DE60318614D1 - Riegel zur Fixierung des Segments eines optischen Weltraumteleskops - Google Patents
Riegel zur Fixierung des Segments eines optischen WeltraumteleskopsInfo
- Publication number
- DE60318614D1 DE60318614D1 DE60318614T DE60318614T DE60318614D1 DE 60318614 D1 DE60318614 D1 DE 60318614D1 DE 60318614 T DE60318614 T DE 60318614T DE 60318614 T DE60318614 T DE 60318614T DE 60318614 D1 DE60318614 D1 DE 60318614D1
- Authority
- DE
- Germany
- Prior art keywords
- petal
- latch
- hub
- optical space
- central hub
- 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
- 230000003287 optical effect Effects 0.000 title abstract 2
Classifications
-
- 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
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/30—Parts of ball or roller bearings
- F16C33/32—Balls
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/222—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/222—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
- B64G1/2228—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state characterised by the hold-down or release mechanisms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/222—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
- B64G1/2229—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state characterised by the deployment actuating mechanism
-
- 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
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C31/00—Bearings for parts which both rotate and move linearly
- F16C31/04—Ball or roller bearings
-
- 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
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/30—Parts of ball or roller bearings
- F16C33/38—Ball cages
- F16C33/40—Ball cages for multiple rows of balls
-
- 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
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/30—Parts of ball or roller bearings
- F16C33/46—Cages for rollers or needles
- F16C33/56—Selection of substances
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B7/00—Mountings, adjusting means, or light-tight connections, for optical elements
- G02B7/18—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors
- G02B7/182—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors for mirrors
- G02B7/183—Mountings, adjusting means, or light-tight connections, for optical elements for prisms; for mirrors for mirrors specially adapted for very large mirrors, e.g. for astronomy, or solar concentrators
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/66—Arrangements or adaptations of apparatus or instruments, not otherwise provided for
-
- 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
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2326/00—Articles relating to transporting
- F16C2326/47—Cosmonautic vehicles, i.e. bearings adapted for use in outer-space
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Sustainable Development (AREA)
- Astronomy & Astrophysics (AREA)
- Life Sciences & Earth Sciences (AREA)
- General Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Telescopes (AREA)
- Mounting And Adjusting Of Optical Elements (AREA)
- Pivots And Pivotal Connections (AREA)
- Rolling Contact Bearings (AREA)
- Lenses (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/216,255 US6768582B1 (en) | 2002-08-09 | 2002-08-09 | System for deploying the petals of a sectored mirror of an optical space telescope |
| US216255 | 2002-08-09 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| DE60318614D1 true DE60318614D1 (de) | 2008-02-21 |
