The invention discloses a fixed-wing freight aircraft with an inflected fuselage to extend the available length of a continuous internal freight cabin while still meeting the tail rubbing prevention requirements. The fuselage defines a continuous internal cargo compartment extending along a majority of its length and a pitch axis about which the freight aircraft rotates during takeoff while it is still on the ground. The fuselage includes a front fuselage portion defining a longitudinal-transverse plane of the freight aircraft and a rear fuselage portion extending from a pitch axis to a rear fuselage end and containing a rear fuselage region of a continuous internal cargo compartment extending along a majority of a length of the rear fuselage portion. The aft fuselage portion has a centerline extending above an upper surface of a front fuselage portion of the aircraft.

    本发明公开一种具有拐折式机身的固定翼货运飞机,以延长连续内部货运机舱的可用长度同时仍满足防擦尾要求。机身限定沿其大部分长度延伸的连续内部货舱和俯仰轴线,货运飞机当其仍在地面时在起飞期间围绕俯仰轴线旋转。所述机身包含前机身部分和后机身部分,前机身部分限定货运飞机的纵向‑横向平面,后机身部分自俯仰轴线延伸至后机身端,并且含有沿所述后机身部分的大部分长度延伸的连续内部货舱的后机身区域。后机身部分具有在所述飞机的前机身部的上表面上方延伸的中心线。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft fuselage configuration free from tail wiping allowing long payload


    Weitere Titelangaben:

    免于擦尾的允许长有效载荷的飞机机身构型


    Beteiligte:

    Erscheinungsdatum :

    2022-06-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B65G TRANSPORT OR STORAGE DEVICES, e.g. CONVEYORS FOR LOADING OR TIPPING, SHOP CONVEYOR SYSTEMS OR PNEUMATIC TUBE CONVEYORS , Transport- oder Lagervorrichtungen, z.B. Förderer zum Laden oder Abladen



    AIRCRAFT FUSELAGE CONFIGURATIONS FOR AVOIDING TAIL STRIKE WHILE ALLOWING LONG PAYLOADS

    REWERTS SCOTT / BELL JASON / LUNDSTROM MARK | Europäisches Patentamt | 2021

    Freier Zugriff

    AIRCRAFT FUSELAGE CONFIGURATIONS FOR AVOIDING TAIL STRIKE WHILE ALLOWING LONG PAYLOADS

    REWERTS SCOTT DAVID / BELL JASON C / LUNDSTROM MARK EMIL | Europäisches Patentamt | 2021

    Freier Zugriff

    Aircraft fuselage configurations for avoiding tail strike while allowing long payloads

    REWERTS SCOTT DAVID / BELL JASON C / LUNDSTROM MARK EMIL | Europäisches Patentamt | 2024

    Freier Zugriff

    AIRCRAFT FUSELAGE CONFIGURATIONS FOR AVOIDING TAIL STRIKE WHILE ALLOWING LONG PAYLOADS

    REWERTS SCOTT DAVID / BELL JASON C / LUNDSTROM MARK EMIL | Europäisches Patentamt | 2023

    Freier Zugriff

    AIRCRAFT FUSELAGE CONFIGURATIONS FOR AVOIDING TAIL STRIKE WHILE ALLOWING LONG PAYLOADS

    REWERTS SCOTT DAVID / BELL JASON C / LUNDSTROM MARK EMIL | Europäisches Patentamt | 2021

    Freier Zugriff