发明名称 Drive mechanism for fast and controlled separation of two coupled elements.
摘要 <p>An injection-control mechanism, which can be used in particular on a spacecraft, comprises a resilient element (36) such as a spring or a gas capacity, placed in between a drive element (18) and a pushing element (26). The driving energy supplied, for example, by a pyrotechnic charge (24) is applied to the drive element (18) which has a limited travel. An appropriately determined proportion of this energy is transmitted to the resilient element (36) which releases it to the pushing element (26). The speed and the acceleration are thus perfectly controlled. The mechanism can also effect the separation of the pieces before ejection. &lt;IMAGE&gt;</p>
申请公布号 EP0296936(A1) 申请公布日期 1988.12.28
申请号 EP19880401467 申请日期 1988.06.14
申请人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE 发明人 CAREL, CLAUDE;LESINEAU, BERNARD;SPARIAT, JACQUES
分类号 B64G1/64;F15B15/19;F42B3/00;(IPC1-7):B64G1/64 主分类号 B64G1/64
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