity Effects 0.000 claims description 2
- 239000000463 material Substances 0.000 claims description 2
- 230000007704 transition Effects 0.000 claims 1
- 238000013461 design Methods 0.000 description 6
- 229910000831 Steel Inorganic materials 0.000 description 5
- 239000010959 steel Substances 0.000 description 5
- 230000008878 coupling Effects 0.000 description 4
- 238000010168 coupling process Methods 0.000 description 4
- 238000005859 coupling reaction Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 238000005259 measurement Methods 0.000 description 4
- 230000008901 benefit Effects 0.000 description 3
- 238000002474 experimental method Methods 0.000 description 3
- 230000000737 periodic effect Effects 0.000 description 3
- 229910001374 Invar Inorganic materials 0.000 description 2
- 239000000919 ceramic Substances 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 239000000956 alloy Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000969 carrier Substances 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 239000013013 elastic material Substances 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 230000010287 polarization Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 239000013598 vector Substances 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C07—ORGANIC CHEMISTRY
- C07F—ACYCLIC, CARBOCYCLIC OR HETEROCYCLIC COMPOUNDS CONTAINING ELEMENTS OTHER THAN CARBON, HYDROGEN, HALOGEN, OXYGEN, NITROGEN, SULFUR, SELENIUM OR TELLURIUM
- C07F9/00—Compounds containing elements of Groups 5 or 15 of the Periodic Table
- C07F9/02—Phosphorus compounds
- C07F9/28—Phosphorus compounds with one or more P—C bonds
- C07F9/38—Phosphonic acids [RP(=O)(OH)2]; Thiophosphonic acids ; [RP(=X1)(X2H)2(X1, X2 are each independently O, S or Se)]
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
- G01C19/58—Turn-sensitive devices without moving masses
- G01C19/64—Gyrometers using the Sagnac effect, i.e. rotation-induced shifts between counter-rotating electromagnetic beams
- G01C19/66—Ring laser gyrometers
- G01C19/68—Lock-in prevention
- G01C19/70—Lock-in prevention by mechanical means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F1/00—Tubular elements; Assemblies of tubular elements
- F28F1/10—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses
- F28F1/40—Tubular elements and assemblies thereof with means for increasing heat-transfer area, e.g. with fins, with projections, with recesses the means being only inside the tubular element
Definitions
- the invention relates to a torsional vibration drive with the features of the preamble of claim 1.
- Ring laser gyroscopes can measure rotational speeds with great accuracy.
- ring laser gyroscopes cannot measure very small rotational speeds without special countermeasures, since the frequencies of the two light waves rotating in opposite directions, due to an inertial rotation, converge on a common one Pull intermediate frequency together (pull-in effect of coupled oscillators, so-called lock-in effect).
- the size of this Tatzone which extends around the rotational speed zero point, can be influenced by a number of laser gyro-specific design criteria, but remains so large even with the best possible design of the relevant parameters that the rotational speed measurement error in almost all practical applications, e.g. B. in position control or even more so in navigation systems is unacceptable.
- the laser gyroscope is set in uniform rotational vibrations about an axis that is perpendicular to the beam path plane.
- the time period during which frequency synchronization takes place at the turning points of the torsional vibration of the laser gyroscope is determined by the maximum amplitude and the frequency of the vibration and can thus be minimized.
- the measurement error of the laser gyro still remaining in this regard is thus significantly reduced. Due to the torsional vibration, no structural deformation of the base body, such as B periodic stretching, compression or bending are caused, since this leads to incorrect measurement behavior of the laser gyro due to a periodic or non-periodic loss modulation of the optical resonator.
- the torsion transducers have spokes of uniform cross-section, on which piezoceramic plates are applied and which thus represent multilayer bending elements. If an electrical voltage is applied r , a bending moment is generated in the spokes, which results in a torque acting on the wheel rim. Usually, the voltage is excited, the frequency of which corresponds to the resonance frequency of the system.
