The invention discloses a fixed-wing freight aircraft with an inflected fuselage. The fuselage contains a continuous internal cargo compartment and includes a front portion, a rear portion, and an inflection in the fuselage between the front portion of the fuselage and the rear portion of the fuselage. The inflection contains a transition region of the internal cargo hold and defines a bend angle between a front centerline and a rear centerline. The inflection is formed with a front transverse frame coupled to the front fuselage end, a separate rear transverse frame coupled to the rear fuselage end, and a plurality of longitudinal frame elements extending between the front transverse frame and the rear transverse frame, the front transverse frame coupled to the front fuselage end, the rear transverse frame coupled to the rear fuselage end, and the plurality of longitudinal frame elements extending between the front transverse frame and the rear transverse frame. The rear transverse frame is angled relative to the front transverse frame about a transverse axis of the freight aircraft.

    公开了一种具有拐折机身的固定翼货运飞机。该机身包含连续内部货舱,并且包括前部、后部和拐折部,该拐折部在所述机身中在所述机身的前部和所述机身的后部之间。拐折部包含所述内部货舱的过渡区并且在前中心线和后中心线之间限定出弯折角。拐折部形成有前部横向框架、单独的后部横向框架和在所述前部横向框架和所述后部横向框架之间延伸的多个纵向框架元件,前部横向框架联接到所述前部的后机身端,所述后部横向框架联接到所述后部的前机身端,使得所述后部横向框架相对于所述前部横向框架绕所述货运飞机的横向轴线成一定角度。


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    Title :

    Aircraft fuselage configuration with upwardly deflected rear fuselage


    Additional title:

    后机身向上偏折的飞机机身构型


    Contributors:

    Publication date :

    2023-12-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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