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Modular faucet system for aircraft

机译:飞机模块化龙头系统

摘要

A modular faucet system for an aircraft comprising a faucet outlet, a flow valve, and an actuator. The faucet outlet is configured to be installed on the aircraft. The flow valve is configured to be installed on the aircraft separately from the faucet outlet, to be connected by a first water line to a water supply comprising a water tank on the aircraft, and to be connected by a second water line to the faucet outlet. The actuator is configured to be installed on the aircraft separately from the faucet outlet and the flow valve. The actuator comprises a touchless sensor that is configured to detect a user of the modular faucet system. The actuator is configured to generate a control signal to open the flow valve to provide water from the water supply to the faucet outlet in response to detection of the user by the touchless sensor.
机译:用于飞机的模块化龙头系统,包括龙头出口,流动阀和致动器。水龙头出口配置为安装在飞机上。流动阀配置成分开地从龙头出口安装在飞机上,通过第一水线连接到包括在飞机上的水箱的供水,并通过第二水线连接到龙头出口。 。致动器配置成分开地从龙头出口和流动阀安装在飞机上。致动器包括一种不等型的传感器,该传感器被配置为检测模块化龙头系统的用户。致动器被配置为产生控制信号以打开流动阀,以响应于用户通过不用传感器检测用户的供水从供水到水龙头出口。

著录项

  • 公开/公告号US10994844B2

    专利类型

  • 公开/公告日2021-05-04

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号US201816172247

  • 发明设计人 STEPHEN M. YOUNG;

    申请日2018-10-26

  • 分类号B64D11/02;E03C1/042;E03C1/05;E03C1/04;F16K21;

  • 国家 US

  • 入库时间 2022-08-24 18:32:13

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