JPH0215598U - - Google Patents

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Publication number
JPH0215598U
JPH0215598U JP9428388U JP9428388U JPH0215598U JP H0215598 U JPH0215598 U JP H0215598U JP 9428388 U JP9428388 U JP 9428388U JP 9428388 U JP9428388 U JP 9428388U JP H0215598 U JPH0215598 U JP H0215598U
Authority
JP
Japan
Prior art keywords
solar cell
deployed
panels
spin
satellite
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
JP9428388U
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 JP9428388U priority Critical patent/JPH0215598U/ja
Publication of JPH0215598U publication Critical patent/JPH0215598U/ja
Pending legal-status Critical Current

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  • Photovoltaic Devices (AREA)

Description

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

第1図、第2図はこの考案の実施例を示す図で
あり、第1図は収納状態を示す図、第2図は展開
状態を示す図、第3図、第4図は従来の実施例を
示す図であり、第3図は収納状態を示す図、第4
図は展開状態を示す図である。 図中1は太陽電池パネル、3は衛星構体、4は
展開機構、Sはスピン軸である。なお図中同一あ
るいは相当部分には同一符号を付して示してある
Figures 1 and 2 are diagrams showing an embodiment of this invention. Figure 1 is a diagram showing a stored state, Figure 2 is a diagram showing an unfolded state, and Figures 3 and 4 are diagrams showing a conventional implementation. 3 is a diagram showing an example, FIG. 3 is a diagram showing a stored state,
The figure shows a developed state. In the figure, 1 is a solar cell panel, 3 is a satellite structure, 4 is a deployment mechanism, and S is a spin axis. Note that the same or corresponding parts in the figures are indicated by the same reference numerals.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 収納時衛星構体の周囲に互いに1部が重なるよ
うに設けられ、展開時は1つの円筒面を形成する
複数の太陽電池パネルと、これらをスピン型人工
衛星のスピン軸から遠ざかる方向へ展開させる展
開機構とを備えたことを特徴とする、展開型太陽
電池パネル。
A plurality of solar cell panels are provided around the satellite structure so that parts overlap each other when stored, and form a single cylindrical surface when deployed, and deployment that allows these panels to be deployed in a direction away from the spin axis of the spin-type artificial satellite. A deployable solar cell panel characterized by being equipped with a mechanism.
JP9428388U 1988-07-16 1988-07-16 Pending JPH0215598U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP9428388U JPH0215598U (en) 1988-07-16 1988-07-16

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP9428388U JPH0215598U (en) 1988-07-16 1988-07-16

Publications (1)

Publication Number Publication Date
JPH0215598U true JPH0215598U (en) 1990-01-31

Family

ID=31318792

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9428388U Pending JPH0215598U (en) 1988-07-16 1988-07-16

Country Status (1)

Country Link
JP (1) JPH0215598U (en)

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