发明名称 |
DEVICE FOR SUPPLYING AIR TO AN AUXILIARY POWER UNIT OF AN AIRCRAFT AND AIRCRAFT |
摘要 |
A device for supplying air to an auxiliary power unit for aircraft, including the auxiliary power unit; a turbocharger, and a cabin, the auxiliary power unit including a diesel engine coupled to the turbocharger in such a way that: the turbocharger includes a first air inlet in a compressor of the turbocharger coming from the cabin for its intake into a combustion chamber of the diesel engine, the diesel engine including: a first outlet carrying the air burnt by the combustion chamber to the turbocharger, the diesel engine delivering a power making it possible to supply an electric alternator and pressurising compressor, intended to pressurise a second air inlet, wherein the first air inlet is supplied by a fraction of pressurised air from the cabin of an aircraft. |
申请公布号 |
EP2814738(A2) |
申请公布日期 |
2014.12.24 |
申请号 |
EP20130711073 |
申请日期 |
2013.02.12 |
申请人 |
SOCIETE DE MOTORISATIONS AERONAUTIQUES |
发明人 |
JOUBERT, HUGUES DENIS;FERRARI, SÉBASTIEN |
分类号 |
B64D41/00;B64D13/00;B64D13/06;B64D27/08;B64D33/02 |
主分类号 |
B64D41/00 |
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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