ES2109432T3 - Sistema cardan de aislamiento de la vibracion. - Google Patents
Sistema cardan de aislamiento de la vibracion.Info
- Publication number
- ES2109432T3 ES2109432T3 ES93301501T ES93301501T ES2109432T3 ES 2109432 T3 ES2109432 T3 ES 2109432T3 ES 93301501 T ES93301501 T ES 93301501T ES 93301501 T ES93301501 T ES 93301501T ES 2109432 T3 ES2109432 T3 ES 2109432T3
- Authority
- ES
- Spain
- Prior art keywords
- platform
- actuator
- vibration
- around
- motor ring
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000009413 insulation Methods 0.000 title abstract 2
- 230000004913 activation Effects 0.000 abstract 1
- 239000013013 elastic material Substances 0.000 abstract 1
- 238000002955 isolation Methods 0.000 abstract 1
- 230000003287 optical effect Effects 0.000 abstract 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
- G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
- G01C21/12—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
- G01C21/16—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
- G01C21/18—Stabilised platforms, e.g. by gyroscope
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Acoustics & Sound (AREA)
- Automation & Control Theory (AREA)
- General Physics & Mathematics (AREA)
- Accessories Of Cameras (AREA)
- Vibration Prevention Devices (AREA)
- Gyroscopes (AREA)
- Apparatuses For Generation Of Mechanical Vibrations (AREA)
Abstract
UN SISTEMA DE AISLAMIENTO DE VIBRACION CARDANICO ADECUADO PARA USO CON UNA PLATAFORMA DE INERCIA PARA PERMITIR UNA POSICION EXACTA DE LA PLATAFORMA INDEPENDIENTEMENTE DE LA PRESENCIA DE UN MOVIMIENTO DE TRASLACION VIBRATORIO SOBRE UNA CAJA CARDANICA QUE ENCIERRA LA PLATAFORMA EMPLEA UN CONJUNTO DE ESTRUCTURA LOCALIZADO CENTRALMENTE DENTRO DE LA PLATAFORMA PARA PIVOTAR LA PLATAFORMA Y PARA AISLAR LA PLATAFORMA DE LA VIBRACION. LA PLATAFORMA ESTA FORMADA POR DOS CONJUNTOS DE PLACAS DISPUESTOS EN LATERALES OPUESTOS DEL CONJUNTO DE ESTRUCTURA, LLEVANDO CADA UNA DE LAS PLACAS PARTES DE UN GIROSCOPIO LASER Y EQUIPO ELECTRONICO Y OPTICO AUXILIAR. LA CAJA CARDANICA INCLUYE UN ANILLO MOTOR ROTATORIO ALREDEDOR DE UN EJE CENTRAL Y QUE RODEA EL CONJUNTO DE ESTRUCTURA QUE ESTA CONECTADO AL ANILLO MOTOR. UNA PARTE CENTRAL DEL CONJUNTO DE ESTRUCTURA LLEVA UN PIVOTE QUE SOPORTA PIVOTALMENTE LA PLATAFORMA. SE LOCALIZA UN ACTUADOR ELECTROMAGNETICO EN CADA UNA DE UNA SERIE DE POSICIONES LOCALIZADAS CIRCUNFERICAMENTE ALREDEDOR DEL EJE CENTRAL DONDE CADA ACTUADOR TIENE UNA PARTE PRIMERA QUE CONECTA CON LA ESTRUCTURA Y UNA PARTE SEGUNDA QUE CONECTA CON AMBOS CONJUNTOS DE PLACA DE LA PLATAFORMA PARA REALIZAR UNA PIVOTACION ENTRE LA PLATAFORMA Y CONJUNTO DE ESTRUCTURA POR ACTIVACION DE CADA ACTUADOR. EL CONJUNTO DE ESTRUCTURA INCLUYE ADEMAS UNA SERIE DE ELEMENTOS DE AISLAMIENTO DE VIBRACION DE MATERIAL ELASTICO DISPUESTOS SIMETRICAMENTE ALREDEDOR DEL EJE CENTRAL Y CONECTADOS ENTRE LAS PARTES PRIMERAS DE PARTES RESPECTIVAS DE LOS ACTUADORES Y EL ANILLO MOTOR PARA PERMITIR LA OPERACION DE LOS ACTUADORES EN UN MEDIO BASICAMENTE LIBRE DE MOVIMIENTO VIBRATORIO DE TRASLACION.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US07/844,033 US5368271A (en) | 1992-03-02 | 1992-03-02 | Gimbal vibration isolation system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ES2109432T3 true ES2109432T3 (es) | 1998-01-16 |
Family
ID=25291618
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES93301501T Expired - Lifetime ES2109432T3 (es) | 1992-03-02 | 1993-02-26 | Sistema cardan de aislamiento de la vibracion. |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US5368271A (es) |
| EP (1) | EP0559402B1 (es) |
| JP (1) | JPH0772691B2 (es) |
| CA (1) | CA2088381C (es) |
| DE (1) | DE69315102T2 (es) |
