An aircraft 100 and method of operating the aircraft 100 are provided. The aircraft 100 includes a fuselage 102 including a nose 104, a tail 106, and a hollow, elongate body 108 extending therebetween, a wing 110 extending laterally away from the fuselage 102, the wing 110 including a leading edge 114 in a direction 116 of motion of the aircraft 100 during normal flight and a trailing edge 118 on an opposing edge of the wing 110, and an engine 120 configured to drive a bladed rotatable member 122, the engine 120 coupled to at least one of the wing 110 and the fuselage 102. The aircraft 100 further includes at least one of a forward chine member 123 and an aft chine member 132 extending from the fuselage 102 at a point 124 forward of the engine 120 aftward to a point 128 aft of the bladed rotatable member 122.


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    Title :

    METHOD AND SYSTEM FOR OPEN ROTOR ENGINE FUSELAGE PROTECTION


    Additional title:

    VERFAHREN UND SYSTEM ZUM SCHUTZ EINES OFFENEN ROTORMOTORRUMPFES
    PROCÉDÉ ET SYSTÈME DE PROTECTION DE FUSELAGE D'UN MOTEUR À ROTOR OUVERT



    Publication date :

    2017-07-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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