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公开(公告)号：EP3517439A1
公开(公告)日：2019-07-31
申请号：EP19150703.7
申请日：2019-01-08
摘要： An environmental control system of an aircraft with a power turbine includes a heat exchanger (12) and a plenum (28) attached to and in fluid communication with the heat exchanger (12). The plenum (28) includes a housing (108) with a first inlet (110) fluidly connected to the power turbine, a second inlet (112) fluidly connected to a source of ram air, and an outlet (114) fluidly connected to the heat exchanger (12).
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公开(公告)号：EP2837563A2
公开(公告)日：2015-02-18
申请号：EP14174067.0
申请日：2014-06-26
IPC分类号： B64D13/06
CPC分类号： F04F5/14 , B64D13/06 , B64D2013/0644 , B64D2013/0685 , F04F5/18 , F04F7/00 , Y02T50/56
摘要： An Environmental Control System (ECS) 10 for an aircraft includes a ram air system having a ram inlet 12 and a ram outlet 28. The ECS includes a cabin air compressor motor, a diverter valve 20, and a dedicated outlet 60. The cabin air compressor motor has a motor inlet passage and a motor outlet passage with the motor inlet passage being coupled to the ram inlet. The diverter valve includes a first diverter inlet, a first diverter outlet, and a second diverter outlet. The first diverter inlet is coupled to the motor outlet passage, The dedicated outlet 60 is connected to the first diverter outlet in a flight mode of operation of the aircraft and the ram outlet 28 is connected to the second diverter outlet in a ground mode of operation of the aircraft.
摘要翻译： 用于飞行器的环境控制系统（ECS）10包括具有冲头入口12和冲头出口28的冲压空气系统.ECS包括机舱空气压缩机马达，转向阀20和专用出口60.机舱空气 压缩机马达具有马达入口通道和马达出口通道，马达入口通道联接到冲头入口。 分流阀包括第一分流器入口，第一分流器出口和第二分流器出口。 第一分流器入口联接到电动机出口通道。专用出口60以飞行器的飞行操作模式连接到第一分流器出口，并且压头出口28以地面操作模式连接到第二转向器出口 的飞机。
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公开(公告)号：EP4186579A1
公开(公告)日：2023-05-31
申请号：EP22210011.7
申请日：2022-11-28
摘要： A water extractor for use in an environmental control system, the water extractor comprising a housing (34) having an inlet end and an outlet end, a swirling mechanism (46) mounted within the housing (34), and a fog harvester assembly (50) mounted within the housing (34) at a location between the inlet end and the outlet end.
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公开(公告)号：EP4112473A1
公开(公告)日：2023-01-04
申请号：EP22181667.1
申请日：2022-06-28
发明人： ARMY, Donald E. , McCord, Patrick
摘要： A water extractor (60) for an environmental control system of an aircraft includes a separation mechanism (70) configured to divide an airflow into a first airflow and a second airflow. The separation mechanism (70) includes an inlet conduit (84), a body (74) in fluid communication with the inlet conduit, and at least one coalescing feature arranged within an interior of the body (74). A water extraction vessel (72) is arranged in fluid communication with the separation mechanism (70). The water extraction vessel (72) includes a first portion for receiving the first airflow and a second portion for receiving the second airflow. The first portion is configured to collect and remove water from the first airflow.
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公开(公告)号：EP2837563B1
公开(公告)日：2017-08-02
申请号：EP14174067.0
申请日：2014-06-26
IPC分类号： B64D13/06
CPC分类号： F04F5/14 , B64D13/06 , B64D2013/0644 , B64D2013/0685 , F04F5/18 , F04F7/00 , Y02T50/56
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公开(公告)号：EP2837563A3
公开(公告)日：2015-10-28
申请号：EP14174067.0
申请日：2014-06-26
IPC分类号： B64D13/06
CPC分类号： F04F5/14 , B64D13/06 , B64D2013/0644 , B64D2013/0685 , F04F5/18 , F04F7/00 , Y02T50/56
摘要： An Environmental Control System (ECS) 10 for an aircraft includes a ram air system having a ram inlet 12 and a ram outlet 28. The ECS includes a cabin air compressor motor, a diverter valve 20, and a dedicated outlet 60. The cabin air compressor motor has a motor inlet passage and a motor outlet passage with the motor inlet passage being coupled to the ram inlet. The diverter valve includes a first diverter inlet, a first diverter outlet, and a second diverter outlet. The first diverter inlet is coupled to the motor outlet passage, The dedicated outlet 60 is connected to the first diverter outlet in a flight mode of operation of the aircraft and the ram outlet 28 is connected to the second diverter outlet in a ground mode of operation of the aircraft.
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