FR2756619B1 - Dispositif de liberation pour des elements de retenue, par exemple de panneaux solaires - Google Patents

Dispositif de liberation pour des elements de retenue, par exemple de panneaux solaires

Info

Publication number
FR2756619B1
FR2756619B1 FR9714826A FR9714826A FR2756619B1 FR 2756619 B1 FR2756619 B1 FR 2756619B1 FR 9714826 A FR9714826 A FR 9714826A FR 9714826 A FR9714826 A FR 9714826A FR 2756619 B1 FR2756619 B1 FR 2756619B1
Authority
FR
France
Prior art keywords
solar panels
release device
retaining elements
retaining
elements
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 - Fee Related
Application number
FR9714826A
Other languages
English (en)
Other versions
FR2756619A1 (fr
Inventor
Martin Roth
Robert Apfelbeck
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
Daimler Benz Aerospace 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 Daimler Benz Aerospace AG filed Critical Daimler Benz Aerospace AG
Publication of FR2756619A1 publication Critical patent/FR2756619A1/fr
Application granted granted Critical
Publication of FR2756619B1 publication Critical patent/FR2756619B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • B64G1/42—Arrangements or adaptations of power supply systems
    • B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
    • B64G1/443—Photovoltaic cell arrays
    • 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
    • B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/645—Separators
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining
    • Y10T29/49863—Assembling or joining with prestressing of part
    • Y10T29/49874—Prestressing rod, filament or strand

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Clamps And Clips (AREA)
  • Photovoltaic Devices (AREA)
FR9714826A 1996-11-30 1997-11-26 Dispositif de liberation pour des elements de retenue, par exemple de panneaux solaires Expired - Fee Related FR2756619B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19649739A DE19649739C2 (de) 1996-11-30 1996-11-30 Freigabevorrichtung für Niederhalter z. B. an Solargeneratoren

Publications (2)

Publication Number Publication Date
FR2756619A1 FR2756619A1 (fr) 1998-06-05
FR2756619B1 true FR2756619B1 (fr) 2000-06-30

Family

ID=7813268

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9714826A Expired - Fee Related FR2756619B1 (fr) 1996-11-30 1997-11-26 Dispositif de liberation pour des elements de retenue, par exemple de panneaux solaires

Country Status (5)

Country Link
US (1) US6073914A (fr)
JP (1) JP2942526B2 (fr)
DE (1) DE19649739C2 (fr)
FR (1) FR2756619B1 (fr)
NL (1) NL1007648C2 (fr)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19843966C1 (de) * 1998-09-24 2000-04-13 Daimler Chrysler Ag Temperaturgesteuerter Drahthalter
DE19843965C2 (de) * 1998-09-24 2000-07-13 Daimler Chrysler Ag Halte- und Auslösemechanismus mit einem Formgedächtnis-Aktuator
DE19856446C2 (de) * 1998-12-08 2001-01-25 Daimler Chrysler Ag Niederhalte- und Auslösevorrichtung für entfaltbare Satellitenkomponenten
US6133818A (en) * 1999-08-11 2000-10-17 Space Systems/Loral, Inc. Redundant fuse wire release device
US6433990B1 (en) 2000-02-02 2002-08-13 Nea Electronics, Inc. Frangible actuator with redundant power supply
DE10043631C2 (de) 2000-06-29 2003-04-10 Astrium Gmbh Linearbetätigungsvorrichtung, insbesondere für Raumfahrzeuge sowie Solargenerator-Entfaltsystem
FR2857936B1 (fr) * 2003-07-22 2005-09-30 Cit Alcatel Dispositif de liberation de tirant de gerbage pour structure deployable
CN102400990B (zh) 2003-11-17 2014-08-20 远程接合技术公司 固定器组件
US8568053B2 (en) * 2008-04-14 2013-10-29 Space Systems/Loral, Llc Radial release device
FR2930306A1 (fr) * 2008-04-16 2009-10-23 Conseil Et Tech Sarl Dispositif de fixation servant a assembler des objets, puis a les liberer rapidement
CN102152860B (zh) * 2010-11-25 2013-05-08 西北工业大学 机电一体化通用对接装置
US9085377B2 (en) * 2011-05-17 2015-07-21 Space Systems/Loral, Llc Redundant fuse wire release device
AT512487B1 (de) * 2012-01-25 2016-05-15 Ruag Space Gmbh Stellmechanismus
US9657863B2 (en) * 2012-08-30 2017-05-23 Schlumberger Technology Corporation Sample valve systems and methods
CN104085540B (zh) * 2014-07-07 2016-01-06 中国科学院长春光学精密机械与物理研究所 一种采用形状记忆材料的解锁装置
CN106043744A (zh) * 2016-07-11 2016-10-26 上海宇航系统工程研究所 点式星箭连接解锁机构
FR3061353B1 (fr) * 2016-12-22 2019-05-10 Saft Dispositif autoporte d'activation pour commutateur electromecanique
FR3086354B1 (fr) * 2018-09-26 2020-12-25 Conseil & Technique Dispositif de fixation servant a assembler entre eux des objets, puis a les liberer rapidement
CN109625328A (zh) * 2018-12-12 2019-04-16 上海卫星装备研究所 熔断式压紧释放装置
CN112319864B (zh) * 2020-09-29 2022-10-21 上海航天控制技术研究所 一种采用同步解锁双拔销器的空间保护罩装置
CN113148229B (zh) * 2021-03-24 2022-08-12 上海埃依斯航天科技有限公司 一种卫星用二维三折太阳电池阵

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1021110A (en) * 1911-09-18 1912-03-26 John Niewohner Nut-lock.
US3597919A (en) * 1969-03-24 1971-08-10 Gen Electric Linear gas generator actuated latching and thrusting device
DE2853070C3 (de) * 1978-12-08 1981-10-29 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Niederhaltersystem für entfaltbare oder entklappbare Trägerelemente an Raumflugkörpern
US5129753A (en) * 1990-11-13 1992-07-14 Trw Inc. Shape memory wire latch mechanism
US5282709A (en) * 1993-05-04 1994-02-01 G & H Technology, Inc. Separation nut with a restraining wire
JP2671794B2 (ja) * 1993-12-27 1997-10-29 日本電気株式会社 宇宙構造物の分離機構
DE69420735T2 (de) * 1994-12-14 2000-03-02 Fokker Space B.V., Leiden System zum Festhalten und Trennen von Konstruktionselementen

Also Published As

Publication number Publication date
NL1007648C2 (nl) 1998-11-03
NL1007648A1 (nl) 1998-06-03
US6073914A (en) 2000-06-13
JP2942526B2 (ja) 1999-08-30
FR2756619A1 (fr) 1998-06-05
DE19649739C2 (de) 1998-11-12
JPH10244998A (ja) 1998-09-14
DE19649739A1 (de) 1998-06-04

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Legal Events

Date Code Title Description
ST Notification of lapse