JP5272179B2 - 空間的付加物展開用装置およびそのような装置を備える空間的付加物 - Google Patents
空間的付加物展開用装置およびそのような装置を備える空間的付加物 Download PDFInfo
- Publication number
- JP5272179B2 JP5272179B2 JP2009514774A JP2009514774A JP5272179B2 JP 5272179 B2 JP5272179 B2 JP 5272179B2 JP 2009514774 A JP2009514774 A JP 2009514774A JP 2009514774 A JP2009514774 A JP 2009514774A JP 5272179 B2 JP5272179 B2 JP 5272179B2
- Authority
- JP
- Japan
- Prior art keywords
- main shaft
- deployment
- driven
- phase
- spindle
- 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.)
- Active
Links
- 230000007246 mechanism Effects 0.000 claims abstract description 14
- 230000001360 synchronised effect Effects 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000002441 reversible effect Effects 0.000 description 2
- 210000000078 claw Anatomy 0.000 description 1
- 230000002427 irreversible effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Images
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
- B64G1/2224—Folding about multiple axes
-
- 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
- B64G1/2229—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 deployment actuating mechanism
-
- 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
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/08—Means for collapsing antennas or parts thereof
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/27—Adaptation for use in or on movable bodies
- H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
- H01Q1/288—Satellite antennas
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
- H02S30/00—Structural details of PV modules other than those related to light conversion
- H02S30/20—Collapsible or foldable PV modules
-
- 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
- B64G1/66—Arrangements or adaptations of apparatus or instruments, not otherwise provided for
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
-
- 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
- Y10T74/00—Machine element or mechanism
- Y10T74/18—Mechanical movements
- Y10T74/18568—Reciprocating or oscillating to or from alternating rotary
- Y10T74/18832—Reciprocating or oscillating to or from alternating rotary including flexible drive connector [e.g., belt, chain, strand, etc.]
-
- 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
- Y10T74/00—Machine element or mechanism
- Y10T74/18—Mechanical movements
- Y10T74/18568—Reciprocating or oscillating to or from alternating rotary
- Y10T74/18832—Reciprocating or oscillating to or from alternating rotary including flexible drive connector [e.g., belt, chain, strand, etc.]
- Y10T74/18848—Reciprocating or oscillating to or from alternating rotary including flexible drive connector [e.g., belt, chain, strand, etc.] with pulley
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Astronomy & Astrophysics (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Sustainable Development (AREA)
- Life Sciences & Earth Sciences (AREA)
- Photovoltaic Devices (AREA)
- Telephone Function (AREA)
- Details Of Aerials (AREA)
- Transmission Devices (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
- Automobile Manufacture Line, Endless Track Vehicle, Trailer (AREA)
- Prostheses (AREA)
Description
Claims (4)
- 一方が被駆動主軸(10)であり他方が駆動主軸(20)である2つの回転主軸(10、20)を備える少なくとも1つの2フェーズ関節式展開ラインを含む空間的付属物用の展開装置であって、前記2つの回転主軸用に同期機構(101、102、103、106、107)を備えて、第1の展開フェーズ中に前記駆動主軸(20)が回転するとき、前記被駆動主軸(10)は回転せず、次に、第2の展開フェーズ中に前記駆動主軸が回転するとき、前記被駆動主軸が前記駆動主軸と同期して回転するようにする展開装置において、
