| 发明名称 |
AIRCRAFT POWER ASSEMBLY AND AIRCRAFT PROVIDED WITH SUCH AN ASSEMBLY |
| 摘要 |
<p>An aircraft propulsion system comprising two uncoupled separately operable turboprop gas turbine engines (1, 2), the rotary axes (5, 7) of which are inclined to each other in a horizontal and/or vertical plane and each of which is connected by a drive shaft to a compound gearbox (6) which drives a pair of coaxial contra-rotating airscrew shafts (11, 13).</p> |
| 申请公布号 |
WO2005044662(A1) |
申请公布日期 |
2005.05.19 |
| 申请号 |
WO2004GB04584 |
申请日期 |
2004.10.29 |
| 申请人 |
ADVANCED CREATIVE ENGINEERING LTD.;AYERS, RONALD, FREDERICK |
发明人 |
AYERS, RONALD, FREDERICK |
| 分类号 |
B64C11/48;B64D35/06;B64D35/08;(IPC1-7):B64D35/08 |
主分类号 |
B64C11/48 |
| 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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