- the mass of the laser body is usually very large and the space allowed for the vibration mechanism is very small. This means that the rotary transducer must be made of a material that has a modulus of elasticity that is comparable to that of steel.
- the axis of rotation must be kept stable. This requires that the rotary oscillator has extremely high stiffness about all axes except the axis of rotation, which in turn requires that the spokes parallel to the axis of rotation are as extensive as possible.
- the operating amplitude is usually limited by the surface tensile strength of the piezoceramic.
- the finished device must be suitable to be operated in an extended ambient temperature range, as is required by various user specifications.
- the vibration generator must be connected to the gyro block by means of a coupling which prevents structural deformation of the gyro block due to thermal expansion in the radial direction.
- This coupling can be simple, such as. B. a thick layer of elastic material or complicated, such as. B. a multi-part three-dimensional bending element.
- the result is a coupling that is very stiff in the direction of rotation and very flexible in the radial direction.
- this coupling represents a limitation in the performance of the gyroscope, since it reduces the axis rigidity.
- Arrangements according to the prior art are made of steel with a low coefficient of expansion, e.g. Made in Invar and consist of a central pin, four or six flat spokes with a uniform rectangular cross-section and a cylindrical wheel rim, which also has a uniform rectangular cross-section.
- Piezoceramic plates are applied to the side surfaces of each spoke, all of which are simultaneously subjected to a high voltage of such a frequency that the system oscillates at its resonance frequency.
- the present invention proposes a specially designed rotary oscillator with a piezo drive for laser gyroscope, which is suitable for being operated at a significantly increased frequency and amplitude.
- the rotary transducer according to the invention is constructed similarly to the previous rotary transducers: it is made from a single block of steel with low thermal expansion and has a central hub which, for. B. is attached to the carrier vehicle, and further has spokes and a wheel rim, both of which have a uniform rectangular cross-section.
- the spokes are attached to the wheel rim using a special bending element.
- This bending element is designed in such a way that it works like a joint which has a great flexibility for bending movements in the plane perpendicular to the axis of rotation, but which has a high rigidity for bending movements outside this plane.
- the joint decouples the wheel rim from the bending moment at the outer end of the spokes. This avoids the usual deformation of the wheel rim, which would either be transferred to the gyro block, or dissipate valuable vibration energy into the wheel rim / gyro base body connection. The result is that higher mechanical quality can be achieved. Exemplary embodiments are explained on the basis of the drawing.
- FIG. 1 shows a top view of a rotary oscillator according to the invention
- Fig. 2 shows a connection of Fig. 1 in detail
- 3A and 3B show spoke connections with or without the special joint according to the invention.
- 5A and 5B show spoke and wheel rim deflections, as are typical for the prior art and for the invention.
- Fig. 1 an embodiment of a rotary oscillator according to the invention is shown in supervision.
- a hub 1 is held by four projections 2, which are fixed to a fastening plate (not shown) with the aid of four bolts, not shown, which are inserted through bores 3.
- Four spokes 4 are provided which extend outward from the hub 1 and which are connected to a cylindrical wheel rim 5 via special joints 6.
- a laser gyroscope block which is not shown, has a central fastening opening into which the wheel rim 5 is fitted. This connection represents the only holder of the laser gyroscope block.
- Thin piezoceramic plates 7 and 8, which are provided with electrodes on their large surfaces, are applied to the two sides of each spoke in a form-fitting manner over the entire surface.
- the outer electrodes 9 and 10 of the plates 7 and 8 are all electrically connected to a terminal of an AC voltage source (not shown).
- the other source clamp is connected to the body of the rotary transducer.
- the piezoceramic plates all have retentive polarization vectors which are directed in the anti-clockwise direction in FIG. Then the application of a positive potential to the outer electrodes of the piezo-ceramic plates causes a moment on the wheel rim 5 in the clockwise direction.
- the rotary transducer can be made of Invar or a similar alloy and has a diameter of approximately 5.5 cm and a height (thickness) of approximately 3 cm.
- Four spokes 4 are preferably provided, which have a width (dimension between the plates 7 and 8) of a few millimeters and radial lengths of about 10 or more millimeters.
