The invention relates to the technical field of aircraft tests, and discloses an aircraft conical cabin joint thermal intensity assessment test device which comprises a test piece fixing tool. The pneumatic thermal simulation device is arranged at the front end of the test piece fixing tool along the central axis of the test piece fixing tool; the pneumatic pressure simulation device is arranged at the front end of the pneumatic thermal simulation device; the pneumatic thermal simulation device is installed on a position adjusting mechanism which can linearly move to adjust the front-back position of the pneumatic thermal simulation device, and the pneumatic thermal simulation device is used for providing thermal loads for the connection position of the front section and the rear section of a test piece restrained by the restraining mechanism at the rear end and the front-back area of the test piece. And the pneumatic pressure simulation device is arranged below the conical front section of the test piece and applies an upward force load to the lower part of the front section of the test piece. According to the invention, the flight environment of the aircraft during flight can be reproduced more truly, and the reproduction of aerodynamic heat and aerodynamic pressure during high-speed flight of the aircraft in a high-altitude environment is met.

    本发明涉及飞行器试验技术领域,公开一种飞行器锥形舱段连接处热强度考核试验装置,包括试验件固定工装,沿所述试验件固定工装的中心轴线布置于所述试验件固定工装的前端的锥形筒状的气动热模拟装置及布置于所述气动热模拟装置的前端的气动压力模拟装置;所述气动热模拟装置安装于可直线移动前后调节其前后位置的位置调节机构上,所述气动热模拟装置用于向由约束机构在后端约束的试验件的前段与后段的连接位置及其前后区域提供热载荷,所述气动压力模拟装置布置于试验件的锥形状的前段的下方,向试验件的前段的下方施加向上的力载荷。本发明能更加真实复现飞行器飞行时的飞行环境,满足飞行器在高空环境中高速飞行时气动热与气动压力的复现。


    Access

    Download


    Export, share and cite



    Title :

    Thermal intensity assessment test device for joint of conical cabin section of aircraft


    Additional title:

    飞行器锥形舱段连接处热强度考核试验装置


    Contributors:
    DING ZHILI (author) / CUI YINGWEI (author) / LU ZIZHAO (author) / SUN LIMING (author) / JIA YENING (author) / YAN XUDONG (author) / XU HAIBO (author) / CHEN HAOHUI (author) / XUE CHENCHAO (author) / WANG YOUJIE (author)

    Publication date :

    2023-03-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    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 / G01N Untersuchen oder Analysieren von Stoffen durch Bestimmen ihrer chemischen oder physikalischen Eigenschaften , INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES



    AIRCRAFT CABIN SECTION AND AIRCRAFT HAVING AN AIRCRAFT CABIN SECTION

    WENG ALEXANDER / KIRSTEIN HAUKE / TEICHMANN SVEN et al. | European Patent Office | 2022

    Free access

    AIRCRAFT CABIN SECTION AND AIRCRAFT HAVING AN AIRCRAFT CABIN SECTION

    WENG ALEXANDER / KIRSTEIN HAUKE / TEICHMANN SVEN et al. | European Patent Office | 2022

    Free access

    AIRCRAFT CABIN SECTION AND AIRCRAFT HAVING AN AIRCRAFT CABIN SECTION

    WENG ALEXANDER / KIRSTEIN HAUKE / TEICHMANN SVEN et al. | European Patent Office | 2023

    Free access

    Aircraft cabin section, door insulation and aircraft

    KIRSTEIN HENNING / KYAS GYORGY | European Patent Office | 2022

    Free access

    Aircraft cabin section with liquid collector and aircraft

    WEN AMY | European Patent Office | 2023

    Free access