公开(公告)号：US10427797B2

公开(公告)日：2019-10-01

申请号：US15541258

申请日：2017-01-20

申请人： Honeywell International Inc. ,  Dinkar Mylaraswamy ,  C. Arthur Dins ,  Qixiang Li ,  Eric Blumer ,  Garry H Lee ,  Henry Claeys ,  Michael Easley

发明人： Dinkar Mylaraswamy ,  C. Arthur Dins ,  Qixiang Li ,  Eric Blumer ,  Garry H Lee ,  Henry Claeys ,  Michael Easley

IPC分类号： B64D13/08 ,  B64D13/06

摘要： In one embodiment, a method is provided. The method comprises: receiving, in a vehicle, at least one pollution parameter; and adjusting at least one fluid flow regulating mechanism position, to regulate an intake of pollutants into an environmental control system of the vehicle, based upon the at least one pollution parameter.

公开(公告)号：US20070113579A1

公开(公告)日：2007-05-24

申请号：US11192970

申请日：2005-07-29

申请人： Henry Claeys ,  Katherine Clarke ,  David Elpern

发明人： Henry Claeys ,  Katherine Clarke ,  David Elpern

IPC分类号： F25D9/00

CPC分类号： F25B9/004 ,  B64D13/02 ,  B64D13/06 ,  B64D2013/0618 ,  B64D2013/064 ,  B64D2013/0644 ,  Y02T50/44 ,  Y02T50/56

摘要： An environmental control system for an aircraft cabin includes a plurality of electrically-driven ported shroud cabin air compressors, each cabin air compressor compressing ram air received from the aircraft exterior, a heat exchange circuit comprising a primary heat exchanger receiving airflow from at least one of the cabin air compressors, and the secondary heat exchanger supplying airflow to the aircraft cabin, and an air cycle machine comprising a compressor adapted to receive airflow from the primary heat exchanger and supply compressed air to the secondary heat exchanger. The environmental control system may further comprise an air recirculation system, having an aft recirculation fan adapted to receive a portion of recirculation air from the aircraft cabin, and a recirculation heat exchanger, disposed in the heat exchange circuit in series with the primary and secondary heat exchangers, and adapted to receive airflow from the aft recirculation fan.

摘要翻译： 一种用于飞机机舱的环境控制系统包括多个电驱动的端面式护罩舱空气压缩机，每个机舱空气压缩机压缩从飞行器外部接收的冲压空气;热交换电路，包括主热交换器，其接收来自以下各项中的至少一个的气流： 机舱空气压缩机和向飞机机舱供应气流的二次热交换器，以及包括压缩机的空气循环机，所述压缩机适于接收来自主热交换器的气流并将压缩空气供应到二次热交换器。 环境控制系统还可以包括空气再循环系统，其具有适于接收来自飞机机舱的一部分再循环空气的后再循环风扇，以及再循环热交换器，其设置在与第一和第二热量串联的热交换回路中 交换器，并且适于接收来自后再循环风扇的气流。

公开(公告)号：US11202987B2

公开(公告)日：2021-12-21

申请号：US16164461

申请日：2018-10-18

申请人： Honeywell International Inc.

发明人： Phoebe Henson ,  Stephen Yates ,  Henry Claeys ,  David Loeffelholz

IPC分类号： B01D53/26 ,  C07C1/12 ,  F04B37/12 ,  F04B39/06 ,  B01D5/00 ,  B01D53/00

摘要： A gas compression system includes a system inlet to receive a gas stream containing a first component and a second component, a vapor system outlet to discharge the gas stream, and a plurality of compression stages coupled in series between the system inlet and the vapor system outlet. Each of the plurality of compression stages includes a compressor, a condenser coupled to the compressor, and a gravity-independent phase separator coupled to the condenser. The compressor is configured to receive the gas stream from either the system inlet or another of the plurality of compression stages and compress the gas stream. The condenser is configured to condense the second component from the gas stream. The gravity-independent phase separator is configured to remove the second component from the gas stream and discharge the gas stream to either the system outlet or another of the plurality of compression stages.