发明名称 Aircraft environmental control system and method
摘要 An environmental control system including a turbomachine assembly having a shaft, motor, turbine and compressor, the compressor outputting a compressed air stream, a first valve that splits the compressed air stream into first and second compressed air streams, a heat exchanger to cool the first compressed air stream and output a cooled air stream, a second valve positioned to receive the cooled air stream and split the cooled air stream into first and second cooled air streams, wherein the first cooled stream is expanded in the turbine to produce an expanded air stream that is combined with the second compressed air stream and the second cooled air stream to provide a combined air stream having a temperature and a flow rate, and a controller that communicates control signals to the compressor, motor and first and second valves to control the temperature and flow rate of the combined air stream.
申请公布号 US9016075(B1) 申请公布日期 2015.04.28
申请号 US201213343059 申请日期 2012.01.04
申请人 The Boeing Company 发明人 Johnson Andrew T.
分类号 F25B1/00;F25B9/06 主分类号 F25B1/00
代理机构 Walters & Wasylyna LLC 代理人 Walters & Wasylyna LLC
主权项 1. An environmental control method comprising the steps of: providing a turbomachine assembly comprising a compressor, a motor and a turbine, wherein said compressor has a variable compressor geometry and is driven by a shaft, said motor and said turbine being coupled to said shaft; obtaining an input air stream; passing said input air stream through said compressor to obtain a compressed air stream; using a first valve to split said compressed air stream into a first compressed air stream and a second compressed air stream; cooling said first compressed air stream to obtain a cooled air stream; using a second valve to split said cooled air stream into a first cooled air stream and a second cooled air stream; passing said first cooled air stream through said turbine to obtain a turbine output stream; combining said turbine output stream with said second cooled air stream and said second compressed air stream to obtain a combined air stream, said combined air stream having a temperature and a flow rate; and controlling said compressor geometry, said motor, said first valve and said second valve to minimize a first difference between said temperature and a target temperature and a second difference between said flow rate and a target flow rate.
地址 Chicago IL US