The main fuselage 12 and the pair of left and right auxiliary fuselage 14, 16 are connected by three wings, the front wing 30, the main wing 26, and the horizontal stabilizer 32. At the connecting portion between the main fuselage 12 and the main wing 26, a narrow portion 28 is provided in the chord of the main wing 26 that is narrower than the other portions of the main wing 26. The narrow portion 28 of the main wing 26 is connected to the side surface of the main fuselage 12 or the narrow portion 28 penetrates the main fuselage 12. The main wing 26 and the pair of left and right auxiliary fuselage 14 and 16 were connected by interposing a flat columnar support 48. The aircraft can fly stably with less turbulence of airflow and is suitable for aerial refueling and the like.


    Access

    Download


    Export, share and cite



    Title :

    Aerial refueling aircraft


    Contributors:

    Publication date :

    2023-12-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Design method for refitting aircraft gravity refueling system into aerial refueling system

    LIU MINGHUI / LI YUFEI / XU WEI et al. | European Patent Office | 2020

    Free access

    Aircraft aerial refueling hose whip-throwing prevention device

    WANG BIN / ZHANG RUIPING / JING KE et al. | European Patent Office | 2024

    Free access


    Aerial refueling lamp with hidden refueling function and manufacturing method of aerial refueling lamp

    BI JING / LU JIANFEI / LUO FEI et al. | European Patent Office | 2023

    Free access

    Flying boom mast for multi-purpose aerial refueling aircraft

    HASMANN PAULO HENRIQUE / VINICIUS MARCOS / KOIKE GABRIEL KENDJY et al. | European Patent Office | 2021

    Free access