发明名称 |
Bypass turbojet thrust reverser having doors with integrally stiffened external structure |
摘要 |
The turbojet thrust reverser comprises pivoting doors which when closed are integral with the external wall of the pipe for the flow behind the turbojet. They are each able to pivot under the action of a control (8) so as to constitute flow diversion obstacles. The door has an external structure formed by a panel (23) and an internal structure (22) connected by a local structural zone (25). The remainder of the external structure is independent from the internal structure. A lock (27) holds the door in the closed position and sealing joints (5) edging the door are integral with the internal structure. |
申请公布号 |
AU6922698(A) |
申请公布日期 |
1998.09.29 |
申请号 |
AU19980069226 |
申请日期 |
1998.03.12 |
申请人 |
HISPANO-SUIZA AEROSTRUCTURES |
发明人 |
PATRICK GONIDEC;PASCAL ROUYER;GUY BERNARD VAUCHEL |
分类号 |
B64D33/00;F02K1/70 |
主分类号 |
B64D33/00 |
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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