A device for producing electrical power has a thermoelectric device coupled to an aircraft bleed system for generating electrical power using temperature differentials between ram air and bleed air. A system control is coupled to the ram air and the bleed air to control a temperature of the bleed air and to control a temperature gradient of the thermoelectric device.


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    Title :

    THERMOELECTRIC GENERATOR ON AN AIRCRAFT BLEED SYSTEM


    Additional title:

    THERMOELEKTRISCHER GENERATOR AUF DEM ZAPFLUFTSYSTEM EINES FLUGZEUGS
    GÉNÉRATEUR THERMOÉLECTRIQUE SUR UN SYSTÈME DE PRÉLÈVEMENT D'AIR À BORD D'UN AVION


    Contributors:
    GAO LIJUN (author) / SHENGYI LIU (author) / CHIEN CHIN-HSI (author)

    Publication date :

    2016-08-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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