A system includes a turbo pump configured to convert a tank compressed gas or an engine compressed gas into at least one of electrical power, hydraulic power, or pneumatic power. The system also includes a storage tank configured to store the tank compressed gas. The system also includes a bleed line configured to port the engine compressed gas from the gas turbine engine to the turbo pump. The system also includes a propellant selector valve having an off position in which the turbo pump is prevented from receiving either the tank compressed gas or the engine compressed gas, a tank position in which the tank compressed gas from the storage tank is ported through the propellant selector valve to the turbo pump, and an engine position in which the engine compressed gas from the bleed line is ported through the propellant selector valve to the turbo pump.


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    Titel :

    UTILIZATION OF ENGINE BLEED AIR TO PROVIDE EXTENDED DURATION EMERGENCY AIRCRAFT POWER


    Weitere Titelangaben:

    NUTZUNG VON TRIEBWERKSZAPFLUFT ZUR BEREITSTELLUNG VON NOTFALLENERGIEVERSORGUNG VON ERWEITERTER DAUER
    UTILISATION D'AIR DE PRÉLÈVEMENT DE MOTEUR POUR FOURNIR UNE ALIMENTATION D'URGENCE À DURÉE PROLONGÉE À UN AÉRONEF


    Beteiligte:

    Erscheinungsdatum :

    06.01.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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