JPH0471760B2 - - Google Patents

Info

Publication number
JPH0471760B2
JPH0471760B2 JP58056784A JP5678483A JPH0471760B2 JP H0471760 B2 JPH0471760 B2 JP H0471760B2 JP 58056784 A JP58056784 A JP 58056784A JP 5678483 A JP5678483 A JP 5678483A JP H0471760 B2 JPH0471760 B2 JP H0471760B2
Authority
JP
Japan
Prior art keywords
spiral spring
hinge pin
sleeve
hinge
solar battery
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
JP58056784A
Other languages
English (en)
Japanese (ja)
Other versions
JPS58188800A (ja
Inventor
Kiindoru Herumuuto
Etsushenfueruderu Peeteru
Masaru Okamoto
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.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric Corp
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 Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Publication of JPS58188800A publication Critical patent/JPS58188800A/ja
Publication of JPH0471760B2 publication Critical patent/JPH0471760B2/ja
Granted 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
    • 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
    • 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
    • Y02E10/50Photovoltaic [PV] energy

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Photovoltaic Devices (AREA)
  • Pivots And Pivotal Connections (AREA)
JP58056784A 1982-04-24 1983-03-31 展開型太陽電池パドルの展開機構 Granted JPS58188800A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3215431A DE3215431C2 (de) 1982-04-24 1982-04-24 Einrichtung zum Entfalten von Solargeneratoren
DE3215431.3 1982-04-24

Publications (2)

Publication Number Publication Date
JPS58188800A JPS58188800A (ja) 1983-11-04
JPH0471760B2 true JPH0471760B2 (en]) 1992-11-16

Family

ID=6161917

Family Applications (1)

Application Number Title Priority Date Filing Date
JP58056784A Granted JPS58188800A (ja) 1982-04-24 1983-03-31 展開型太陽電池パドルの展開機構

Country Status (2)

Country Link
JP (1) JPS58188800A (en])
DE (1) DE3215431C2 (en])

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IT1222756B (it) * 1987-09-29 1990-09-12 Contraves Italiana Spa Meccanismo di articolazione piana a moto diretto e inverso privo di attuatori di movimento elettrici,per applicazioni spaziali
DE4032112A1 (de) * 1990-10-10 1992-04-16 Marcus Metzger Entfaltungsunterstuetzender, steifigkeitsoptimierter verriegelungsmechanismus fuer entfaltbare solargeneratoren von satelliten
US5509747A (en) * 1992-10-24 1996-04-23 Deutsche Aerospace Ag Articulation arrangement for connecting folding structure elements
US5673459A (en) * 1994-09-28 1997-10-07 Space Systems/Loral, Inc. Deployment hinge apparatus
DE19610297C1 (de) * 1996-03-15 1997-01-23 Daimler Benz Aerospace Ag Vorrichtung zum Entfalten von zwei Paneelen für Solargeneratoren
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
DE102011114473B3 (de) * 2011-09-28 2013-01-31 Astrium Gmbh Gelenk zum Entfalten und Verriegeln eines Solargenerators oder eines Reflektors
US12323086B2 (en) 2019-12-20 2025-06-03 Ecoquip Australia Pty Ltd Mobile solar panel unit
BG67602B1 (bg) * 2020-09-02 2024-01-15 "Ендуросат" Ад Система за разгъване на соларни панели и наносателити
DE102021102980A1 (de) 2021-02-09 2022-08-11 Deployables Cubed GmbH Auslegersystem für einen Satelliten
US20250119093A1 (en) * 2023-10-10 2025-04-10 Xplore Inc. Hinge-locking mechanism for deployable solar array

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2371343A1 (fr) * 1976-11-17 1978-06-16 Aerospatiale Dispositif pour le deploiement synchronise d'elements articules porteurs de cellules solaires dans un panneau forme d'une succession de tels elements

Also Published As

Publication number Publication date
DE3215431A1 (de) 1983-10-27
DE3215431C2 (de) 1985-11-07
JPS58188800A (ja) 1983-11-04

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