发明名称 DISPOSITIF DE COMMANDE D'UNE ROTATION RELATIVE ENTRE DEUX ELEMENTS ARTICULES ET STRUCTURE MECANIQUE DEPLOYABLE, NOTAMMENT POUR VEHICULE SPATIAL, UTILISANT AU MOINS UN DISPOSITIF DE CE TYPE
摘要 In order to control relative rotation between two elements (10, 12), such as an unfolding mechanical structure flaps, on a space vehicle, a bistable shape-memory alloy torque shaft, heated over its whole length by heaters bonded on the bar and maintained by banding rings, is used. A stop (22) limits the pivoting to the predetermined pivoting angle to be controlled. The torque shaft (16) excess pivoting is applied to a mechanical fuse (18), inserted between the bar and one of the elements (12).
申请公布号 FR2776984(A1) 申请公布日期 1999.10.08
申请号 FR19980004242 申请日期 1998.04.06
申请人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE 发明人 VEZAIN GERARD ALBERT PIERRE;KERHOUSEE PATRICE;VIALE DANIEL;BAUDASSE YANNICK;REIMBOLD FRANCOIS
分类号 B64G1/22;B64G1/44;B64G1/64;E05F1/00;E05F1/12;F03G7/06;(IPC1-7):B64G1/64 主分类号 B64G1/22
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