| ES (1) | ES2109432T3 (es) |
| IL (1) | IL104733A (es) |
Families Citing this family (42)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2728695B1 (fr) * | 1994-12-22 | 1997-03-28 | Aerospatiale | Dispositif de commande en rotation de grande precision, notamment pour telescope |
| US5818353A (en) * | 1996-04-29 | 1998-10-06 | Hughes Aircraft Company | Self leveling sensor/device package |
| US6022005A (en) * | 1996-09-27 | 2000-02-08 | Trw Inc. | Semi-active vibration isolator and fine positioning mount |
| US5820078A (en) * | 1996-09-27 | 1998-10-13 | Hughes Electronics Corporation | Control motion gyro with vibration isolation |
| US5844815A (en) * | 1996-10-08 | 1998-12-01 | Mcdonnell Douglas Corporation | Umbilical and follower assembly utilized in microgravity platform system |
| US5890569A (en) * | 1997-06-06 | 1999-04-06 | Honeywell Inc. | Vibration isolation system for an inertial sensor assembly |
| SE513691C2 (sv) * | 1997-09-30 | 2000-10-23 | Tigercat Ind Inc | Hytt avsedd för framförallt terränggående fordon |
| US5897223A (en) * | 1997-11-17 | 1999-04-27 | Wescam Inc. | Stabilized platform system for camera |
| EP1085294B1 (en) | 1999-08-16 | 2001-12-05 | Advantest Corporation | System for inspecting and/or processing a sample |
| US6484978B2 (en) * | 2000-04-19 | 2002-11-26 | Che Ram Souza Voigt | Cardan support |
| US6653611B2 (en) * | 2001-04-09 | 2003-11-25 | A-Tech Corporation | Optical line of sight pointing and stabilization system |
| US6897821B2 (en) * | 2003-08-04 | 2005-05-24 | The Aerospace Corporation | Spacecraft off-gimbal IRU precision payload pointing and disturbance rejection system |
| US20060139930A1 (en) * | 2004-12-23 | 2006-06-29 | Matthew Feinsod | Motion-compensating light-emitting apparatus |
| US7728964B2 (en) * | 2004-12-23 | 2010-06-01 | Matthew Feinsod | Motion compensated light-emitting apparatus |
| US7312863B2 (en) * | 2004-12-23 | 2007-12-25 | Matthew Feinsod | Motion-compensating light-emitting apparatus |
| US7325792B2 (en) * | 2005-03-11 | 2008-02-05 | Enidine, Inc. | Multi-axial base isolation system |
| US20070113702A1 (en) * | 2005-11-18 | 2007-05-24 | Honeywell International Inc. | Isolation system for an inertial measurement unit |
| FR2907423B1 (fr) * | 2006-10-23 | 2009-07-03 | Astrium Sas Soc Par Actions Si | Gyrodyne et son dispositif de montage |
| US8091833B2 (en) * | 2008-02-29 | 2012-01-10 | Insitu, Inc. | Vibration isolation devices and associated systems and methods |
| US7950633B2 (en) * | 2008-08-07 | 2011-05-31 | Drs Rsta, Inc. | Vibration isolator system |
| US8498055B2 (en) | 2010-08-13 | 2013-07-30 | Honeywell International Inc. | Space telescope system |
| US8711223B2 (en) | 2011-06-21 | 2014-04-29 | Flir Systems, Inc. | Vehicle-mounted camera stabilized passively by vibration isolators |
| DE102012002728A1 (de) | 2012-02-10 | 2013-08-14 | Somag Ag Jena | "Lagestabilisiertes Trägersystem für Luftbildkameras und analoge Einrichtungen" |
| US9450286B1 (en) * | 2012-09-12 | 2016-09-20 | Viasat, Inc. | Systems, devices, and methods for stabilizing an antenna |
| DE102013008994B4 (de) | 2013-05-18 | 2019-06-06 | Somag Ag Jena | "Lagestabilisiertes Trägersystem für die Luftbildfotografie" |
| US9164292B2 (en) | 2013-06-14 | 2015-10-20 | Ian Brooke | Track and bogie based optically centered gimbal |
| US9348197B2 (en) | 2013-12-24 | 2016-05-24 | Pv Labs Inc. | Platform stabilization system |
| AT514011A2 (de) * | 2014-04-25 | 2014-09-15 | Dynamic Perspective Gmbh | Kardanische Aufhängung für einen Sensor |
| US10906636B2 (en) * | 2014-10-21 | 2021-02-02 | Sikorsky Aircraft Corporation | Vibration control assembly for an aircraft and method of controlling aircraft vibration |
