FR2531033B1 - Dispositif de maintien en position abaissee d'elements fonctionnels deployables - Google Patents

Dispositif de maintien en position abaissee d'elements fonctionnels deployables

Info

Publication number
FR2531033B1
FR2531033B1 FR8312096A FR8312096A FR2531033B1 FR 2531033 B1 FR2531033 B1 FR 2531033B1 FR 8312096 A FR8312096 A FR 8312096A FR 8312096 A FR8312096 A FR 8312096A FR 2531033 B1 FR2531033 B1 FR 2531033B1
Authority
FR
France
Prior art keywords
holding
lower position
functional elements
deployable functional
position deployable
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
Application number
FR8312096A
Other languages
English (en)
Other versions
FR2531033A1 (fr
Inventor
Rudiger Ewald
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 FR2531033A1 publication Critical patent/FR2531033A1/fr
Application granted granted Critical
Publication of FR2531033B1 publication Critical patent/FR2531033B1/fr
Expired 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24HEATING; RANGES; VENTILATING
    • F24SSOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
    • F24S20/00Solar heat collectors specially adapted for particular uses or environments
    • F24S20/50Rollable or foldable solar heat collector modules
    • 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
    • B64G1/2228Parts 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24HEATING; RANGES; VENTILATING
    • F24SSOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
    • F24S30/00Arrangements for moving or orienting solar heat collector modules
    • F24S30/40Arrangements for moving or orienting solar heat collector modules for rotary movement
    • F24S30/45Arrangements for moving or orienting solar heat collector modules for rotary movement with two rotation 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
    • B64G1/222Parts 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
    • 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F24HEATING; RANGES; VENTILATING
    • F24SSOLAR HEAT COLLECTORS; SOLAR HEAT SYSTEMS
    • F24S25/00Arrangement of stationary mountings or supports for solar heat collector modules
    • F24S2025/01Special support components; Methods of use
    • F24S2025/023Means for preventing theft; Locking means
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/40Solar thermal energy, e.g. solar towers
    • Y02E10/47Mountings or tracking

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Thermal Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Sustainable Energy (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Sustainable Development (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Photovoltaic Devices (AREA)
  • Clamps And Clips (AREA)
  • Surgical Instruments (AREA)
  • Massaging Devices (AREA)
  • Magnetic Resonance Imaging Apparatus (AREA)
FR8312096A 1982-07-29 1983-07-21 Dispositif de maintien en position abaissee d'elements fonctionnels deployables Expired FR2531033B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3228284A DE3228284C2 (de) 1982-07-29 1982-07-29 Niederhaltevorrichtung für entfaltbare Funktionselemente

Publications (2)

Publication Number Publication Date
FR2531033A1 FR2531033A1 (fr) 1984-02-03
FR2531033B1 true FR2531033B1 (fr) 1986-02-07

Family

ID=6169579

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8312096A Expired FR2531033B1 (fr) 1982-07-29 1983-07-21 Dispositif de maintien en position abaissee d'elements fonctionnels deployables

Country Status (5)

