| 发明名称 |
Aircraft engine mounting assembly |
| 摘要 |
A mounting assembly ( 10 ) for mounting a gas turbine engine on an aircraft. The assembly ( 10 ) comprising four equispaced hydraulic piston and cylinder thrust links ( 16 ) connecting between the engine fan case ( 12 ) and the air intake ( 14 ), which intake ( 14 ) is mounted to the airframe.
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| 申请公布号 |
US7296414(B2) |
申请公布日期 |
2007.11.20 |
| 申请号 |
US20040954277 |
申请日期 |
2004.10.01 |
| 申请人 |
ROLLS-ROYCE PLC |
发明人 |
STRETTON RICHARD G;BEARDSLEY PETER K;BEAVEN DAVID M |
| 分类号 |
B64D27/00;B64D27/16;B64D27/26;F02K3/02 |
主分类号 |
B64D27/00 |
| 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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