| DE60318614T2 DE60318614T2 (de) | 2008-06-05 |
Family
ID=31187910
Family Applications (5)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE60318614T Expired - Lifetime DE60318614T2 (de) | 2002-08-09 | 2003-08-08 | Riegel zur Fixierung des Segments eines optischen Weltraumteleskops |
| DE20321565U Expired - Lifetime DE20321565U1 (de) | 2002-08-09 | 2003-08-08 | Blütenblattelement-Ausfahr-Riegelanord. für einen in Sektoren aufgeteilten Spiegel e. optischen Weltraumteleskops |
| DE60325661T Expired - Lifetime DE60325661D1 (de) | 2002-08-09 | 2003-08-08 | Optischen Weltraumteleskop mit einem Verriegelungssystem zum Feststellen der Spiegelsegmente |
| DE60313488T Expired - Lifetime DE60313488T2 (de) | 2002-08-09 | 2003-08-08 | Gelenk zur Entfaltung der Segmente eines optischen Weltraumteleskops |
| DE60306047T Expired - Lifetime DE60306047D1 (de) | 2002-08-09 | 2003-08-08 | Mechanismus zur Entfaltung der Segmente eines optischen Weltraumteleskops |
Family Applications After (4)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE20321565U Expired - Lifetime DE20321565U1 (de) | 2002-08-09 | 2003-08-08 | Blütenblattelement-Ausfahr-Riegelanord. für einen in Sektoren aufgeteilten Spiegel e. optischen Weltraumteleskops |
| DE60325661T Expired - Lifetime DE60325661D1 (de) | 2002-08-09 | 2003-08-08 | Optischen Weltraumteleskop mit einem Verriegelungssystem zum Feststellen der Spiegelsegmente |
| DE60313488T Expired - Lifetime DE60313488T2 (de) | 2002-08-09 | 2003-08-08 | Gelenk zur Entfaltung der Segmente eines optischen Weltraumteleskops |
| DE60306047T Expired - Lifetime DE60306047D1 (de) | 2002-08-09 | 2003-08-08 | Mechanismus zur Entfaltung der Segmente eines optischen Weltraumteleskops |
Country Status (5)
| Country | Link |
|---|---|
| US (4) | US6768582B1 (de) |
| EP (4) | EP1566678B1 (de) |
| JP (3) | JP4047781B2 (de) |
| AT (4) | ATE383590T1 (de) |
| DE (5) | DE60318614T2 (de) |
Families Citing this family (33)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| USD615071S1 (en) * | 2003-09-09 | 2010-05-04 | Qinetiq Limited | Deployable sensor module |
| GB0321041D0 (en) * | 2003-09-09 | 2004-02-04 | Qinetiq Ltd | Sensor apparatus and system |
| FR2890454B1 (fr) * | 2005-09-05 | 2007-10-12 | Alcatel Sa | Reflecteur deployable en forme de triangle de reuleaux, pour un instrument d'observation spatiale |
| US7913953B2 (en) * | 2005-12-28 | 2011-03-29 | Frank Werner Ellinghaus | Solar sail launch system and solar sail attitude control system |
| US7782530B1 (en) * | 2006-06-26 | 2010-08-24 | Sandia Corporation | Deployable telescope having a thin-film mirror and metering structure |
| FR2902764B1 (fr) * | 2006-06-27 | 2009-09-25 | Alcatel Sa | Structure deployable comportant des elements rigides, embarquee sur un engin spatial |
| FR2902765B1 (fr) * | 2006-06-27 | 2008-08-29 | Alcatel Sa | Dispositif de positionnement en rotation a grande duree de vie pour applications spatiales |
| FR2903387B1 (fr) * | 2006-07-05 | 2008-08-29 | Alcatel Sa | Actionneur pour systemes de guidage d'equipements spatiaux a taux de rotation variable |
| FR2905804B1 (fr) * | 2006-09-13 | 2010-10-22 | Cit Alcatel | Instrument d'acquisition spatiale a reflecteur(s) deployable(s) et a compacite elevee |
| JP5276952B2 (ja) * | 2008-11-05 | 2013-08-28 | サカセ・アドテック株式会社 | 伸展構造物 |
| US9366853B2 (en) | 2011-02-25 | 2016-06-14 | Utah State University Research Foundation | Multiple petal deployable telescope |
