发明名称 Retractable wing for missile - has angled body recesses for housing pivoted lift surfaces protruding upwards in flight
摘要 <p>The projectile with control- and stabilising fittings and an elongated body is distinguished by two elongated blades (354,355) connected to that body, each with an elongated flat lift-portion (356-357) projecting upwards from the body in flight. Both lift portions are mounted rotatably about axes near one lift-portion end and perpendicular to its surface. The axes meet in the body (350) centre plane and diverge downwards from that. Recesses (352,353) on opposite sides of the body each accommodate on blade which rotates between an operation/flying position and one retracted into the recess, when no part projects beyond the body contour. The body may also have wings (364,365).</p>
申请公布号 DE3042904(A1) 申请公布日期 1982.07.01
申请号 DE19803042904 申请日期 1980.11.14
申请人 JONES JUN.,ALLEN 发明人 JUN.,ALLEN JONES
分类号 F42B10/64;(IPC1-7):64C9/12 主分类号 F42B10/64
代理机构 代理人
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