发明名称 Electric power generating device for aircraft, has conversion units including hydraulic motors, gear boxes and constant speed electric generators for converting hydraulic power into mechanical energy and into electric power
摘要 <p>The device has transformation units including hydraulic pumps (37d, 37g) for transforming mechanical energy of turbojet engines (4d, 4g) into hydraulic power. Transfer units include hydraulic lines (38d, 38g), return lines (40d, 40g), hydraulic fluid tanks (41d, 41g) and main return lines (42d, 42g) for transferring the hydraulic power away from a propulsive unit. Conversion units include hydraulic motors (39d, 39g), gear boxes (44d, 44g) and constant speed electric generators (23d, 23g) for converting the hydraulic power into the mechanical energy and into electric power.</p>
申请公布号 FR2944260(A1) 申请公布日期 2010.10.15
申请号 FR20090052438 申请日期 2009.04.14
申请人 AIRBUS FRANCE 发明人 BULIN GUILLAUME;ABRIAL PHILIPPE;DELMAS ERIC
分类号 B64D41/00 主分类号 B64D41/00
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