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1. 发明授权

US4491289A Multiple locking device insensitive to thermal variations especially applicable to space vehicles 失效
标题翻译：多个锁定装置对于特别适用于太空车辆的热变化不敏感
公开(公告)号：US4491289A
公开(公告)日：1985-01-01
申请号：US458690
申请日：1983-01-17
申请人： Christian Rinn , Gerard Vezain
发明人： Christian Rinn , Gerard Vezain
IPC分类号： B64G1/22 , B64G1/44 , B64G1/66
CPC分类号： B64G1/222 , B64G1/44 , B64G1/66
摘要： A locking device for clamping or sheaving appendices aboard a satellite during the launching phase provides for temporary locking thereof which both limits the required holding forces and authorizes multiplication of the clamping or sheaving points for each appendix while being insensitive to temperature variations. It comprises a stop catch jointed to a foot rigidly secured to the satellite structure, to ensure immobilization of the element to be temporarily locked thereby, an elbow lever hinged to the stop catch and connected to a sheaving cable, and an elastic link exerting upon the lever a force to balance the holding force exerted by the sheaving cable. The locking device remains in the locked position as long as the shearing device for cutting off the cable has not been operated. Furthermore the combination of the elbow lever and the elastic link provides means for ensuring perfect locking, even in the case of significant differential dilatations between the body of the space vehicle and the sheaving cable.
摘要翻译：在发射阶段，用于在卫星上夹紧或剪接附件的锁定装置提供临时锁定，这两者限制了所需的保持力，并且授权每个附件的夹紧或剪切点的乘法，同时对温度变化不敏感。它包括连接到牢固地固定到卫星结构上的脚的止挡钩，以确保被暂时锁定的元件的固定，肘杆铰接到止动钩并连接到绳索，并且弹性连杆施加在杠杆力平衡由滑轮电缆施加的保持力。只要切断电缆的剪切装置未被操作，锁定装置保持在锁定位置。此外，肘杆和弹性连杆的组合提供了用于确保完美锁定的装置，即使在空间车辆的主体和滑轮之间存在显着的差异扩张的情况下。

2. 发明授权

US4529154A Device for derivation of temporary force for maintaining a displayable appendix in its stored position on a space vehicle 失效
标题翻译：用于推导临时力量的装置，用于将可显示阑尾保持在其在空间车辆上的存储位置
公开(公告)号：US4529154A
公开(公告)日：1985-07-16
申请号：US518269
申请日：1983-07-28
申请人： Christian Rinn , Georges Marello , Gerard Vezain
发明人： Christian Rinn , Georges Marello , Gerard Vezain
IPC分类号： H01Q1/08 , B64G1/22 , B64G1/44 , B64G1/66 , H01Q1/28
CPC分类号： B64G1/222 , B64G1/443 , B64G1/66 , Y10T16/551
摘要： A displayable appendix linked to the structure of a space vehicle movable about an articulation axis from a stored position along the structure of the space vehicle to a display position by a control mechanism with abutments on the appendix and on the structure of the space vehicle so distributed and located as to prevent warping or distortion of the articulation axis and the control mechanism by exerting upon the appendix bending prestresses which are reduced near the articulation axis to a pure prestress torque tending to cause the appendix to move to the display position and temporary forces obtained from use of the abutments to hold the displayable appendix in the stored position during launch of the space vehicle.
摘要翻译：一种可显示的附件，其与可沿关节运动轴线从沿着空间飞行器的结构的存储位置运动到可显示位置的空间车辆的结构相连接，该控制机构具有邻接在该附录上的基座和如此分布的空间车辆的结构并且定位为通过施加附近的弯曲预应力来防止关节轴线和控制机构的翘曲或变形，所述附加弯曲预应力在关节轴线附近减小到具有倾向于使附件移动到显示位置的纯预应力扭矩和获得的临时力在使用该基座以将该可显示附件保持在该空间车辆的发射期间的存储位置。

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