公开(公告)号：US20150090120A1

公开(公告)日：2015-04-02

申请号：US14042883

申请日：2013-10-01

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Henry Au ,  Dennis M. Morita ,  Daniel R. Robles ,  Hal J. Strumpf

IPC: B03C3/017 ,  B01D45/12

CPC classification number: B03C9/00 ,  B01D45/12

Abstract: An Environmental Control System may use an electronic particle separation system to control humidity in an aircraft. The electronic particle separation system may include a charging stage and a collecting stage. The charging stage may charge airflow passing through to repel liquid particles away from the airflow. Liquid droplets may be collected by the collecting stage and centrifugally flung toward a periphery of a separator. The liquid particles may be collected outside of the airflow which may be allowed to pass through the separator and out to a destination in the aircraft without the collected liquid.

Abstract translation: 环境控制系统可以使用电子粒子分离系统来控制飞机中的湿度。 电子粒子分离系统可以包括充电阶段和收集阶段。 充电阶段可以对通过的气流进行充电以排除液体颗粒远离气流。 液滴可以通过收集阶段收集并离心地朝向分离器的周边方向倾倒。 液体颗粒可以被收集在可被允许通过分离器的空气流的外部，并且在没有收集的液体的情况下出来到飞机的目的地。

公开(公告)号：US20240318883A1

公开(公告)日：2024-09-26

申请号：US18188220

申请日：2023-03-22

Applicant: Honeywell International Inc.

Inventor： Sung-Han Jung ,  Siamak Nikbin ,  Daniel R. Robles

IPC: F25B49/02 ,  B64D13/08 ,  F25B5/02 ,  F25B40/02 ,  F25B40/04 ,  F25B41/385 ,  F25B43/00

CPC classification number: F25B49/022 ,  B64D13/08 ,  F25B5/02 ,  F25B40/02 ,  F25B40/04 ,  F25B41/385 ,  F25B43/003 ,  B64D2013/064 ,  F25B2400/06 ,  F25B2600/0253

Abstract: A vapor cycle cooling system includes first and second compressor systems in parallel with one another, each compressor system including a motor, a motor controller, and a first compressor in series with a second compressor; a condenser fluidically coupled to each compressor system; a filter drier, in series with, and fluidically coupled to the condenser; a first expansion device in series with, and fluidically coupled to, a flash heat exchanger, the flash heat exchanger fluidically coupled to a second expansion device, the second expansion device fluidically coupled to a first evaporator, the first evaporator fluidically coupled to each compressor system; a system controller electrically coupled to each motor controller; and a motor and motor controller cooling loop fluidically coupled to the filter drier and each motor, wherein the vapor cycle cooling system is configured to cool one or more thermal loads for a vehicle.

公开(公告)号：US20170057641A1

公开(公告)日：2017-03-02

申请号：US14991155

申请日：2016-01-08

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Mike Koerner ,  Allen MacKnight ,  Siamak Nikbin ,  Myron Quan ,  Daniel R. Robles

IPC: B64D13/06 ,  B64D37/34

CPC classification number: B64D13/06 ,  B64D13/08 ,  B64D37/34 ,  B64D2013/0618 ,  B64D2013/064 ,  B64D2013/0648 ,  B64D2013/0659 ,  B64D2013/0674 ,  F25B25/005 ,  Y02T50/56

Abstract: A cooling system in which an ACS (air cycle system) turbine may be driven by high pressure air from a turbo-fan engine and a VCS (vapor cycle system) having an evaporator and a VCS refrigerant compressor may be driven by the ACS turbine. Fluid of the chilled fluid reservoir, which may be chilled fuel, may be circulated through and cooled in the evaporator. In some embodiments, the ACS turbine may be coupled to the VCS refrigerant compressor by a magnetic coupling.