- the hub 1 is made as stable as possible in the remaining space in order to avoid bending contributions of the hub.
- the height of the joint is preferably as large as that of the entire rotary oscillator (about 3 cm).
- both a translatory force 8 and a torque 9 act on the end of the spoke 4 at 6D.
- the joint is designed so that when the forces occur, the segments 6A, 6B and 6C together form a flexible torsion spring around the point 6D and thus decouple the moment 9 from the end of the spoke.
- the segments 6A and 6C are, however, very rigid with regard to compression or pull in the direction of the translational force 8. As a result, the full translational force 8 actually reaches the spoke end 6D. As a result, the spoke behaves almost like a free bar that is only clamped on one side to the hub and is exposed to a point load at the tip.
- the bending element 6B is also pressure-resistant in the radial direction, as a result of which undesirable transverse vibrations that would otherwise occur are avoided.
- the elements 6A, 6B and 6C have the same height (thickness) as the rotary oscillator, they have a high torsional stiffness for forces which act around axes which do not coincide with the desired axis of the gyro rotation.
- the thickness and length of the elements 6A, 6B and 6C are of the order of 1 mm.
- FIG. 3A shows a spoke 11 according to the prior art, which starts from the hub 12 and here is rigidly connected to the wheel rim 13. If the wheel rim 13 is rotated by the angle x, then the dashed curve of the bent spoke results.
- the spoke has a characteristic double bend, that is to say it has an S shape.
- FIG. 3B shows a similar spoke 11, which is connected to the wheel rim 13 via a flexible joint 15. If the wheel rim 13 is rotated by the same angle x, the spoke 11 must be subjected to less bending in this embodiment; this results in a much smaller surface stress on the piezo elements 14. It has been shown that, even if the spokes according to FIGS. 3A and 3B have the same stiffness, the advantage of the design of FIG. 3B is retained, that is to say the surface tension of the ceramic does not represent any limitation with respect to the achievable amplitude.
- bending elements 22A and 22B which are intended to represent two adjacent spokes of the rotary oscillator, are fastened to a base body 21 which is to correspond to the hub and to a rigid block 23 which is to correspond to the wheel rim.
- flexure 22B When flexure 22B is energized to move its right end in the direction of arrow 24, flexure 22A, which is pressurized as a passive column and acts as a lever through block 23, generates torque at the tip of flexure 22B , which almost completely counteracts the bending element produced by the piezo elements.
- joints 26, which represent the bending elements of the present invention decouple the rotary activities of the bending elements 22A and 22B from the translational activity, which makes it possible to derive almost all of the work that can be achieved from the bending elements.
- 5A schematically shows the bending pattern of a rotary oscillator, the spokes of which are rigidly connected to the wheel rim and which was rotated in the direction of arrow 31.
- the resulting movements of parts of the wheel rim in radial directions 32 create difficulties for fastening the gyro block to the rotary oscillator.
- connection is rigid and even, the oscillating deformations are transferred to the gyro block.
- 5B shows the bending pattern of a rotary oscillator which, according to the invention, has bends influenced by joints. In this case, the previously shown difficulties with the attachment of the wheel cross / gyro block cannot occur.