| WO2012116366A2 (en) * | 2011-02-25 | 2012-08-30 | Utah State University Research Foundation | Multiple petal deployable telescope |
| FR2974787B1 (fr) * | 2011-05-05 | 2014-11-28 | Thales Sa | Dispositif de protection d'un instrument optique multifaisceaux |
| US9004409B1 (en) * | 2011-08-23 | 2015-04-14 | Space Systems/Loral, Llc | Extendable antenna reflector deployment techniques |
| US9248922B1 (en) * | 2011-08-23 | 2016-02-02 | Space Systems/Loral, Llc | Reflector deployment techniques for satellites |
| US9331394B2 (en) | 2011-09-21 | 2016-05-03 | Harris Corporation | Reflector systems having stowable rigid panels |
| US20130201571A1 (en) | 2012-02-03 | 2013-08-08 | Raytheon Company | Hinge mechanism for small optics and related methods |
| US9134599B2 (en) | 2012-08-01 | 2015-09-15 | Pentair Water Pool And Spa, Inc. | Underwater image projection controller with boundary setting and image correction modules and interface and method of using same |
| US9423608B2 (en) | 2012-08-01 | 2016-08-23 | Pentair Water Pool And Spa, Inc. | Multidimensional rotary motion apparatus moving a reflective surface and method of operating same |
| FR3023011B1 (fr) * | 2014-06-27 | 2017-10-20 | Thales Sa | Procede de fabrication d'un miroir |
| CN104765122B (zh) * | 2015-04-29 | 2017-01-18 | 哈尔滨工业大学 | 空间可伸缩桁架式二元光学相机及其在轨工作方法 |
| USD843635S1 (en) * | 2015-11-12 | 2019-03-19 | Antoinetta Jacoba Hendrika Van Egmond | Solar powered lamp |
| US10683107B2 (en) * | 2017-08-04 | 2020-06-16 | The Aerospace Corporation | Release apparatus and methods of assembling same |
| US10811759B2 (en) | 2018-11-13 | 2020-10-20 | Eagle Technology, Llc | Mesh antenna reflector with deployable perimeter |
| US11139549B2 (en) | 2019-01-16 | 2021-10-05 | Eagle Technology, Llc | Compact storable extendible member reflector |
| US10797400B1 (en) | 2019-03-14 | 2020-10-06 | Eagle Technology, Llc | High compaction ratio reflector antenna with offset optics |
| CN110703408B (zh) * | 2019-11-30 | 2022-05-31 | 中国人民解放军战略支援部队航天工程大学 | 一种主次镜伸缩系统 |
| CN111610738B (zh) * | 2020-05-26 | 2021-06-01 | 清华大学深圳国际研究生院 | 一种空间望远镜展开机构、控制系统和方法 |
| US12043416B2 (en) | 2020-11-26 | 2024-07-23 | Wyvern Incorporated | Satellite with deployable optical assembly |
| CN115508997B (zh) * | 2022-06-22 | 2024-08-06 | 中国科学院微小卫星创新研究院 | 一种超大口径太空望远镜及其展开方式 |
| KR102697244B1 (ko) * | 2023-11-14 | 2024-08-23 | 대한민국(방위사업청장) | 전자 광학 탑재체용 광학모듈 및 이를 구비하는 전자 광학 탑재체 |
| KR102697241B1 (ko) * | 2023-11-14 | 2024-08-23 | 대한민국(방위사업청장) | 전자 광학 탑재체용 광학모듈 및 이를 구비하는 전자 광학 탑재체 |
| KR102697245B1 (ko) * | 2023-11-14 | 2024-08-22 | 대한민국(방위사업청장) | 전자 광학 탑재체 |
Family Cites Families (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3043634A (en) * | 1960-08-11 | 1962-07-10 | Coley Samuel Ernest | Bearings |
| US3446540A (en) * | 1966-10-12 | 1969-05-27 | Ted Geffner | Anti-friction bearings |
| US3433436A (en) * | 1967-03-20 | 1969-03-18 | Us Navy | Ball release mechanism |
| FR1524355A (fr) * | 1967-03-31 | 1968-05-10 | Sud Aviation | Dispositif d'articulation adapté aux éléments de déploiement d'engins spatiaux |
| US3469894A (en) * | 1967-10-12 | 1969-09-30 | Superior Die Set Corp | Die set leader pin with sectional bearing cage |
| US3635425A (en) * | 1969-10-01 | 1972-01-18 | Us Navy | Deployment method for a telescoping solar array |
| CH654886A5 (de) * | 1981-11-03 | 1986-03-14 | Schmid Sro Kugellager | Kugelbuechse fuer unbegrenzte laengsbewegungen. |
| US4753465A (en) * | 1986-04-11 | 1988-06-28 | James F. Dalby | Remotely operable locking mechanism |
| US4997218A (en) * | 1990-01-22 | 1991-03-05 | The United States Of America As Represented By The Secretary Of The Army | Pin lock mechanism with bias change feature |
| JP2914804B2 (ja) * | 1991-11-20 | 1999-07-05 | 日本トムソン株式会社 | ストロークベアリング |
| US5290107A (en) * | 1992-09-24 | 1994-03-01 | Hanaway Ronald L | Guide post, guide sleeve and improved air impulse rotary ball cage assembly |
| DE4337968C2 (de) * | 1992-11-10 | 1994-09-08 | Deutsche Aerospace | Gelenk zum Entfalten und Verriegeln von Raumfahrtelementen |
| US5451975A (en) | 1993-02-17 | 1995-09-19 | Space Systems/Loral, Inc. | Furlable solid surface reflector |
| US5600868A (en) * | 1995-03-07 | 1997-02-11 | Santa Barbara Research Center | Deployment hinge |
| US5785280A (en) * | 1995-07-20 | 1998-07-28 | Space Systems/Loral, Inc. | Hybrid solar panel array |
| DE19649741C2 (de) * | 1996-11-30 | 1999-07-15 | Daimler Benz Aerospace Ag | Gelenk zum Entfalten und Verriegeln einer Solarpaneele oder eines Reflektors |
| US5898529A (en) | 1997-06-20 | 1999-04-27 | Ball Aerospace & Technologies, Inc. | Deployable space-based telescope |
| GB9803918D0 (en) * | 1997-07-05 | 1998-04-22 | Matra Marconi Space Uk Ltd | Spacecraft platforms |
| US6047928A (en) | 1998-05-19 | 2000-04-11 | Hughes Electronics Corporation | Friction clamp restraint mechanism for springback reflectors |
| US6175989B1 (en) | 1998-05-26 | 2001-01-23 | Lockheed Corp | Shape memory alloy controllable hinge apparatus |
| US6191757B1 (en) | 1999-04-08 | 2001-02-20 | Hughes Electronics Corporation | System for compact stowage of segmented dish reflectors |
| US6505381B1 (en) * | 1999-07-30 | 2003-01-14 | Trw Astro Aerospace | Pulley actuated translational hinge system |
| US6767155B2 (en) * | 2002-04-05 | 2004-07-27 | Eastman Kodak Company | High stability latch mechanism |
-
2002
- 2002-08-09 US US10/216,255 patent/US6768582B1/en not_active Expired - Fee Related
-
2003
- 2003-08-08 DE DE60318614T patent/DE60318614T2/de not_active Expired - Lifetime
- 2003-08-08 EP EP05010787A patent/EP1566678B1/de not_active Expired - Lifetime
- 2003-08-08 DE DE20321565U patent/DE20321565U1/de not_active Expired - Lifetime
- 2003-08-08 EP EP03018138A patent/EP1391766B1/de not_active Expired - Lifetime
- 2003-08-08 DE DE60325661T patent/DE60325661D1/de not_active Expired - Lifetime
- 2003-08-08 AT AT05010787T patent/ATE383590T1/de not_active IP Right Cessation
- 2003-08-08 DE DE60313488T patent/DE60313488T2/de not_active Expired - Lifetime
- 2003-08-08 JP JP2003290228A patent/JP4047781B2/ja not_active Expired - Fee Related
- 2003-08-08 AT AT07011070T patent/ATE419552T1/de not_active IP Right Cessation
- 2003-08-08 EP EP05010788A patent/EP1566679B1/de not_active Expired - Lifetime
- 2003-08-08 AT AT05010788T patent/ATE360834T1/de not_active IP Right Cessation
- 2003-08-08 AT AT03018138T patent/ATE330243T1/de not_active IP Right Cessation
- 2003-08-08 EP EP07011070A patent/EP1835321B1/de not_active Expired - Lifetime
- 2003-08-08 DE DE60306047T patent/DE60306047D1/de not_active Expired - Lifetime
-
2004
- 2004-06-16 US US10/869,072 patent/US6863408B2/en not_active Expired - Fee Related
- 2004-06-16 US US10/869,517 patent/US6972901B2/en not_active Expired - Fee Related
- 2004-11-16 US US10/990,240 patent/US6956696B2/en not_active Expired - Fee Related
-
2007
- 2007-08-13 JP JP2007210998A patent/JP4677430B2/ja not_active Expired - Fee Related
- 2007-08-13 JP JP2007211000A patent/JP4782081B2/ja not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 8364 | No opposition during term of opposition |