An in-line heater system on board an aircraft includes a heater element positioned within a tubing, at least one sensor positioned within the tubing configured to monitor the temperature within the tubing, and an inline heater controller configured to receive information regarding the heater element via the at least one sensor. The inline heater controller is positioned at a location spaced away from the heater element and the tubing. The inline heater controller includes a printed circuit board configured to receive the information regarding the heater element via the at least one sensor, and an aerospace connector configured to transmit the information regarding the heater element via the at least one sensor to the aircraft.


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    Titel :

    Inline heater controller


    Beteiligte:
    WHITE ALAN L (Autor:in) / KING GREG (Autor:in)

    Erscheinungsdatum :

    2020-03-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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