发明名称 |
ARTIFICIAL SATELLITE UNFOLDING STRUCTURE |
摘要 |
PROBLEM TO BE SOLVED: To provide an artificial satellite unfolding structure capable of increasing natural frequency without increasing the number of retaining mechanisms even if the thickness of a panel is reduced as much as possible. SOLUTION: In a solar array 1 composed of a plurality of panels 2 connected to a main body part of the artificial satellite and rotatably connected each other, a plurality of elastic vibration isolation insertion members 6 are provided in gaps between each panel 2 and gaps between the main body part and the panels 2 adjacent to the main body part when the panel 2 is in a shape folded and laminated. The vibration isolation insertion members 6 are inserted in the gaps between each panel 2 and the gaps between the main body part of the artificial satellite and the panels 2 adjacent to the main body part in such a manner that the same get into contact on one surfaces and are bonded on another surfaces. COPYRIGHT: (C)2003,JPO
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申请公布号 |
JP2003267299(A) |
申请公布日期 |
2003.09.25 |
申请号 |
JP20020072774 |
申请日期 |
2002.03.15 |
申请人 |
MITSUBISHI ELECTRIC CORP |
发明人 |
OZAWA TAKUO;OZAKI TAKESHI |
分类号 |
B64G1/44;B64G1/22;B64G1/64;B64G1/66;(IPC1-7):B64G1/44 |
主分类号 |
B64G1/44 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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