发明名称 |
Thrust reverser for a jet engine, more especially for equipping an aircraft |
摘要 |
The engine is of the type having a central body surrounded by a casing defining therebetween a duct for the passage of the flux. The casing comprises a fixed upstream section extended downstream by means in which are housed jacks; a downstream section movable axially to which are fixed the rods of the jacks; and an intermediate section formed of swinging doors mounted between the beams and hinged thereto by lateral pivots, each door being coupled to the mobile downstream section by means of a hinged link so that the movement of the downstream section causes the doors to swing. This type of reverser is designed more especially for turbo-fan engines having a lateral nacelle configuration in which the whole of the flux flows in the annular duct between the central body and the casing.
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申请公布号 |
US4410152(A) |
申请公布日期 |
1983.10.18 |
申请号 |
US19810279238 |
申请日期 |
1981.07.01 |
申请人 |
HUREL-DUBOIS CONST AVIONS |
发明人 |
KENNEDY, JOHN F.;FOURNIER, ALAIN |
分类号 |
F02K1/56;F02K1/70;F02K1/72;(IPC1-7):B64C15/00;F02K3/06 |
主分类号 |
F02K1/56 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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