Liquid level sensing systems
    1.
    发明授权
    Liquid level sensing systems 有权
    液位传感系统

    公开(公告)号:US09574928B2

    公开(公告)日:2017-02-21

    申请号:US14318181

    申请日:2014-06-27

    CPC classification number: G01F23/268

    Abstract: A liquid level sensing system includes a vessel and an electrode. The vessel includes a vessel wall separating a vessel interior from a vessel exterior. The electrode is mounted to an exterior side of the vessel wall spanning a distance corresponding to a desired-level-determining range. The vessel wall is a dielectric gap between the electrode and the vessel interior. The electrode is configured to collect a charge corresponding to a liquid level. A method for determining a liquid level in a vessel includes collecting a charge on an electrode, sensing the collected charge on the electrode with a capacitance sensor through an electrical line, and determining a liquid level in a vessel based on the collected charge sensed by the capacitance sensor.

    Abstract translation: 液位感测系统包括容器和电极。 该容器包括将容器内部与容器外部分开的容器壁。 电极安装到血管壁的外侧,跨越对应于期望水平确定范围的距离。 血管壁是电极和血管内部之间的电介质间隙。 电极被配置为收集对应于液位的电荷。 用于确定容器中的液位的方法包括:在电极上收集电荷,通过电线检测电容传感器在电极上收集的电荷,并且基于由所述电容感测的所收集的电荷来确定容器中的液位 电容传感器

    Vacuum breaker with back flow preventer

    公开(公告)号:US10889967B2

    公开(公告)日:2021-01-12

    申请号:US16413270

    申请日:2019-05-15

    Abstract: A dual purpose valve assembly may comprise a conduit, a first valve, and a second valve. The first valve may comprise a vacuum breaker valve. The second valve may comprise a check valve. A drain system may comprise a supply tube, a drain tube, and a dual purpose valve disposed between the supply tube and the drain tube. The drain system may allow fluid to drain based on gravity alone, and the dual purpose valve assembly may operate based on gravity alone.

    LIQUID LEVEL SENSING SYSTEMS
    4.
    发明申请
    LIQUID LEVEL SENSING SYSTEMS 有权
    液位感测系统

    公开(公告)号:US20140305202A1

    公开(公告)日:2014-10-16

    申请号:US14318181

    申请日:2014-06-27

    CPC classification number: G01F23/268

    Abstract: A liquid level sensing system includes a vessel and an electrode. The vessel includes a vessel wall separating a vessel interior from a vessel exterior. The electrode is mounted to an exterior side of the vessel wall spanning a distance corresponding to a desired-level-determining range. The vessel wall is a dielectric gap between the electrode and the vessel interior. The electrode is configured to collect a charge corresponding to a liquid level. A method for determining a liquid level in a vessel includes collecting a charge on an electrode, sensing the collected charge on the electrode with a capacitance sensor through an electrical line, and determining a liquid level in a vessel based on the collected charge sensed by the capacitance sensor.

    Abstract translation: 液位感测系统包括容器和电极。 该容器包括将容器内部与容器外部分开的容器壁。 电极安装到血管壁的外侧,跨越对应于期望水平确定范围的距离。 血管壁是电极和血管内部之间的电介质间隙。 电极被配置成收集与液位对应的电荷。 用于确定容器中的液位的方法包括:在电极上收集电荷,通过电线检测电容传感器在电极上收集的电荷,并且基于由所述电容感测的所收集的电荷来确定容器中的液位 电容传感器

    Hybrid water storage system for aircraft

    公开(公告)号:US12172755B2

    公开(公告)日:2024-12-24

    申请号:US18487943

    申请日:2023-10-16

    Abstract: A hybrid water storage system for an aircraft includes separate variable volumes for respectively storing/holding potable water and gray water occupying a common container. The hybrid water storage system is generally configured to draw potable water from a first variable volume in order to provide fresh water to one or more aircraft appliances (e.g., sinks, showers, ice-makers, etc.), and the used potable water (i.e., the potable water that is collected in drains from the aircraft appliances), referred to herein as gray water, is routed to a second variable volume that occupies the same container as the first variable volume.

    Hybrid Water Storage System for Aircraft
    6.
    发明公开

    公开(公告)号:US20240043120A1

    公开(公告)日:2024-02-08

    申请号:US18487943

    申请日:2023-10-16

    CPC classification number: B64D11/02 B64D11/0007 Y10T137/6906

    Abstract: A hybrid water storage system for an aircraft includes separate variable volumes for respectively storing/holding potable water and gray water occupying a common container. The hybrid water storage system is generally configured to draw potable water from a first variable volume in order to provide fresh water to one or more aircraft appliances (e.g., sinks, showers, ice-makers, etc.), and the used potable water (i.e., the potable water that is collected in drains from the aircraft appliances), referred to herein as gray water, is routed to a second variable volume that occupies the same container as the first variable volume.

    Hybrid water storage system for aircraft

    公开(公告)号:US11820513B2

    公开(公告)日:2023-11-21

    申请号:US17181029

    申请日:2021-02-22

    CPC classification number: B64D11/02 B64D11/0007 Y10T137/6906

    Abstract: A hybrid water storage system for an aircraft includes separate variable volumes for respectively storing/holding potable water and gray water occupying a common container. The hybrid water storage system is generally configured to draw potable water from a first variable volume in order to provide fresh water to one or more aircraft appliances (e.g., sinks, showers, ice-makers, etc.), and the used potable water (i.e., the potable water that is collected in drains from the aircraft appliances), referred to herein as gray water, is routed to a second variable volume that occupies the same container as the first variable volume.

    Hybrid Water Storage System for Aircraft

    公开(公告)号:US20210323674A1

    公开(公告)日:2021-10-21

    申请号:US17181029

    申请日:2021-02-22

    Abstract: A hybrid water storage system for an aircraft includes separate variable volumes for respectively storing/holding potable water and gray water occupying a common container. The hybrid water storage system is generally configured to draw potable water from a first variable volume in order to provide fresh water to one or more aircraft appliances (e.g., sinks, showers, ice-makers, etc.), and the used potable water (i.e., the potable water that is collected in drains from the aircraft appliances), referred to herein as gray water, is routed to a second variable volume that occupies the same container as the first variable volume.

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