An aircraft is provided including a boundary layer ingestion fan mounted to an aft end of a fuselage. A stabilizer is mounted to the fuselage and extends between a root portion and a tip portion to define a span-wise length and extends between a leading edge and a trailing edge along the longitudinal direction. The stabilizer defines a line of maximum thickness that corresponds to the thickest cross sectional portion of the stabilizer along the span-wise length of the stabilizer. The line of maximum thickness is closer to the leading edge of the stabilizer proximate the root portion than at the tip portion, resulting in a pressure distribution that draws higher velocity air away from an inlet of the boundary layer ingestion fan.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft having an AFT engine and stabilizer with a varying line of maximum thickness


    Beteiligte:

    Erscheinungsdatum :

    2019-11-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Aircraft having an aft engine and stabilizer root fillet

    PASTOUCHENKO NIKOLAI N / MALCEVIC IVAN | Europäisches Patentamt | 2019

    Freier Zugriff

    AIRCRAFT ENGINE WITH STATOR HAVING VARYING PITCH

    ANAND KARAN | Europäisches Patentamt | 2023

    Freier Zugriff

    AIRCRAFT ENGINE WITH STATOR HAVING VARYING GEOMETRY

    CAPRON ALEXANDRE / ANAND KARAN / YAM TAMMY et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Aircraft engine with stator having varying pitch

    ANAND KARAN | Europäisches Patentamt | 2024

    Freier Zugriff

    ENGINE-PROPELLER AIRCRAFT SCREW AIR FLOW STABILIZER

    ABRAMISHVILI MARLEN MELITONOVICH | Europäisches Patentamt | 2021

    Freier Zugriff