DE3804202C2 - - Google Patents

Info

Publication number
DE3804202C2
DE3804202C2 DE3804202A DE3804202A DE3804202C2 DE 3804202 C2 DE3804202 C2 DE 3804202C2 DE 3804202 A DE3804202 A DE 3804202A DE 3804202 A DE3804202 A DE 3804202A DE 3804202 C2 DE3804202 C2 DE 3804202C2
Authority
DE
Germany
Prior art keywords
bolt
locking
joint
stop
bore
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
DE3804202A
Other languages
German (de)
English (en)
Other versions
DE3804202A1 (de
Inventor
Martin 8028 Taufkirchen De Roth
Helmut 8000 Muenchen De 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
Priority to DE3804202A priority Critical patent/DE3804202A1/de
Priority to FR888815592A priority patent/FR2627150B1/fr
Priority to US07/306,812 priority patent/US4880188A/en
Publication of DE3804202A1 publication Critical patent/DE3804202A1/de
Application granted granted Critical
Publication of DE3804202C2 publication Critical patent/DE3804202C2/de
Granted 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
    • B64G1/222—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
    • B64G1/2221—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 manner of deployment
    • B64G1/2222—Folding
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Pivots And Pivotal Connections (AREA)
  • Photovoltaic Devices (AREA)
DE3804202A 1988-02-11 1988-02-11 Gelenk fuer die zweistufige entfaltung eines solarpanels Granted DE3804202A1 (de)

Priority Applications (3)

Application Number Priority Date Filing Date Title
DE3804202A DE3804202A1 (de) 1988-02-11 1988-02-11 Gelenk fuer die zweistufige entfaltung eines solarpanels
FR888815592A FR2627150B1 (fr) 1988-02-11 1988-11-29 Articulation pour le deploiement en deux etapes d'un panneau solaire
US07/306,812 US4880188A (en) 1988-02-11 1989-02-03 Joint for unfolding panels of a solar collector

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
DE3804202A1 DE3804202A1 (de) 1989-08-24
DE3804202C2 true DE3804202C2 (US06265458-20010724-C00056.png) 1990-12-06

Family

ID=6347167

Family Applications (1)

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

Country Status (3)

Country Link
US (1) US4880188A (US06265458-20010724-C00056.png)
DE (1) DE3804202A1 (US06265458-20010724-C00056.png)
FR (1) FR2627150B1 (US06265458-20010724-C00056.png)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4032112A1 (de) * 1990-10-10 1992-04-16 Marcus Metzger Entfaltungsunterstuetzender, steifigkeitsoptimierter verriegelungsmechanismus fuer entfaltbare solargeneratoren von satelliten
DE19922849A1 (de) * 1999-05-19 2000-12-07 Daimler Chrysler Ag Aufklappbare Raumfahrtstruktur

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3927941C1 (US06265458-20010724-C00056.png) * 1989-08-24 1991-01-31 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De
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
US5509747A (en) * 1992-10-24 1996-04-23 Deutsche Aerospace Ag Articulation arrangement for connecting folding structure elements
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.
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
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

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4032112A1 (de) * 1990-10-10 1992-04-16 Marcus Metzger Entfaltungsunterstuetzender, steifigkeitsoptimierter verriegelungsmechanismus fuer entfaltbare solargeneratoren von satelliten
DE19922849A1 (de) * 1999-05-19 2000-12-07 Daimler Chrysler Ag Aufklappbare Raumfahrtstruktur

Also Published As

Publication number Publication date
DE3804202A1 (de) 1989-08-24
US4880188A (en) 1989-11-14
FR2627150A1 (fr) 1989-08-18
FR2627150B1 (fr) 1991-11-29

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Legal Events

Date Code Title Description
8110 Request for examination paragraph 44
D2 Grant after examination
8320 Willingness to grant licences declared (paragraph 23)
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: DEUTSCHE AEROSPACE AG, 8000 MUENCHEN, DE

8339 Ceased/non-payment of the annual fee