The invention discloses an aircraft with a fused canard layout, and particularly relates to the field of aircraft starting design. Comprising an aircraft with a pair of canards, and the pair of canards are symmetrically arranged on the front portion of a fuselage of the aircraft and rotationally connected with the fuselage of the aircraft. By the adoption of the technical scheme, the problem that an existing flying wing aircraft cannot give consideration to the aerodynamic performance and the stealth performance at the same time is solved, and the aerodynamic performance and the stealth performance of the aircraft can be both considered.

    本发明专利公开了一种具有融合式鸭翼布局的飞行器,具体涉及飞行器启动设计领域。包括带有一对鸭翼的飞行器,一对所述鸭翼对称设置在飞行器的机身前部,一对所述鸭翼均与飞行器机身转动连接。采用本发明技术方案解决了现有的飞翼布局飞行器无法同时兼顾气动性能与隐身性能的问题,可兼顾飞行器的气动性能与隐身性能。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft with fused canard layout


    Weitere Titelangaben:

    一种具有融合式鸭翼布局的飞行器


    Beteiligte:
    HUANG JIANGTAO (Autor:in) / CHEN XIAN (Autor:in) / ZHONG SHIDONG (Autor:in) / YU LONGZHOU (Autor:in) / CHEN CHENG (Autor:in) / HE CHENGJUN (Autor:in) / CHEN LILI (Autor:in)

    Erscheinungsdatum :

    2022-07-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    AIRCRAFT OF FEATHERED CANARD ARRANGEMENT (KRASNOV-CANARD)

    KRASNOV JURY KONSTANTINOVICH | Europäisches Patentamt | 2017

    Freier Zugriff

    AIRCRAFT WITH CANARD CONFIGURATION

    KRASNOV JURY KONSTANTINOVICH | Europäisches Patentamt | 2016

    Freier Zugriff

    H-shaped aircraft with canard

    ZHANG YULIN / XIANG JUNHUA / HE YUNHAN et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    Canard aircraft with rear loading

    LLAMAS SANDÍN RAUL | Europäisches Patentamt | 2015

    Freier Zugriff

    CANARD AIRCRAFT WITH REAR LOADING

    LLAMAS SANDIN RAUL | Europäisches Patentamt | 2015

    Freier Zugriff