发明名称 BLEED AIR SYSTEMS FOR USE WITH AIRCRAFT AND RELATED METHODS
摘要 Bleed air systems for use with aircraft and related methods are disclosed. An example apparatus includes a compressor having a compressor inlet, a compressor outlet, and a first drive shaft. The compressor outlet is to be fluidly coupled to a system of an aircraft that receives pressurized air, and the compressor inlet is to receive bleed air from a low-pressure compressor of an engine of the aircraft. The example apparatus includes a gearbox operatively coupled to the first drive shaft to drive the compressor. The gearbox is to be operatively coupled to and powered by a second drive shaft extending from the engine. The example apparatus also includes a clutch disposed between the first drive shaft and the gearbox to selectively disconnect the first drive shaft from the gearbox.
申请公布号 US2015275769(A1) 申请公布日期 2015.10.01
申请号 US201414242570 申请日期 2014.04.01
申请人 The Boeing Company 发明人 Foutch David W.;Mackin Steve G.
分类号 F02C9/18;F02C7/32;F02C7/047;F02C7/27;F02K3/02;F02C3/10 主分类号 F02C9/18
代理机构 代理人
主权项 1. An apparatus comprising: a compressor having a compressor inlet, a compressor outlet, and a first drive shaft, the compressor outlet to be fluidly coupled to a system of an aircraft that receives pressurized air, the compressor inlet to receive bleed air from a low-pressure compressor of an engine of the aircraft; a gearbox operatively coupled to the first drive shaft to drive the compressor, the gearbox operatively coupled to and powered by a second drive shaft extending from the engine; and a clutch disposed between the first drive shaft and the gearbox to selectively disconnect the first drive shaft from the gearbox.
地址 Chicago IL US