发明名称 |
Turbojet-engine thrust reverser with internal clamshells |
摘要 |
A turbojet-engine thrust reverser comprises a displaceable sub-assembly including two internal clamshells (12) mounted on stationary pivots (18) of a stationary structure (1) and an annular, axially displaceable structure (11). The displaceable structure forms the external, downstream part (13) of a cowling. In the forward-thrust mode, the displaceable structure forms a downstream portion (15) of a radial outer wall of the flow path and forms the entire trailing edge by covering the clamshells (12) such that the clamshells form part of the radial outer wall of the flow path.
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申请公布号 |
US6151885(A) |
申请公布日期 |
2000.11.28 |
申请号 |
US19980159549 |
申请日期 |
1998.09.24 |
申请人 |
SOCIETE HISPANO SUIZA AEROSTRUCTURES |
发明人 |
METEZEAU, FABRICE HENRI EMILE;VAUCHEL, BERNARD GUY |
分类号 |
F02K1/32;F02K1/60;(IPC1-7):F02K1/60 |
主分类号 |
F02K1/32 |
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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