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- General Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Electromagnetism (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Organic Chemistry (AREA)
- Power Engineering (AREA)
- General Health & Medical Sciences (AREA)
- Biochemistry (AREA)
- Life Sciences & Earth Sciences (AREA)
- Molecular Biology (AREA)
- Health & Medical Sciences (AREA)
- Geometry (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gyroscopes (AREA)
- Treatments For Attaching Organic Compounds To Fibrous Goods (AREA)
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3805631A DE3805631A1 (de) | 1988-02-24 | 1988-02-24 | Drehschwingungsantrieb |
DEP3805631.3 | 1988-02-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1989008237A1 true WO1989008237A1 (en) | 1989-09-08 |
Family
ID=6347974
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP1988/001152 WO1989008237A1 (en) | 1988-02-24 | 1988-12-14 | Torsional vibration drive |
Country Status (6)
Country | Link |
---|---|
US (1) | US5063321A (de) |
EP (1) | EP0436532A1 (de) |
JP (1) | JPH03502856A (de) |
KR (1) | KR890013041A (de) |
DE (1) | DE3805631A1 (de) |
WO (1) | WO1989008237A1 (de) |
Families Citing this family (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4038020A1 (de) * | 1989-12-16 | 1991-06-20 | Teldix Gmbh | Schrittmotor zum antrieb eines koerpers, insbesondere einer welle, um kleine drehwinkel pro schritt |
WO1992019018A1 (en) * | 1991-04-17 | 1992-10-29 | Motorola, Inc. | Piezo-electric resonant vibrator for a selective call receiver |
US5281884A (en) * | 1992-06-03 | 1994-01-25 | At&T Bell Laboratories | Adjustable X-Y stage |
IT1279061B1 (it) * | 1995-11-21 | 1997-12-04 | Pirelli | Vibratore torsionale |
US5950995A (en) * | 1997-12-04 | 1999-09-14 | Honeywell Inc. | Ring laser gyroscope dither motor structure |
US5867270A (en) * | 1997-12-04 | 1999-02-02 | Honeywell Inc. | Mechanism and method for mounting piezoelectric transducers |
JP3939048B2 (ja) * | 1999-05-17 | 2007-06-27 | セイコーインスツル株式会社 | 圧電アクチュエータ |
JP3436727B2 (ja) | 1999-10-01 | 2003-08-18 | 日本碍子株式会社 | 圧電/電歪デバイス及びその製造方法 |
JP3436735B2 (ja) * | 1999-10-01 | 2003-08-18 | 日本碍子株式会社 | 圧電/電歪デバイス及びその製造方法 |
EP1139450A4 (de) * | 1999-10-01 | 2007-04-04 | Ngk Insulators Ltd | Piezoelektrisches / elektrostriktives bauelement |
US6404109B1 (en) | 1999-10-01 | 2002-06-11 | Ngk Insulators, Ltd. | Piezoelectric/electrostrictive device having increased strength |
JP3845544B2 (ja) * | 1999-10-01 | 2006-11-15 | 日本碍子株式会社 | 圧電/電歪デバイス及びその製造方法 |
US6525448B1 (en) | 1999-10-01 | 2003-02-25 | Ngk Insulators Ltd | Piezoelectric/electrostrictive device |
JP3845543B2 (ja) * | 1999-10-01 | 2006-11-15 | 日本碍子株式会社 | 圧電/電歪デバイス及びその製造方法 |
US6873087B1 (en) * | 1999-10-29 | 2005-03-29 | Board Of Regents, The University Of Texas System | High precision orientation alignment and gap control stages for imprint lithography processes |
US7432634B2 (en) | 2000-10-27 | 2008-10-07 | Board Of Regents, University Of Texas System | Remote center compliant flexure device |
CN1262883C (zh) | 2000-07-17 | 2006-07-05 | 得克萨斯州大学***董事会 | 影印用于平版印刷工艺中的自动化液体分配的方法和*** |
JP4669222B2 (ja) * | 2001-10-22 | 2011-04-13 | ミニスイス・ソシエテ・アノニム | 圧電駆動装置 |
US7027156B2 (en) | 2002-08-01 | 2006-04-11 | Molecular Imprints, Inc. | Scatterometry alignment for imprint lithography |
US8349241B2 (en) | 2002-10-04 | 2013-01-08 | Molecular Imprints, Inc. | Method to arrange features on a substrate to replicate features having minimal dimensional variability |
