AIRCRAFT ELECTRONIC PARTICLE SEPARATION SYSTEM
    1.
    发明申请
    AIRCRAFT ELECTRONIC PARTICLE SEPARATION SYSTEM 有权
    飞机电子颗粒分离系统

    公开(公告)号:US20150090120A1

    公开(公告)日:2015-04-02

    申请号:US14042883

    申请日:2013-10-01

    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。

    SELF-CONTAINED AIRCRAFT ELECTRONIC AIR TREATMENT SYSTEM
    2.
    发明申请
    SELF-CONTAINED AIRCRAFT ELECTRONIC AIR TREATMENT SYSTEM 有权
    自含飞机电子空气处理系统

    公开(公告)号:US20150090119A1

    公开(公告)日:2015-04-02

    申请号:US14042936

    申请日:2013-10-01

    Abstract: An Environmental Control System may use an electronic air treatment system to control humidity in an aircraft. The electronic air treatment system may use an electronic charging system and a separation system. A turbine rotor may drive a power generating stage to provide high voltage power to the electronic charging system. The charging stage may charge airflow passing through to repel liquid particles away from the airflow. Liquid droplets may be collected and centrifugally flung toward a periphery of the separation system. The liquid particles may be collected outside of the airflow, which may be allowed to pass through the separation system 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空气处理系统来控制飞机中的湿度。 电子空气处理系统可以使用电子充电系统和分离系统。 涡轮转子可以驱动发电级以向电子充电系统提供高压电力。 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。 液滴可以被收集并离心地朝着分离系统的周边方向倾倒。 液体颗粒可以被收集在空气流的外部,这可以被允许通过分离系统并且出来到没有收集液体的飞行器的目的地。

    AIRCRAFT ELECTROSTATIC PARTICLE SEPARATION CONTROL SYSTEM
    3.
    发明申请
    AIRCRAFT ELECTROSTATIC PARTICLE SEPARATION CONTROL SYSTEM 有权
    飞机静电颗粒分离控制系统

    公开(公告)号:US20150090114A1

    公开(公告)日:2015-04-02

    申请号:US14042926

    申请日:2013-10-01

    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。

    Aircraft electrostatic particle separation control system
    4.
    发明授权
    Aircraft electrostatic particle separation control system 有权
    飞机静电颗粒分离控制系统

    公开(公告)号:US09427746B2

    公开(公告)日:2016-08-30

    申请号:US14042926

    申请日:2013-10-01

    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。

    Aircraft electronic particle separation system
    5.
    发明授权
    Aircraft electronic particle separation system 有权
    飞机电子粒子分离系统

    公开(公告)号:US09199248B2

    公开(公告)日:2015-12-01

    申请号:US14042883

    申请日:2013-10-01

    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。

    Adjustable sensor or sensor network to selectively enhance identification of select chemical species

    公开(公告)号:US10329022B2

    公开(公告)日:2019-06-25

    申请号:US15339405

    申请日:2016-10-31

    Abstract: An environmental control system (ECS) having contaminants in supply air that flows into an environment includes an outside air contaminant component that senses contaminants in outside air, wherein the outside air contaminant component is upstream of the environment, A recirculated air contaminant component is provided and that senses contaminants in recirculated air supplied by the environment, wherein the recirculated air contaminant component is downstream of the environment. A voltage supply provides a non-linear variable voltage to at least one of the components. A controller is in communication with the components and the voltage supply; wherein, upon a measured resistance, from at least one of the components, that exceeds a threshold, the controller varies at least one of an outside air flow and a recirculated air flow in the ECS.

    Self-contained aircraft electronic air treatment system
    8.
    发明授权
    Self-contained aircraft electronic air treatment system 有权
    独立飞机电子空气处理系统

    公开(公告)号:US09216827B2

    公开(公告)日:2015-12-22

    申请号:US14042936

    申请日:2013-10-01

    Abstract: An Environmental Control System may use an electronic air treatment system to control humidity in an aircraft. The electronic air treatment system may use an electronic charging system and a separation system. A turbine rotor may drive a power generating stage to provide high voltage power to the electronic charging system. The charging stage may charge airflow passing through to repel liquid particles away from the airflow. Liquid droplets may be collected and centrifugally flung toward a periphery of the separation system. The liquid particles may be collected outside of the airflow, which may be allowed to pass through the separation system 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空气处理系统来控制飞机中的湿度。 电子空气处理系统可以使用电子充电系统和分离系统。 涡轮转子可以驱动发电级以向电子充电系统提供高压电力。 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。 液滴可以被收集并离心地朝着分离系统的周边方向倾倒。 液体颗粒可以被收集在空气流的外部,这可以被允许通过分离系统并且出来到没有收集液体的飞行器的目的地。

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