−前記同期機構は、前記第1のフェーズ中に、前記駆動主軸が折り畳み位置から中間位置へ回転するとき、前記被駆動主軸を保持することを可能とする保持手段(101、102、103)と、前記第2のフェーズ中に、前記駆動主軸が中間位置から最終位置へ回転するとき、前記被駆動主軸を前記駆動主軸と同期して回転させ前記最終位置に達するようにする解除手段(106、107)とを備え;
−前記保持手段が、前記被駆動主軸(10)にプーリ系(101)を備え、そこから、前記解除手段に互いに独立して取り付けられた2本のケーブル撚り線(102、103)が出て;前記解除手段は、第1の巻取機−巻出機装置(106)、第2の巻取機−巻出機装置(107)を備え、これら装置は偏心しており、前記ケーブル撚り線の一方は前記第1の巻取機−巻出機装置への付着点(104)を備える一方で、他方の撚り線は前記第2の巻取機−巻出機装置への付着点(105)を備え、前記プーリ系および前記巻取機−巻出機装置は前記2本のケーブル撚り線によってつながれていて、前記装置の一方により、ケーブル撚り線を前記駆動主軸の前記中間位置から前記最終位置へと巻き取ることが可能となる一方で、他方の装置により、前記被駆動主軸が前記最終位置に達するまで他方のケーブル撚り線を巻き出すことが可能となることを特徴とする展開装置。 - 前記巻取機−巻出機装置が各々プーリセクタ(106、107)を備えることを特徴とする請求項1に記載の展開装置。
- 前記中間位置までの前記駆動主軸の回転が90°であり、前記最終位置までの回転が180°であることを特徴とする請求項1または2に記載の展開装置。
- 請求項1〜3のいずれか一項に記載の展開装置を備える太陽発電機。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0652090A FR2902082B1 (fr) | 2006-06-12 | 2006-06-12 | Systeme de deploiement d'appendices spatiaux et appendice spatial comportant un tel systeme |
FR0652090 | 2006-06-12 | ||
PCT/EP2007/055727 WO2007144329A1 (fr) | 2006-06-12 | 2007-06-11 | Systeme de deploiement d'appendices spatiaux et appendice spatial comportant un tel systeme |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2009539688A JP2009539688A (ja) | 2009-11-19 |
JP5272179B2 true JP5272179B2 (ja) | 2013-08-28 |
Family
ID=37780189
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2009514774A Active JP5272179B2 (ja) | 2006-06-12 | 2007-06-11 | 空間的付加物展開用装置およびそのような装置を備える空間的付加物 |
Country Status (8)
Country | Link |
---|---|
US (1) | US8245587B2 (ja) |
EP (1) | EP2027016B1 (ja) |
JP (1) | JP5272179B2 (ja) |
AT (1) | ATE451303T1 (ja) |
DE (1) | DE602007003717D1 (ja) |
ES (1) | ES2337100T3 (ja) |
FR (1) | FR2902082B1 (ja) |
WO (1) | WO2007144329A1 (ja) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2902082B1 (fr) * | 2006-06-12 | 2009-10-30 | Alcatel Sa | Systeme de deploiement d'appendices spatiaux et appendice spatial comportant un tel systeme |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3525483A (en) * | 1968-01-17 | 1970-08-25 | North American Rockwell | Deployment mechanism |
FR2517626A1 (fr) * | 1981-12-04 | 1983-06-10 | Europ Agence Spatiale | Engin spatial orbital, notamment satellite, a missions multiples |
US4771293A (en) * | 1984-11-07 | 1988-09-13 | The General Electric Company P.L.C. | Dual reflector folding antenna |
US4703907A (en) * | 1986-11-05 | 1987-11-03 | Aerospatiale Societe Nationale Industrielle | Mechanism for the automatic extension of an appendage of a space vehicle performing a rotary movement on itself |
JP2634162B2 (ja) * | 1986-11-10 | 1997-07-23 | アエロスパテイアル ソシエテ ナシヨナル アンデユストリエル | 自転運動する宇宙ビークルの付属品の自動展開機構 |
JPS6467499A (en) * | 1987-09-07 | 1989-03-14 | Toshiba Corp | Solar-cell paddle folding expansion device |
JPH10233277A (ja) * | 1997-02-18 | 1998-09-02 | Tokyo Electron Ltd | 熱処理装置 |
DE19728844C2 (de) | 1997-07-05 | 1999-04-15 | Daimler Benz Aerospace Ag | Getriebe zur Bewegung von mit Solarzellen versehenen Paneelen an einem Raumfahrzeug |
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 |
US6124835A (en) * | 1999-07-01 | 2000-09-26 | Trw Inc. | Deployment of dual reflector systems |
FR2864033B1 (fr) * | 2003-12-23 | 2007-01-19 | Cit Alcatel | Dispositif de sequencement pour une structure deployable en fonction de la cinematique de l'un de ses corps mobiles |
FR2902082B1 (fr) * | 2006-06-12 | 2009-10-30 | Alcatel Sa | Systeme de deploiement d'appendices spatiaux et appendice spatial comportant un tel systeme |
-
2006
- 2006-06-12 FR FR0652090A patent/FR2902082B1/fr not_active Expired - Fee Related
-
2007
