Aspects of this disclosure relate to externally accessible auxiliary power unit (APU) pump assembly, comprising: a pump configured to pressurize an accumulator that is used to start an APU of an aircraft; a pressure gauge for the accumulator; and a support frame configured to be mounted within an outer wall of the aircraft, wherein the support frame defines an externally accessible compartment and secures the pump and the pressure gauge within the externally accessible compartment.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Externally accessible auxiliary power unit pump assembly


    Beteiligte:
    BARTON RANDY L (Autor:in) / OGLE TRACY L (Autor:in)

    Erscheinungsdatum :

    2024-01-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



    EXTERNALLY ACCESSIBLE AUXILIARY POWER UNIT PUMP ASSEMBLY

    BARTON RANDY L / OGLE TRACY L | Europäisches Patentamt | 2023

    Freier Zugriff

    Dump body that includes a pivot assembly with externally accessible gussets

    ARUL SAMUEL JUDSON WILLIAM | Europäisches Patentamt | 2020

    Freier Zugriff

    DUMP BODY THAT INCLUDES A PIVOT ASSEMBLY WITH EXTERNALLY ACCESSIBLE GUSSETS

    ARUL SAMUEL JUDSON WILLIAM | Europäisches Patentamt | 2019

    Freier Zugriff

    DUMP BODY THAT INCLUDES A PIVOT ASSEMBLY WITH EXTERNALLY ACCESSIBLE GUSSETS

    ARUL SAMUEL JUDSON WILLIAM | Europäisches Patentamt | 2019

    Freier Zugriff

    DUMP BODY THAT INCLUDES A PIVOT ASSEMBLY WITH EXTERNALLY ACCESSIBLE GUSSETS

    ARUL SAMUEL JUDSON WILLIAM | Europäisches Patentamt | 2020

    Freier Zugriff