To protect a payload loaded in a missile or a space craft from high temperature.SOLUTION: A flow straightening structure includes: an outer shell (11) having an outer surface (11a) and an inner surface (11b) and configured to control airflow along the outer surface (11a); an inner shell (12) which is provided so as to face the inner surface (11b) of the outer shell (11) and houses a payload (13) therein; and a plate (22) which is coupled to the inner shell (12) while forming a space therebetween. The outer shell (11) is coupled to the plate (22).SELECTED DRAWING: Figure 3

    【課題】飛翔体や宇宙機に搭載されるペイロードを高温から保護する。【解決手段】整流構造が、外側表面(11a)と内側表面(11b)とを有し、外側表面(11a)に沿った空気の流れを制御するように構成された外殻(11)と、外殻(11)の内側表面(11b)に対向するように設けられ、内部にペイロード(13)を収容する内殻(12)と、内殻(12)に隙間を挟んで離間されて結合されたプレート(22)とを備えている。外殻(11)は、プレート(22)に結合されている。【選択図】図3


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    Title :

    FLOW STRAIGHTENING STRUCTURE, MISSILE, AND SPACE CRAFT


    Additional title:

    整流構造、飛翔体及び宇宙機


    Contributors:

    Publication date :

    2021-12-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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