- 2007-06-11 EP EP07730061A patent/EP2027016B1/fr active Active
- 2007-06-11 ES ES07730061T patent/ES2337100T3/es active Active
- 2007-06-11 JP JP2009514774A patent/JP5272179B2/ja active Active
- 2007-06-11 WO PCT/EP2007/055727 patent/WO2007144329A1/fr active Application Filing
- 2007-06-11 DE DE602007003717T patent/DE602007003717D1/de active Active
- 2007-06-11 AT AT07730061T patent/ATE451303T1/de active
- 2007-06-11 US US12/304,556 patent/US8245587B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR2902082A1 (fr) | 2007-12-14 |
US20090199664A1 (en) | 2009-08-13 |
WO2007144329A1 (fr) | 2007-12-21 |
ATE451303T1 (de) | 2009-12-15 |
US8245587B2 (en) | 2012-08-21 |
JP2009539688A (ja) | 2009-11-19 |
DE602007003717D1 (de) | 2010-01-21 |
EP2027016A1 (fr) | 2009-02-25 |
ES2337100T3 (es) | 2010-04-20 |
FR2902082B1 (fr) | 2009-10-30 |
EP2027016B1 (fr) | 2009-12-09 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
JP6069670B2 (ja) | 宇宙環境における構造要素の展開及び照準合わせ用の装置 | |
JPH0930499A (ja) | ハイブリッドソーラパネルアレイ | |
US10214302B2 (en) | Deployable structure comprising a set of solar generators, system for deploying such a deployable structure and satellite comprising such a system | |
JP2006517487A (ja) | 太陽発電パネルのヒンジ式アセンブリおよび宇宙船 | |
JP2014114011A (ja) | 柔軟構造を展開および再格納する装置、並びにそのような装置を共に備えた柔軟且つ展開可能な構造および衛星 | |
US9731843B2 (en) | Articulated joint for deploying and locking a solar generator or a reflector | |
CN108810210B (zh) | 电子设备及电子设备的变形方法 | |
US20030031505A1 (en) | Unfolding joint for satellite solar generators | |
JP5272179B2 (ja) | 空間的付加物展開用装置およびそのような装置を備える空間的付加物 | |
JP4124766B2 (ja) | 構造体の一可動本体の運動に応じて構造体を展開配置するシーケンス装置 | |
WO2024022208A1 (zh) | 一种可分步二次展开的大面积柔性太阳电池翼 | |
CN205366105U (zh) | 集中式变角度展开锁定机构 | |
RU207349U1 (ru) | Механическое устройство батареи солнечной космического аппарата | |
CN115832665A (zh) | 一种星载大型控速展开构架天线 | |
CN101369681B (zh) | 构架式天线顺序展开控制装置 | |
JP6231943B2 (ja) | 展開構造体、反射鏡、及び宇宙太陽光発電システム | |
RU2309875C1 (ru) | Способ формирования бескаркасной центробежной конструкции (варианты) и устройство для его осуществления | |
JP3944571B2 (ja) | 薄膜展開構造物、そのための薄膜展開方法、並びに薄膜展開ユニット及び薄膜展開システム | |
JP6185881B2 (ja) | 宇宙大型構造物及びその構築方法 | |
JP2015085885A (ja) | 展開構造物およびこれを備える宇宙機 | |
JP2685752B2 (ja) | 太陽電池パドル展開機構 | |
JPH04163296A (ja) | 伸長構造体の伸長装置 | |
JPH0755679B2 (ja) | 展開ラツチ機構 | |
JP2004276646A (ja) | 展開構造体 | |
CN115946879A (zh) | 一种卫星太阳能电池阵展开机构 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20100517 |
|
A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20110720 |
|
A977 | Report on retrieval |
Free format text: JAPANESE INTERMEDIATE CODE: A971007 Effective date: 20120531 |
|
A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20120605 |
|
A521 | Request for written amendment filed |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20120711 |
|
TRDD | Decision of grant or rejection written | ||
A01 | Written decision to grant a patent or to grant a registration (utility model) |
Free format text: JAPANESE INTERMEDIATE CODE: A01 Effective date: 20130205 |
|
A61 | First payment of annual fees (during grant procedure) |
Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20130214 |
|
A61 | First payment of annual fees (during grant procedure) |
Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20130418 |
|
R150 | Certificate of patent or registration of utility model |
Free format text: JAPANESE INTERMEDIATE CODE: R150 Ref document number: 5272179 Country of ref document: JP Free format text: JAPANESE INTERMEDIATE CODE: R150 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |