A rectification structure body 100 of a flying vehicle is provided with a rectification section 30, a heat input control section 20 and a vacuum thermal insulation section 10. The rectification section 30 has a rectification surface 30a and a back surface 30b. The rectification surface 30a rectifies airflow 5 from a travelling direction. The back surface 30b is arranged opposite to the rectification surface 30a. The heat input control section 20 is connected to the back surface 30b. The vacuum thermal insulation section 10 is connected to the heat input control section 20 and its surface is formed of rigid body. In addition, the heat input control section 20 is sandwiched between the back surface 30b and the vacuum thermal insulation section 10.


    Access

    Download


    Export, share and cite



    Title :

    Rectification structure body and flying vehicle


    Contributors:

    Publication date :

    2022-04-12


    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 / F02K JET-PROPULSION PLANTS , Strahltriebwerke



    RECTIFICATION STRUCTURE BODY AND FLYING VEHICLE

    YOSHIDA RIKAKO / NISHIKAWA KOSUKE | European Patent Office | 2020

    Free access

    Rectification Structure Body and Flying Vehicle

    YOSHIDA RIKAKO / NISHIKAWA KOSUKE | European Patent Office | 2021

    Free access

    VEHICLE RECTIFICATION STRUCTURE

    IKAWA YUKI / OKAMOTO SATORU / TASHIRO KUNIYOSHI et al. | European Patent Office | 2018

    Free access

    Modular wing body rectification structure of unmanned aerial vehicle

    ZHAO JIANXING / ZHOU YI / ZHANG YULIN et al. | European Patent Office | 2023

    Free access

    VEHICLE AND FLYING BODY

    YAMABE ATSUSHI / KOWA MUNETAKA / SHIDA HAYATO et al. | European Patent Office | 2023

    Free access