发明名称 Release mechanism in a missile.
摘要 A retarding and locking mechanism for use between two mutually translatable bodies. A first body can be induced into motion and guided into a second body and, after a predetermined movement of the first body, the first body is subject to retardation and interlocked to the second body, such that the first and second bodies together form a unitary, integrated body. The first body has a radially outwardly directed shoulder and the second body has a radially inwardly directed shoulder corresponding to the radially outwardly directed shoulder of the first body. A compressible element is provided between the shoulders of the first and second bodies.
申请公布号 ZA200110261(B) 申请公布日期 2002.12.13
申请号 ZA20010010261 申请日期 2001.12.13
申请人 NAMMO RAUFOSS AS. 发明人 HANS B. BISEROD
分类号 F15B15/19;F15B15/22;F42B12/06;F42B15/00;F42B15/36 主分类号 F15B15/19
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