FR2518494A1 - Mecanisme de depliage et de repliage d'une structure pliante - Google Patents

Mecanisme de depliage et de repliage d'une structure pliante Download PDF

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Publication number
FR2518494A1
FR2518494A1 FR8221223A FR8221223A FR2518494A1 FR 2518494 A1 FR2518494 A1 FR 2518494A1 FR 8221223 A FR8221223 A FR 8221223A FR 8221223 A FR8221223 A FR 8221223A FR 2518494 A1 FR2518494 A1 FR 2518494A1
Authority
FR
France
Prior art keywords
folding
cable
cables
central body
unfolding
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.)
Withdrawn
Application number
FR8221223A
Other languages
English (en)
French (fr)
Inventor
Herbert Metz
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 FR2518494A1 publication Critical patent/FR2518494A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/222Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
    • B64G1/2221Parts 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
    • B64G1/2222Folding
    • B64G1/2224Folding about multiple axes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/42Arrangements or adaptations of power supply systems
    • B64G1/44Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
    • B64G1/443Photovoltaic cell arrays
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2201/00Constructional elements; Accessories therefor
    • E05Y2201/60Suspension or transmission members; Accessories therefor
    • E05Y2201/606Accessories therefor
    • E05Y2201/62Synchronisation of suspension or transmission members
    • EFIXED CONSTRUCTIONS
    • E05LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
    • E05YINDEXING SCHEME ASSOCIATED WITH SUBCLASSES E05D AND E05F, RELATING TO CONSTRUCTION ELEMENTS, ELECTRIC CONTROL, POWER SUPPLY, POWER SIGNAL OR TRANSMISSION, USER INTERFACES, MOUNTING OR COUPLING, DETAILS, ACCESSORIES, AUXILIARY OPERATIONS NOT OTHERWISE PROVIDED FOR, APPLICATION THEREOF
    • E05Y2201/00Constructional elements; Accessories therefor
    • E05Y2201/60Suspension or transmission members; Accessories therefor
    • E05Y2201/622Suspension or transmission members elements
    • E05Y2201/644Flexible elongated pulling elements
    • E05Y2201/654Cables

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Photovoltaic Devices (AREA)
  • Aerials With Secondary Devices (AREA)
FR8221223A 1981-12-19 1982-12-17 Mecanisme de depliage et de repliage d'une structure pliante Withdrawn FR2518494A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19813150463 DE3150463A1 (de) 1981-12-19 1981-12-19 Mechanismus zum ausfahren und wiedereinholen einer faltstruktur

Publications (1)

Publication Number Publication Date
FR2518494A1 true FR2518494A1 (fr) 1983-06-24

Family

ID=6149234

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8221223A Withdrawn FR2518494A1 (fr) 1981-12-19 1982-12-17 Mecanisme de depliage et de repliage d'une structure pliante

Country Status (4)

Country Link
JP (1) JPS58112900A (ja)
DE (1) DE3150463A1 (ja)
FR (1) FR2518494A1 (ja)
GB (1) GB2114812A (ja)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2697316A1 (fr) * 1992-10-24 1994-04-29 Deutsche Aerospace Dispositif d'articulation avec verrouillage et déverrouillage pour relier entre eux les éléments d'une structure pliante.
CN103274065A (zh) * 2013-05-17 2013-09-04 中国科学院空间科学与应用研究中心 一种卫星软伸杆
CN105204529A (zh) * 2015-09-30 2015-12-30 黑龙江兴安新能源股份有限公司 一种带有倾动功能的链条展开式太阳能发电站
CN108706047A (zh) * 2018-06-25 2018-10-26 汕头大学 一种基于利用太阳能的无动力除草小车

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE29506718U1 (de) * 1995-04-20 1995-09-21 Image Concepts Bildkommunikati Folienartiger Werbeträger
DE19728844C2 (de) * 1997-07-05 1999-04-15 Daimler Benz Aerospace Ag Getriebe zur Bewegung von mit Solarzellen versehenen Paneelen an einem Raumfahrzeug
DE19922849A1 (de) * 1999-05-19 2000-12-07 Daimler Chrysler Ag Aufklappbare Raumfahrtstruktur
KR100832874B1 (ko) 2007-06-11 2008-05-28 한국항공우주연구원 태양전지판의 전개 구현장치
CN102253322B (zh) * 2011-05-11 2013-02-27 清华大学 太阳电池阵模拟装置
CN103991560B (zh) * 2014-06-09 2015-10-28 哈尔滨工业大学 双电机绳索式太阳翼辅助翻转机构
CN104015941B (zh) * 2014-06-09 2015-10-28 哈尔滨工业大学 齿轮齿条往复驱动绳索式太阳翼辅助翻转机构
WO2023133405A1 (en) * 2022-01-07 2023-07-13 Northrop Grumman Systems Corporation Deployable panel array and related assemblies and methods

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2697316A1 (fr) * 1992-10-24 1994-04-29 Deutsche Aerospace Dispositif d'articulation avec verrouillage et déverrouillage pour relier entre eux les éléments d'une structure pliante.
CN103274065A (zh) * 2013-05-17 2013-09-04 中国科学院空间科学与应用研究中心 一种卫星软伸杆
CN103274065B (zh) * 2013-05-17 2015-08-05 中国科学院空间科学与应用研究中心 一种卫星软伸杆
CN105204529A (zh) * 2015-09-30 2015-12-30 黑龙江兴安新能源股份有限公司 一种带有倾动功能的链条展开式太阳能发电站
CN108706047A (zh) * 2018-06-25 2018-10-26 汕头大学 一种基于利用太阳能的无动力除草小车
CN108706047B (zh) * 2018-06-25 2023-06-20 汕头大学 一种基于利用太阳能的无动力除草小车

Also Published As

Publication number Publication date
GB2114812A (en) 1983-08-24
DE3150463A1 (de) 1983-06-30
JPS58112900A (ja) 1983-07-05

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