发明名称 Two position exhaust nozzle for missile rocket motor
摘要 The nozzle consists of an outer envelope (16) with an inner continuous surface (18) defining the shape of the nozzle at its maximum cross-section. It also has surfaces (14) inside the inner surface which co-operate with one another to form the nozzle shape at minimum cross-section and are able to move between the two positions. These surfaces are covered with a skin to prevent leakages between their edges, while the skin tears along the edges when the components move from minimum to maximum nozzle diameter. The moving surfaces (14) are made in the form of fore and aft vanes which are articulated to the outer envelope, with springs between the two which are under tension when the nozzle is at minimum diameter. The vanes are actuated by rods (28) between them and the outer envelope.
申请公布号 FR2745334(A1) 申请公布日期 1997.08.29
申请号 FR19800014788 申请日期 1980.07.03
申请人 ROLLS ROYCE PLC 发明人 SCRACE HAROLD ALAN
分类号 F02K1/10;F02K1/12;F02K9/86;(IPC1-7):F02K7/18;F02K1/08;F02K9/08;F02K9/97 主分类号 F02K1/10
代理机构 代理人
主权项
地址