An electrical power system for an aircraft including a turbine engine coupled to the aircraft and providing propulsive thrust and emitting heat during operation to define a high temperature source, a cryogenic fuel system located within the aircraft and providing fuel for the turbine and emitting heat at a lower temperature than the heat from the turbine engine to define a low temperature source and an electrical power generator located on the aircraft and having a thermodynamic generator using the temperature difference to generate electrical power and a method for producing electric power.


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    Title :

    SYSTEM AND METHOD FOR AVIATION ELECTRIC POWER PRODUCTION


    Additional title:

    SYSTEM UND VERFAHREN ZUR ERZEUGUNG ELEKTRISCHER ENERGIE AUS DER LUFT
    SYSTÈME ET PROCÉDÉ POUR LA PRODUCTION D'ÉNERGIE ÉLECTRIQUE D'AVION


    Contributors:

    Publication date :

    2015-11-04


    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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