Disclosed is an air cycle machine (ACM) having: a turbine (210); a compressor (200); a compressor shaft (255) connected to the compressor and configured to receive rotational energy from a gearbox (75); and a turbine shaft (260) connected to the turbine and configured to provide rotational energy to the gearbox; wherein the turbine shaft and the compressor shaft operate at different rotational speeds.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIRCRAFT SYSTEM


    Weitere Titelangaben:

    LUFTFAHRZEUGSYSTEM
    SYSTÈME D'AVION


    Beteiligte:

    Erscheinungsdatum :

    2023-04-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Aircraft cooling system and aircraft with aircraft cooling system

    KLIMPEL FRANK | Europäisches Patentamt | 2022

    Freier Zugriff

    Aircraft environment control system, aircraft power system and aircraft

    YANG HAN / YANG CHUNXIN / ZHANG XINGJUAN et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Aircraft onboard control system, aircraft control system and aircraft

    HU HUAZHI / XUE PENG | Europäisches Patentamt | 2022

    Freier Zugriff

    AIRCRAFT CONTROL SYSTEM, AIRCRAFT CONTROL METHOD, AND AIRCRAFT

    MIYAWAKI TAKASHI / ABE MASAKATSU / KATO HIROKI | Europäisches Patentamt | 2019

    Freier Zugriff

    AIRCRAFT CONTROL SYSTEM, AIRCRAFT CONTROL METHOD AND AIRCRAFT

    MIYAWAKI TAKASHI / ABE MASAKATSU / KATO HIROMOTO | Europäisches Patentamt | 2019

    Freier Zugriff