This rectifying structural body 100 of a flying object is provided with a rectifying part 30, a heat input control part 20, and a vacuum heat insulated part 10. The rectifying part 30 has a rectifying surface 30a and a rear surface 30b. The rectifying surface 30a rectifies an air flow 5 from the advancing direction. The rear surface 30b is disposed on the opposite side of the rectifying surface 30a. The heat input control part 20 is connected to the rear surface 30b. The vacuum heat insulated part 10 is connected to the heat input control part 20 and has an outer surface formed as a rigid body. In addition, the heat input control part 20 is interposed between the rear surface 30b and the vacuum heat insulated part 10.


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    Title :

    Rectification Structure Body and Flying Vehicle


    Contributors:

    Publication date :

    2021-05-27


    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



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