Fire seal assemblies for aircraft engines are described herein. An example fire seal assembly includes a first L-cap having a first leg and a second leg extending outward from the first leg, and a second L-cap having a third leg and a fourth leg extending outward from the third leg. The first and third legs are to be coupled to a core service disconnect (CSD) on a pylon of an aircraft, and the second and fourth legs are to extend outward and engage sides of a firewall of an engine of the aircraft. The first seal assembly further includes a seal coupled to the first and third legs and disposed between the second and fourth legs, a first end plug disposed between a first end of the seal and the second leg, and a second end plug disposed between a second end of the seal and the fourth leg.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    FIRE SEAL ASSEMBLIES FOR AIRCRAFT ENGINES


    Beteiligte:
    POND MORGAN A (Autor:in) / SCHNELZ JAMES R (Autor:in)

    Erscheinungsdatum :

    2020-12-17


    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



    Fire seal assemblies for aircraft engines

    POND MORGAN A / SCHNELZ JAMES R | Europäisches Patentamt | 2021

    Freier Zugriff

    FIRE SEAL ASSEMBLIES FOR AIRCRAFT ENGINES

    POND MORGAN A / SCHNELZ JAMES R | Europäisches Patentamt | 2021

    Freier Zugriff

    AIRCRAFT FIRE SEAL STRUCTURE AND AIRCRAFT

    TAKEUCHI AKIRA | Europäisches Patentamt | 2018

    Freier Zugriff

    Aircraft fire seal structure and aircraft

    TAKEUCHI AKIRA | Europäisches Patentamt | 2020

    Freier Zugriff

    AIRCRAFT FIRE SEAL STRUCTURE AND AIRCRAFT

    TAKEUCHI AKIRA | Europäisches Patentamt | 2018

    Freier Zugriff