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In the head of the nose fair ring separable

机译:在鼻子的头部可分离的白皙戒指

摘要

PROBLEM TO BE SOLVED: To allow no deterioration of the attitude stability of a missile, and separate a nose fairing without hitting an embarkation apparatus or the like by regulating so as not to generate rotation movement through a regulation means when the joining state of first fairing half body and second fairing half body is released. ;SOLUTION: First fairing half body 30 and second fairing half body 40 forming a nose fairing are joined mutually on the division faces Ls, and hold members 31, 32 holding energizing means, regulation means, and the like are respectively fixed to the inside faces of the respective half bodies 30, 40. By releasing a joining state, both fairing half bodies 30, 40 are respectively pushed out in reverse directions P1, P2 by the energizing force of a compression spring so as to start separating movement. Since a cylindrical member 43 is guided through a guide member 33 by a predetermined distance L only in the extending direction of the cylindrical member, both fairing half bodies 30, 40 are not allowed to conduct rotation movement against a fuselage part 70, and are separated by only parallel movement.;COPYRIGHT: (C)1999,JPO
机译:要解决的问题:不使导弹的姿态稳定性恶化,并且通过调节将鼻整流罩分离而不撞到登乘装置等,从而在第一整流罩的接合状态下不通过调节装置产生旋转运动。半身和第二个整流罩半身被释放。解决方案:形成鼻子整流罩的第一整流罩半体30和第二整流罩半体40在分隔面Ls上相互连接,并且分别将用于保持通电装置,调节装置等的保持部件31,32固定在其内表面上。通过释放接合状态,两个整流罩半体30、40分别被两个半体30、40沿相反的方向P 1 ,P 2 推出。压缩弹簧的激励力,从而开始分离运动。由于圆筒形构件43仅在圆筒形构件的延伸方向上通过引导构件33被引导预定距离L,所以整流罩半体30、40均不允许相对于机身部70进行旋转运动,并且被分离。只能平行移动。;版权:(C)1999,JPO

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