The invention is related to an aircraft 1 with a fuselage 2 that accommodates at least one air breathing propulsion engine 8a, said fuselage 2 having a maximum fuselage width determined in the region of said at least one air breathing propulsion engine 8a and comprising at least one front fuselage cowling and at least one rear fuselage cowling that are each covering said at least one air breathing propulsion engine 8a at least partly, said at least one front and rear fuselage cowlings being spaced apart from each other in a direction transverse to a longitudinal axis of said at least one air breathing propulsion engine 8a by a predetermined cowling offset to define a dynamic air intake 9 through which an intake air stream is supplied to said at least one air breathing propulsion engine 8a in operation.


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    Title :

    An aircraft with an air intake for an air breathing propulsion engine


    Additional title:

    Flugzeug mit Lufteinlass für ein Strahltriebwerk
    Avion avec une prise d'air pour un moteur à propulsion


    Contributors:

    Publication date :

    2018-11-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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