US6929762B2 (en) | 2002-11-13 | 2005-08-16 | Molecular Imprints, Inc. | Method of reducing pattern distortions during imprint lithography processes |
US6871558B2 (en) | 2002-12-12 | 2005-03-29 | Molecular Imprints, Inc. | Method for determining characteristics of substrate employing fluid geometries |
US7452574B2 (en) | 2003-02-27 | 2008-11-18 | Molecular Imprints, Inc. | Method to reduce adhesion between a polymerizable layer and a substrate employing a fluorine-containing layer |
US7122079B2 (en) | 2004-02-27 | 2006-10-17 | Molecular Imprints, Inc. | Composition for an etching mask comprising a silicon-containing material |
US7157036B2 (en) | 2003-06-17 | 2007-01-02 | Molecular Imprints, Inc | Method to reduce adhesion between a conformable region and a pattern of a mold |
US7136150B2 (en) | 2003-09-25 | 2006-11-14 | Molecular Imprints, Inc. | Imprint lithography template having opaque alignment marks |
US8076386B2 (en) | 2004-02-23 | 2011-12-13 | Molecular Imprints, Inc. | Materials for imprint lithography |
US7906180B2 (en) | 2004-02-27 | 2011-03-15 | Molecular Imprints, Inc. | Composition for an etching mask comprising a silicon-containing material |
CN108288923A (zh) * | 2018-02-13 | 2018-07-17 | 哈尔滨工业大学 | 一种多层式旋转型压电精密驱动器 |
CN110553638B (zh) * | 2019-09-28 | 2024-06-07 | 中科天翼导航技术有限公司 | 一种激光陀螺的谐振子结构 |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2370956A1 (fr) * | 1976-11-15 | 1978-06-09 | Litton Systems Inc | Gyroscope a laser en anneau loge dans un boitier |
GB2072889A (en) * | 1980-03-25 | 1981-10-07 | Litton Systems Inc | Piezoelectric transducer drive |
US4349183A (en) * | 1980-08-04 | 1982-09-14 | Litton Systems Inc. | Spring for a ring laser gyro dither mechanism |
GB2178890A (en) * | 1985-08-06 | 1987-02-18 | Ferranti Plc | Dither mechanism for a ring laser gyroscope |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4436423A (en) * | 1981-09-14 | 1984-03-13 | The Singer Company | Ring laser gyroscope suspension |
GB2111297B (en) * | 1981-10-28 | 1985-06-12 | British Aerospace | Oscillatory drive mechanisms |
DE3150160A1 (de) * | 1981-12-18 | 1983-06-30 | Honeywell Gmbh, 6050 Offenbach | Ringlaserkreisel |
US4790657A (en) * | 1986-03-18 | 1988-12-13 | Litton Systems, Inc. | Ring laser gyroscope curved blade flexure and support ring assembly and method |
-
1988
- 1988-02-24 DE DE3805631A patent/DE3805631A1/de not_active Withdrawn
- 1988-12-14 EP EP89900239A patent/EP0436532A1/de not_active Ceased
- 1988-12-14 JP JP1500337A patent/JPH03502856A/ja active Pending
- 1988-12-14 WO PCT/EP1988/001152 patent/WO1989008237A1/de not_active Application Discontinuation
- 1988-12-14 US US07/573,199 patent/US5063321A/en not_active Expired - Fee Related
-
1989
- 1989-02-20 KR KR1019890001988A patent/KR890013041A/ko not_active Application Discontinuation
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2370956A1 (fr) * | 1976-11-15 | 1978-06-09 | Litton Systems Inc | Gyroscope a laser en anneau loge dans un boitier |
GB2072889A (en) * | 1980-03-25 | 1981-10-07 | Litton Systems Inc | Piezoelectric transducer drive |
US4349183A (en) * | 1980-08-04 | 1982-09-14 | Litton Systems Inc. | Spring for a ring laser gyro dither mechanism |
GB2178890A (en) * | 1985-08-06 | 1987-02-18 | Ferranti Plc | Dither mechanism for a ring laser gyroscope |
Also Published As
Publication number | Publication date |
---|---|
DE3805631A1 (de) | 1989-09-07 |
EP0436532A1 (de) | 1991-07-17 |
KR890013041A (ko) | 1989-09-21 |
US5063321A (en) | 1991-11-05 |
JPH03502856A (ja) | 1991-06-27 |
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