| DE102014018550A1 (de) | 2014-12-12 | 2016-06-16 | Somag Ag Jena | "Lagestabilisiertes Trägersystem für die Aufnahme von Luftbildsensoren" |
| FR3036157A1 (fr) * | 2015-05-12 | 2016-11-18 | Mdm Solutions | Caisson de protection pour un stabilisateur de camera avec systeme gyrostabilise sur trois axes |
| US10283837B2 (en) | 2015-10-23 | 2019-05-07 | Viasat, Inc. | Apparatuses for mounting an antenna assembly |
| CN108168535B (zh) * | 2017-11-30 | 2021-12-07 | 上海航天控制技术研究所 | 一种用于运载火箭光纤速率陀螺的四点减振系统 |
| US11287221B2 (en) | 2019-09-17 | 2022-03-29 | Flir Surveillance, Inc. | Nested gimbal assembly |
| US11243082B2 (en) | 2019-12-19 | 2022-02-08 | Raytheon Company | Cardan joint for inertially stabilizing a payload |
| US11524636B2 (en) * | 2019-12-19 | 2022-12-13 | Raytheon Company | Internally damped crossbar assembly having a slip plate damper |
| US11603961B2 (en) | 2019-12-19 | 2023-03-14 | Raytheon Company | Internally damped crossbar assembly having a friction damped isolator |
| US11554725B2 (en) | 2019-12-19 | 2023-01-17 | Raytheon Company | Internally damped crossbar assembly having wire rope isolator |
| US11448287B2 (en) | 2019-12-19 | 2022-09-20 | Raytheon Company | Internally damped crossbar assembly having elastomeric isolator |
| US11794883B2 (en) * | 2020-04-20 | 2023-10-24 | Lockheed Martin Corporation | Vibration control assembly |
| US11319985B2 (en) | 2020-08-03 | 2022-05-03 | Raytheon Company | Isolation joint with spherical bearing and integral angle measurement |
| CN118640884B (zh) * | 2024-08-16 | 2024-10-25 | 四川图林科技有限责任公司 | 一种用于激光陀螺仪的振动隔离基座 |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3703999A (en) * | 1969-12-12 | 1972-11-28 | Actron Ind Inc | Wide band stabilizer |
| US4101102A (en) * | 1976-04-26 | 1978-07-18 | Westinghouse Electric Corp. | Vibration isolation load support apparatus |
| US4136962A (en) * | 1977-01-18 | 1979-01-30 | Vari-Tech Company | Apparatus for orienting and maintaining the orientation of construction equipment |
| US4324378A (en) * | 1980-03-03 | 1982-04-13 | The United States Of America As Represented By The Secretary Of The Navy | High-torque/acceleration stabilized sensor platform |
| US4645994A (en) * | 1985-04-29 | 1987-02-24 | General Dynamics | Space-referenced, rate-stabilized multiple-gimbal-platform system |
| US4783038A (en) * | 1987-07-07 | 1988-11-08 | Aeroflex International Incorporated | Isolator apparatus |
| US5204573A (en) * | 1991-07-17 | 1993-04-20 | Vision Applications, Inc. | Two-dimensional pointing motor |
-
1992
- 1992-03-02 US US07/844,033 patent/US5368271A/en not_active Expired - Lifetime
-
1993
- 1993-01-29 CA CA002088381A patent/CA2088381C/en not_active Expired - Fee Related
- 1993-02-15 IL IL10473393A patent/IL104733A/en not_active IP Right Cessation
- 1993-02-26 EP EP93301501A patent/EP0559402B1/en not_active Expired - Lifetime
- 1993-02-26 DE DE69315102T patent/DE69315102T2/de not_active Expired - Fee Related
- 1993-02-26 ES ES93301501T patent/ES2109432T3/es not_active Expired - Lifetime
- 1993-03-02 JP JP5041491A patent/JPH0772691B2/ja not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| EP0559402B1 (en) | 1997-11-12 |
| DE69315102T2 (de) | 1998-03-05 |
| IL104733A (en) | 1996-06-18 |
| EP0559402A2 (en) | 1993-09-08 |
| JPH0772691B2 (ja) | 1995-08-02 |
| CA2088381C (en) | 2000-07-18 |
| IL104733A0 (en) | 1993-08-18 |
| DE69315102D1 (de) | 1997-12-18 |
| EP0559402A3 (en) | 1995-01-04 |
| CA2088381A1 (en) | 1993-09-03 |
| JPH063150A (ja) | 1994-01-11 |
| US5368271A (en) | 1994-11-29 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FG2A | Definitive protection |
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