发明名称 Thrust reverser for a jet engine with doors linked to a front panel
摘要 <p>The thrust reverser consists of a number of hinged flaps (7) which form part of the outer wall of the engine nacelle when closed, and are turned by an actuator to form barriers to the jet flow, deflecting it outwards and forwards. Each flap (7) has an inner panel (20) which is connected to the same pivot (27) as the flap itself, which is carried by the fixed structure of the thrust reversal system, and the panel and flap are linked by an epicycloid gear train with a toothed component (31) fixed to the flap and acting as the planet gear, a toothed outer crown wheel (34) on the inner panel, and at least one freely-rotating gear (33) between them acting as a satellite. When the flap is opened into the reverse thrust position the inner panel turns at the same time and in the opposite direction.</p>
申请公布号 EP0790399(A1) 申请公布日期 1997.08.20
申请号 EP19970400320 申请日期 1997.02.13
申请人 HISPANO SUIZA 发明人 JEAN, MICHEL CHRISTIAN MARIE
分类号 B64C15/14;F02K1/70;F02K1/74;F16H3/44;(IPC1-7):F02K1/70 主分类号 B64C15/14
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