An assembly is provided for an aircraft. This assembly includes a first rotating structure, a second rotating structure and a seal assembly. The seal assembly is configured to seal an annular gap radially between the first rotating structure and the second rotating structure. The seal assembly includes an arm, a seal element and a seal land. The arm is cantilevered from and extends axially along the second rotating structure. The seal element is connected to the arm and forms a seal interface with the seal land. The seal land is connected to the first rotating structure.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AIRCRAFT PROPULSION SYSTEM GEARTRAIN


    Beteiligte:

    Erscheinungsdatum :

    15.02.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Aircraft propulsion system geartrain

    HANRAHAN PAUL R / STACHOWIAK DAVID A | Europäisches Patentamt | 2024

    Freier Zugriff

    AIRCRAFT PROPULSION SYSTEM GEARTRAIN

    HANRAHAN PAUL R / STACHOWIAK DAVID A | Europäisches Patentamt | 2024

    Freier Zugriff

    Aircraft propulsion system geartrain

    HANRAHAN PAUL R / MYLREA BENJAMIN T / STACHOWIAK DAVID A | Europäisches Patentamt | 2025

    Freier Zugriff

    AIRCRAFT PROPULSION SYSTEM GEARTRAIN

    HANRAHAN PAUL R / MYLREA BENJAMIN T / STACHOWIAK DAVID A | Europäisches Patentamt | 2025

    Freier Zugriff

    AIRCRAFT PROPULSION SYSTEM GEARTRAIN

    HANRAHAN PAUL R / STACHOWIAK DAVID A | Europäisches Patentamt | 2024

    Freier Zugriff