Disclosed herein is an aircraft (101) that includes an exhaust manifold (200) for combining one or more system exhaust paths located upstream of equipment inlets and directing the exhausts upwards towards the rotor linkages such that the exhaust is expelled and diffused forward of the equipment inlets. According to one aspect of the present disclosure, the exhaust manifold includes a structure (404) for supporting a transmission cowling (115) at the top of the aircraft and/or on the sides of the aircraft. For example, the exhaust manifold may include a platform (202) that contains the exhaust duct (204, 206, 208, 210) and may include a frame extending from the platform that follows the contours of the cowling, such that the cowling lays along the support frame for additional mechanical support.


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    Titel :

    ROTORCRAFT WITH EXHAUST MANIFOLD FOR COMBINING SYSTEM EXHAUST PLUME


    Weitere Titelangaben:

    DREHFLÜGELFLUGZEUG MIT EINEM ABGASKRÜMMER ZUR KOMBINATION EINER SYSTEMABGASFAHNE
    GIRAVION AVEC COLLECTEUR D'ÉCHAPPEMENT PERMETTANT DE COMBINER UN PANACHE D'ÉCHAPPEMENT DE SYSTÈME


    Beteiligte:
    PEDERSEN KEITH C (Autor:in) / SCANNELL BRENT (Autor:in) / TRAN NAM DAI (Autor:in) / MAST THOMAS (Autor:in)

    Erscheinungsdatum :

    2019-09-18


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01P Kühlung von Kraft- und Arbeitsmaschinen oder Kraftmaschinen allgemein , COOLING OF MACHINES OR ENGINES IN GENERAL



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