PROBLEM TO BE SOLVED: To provide a variable oblique wing plane devised to simplify the structure of a variable blade machine, although, in the variable oblique blade machine of the prior art, a tie is needed between a fuselage and a main wing, and it is not practical to set the angle of a main wing to 0 degrees.SOLUTION: Therefore, the present invention provides a method of a variable oblique wing plus terminal wing of wing-fuselage fusion type, and enables a missile having no tie but a main wing variable from 0 degrees.SELECTED DRAWING: Figure 2
【課題】可変斜め翼機は可変翼機の構造を簡易化する為に考案された実験機である。しかしながら、従来の可変斜め翼機では胴体と主翼との間に繋ぎ目を必要とする。また、主翼の角度を0度にすることは現実的ではなかった。【解決手段】そこで本発明は、翼胴融合型で可変斜め翼プラス末端翼、という方法を提供し、繋ぎ目が無く0度から主翼可変可能な飛翔体を可能とする。【選択図】図2
WING-FUSELAGE FUSION TYPE VARIABLE OBLIQUE WING PLUS TERMINAL WING MISSILE
翼胴融合型可変斜め翼プラス末端翼飛翔体
2017-01-26
Patent
Electronic Resource
Japanese
IPC: | B64C AEROPLANES , Flugzeuge |
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