An engine assembly (10) includes a first engine (102), a first exhaust duct (114) coupled in fluid communication only to the first engine, and a first exhaust duct includes a primary outlet and a secondary outlet. An engine assembly (10) further includes a second engine (104) including a second exhaust duct (116) coupled in fluid communication only to the second engine, the second exhaust duct includes a primary outlet and a secondary outlet, and a portion of the first engine secondary outlet is aligned substantially concentrically within a portion of the second engine secondary outlet.


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    Title :

    ENGINE PROPULSION SYSTEM AND METHODS OF ASSEMBLING THE SAME


    Additional title:

    SYSTEME DE PROPULSION DE MOTEURS ET METHODES D'ASSEMBLAGE


    Contributors:

    Publication date :

    2015-06-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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