发明名称 SEGMENTED STRUCTURE, IN PARTICULAR FOR A SATELLITE ANTENNA REFLECTOR, PROVIDED WITH AT LEAST ONE ROTATIONAL AND TRANSLATIONAL DEPLOYMENT DEVICE
摘要 The segmented structure (1) comprises at least two panels (2, 3, 4), a first panel (2) referred to as main panel and a second panel (3, 4) referred to as secondary panel, and also at least one deployment device (5), the deployment device (5) having a connecting arm (6) secured to the rear face (3B, 4B) of the secondary panel (3, 4) and connected to the rear face (2B) of the main panel (2), and a movement system (8) comprising a rotation unit that is able to generate a rotation of the connecting arm (6) about a reference axis, and a translation unit that is able to generate a movement of the connecting arm (6) in translation along this reference axis, so as to be able to bring the secondary panel (3, 4) into a stowed position (P1) or into a deployed position.
申请公布号 WO2015101723(A1) 申请公布日期 2015.07.09
申请号 WO2014FR00268 申请日期 2014.12.10
申请人 AIRBUS DEFENCE AND SPACE SAS 发明人 GROSROYAT, SYLVAIN
分类号 B64G1/22;B64G1/44;B64G1/66;H01Q1/28;H01Q15/16 主分类号 B64G1/22
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