A turboshaft engine includes an inlet, a swirl frame mounted downstream of the inlet, and an inlet seal mounted to one of the inlet and the swirl frame extending toward the other of the inlet and the swirl frame. The inlet seal includes a support member and an elastomeric member extending from a first end portion coupled to the support member to a second, cantilevered end portion.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    INLET SEAL FOR A TURBOSHAFT ENGINE


    Beteiligte:

    Erscheinungsdatum :

    2017-02-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Inlet seal for a turboshaft engine

    STEEVES ZACHARIAH | Europäisches Patentamt | 2020

    Freier Zugriff

    Turboshaft engine air inlet system with efficient filtering function

    ZHONG FEIXIONG / JIAO NAN | Europäisches Patentamt | 2024

    Freier Zugriff

    1995 Turboshaft Engine Survey

    Online Contents | 1995


    2001 Turboshaft Engine Survey

    Online Contents | 2001


    1997 Turboshaft Engine Survey

    Online Contents | 1997