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Modular Faucet System for Aircraft

机译:飞机模块化水龙头系统

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:用于飞机的模块化水龙头系统,包括水龙头出口,流量阀和致动器。水龙头出口被配置为安装在飞机上。流量阀被配置为与水龙头出口分开安装在飞机上,通过第一水管连接到包括飞机上水箱的供水系统,并通过第二水管连接到水龙头出口。 。致动器被配置为与水龙头出口和流量阀分开安装在飞机上。致动器包括被配置为检测模块化水龙头系统的用户的非接触传感器。致动器构造成响应于非接触式传感器对用户的检测而产生控制信号以打开流量阀以将水从供水供应到水龙头出口。

著录项

  • 公开/公告号US2020130841A1

    专利类型

  • 公开/公告日2020-04-30

    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;E03C1/05;E03C1/042;

  • 国家 US

  • 入库时间 2022-08-21 11:22:11

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