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An integrated auxiliary power unit and environmental control unit for an airplane 2, said integrated unit 2 comprising a prime mover 4, a variable geometry compressor 22 operable selectably by bleed air from the propulsion engine of said airplane or connectable via an overrunning clutch 18 to said p

An integrated auxiliary power unit and environmental control unit for an airplane 2, said integrated unit 2 comprising a prime mover 4, a variable geometry compressor 22 operable selectably by bleed air from the propulsion engine of said airplane or connectable via an overrunning clutch 18 to said prime mover, a controlled emission turbine 24 which is shaft-coupled to said compressor 22 and cooperating with said compressor to form an environmental control unit, and means for diverting a portion of the output of said compressor for use as an auxiliary power unit.

대표청구항 ▼

An integrated environmental control and auxiliary power unit for a vehicle having a propulsion engine, said unit comprising: a prime mover; a variable geometry compressor including a diffuser having a plurality of controllable variable exit vanes; means for positioning said variable exit vanes to co

An integrated environmental control and auxiliary power unit for a vehicle having a propulsion engine, said unit comprising: a prime mover; a variable geometry compressor including a diffuser having a plurality of controllable variable exit vanes; means for positioning said variable exit vanes to control the output flow of said compressor; an overrunning clutch operable to couple said prime mover to drive said compressor; means for supplying bleed air from said propulsion engine to drive said compressor when said prime mover is not running; a controlled emission turbine coupled to said compressor by a common drive shaft; means for blocking a selectable portion of the flow supplied to said turbine to match the flow from said compressor to maintain near constant pressure to said turbine over a wide flow operating range; and means for independently utilizing the output flow from said compressor and from said turbine.