A mount for coupling an engine to a vehicle includes an engine bracket to couple to the engine. The engine bracket includes a body that has a first end opposite a second end, and the body defines an offset coupling portion (234) between the first end and the second end. The offset coupling portion (234) protrudes from the body between the first end and the second end to define a receptacle (228). The mount includes a vehicle bracket (204) to couple to the vehicle. The vehicle bracket (204) includes a first bracket end (250) opposite a second bracket end (252). The first bracket end (250) is offset from the second bracket end (252) and the first bracket end is received within the receptacle (228) to couple the engine bracket to the vehicle bracket.


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    Title :

    SYSTEM AND METHOD FOR GAS TURBINE ENGINE MOUNT WITH SEAL


    Additional title:

    SYSTEM UND VERFAHREN ZUR MONTAGE EINES GASTURBINENMOTORS MIT DICHTUNG
    SYSTÈME ET PROCÉDÉ DE MONTAGE D'UN MOTEUR À TURBINE À GAZ COMPORTANT UN JOINT D'ÉTANCHÉITÉ


    Contributors:

    Publication date :

    2021-01-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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