Abstract translation: 可以由ACS涡轮机驱动ACS（空气循环系统）涡轮机可以由来自涡轮风扇发动机的高压空气和具有蒸发器和VCS制冷剂压缩机的VCS（蒸气循环系统）驱动的冷却系统。 可以将冷冻燃料的冷却液储存器的流体循环通过并在蒸发器中冷却。 在一些实施例中，ACS涡轮可以通过磁耦合联接到VCS制冷剂压缩机。

公开(公告)号：US20150090114A1

公开(公告)日：2015-04-02

申请号：US14042926

申请日：2013-10-01

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Henry Au ,  Hal J. Strumpf ,  Dennis M. Morita ,  Daniel R. Robles

IPC: B03C3/34

CPC classification number: B03C3/34 ,  B03C3/68 ,  B03C9/00 ,  B03C2201/24

Abstract: An Environmental Control System may use an electronic particle separation system to control humidity in an aircraft. The electronic particle separation system may include a particle separator, a sensor module, and a controller configured to receive signals from the sensor module, and operate the particle separator based on the received sensor signals. In some embodiments, the controller may include a processor which may determine whether the particle separator is being operated under an ozone related condition exceeding a threshold operating condition. If one of the threshold operating conditions is exceeded, the particle separator may be turned off which may control the amount of ozone present in the aircraft.

Abstract translation: 环境控制系统可以使用电子粒子分离系统来控制飞机中的湿度。 电子粒子分离系统可以包括粒子分离器，传感器模块和被配置为从传感器模块接收信号的控制器，并且基于接收到的传感器信号来操作粒子分离器。 在一些实施例中，控制器可以包括处理器，其可以确定颗粒分离器是否在超过阈值操作条件的臭氧相关状况下操作。 如果超过阈值操作条件之一，则可以关闭颗粒分离器，其可以控制飞行器中存在的臭氧的量。

公开(公告)号：US09427746B2

公开(公告)日：2016-08-30

申请号：US14042926

申请日：2013-10-01

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Henry Au ,  Hal J. Strumpf ,  Dennis M. Morita ,  Daniel R. Robles

IPC: B01D46/46 ,  B01D53/30 ,  B03C3/34 ,  B03C3/68 ,  B03C9/00

CPC classification number: B03C3/34 ,  B03C3/68 ,  B03C9/00 ,  B03C2201/24

Abstract: An Environmental Control System may use an electronic particle separation system to control humidity in an aircraft. The electronic particle separation system may include a particle separator, a sensor module, and a controller configured to receive signals from the sensor module, and operate the particle separator based on the received sensor signals. In some embodiments, the controller may include a processor which may determine whether the particle separator is being operated under an ozone related condition exceeding a threshold operating condition. If one of the threshold operating conditions is exceeded, the particle separator may be turned off which may control the amount of ozone present in the aircraft.

Abstract translation: 环境控制系统可以使用电子粒子分离系统来控制飞机中的湿度。 电子粒子分离系统可以包括粒子分离器，传感器模块和被配置为从传感器模块接收信号的控制器，并且基于接收到的传感器信号来操作粒子分离器。 在一些实施例中，控制器可以包括处理器，其可以确定颗粒分离器是否在超过阈值操作条件的臭氧相关状况下操作。 如果超过阈值操作条件之一，则可以关闭颗粒分离器，其可以控制飞行器中存在的臭氧的量。

公开(公告)号：US09199248B2

公开(公告)日：2015-12-01

申请号：US14042883

申请日：2013-10-01

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Henry Au ,  Dennis M. Morita ,  Daniel R. Robles ,  Hal J. Strumpf

IPC: B03C3/00 ,  B03C9/00 ,  B01D45/12

CPC classification number: B03C9/00 ,  B01D45/12

Abstract: An Environmental Control System may use an electronic particle separation system to control humidity in an aircraft. The electronic particle separation system may include a charging stage and a collecting stage. The charging stage may charge airflow passing through to repel liquid particles away from the airflow. Liquid droplets may be collected by the collecting stage and centrifugally flung toward a periphery of a separator. The liquid particles may be collected outside of the airflow which may be allowed to pass through the separator and out to a destination in the aircraft without the collected liquid.

Abstract translation: 环境控制系统可以使用电子粒子分离系统来控制飞机中的湿度。 电子粒子分离系统可以包括充电阶段和收集阶段。 充电阶段可以对通过的气流进行充电以排除液体颗粒远离气流。 液滴可以通过收集阶段收集并离心地朝向分离器的周边方向倾倒。 液体颗粒可以被收集在可被允许通过分离器的空气流的外部，并且在没有收集的液体的情况下出来到飞机的目的地。