Country Link
US (1) US4491446A (fr)
JP (1) JPS5940999A (fr)
DE (1) DE3228284C2 (fr)
FR (1) FR2531033B1 (fr)
GB (1) GB2124694B (fr)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL8400362A (nl) * 1984-02-06 1985-09-02 Fokker Bv Inrichting voor het vasthouden of vrijgeven van zonnepanelen van een ruimtevaartuig.
JPS61270498A (ja) * 1985-05-24 1986-11-29 松坂貿易株式会社 鋼管の打撃推進工法
US5286150A (en) * 1992-06-16 1994-02-15 Spar Aerospace Limited Tie down device
FR2714358B1 (fr) * 1993-12-24 1996-03-15 Aerospatiale Dispositif de maintien et de libération d'une structure telle qu'une structure déployable embarquée sur un engin spatial.
FR2721583B1 (fr) * 1994-06-27 1996-10-04 Aerospatiale Dispositif de gerbage à déclenchement mécanique pour engin spatial.
DE19548002C2 (de) * 1995-12-21 1997-09-18 Daimler Benz Aerospace Ag Vorrichtung zum Niederhalten und Lösen von Solarpaneelen
US5810296A (en) * 1996-08-29 1998-09-22 Trw Inc. Integrated restraint/release/deployment initiation device
US6505381B1 (en) * 1999-07-30 2003-01-14 Trw Astro Aerospace Pulley actuated translational hinge system
US6308919B1 (en) * 2000-04-25 2001-10-30 Space Systems/Loral, Inc. Spacecraft having a dual reflector holddown for deploying multiple reflectors in a single release event
RU2460676C2 (ru) * 2010-08-16 2012-09-10 Федеральное Государственное Унитарное Предприятие "Государственный научно-производственный ракетно-космический центр "ЦСКБ-Прогресс" (ФГУП "ГНПРКЦ "ЦСКБ-Прогресс") Батарея солнечная космического аппарата
DE102010048176B3 (de) * 2010-10-13 2012-01-05 Thread Guard Technology Ltd. Vorrichtung zur Fixierung einer Mehrzahl von Rohren relativ zueinander bei deren Lagerung und Transport
US8915473B1 (en) * 2011-09-20 2014-12-23 Space Systems/Loral, Llc Hold-down mechanism for a spacecraft appendage
US9086098B2 (en) 2012-02-14 2015-07-21 The Board Of Trustees Of The Leland Stanford Junior University Anti-twist joint, orienting system and method
BR112015022210A8 (pt) 2013-03-13 2018-01-23 Genentech Inc formulações de anticorpo
RU2560213C2 (ru) * 2013-11-06 2015-08-20 Акционерное общество "Ракетно-космический центр "Прогресс" (АО "РКЦ "Прогресс") Устройство крепления крупногабаритных плоских конструкций на космическом аппарате
RU2554901C2 (ru) * 2013-11-06 2015-06-27 Акционерное общество "Ракетно-космический центр "Прогресс" (АО "РКЦ "Прогресс") Устройство раскрытия плоских крупногабаритных конструкций космического аппарата
MX2017003121A (es) 2014-09-15 2017-08-02 Genentech Inc Formulaciones de anticuerpos.
RU2614465C2 (ru) * 2015-07-20 2017-03-28 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Устройство крепления и расфиксации развертываемых панелей
US10390631B2 (en) * 2016-02-10 2019-08-27 Jade Group International Llc Skewer for loading cutlery
CN112429275B (zh) * 2020-12-10 2022-07-29 北京空间机电研究所 一种限位式空间旋转锁定释放机构
CN115783314B (zh) * 2022-11-21 2024-04-26 北京中科宇航技术有限公司 一种多平板堆叠卫星解锁系统

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2583053A (en) * 1947-12-18 1952-01-22 American Ship Building Company Quick action hatch clamp
US3270801A (en) * 1963-06-10 1966-09-06 Fuller Co Automatic holdback device
US3291514A (en) * 1963-12-03 1966-12-13 Goetaverken Ab Latching means for hatch covers
DE2853070C3 (de) * 1978-12-08 1981-10-29 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Niederhaltersystem für entfaltbare oder entklappbare Trägerelemente an Raumflugkörpern
EP0034193A1 (fr) * 1980-02-15 1981-08-26 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Dispositif de maintien pour élément-supports déployables pour vehicules spatiaux
DE3018245C2 (de) * 1980-05-13 1982-12-23 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Niederhaltersystem für entfaltbare oder entklappbare Trägerelemente an Raumflugkörpern
DE3113928A1 (de) * 1981-04-07 1982-10-28 Messerschmitt-Bölkow-Blohm GmbH, 8000 München "niederhalter fuer einrichtungen an raumflugkoerpern"
FR2516893A1 (fr) * 1981-11-26 1983-05-27 Aerospatiale Systeme permettant le maintien temporaire et la liberation de deux parties, plus particulierement dans le domaine spatial

Also Published As

Publication number Publication date
GB2124694A (en) 1984-02-22
DE3228284A1 (de) 1984-02-09
DE3228284C2 (de) 1986-11-27
GB2124694B (en) 1986-05-29
JPS5940999A (ja) 1984-03-06
JPH0443040B2 (fr) 1992-07-15
GB8320015D0 (en) 1983-08-24
FR2531033A1 (fr) 1984-02-03
US4491446A (en) 1985-01-01

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Legal Events

Date Code Title Description
ST Notification of lapse