发明名称 |
Beam mounted rear propulsion system for an aircraft and aircraft with such system |
摘要 |
A propulsive system for an aircraft including an auxiliary jet engine is integrated into a tail cone of a fuselage. A carrying structure of the jet engine is primarily formed with beams and frames or half-frames to which the auxiliary jet engine is fixed by lateral beams. The beams are interdependent of the frames and half-frames, and the beams are overhanging behind a frame behind which is fixed the engine. Each beam includes a lower half-beam and a higher half-beam, separated on at least a part of its length ahead from attachments of the jet engine to determine a space free of structure impediment for lateral air intakes. |
申请公布号 |
US8220739(B2) |
申请公布日期 |
2012.07.17 |
申请号 |
US20090393625 |
申请日期 |
2009.02.26 |
申请人 |
CAZALS OLIVIER;AIRBUS OPERATIONS SAS |
发明人 |
CAZALS OLIVIER |
分类号 |
B64D27/02;B64D29/00;B64D41/00 |
主分类号 |
B64D27/02 |
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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