The disclosure relates to an aircraft lavatory touchless manifold system. A system and related method for touchless control of an aircraft lavatory water supply is disclosed. An aircraft lavatory touchless manifold includes dual solenoid powered water valves opening and closing to regulate water flow through each of a cold conduit and a hot conduit as commanded by user touchless input to a manifold microcontroller commanding the valves. An aircraft input commands a temperature range while a thermal sensor in a mixed water conduit provides output temperature feedback to the manifold microcontroller for positive control of the output temperature. The manifold microcontroller commands opening and closing of the dual solenoid powered valves to create a ratio of opening time between the valves.The solenoid powered valves provide a cost effective and reliable solution offering efficient linear valve operation and effective temperature and flow control.

    本公开涉及飞机卫生间非接触式歧管系统。公开了一种用于对飞机卫生间供水进行非接触式控制的系统和相关方法。飞机卫生间非接触式歧管包括一对螺线管驱动的水阀,其打开和关闭以按照对命令阀的歧管微控制器的用户非接触式输入的命令来调节通过冷导管和热导管中的每一个的水流。飞机输入命令温度范围,而混合水导管中的温度传感器将输出温度反馈提供给歧管微控制器,以对输出温度进行主动控制。歧管微控制器命令一对螺线管驱动的阀的打开和关闭,以形成阀之间的打开时间的比率。螺线管驱动的阀提供了有经济效益且可靠的解决方案,其提供了高效线性的阀操作以及有效的温度和流量控制。


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    Titel :

    AIRCRAFT LAVATORY TOUCHLESS MANIFOLD SYSTEM


    Weitere Titelangaben:

    飞机卫生间非接触式歧管系统


    Beteiligte:
    ORTOLAN CHRISTINA (Autor:in) / CHUH YEN (Autor:in) / HOANG THAO (Autor:in)

    Erscheinungsdatum :

    2020-08-07


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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