发明名称 Apparatus comprising a payload ejection mechanism
摘要 An apparatus that provides shock absorption and ejection for a payload that is to be deployed from a launch capsule is disclosed. The payload ejection mechanism comprises a movable housing that houses a resilient member and a shock-damping system. The rapid acceleration of the capsule upon launch causes the movable housing to move, which compresses the resilient member, thereby storing energy. Movement of the housing also provides shock damping behavior. A locking mechanism maintains the compression of the resilient member until the capsule opens to deploy the payload. As the capsule opens, a restraint decouples from the locking mechanism and permits the resilient member to expand. Expansion of the resilient member causes the movable housing to move, thereby propelling the payload away from the capsule.
申请公布号 US7762194(B2) 申请公布日期 2010.07.27
申请号 US20060531200 申请日期 2006.09.12
申请人 LOCKHEED MARTIN CORPORATION 发明人 GAIGLER RANDY L.
分类号 F42B12/58 主分类号 F42B12/58
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