发明名称 Thrust reverser for a turbofan engine
摘要 In a bypass turbo jet engine thrust reverser including shiftable elements or doors (7), the stationary structural elements are composed of a front frame (10) arranged transversely and of a transverse rear frame (11), both connected by longitudinal spars (beams) (12a, 12b, 12c), enframing the shiftable elements (7), whose shifting means, such as jacks (7a) are fixed to the rear frame (11). <IMAGE>
申请公布号 EP0654598(B1) 申请公布日期 1998.08.26
申请号 EP19940402669 申请日期 1994.11.23
申请人 HISPANO-SUIZA AEROSTRUCTURES 发明人 DE CAMBRAY, ELISABETH, LUCETTE FRANCINE CHRISTINE;VICOGNE, LAURENT MARCEL
分类号 F02K1/60;F02K1/70 主分类号 F02K1/60
代理机构 代理人
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