JPH02117300U - - Google Patents

Info

Publication number
JPH02117300U
JPH02117300U JP2711389U JP2711389U JPH02117300U JP H02117300 U JPH02117300 U JP H02117300U JP 2711389 U JP2711389 U JP 2711389U JP 2711389 U JP2711389 U JP 2711389U JP H02117300 U JPH02117300 U JP H02117300U
Authority
JP
Japan
Prior art keywords
bracket
lever
shaft
attached
paddle
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.)
Pending
Application number
JP2711389U
Other languages
Japanese (ja)
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 filed Critical
Priority to JP2711389U priority Critical patent/JPH02117300U/ja
Publication of JPH02117300U publication Critical patent/JPH02117300U/ja
Pending legal-status Critical Current

Links

Landscapes

  • Photovoltaic Devices (AREA)

Description

【図面の簡単な説明】[Brief explanation of drawings]

第1図は、この考案の一実施例を示す格納状態
の正面図、第2図は同じくこの考案の一実施例を
示す格納状態の平面図、第3図はこの考案の一実
施例を示す、太陽電池パドル展開開始後の正面図
、第4図は、この考案の一実施例を示す展開状態
の正面図、第5図Aは人工衛星と、ソーラーセイ
ルを搭載した展開型太陽電池パドルの展開後状態
を示す概念図、第5図Bは人工衛星と、前記展開
型太陽電池パドルの格納状態を示す概念図、第6
図は従来のソーラセイルの格納状態を示す正面図
、第7図は、同じく従来のソーラーセイルの展開
状態を示す正面図、第8図は、従来のソーラセイ
ルの格納状態を示す平面図である。 図において、1は人工衛星本体、2は展開型太
陽電池パドル、3はブレード、4サポート、5は
熱制御用インシユレーシヨン、6は導電線、7は
形状記憶合金製コイルバネ、8はブラケツト、9
はてこ、10は第1の軸、11は回転軸、12は
第2の軸、13は取付ブラケツト、14はねじり
コイルバネ、15は第1のブラケツト、16は第
2のブラケツト、hは楕円状の長穴である。なお
、各図中、同一符号は同一または相当部分を示す
。
Figure 1 is a front view of an embodiment of this invention in a stored state, Figure 2 is a plan view of an embodiment of this invention in a stored state, and Figure 3 is an embodiment of this invention. , a front view of the solar battery paddle after it has started to deploy, Figure 4 is a front view of the deployed state showing one embodiment of this invention, and Figure 5A is a front view of the deployable solar battery paddle equipped with an artificial satellite and a solar sail. FIG. 5B is a conceptual diagram showing the state after deployment, and FIG. 5B is a conceptual diagram showing the stored state of the deployable solar array paddle.
FIG. 7 is a front view showing a conventional solar sail in a stored state, FIG. 7 is a front view showing a conventional solar sail in an expanded state, and FIG. 8 is a plan view showing a conventional solar sail in a stored state. In the figure, 1 is the satellite body, 2 is the expandable solar array paddle, 3 is the blade, 4 is the support, 5 is the thermal control insulation, 6 is the conductive wire, 7 is the shape memory alloy coil spring, and 8 is the bracket. , 9
Lever, 10 is the first shaft, 11 is the rotating shaft, 12 is the second shaft, 13 is the mounting bracket, 14 is the torsion coil spring, 15 is the first bracket, 16 is the second bracket, h is oval shape It is a long hole. In each figure, the same reference numerals indicate the same or corresponding parts.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 人工衛星に搭載される展開型太陽電池パドルに
おいて、前記展開型太陽電池パドルの最外端のパ
ネルに、取付けられた第1のブラケツト、前記第
1のブラケツトに固定された第1の軸、前記第1
の軸を支点とするてこ、前記第1のブラケツトに
固定された第2のブラケツト、前記てこの一端と
前記第2のブラケツトを連結する形状記憶合金製
コイルバネ、前記てこの他端に明けられた楕円状
の穴、前記楕円状の穴をしゆう動可能な第2の軸
、前記第1のブラケツトに固定された第3の軸、
前記第3の軸を支点とし、前記第2の軸と一体と
なつたサポート、前記サポートに装着されたブレ
ード、前記てこの下縁部に接する様に、前記展開
型太陽電池パドルの外側から2枚目のパネルに取
付けられた第1のストツパ、前記第1のブラケツ
トに取付けられた第2のストツパから構成される
ことを特徴とするソーラーセイル。
In a deployable solar battery paddle mounted on an artificial satellite, a first bracket attached to an outermost panel of the deployable solar battery paddle, a first shaft fixed to the first bracket, and a first shaft fixed to the first bracket; 1st
a lever having a shaft as a fulcrum, a second bracket fixed to the first bracket, a shape memory alloy coil spring connecting one end of the lever to the second bracket, and a coil spring provided at the other end of the lever. an oval hole, a second shaft movable through the oval hole, and a third shaft fixed to the first bracket;
With the third axis as a fulcrum, a support integrated with the second axis, a blade attached to the support, and two parts from the outside of the deployable solar cell paddle so as to be in contact with the lower edge of the lever. A solar sail comprising a first stopper attached to the first panel and a second stopper attached to the first bracket.
JP2711389U 1989-03-09 1989-03-09 Pending JPH02117300U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2711389U JPH02117300U (en) 1989-03-09 1989-03-09

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2711389U JPH02117300U (en) 1989-03-09 1989-03-09

Publications (1)

Publication Number Publication Date
JPH02117300U true JPH02117300U (en) 1990-09-19

Family

ID=31249339

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2711389U Pending JPH02117300U (en) 1989-03-09 1989-03-09

Country Status (1)

Country Link
JP (1) JPH02117300U (en)

Similar Documents

Publication Publication Date Title
JPH0471760B2 (en)
JPH022300U (en)
JPS6447500U (en)
JPH03113299U (en)
JPH0399699U (en)
JPH0263300U (en)
JPS623337U (en)
JPH10129600A (en) Solar battery paddles
JPH03121100U (en)
JPS6280800U (en)
JPS6444896U (en)
JPH0244356U (en)
JPS5950511B2 (en) Sanderutsch structure
JPH03130612U (en)
JPH0475797U (en)
JPH11208599A (en) Solar paddle
JPH0483999U (en)
JPH079423Y2 (en) Cover fixture
JPH01147507U (en)
JPH0399698U (en)
JPS61168652U (en)
JPS5978709U (en) Antenna for satellite
JPH03120300U (en)
JPS61169900U (en)
JPS59121300U (en) Space solar power generation device