FR2627150B1 - Articulation pour le deploiement en deux etapes d'un panneau solaire - Google Patents

Articulation pour le deploiement en deux etapes d'un panneau solaire

Info

Publication number
FR2627150B1
FR2627150B1 FR888815592A FR8815592A FR2627150B1 FR 2627150 B1 FR2627150 B1 FR 2627150B1 FR 888815592 A FR888815592 A FR 888815592A FR 8815592 A FR8815592 A FR 8815592A FR 2627150 B1 FR2627150 B1 FR 2627150B1
Authority
FR
France
Prior art keywords
articulation
deployment
steps
solar panel
solar
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
Application number
FR888815592A
Other languages
English (en)
Other versions
FR2627150A1 (fr
Inventor
Martin Roth
Helmut Kiendl
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of FR2627150A1 publication Critical patent/FR2627150A1/fr
Application granted granted Critical
Publication of FR2627150B1 publication Critical patent/FR2627150B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • B64G1/42—Arrangements or adaptations of power supply systems
    • B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
FR888815592A 1988-02-11 1988-11-29 Articulation pour le deploiement en deux etapes d'un panneau solaire Expired - Lifetime FR2627150B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3804202A DE3804202A1 (de) 1988-02-11 1988-02-11 Gelenk fuer die zweistufige entfaltung eines solarpanels

Publications (2)

Publication Number Publication Date
FR2627150A1 FR2627150A1 (fr) 1989-08-18
FR2627150B1 true FR2627150B1 (fr) 1991-11-29

Family

ID=6347167

Family Applications (1)

Application Number Title Priority Date Filing Date
FR888815592A Expired - Lifetime FR2627150B1 (fr) 1988-02-11 1988-11-29 Articulation pour le deploiement en deux etapes d'un panneau solaire

Country Status (3)

Country Link
US (1) US4880188A (fr)
DE (1) DE3804202A1 (fr)
FR (1) FR2627150B1 (fr)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3927941C1 (fr) * 1989-08-24 1991-01-31 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De
DE4032112A1 (de) * 1990-10-10 1992-04-16 Marcus Metzger Entfaltungsunterstuetzender, steifigkeitsoptimierter verriegelungsmechanismus fuer entfaltbare solargeneratoren von satelliten
US5356095A (en) * 1992-08-04 1994-10-18 Fairchild Space And Defense Corporation Attenuating linged deployment apparatus
US5319905A (en) * 1992-09-28 1994-06-14 Spar Aerospace Limited Panel array deployment apparatus
FR2697316B1 (fr) * 1992-10-24 1995-06-30 Deutsche Aerospace Dispositif d'articulation avec verrouillage et deverrouillage pour relier entre eux les elements d'une structure pliante.
US5509747A (en) * 1992-10-24 1996-04-23 Deutsche Aerospace Ag Articulation arrangement for connecting folding structure elements
DE4337968C2 (de) * 1992-11-10 1994-09-08 Deutsche Aerospace Gelenk zum Entfalten und Verriegeln von Raumfahrtelementen
US5400987A (en) * 1993-04-26 1995-03-28 Hughes Aircraft Company Variable angle latching mechanism for spacecraft
FR2722761B1 (fr) * 1994-07-20 1996-09-27 Aerospatiale Systeme pour deployer/replier deux elements, avec verrouillage par came desdits elements deployes
US5673459A (en) 1994-09-28 1997-10-07 Space Systems/Loral, Inc. Deployment hinge apparatus
US5715573A (en) * 1995-05-22 1998-02-10 Cta Space Systems, Inc. Self latching hinge
DE19610297C1 (de) * 1996-03-15 1997-01-23 Daimler Benz Aerospace Ag Vorrichtung zum Entfalten von zwei Paneelen für Solargeneratoren
DE19649741C2 (de) * 1996-11-30 1999-07-15 Daimler Benz Aerospace Ag Gelenk zum Entfalten und Verriegeln einer Solarpaneele oder eines Reflektors
US6010096A (en) 1998-07-22 2000-01-04 Space Systems/Loral, Inc. Deployment restraint and sequencing device
DE19922849A1 (de) * 1999-05-19 2000-12-07 Daimler Chrysler Ag Aufklappbare Raumfahrtstruktur
JP2001039400A (ja) * 1999-06-17 2001-02-13 Daimlerchrysler Ag 人工衛星太陽光発電機用拡開継手
US7644890B2 (en) * 2006-06-01 2010-01-12 Utah State University Low-energy locking hinge mechanism for deployable devices
CN102790105B (zh) * 2012-08-13 2014-08-06 友达光电股份有限公司 太阳能模块
CN103950558B (zh) * 2014-04-14 2015-12-30 浙江理工大学 一种扇形太阳翼重复折展机构
CN106275515A (zh) * 2015-06-05 2017-01-04 北京信威通信技术股份有限公司 一种卫星太阳帆板的展开机构
US10435182B1 (en) * 2016-09-12 2019-10-08 Space Systems/Loral, Llc Articulation techniques for a spacecraft solar array
CN108016636A (zh) * 2016-10-31 2018-05-11 深圳光启空间技术有限公司 板状物折叠和展开装置及太阳能帆板结构
US10715078B2 (en) 2017-03-22 2020-07-14 Sungeun K. Jeon Compact, self-deploying structures and methods for deploying foldable, structural origami arrays of photovoltaic modules, solar sails, and antenna structures
CN107255149B (zh) * 2017-07-19 2023-05-23 浙江理工大学 行星轮系式折展装置及其折展方法
CN110758773B (zh) * 2019-11-21 2021-07-30 上海卫星工程研究所 航天器及其弹簧预紧高刚度锁定装置
CN116002082B (zh) * 2023-02-07 2024-01-26 银河航天(北京)网络技术有限公司 一种太阳能帆板的对日定向系统及对日定向方法
CN116044895B (zh) * 2023-04-03 2023-09-01 四川省星时代智能卫星科技有限公司 铰链和卫星太阳翼总成

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3525483A (en) * 1968-01-17 1970-08-25 North American Rockwell Deployment mechanism
US4373690A (en) * 1979-04-23 1983-02-15 The United States Of America As Represented By The Secretary Of The Navy Deployable support structure for spacecrafts
DE3215434C2 (de) * 1982-04-24 1985-11-07 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Riegelmechanismus für entfaltbare Solargeneratoren von Satelliten
DE3418413A1 (de) * 1984-05-17 1986-01-09 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Riegelmechanismus fuer einen entfaltbaren solarzellengenerator
DE3615264A1 (de) * 1986-05-06 1987-11-12 Messerschmitt Boelkow Blohm Vorrichtung fuer die teilentfaltung von solargeneratoren

Also Published As

Publication number Publication date
FR2627150A1 (fr) 1989-08-18
DE3804202C2 (fr) 1990-12-06
US4880188A (en) 1989-11-14
DE3804202A1 (de) 1989-08-24

Similar Documents

Publication Publication Date Title
FR2627150B1 (fr) Articulation pour le deploiement en deux etapes d'un panneau solaire
FR2756620B1 (fr) Articulation pour le deploiement et le verrouillage d'un panneau solaire ou d'un reflecteur
GB2221611B (en) Pivot joint
GB2244591B (en) Chord progression finder
GB9010315D0 (en) A joint
GB9104344D0 (en) Structures
ZA913196B (en) Hinge for use in a roof assembly
GB9024667D0 (en) Floatable structures
GB9114041D0 (en) An arrangement in the framing of a collapsible hood
GB9110316D0 (en) Sign structures
GB2262951B (en) Construction joints
GB2250561B (en) Joints
GB9003514D0 (en) Onsite'buildablock'concrete
GB8923121D0 (en) Hinge joint
AU2256292A (en) Interconnection clip for model structures
CA66714S (en) Hinge connecting post
CA65856S (en) Tent hinge
GB8919075D0 (en) A hinge structure
GB8922510D0 (en) A hinge structure
GB8910098D0 (en) Strut-panel joint in a strong-box
AU110937S (en) A footing
HU900850D0 (en) "vk-system-plus" variable small-panel building structure
GB9021105D0 (en) A joint
GB9006244D0 (en) A portable drainpipe
GB9010108D0 (en) Folding joints

Legal Events

Date Code Title Description
ST Notification of lapse