PROBLEM TO BE SOLVED: To provide a missile having intake, in which air pressure does not increase because a front face project area does not increase, and because strong impact wave caused by an intake cover does not occur during boost time, large wave drag does not occur.SOLUTION: A lamp 13 on a supersonic air intake port 2 can slide, and the lamp position is forward slid so as to occlude an intake inlet during boost time, and during ram combustor, the intake is rearward slid for forming a groove 31 for preventing suction of a boundary layer in front of the lamp, thereby engine performance and flight performance are not deteriorated.

    【課題】正面投影面積が増加しないため空気抵抗が増加せず、ブースト時にインテークカバーによる強い衝撃波が発生しないため大きな造波抵抗が発生しないインテークを有する飛しょう体を提供する。【解決手段】超音速空気取り入れ口2のランプ13をスライド可能とし、ブースト時においてはインテーク入口をふさぐようにランプ位置を前方にスライドさせ、ラム燃焼時にはランプの前方に境界層を吸い込まないようにするための溝31を形成するように、インテークを後方にスライドさせることにより、エンジン性能や飛しょう性能の劣化を防止する。【選択図】図2


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    Title :

    MISSILE


    Additional title:

    飛しょう体


    Contributors:

    Publication date :

    2015-09-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02K JET-PROPULSION PLANTS , Strahltriebwerke / F42B EXPLOSIVE CHARGES, e.g. FOR BLASTING , Explosive Ladungen, z.B. für Sprengungen



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