A genset that includes a gas turbine engine (32) having a low pressure shaft (33) wherein the gas turbine engine is adapted to provide mechanical power to a propulsion type load. The genset further includes a generator (40) having an input power shaft wherein the generator is adapted to receive mechanical power to develop electric power. The genset further includes an output power shaft having a first end coupled to the low pressure shaft of the gas turbine and a second end coupled to the input power shaft of the generator and a plurality of struts (54, 56) wherein the first ends of the plurality of struts are coupled to the gas turbine engine and second ends of the plurality of struts are coupled to the generator at locations substantially aligned with a center of gravity of the generator. A suspension apparatus attaches the gas turbine engine and the generator at mounting locations substantially aligned with a gas turbine engine center of gravity and at mounting locations substantially aligned with the generator center of gravity, respectively. A method of producing a genset is also described.


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    Titel :

    GENSET AND METHOD OF PRODUCING A GENSET


    Weitere Titelangaben:

    GENSET UND VERFAHREN ZUR HERSTELLUNG EINES GENSETS
    GROUPE ÉLECTROGÈNE ET PROCÉDÉ DE PRODUCTION D'UN GROUPE ÉLECTROGÈNE


    Beteiligte:
    HUGHES MELISSA (Autor:in) / BANHAM CHRISTOPHER (Autor:in) / BENNETT BRIAN (Autor:in) / SWINDLE JASON (Autor:in)

    Erscheinungsdatum :

    27.01.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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




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