An aircraft for transporting passengers and cargo able to efficiently handle ground operations for loading/unloading cargo and embarking/disembarking passengers at the same time. The lifting structure of the aircraft is formed by a back-swept wing and a fore-plane, the back-swept wing including winglets having a length L allowing them to act as vertical stabilizers. The propulsion system is mounted aft of the center of gravity of the aircraft and the tailcone of the fuselage is configured to act as a rear access door and as a pressure barrier.


    Access

    Download


    Export, share and cite



    Title :

    CANARD AIRCRAFT WITH REAR LOADING


    Contributors:

    Publication date :

    2015-07-02


    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



    Canard aircraft with rear loading

    LLAMAS SANDÍN RAUL | European Patent Office | 2015

    Free access

    AIRCRAFT OF FEATHERED CANARD ARRANGEMENT (KRASNOV-CANARD)

    KRASNOV JURY KONSTANTINOVICH | European Patent Office | 2017

    Free access

    AIRCRAFT WITH CANARD CONFIGURATION

    KRASNOV JURY KONSTANTINOVICH | European Patent Office | 2016

    Free access

    H-shaped aircraft with canard

    ZHANG YULIN / XIANG JUNHUA / HE YUNHAN et al. | European Patent Office | 2022

    Free access

    Aircraft with fused canard layout

    HUANG JIANGTAO / CHEN XIAN / ZHONG SHIDONG et al. | European Patent Office | 2022

    Free access