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    • 2. 发明授权
    • Projectile
    • 射弹
    • US4754707A
    • 1988-07-05
    • US908107
    • 1986-09-16
    • Utz U. Ahlers
    • Utz U. Ahlers
    • F42B14/02F42B31/00
    • F42B14/02
    • A projectile which is fireable in a spin-stabilized manner from a weapon barrel or launch tube through the action of the gas pressure generated by a propellant charge, and which projectile is guidable during flight. The projectile is equipped in the rearward region of its tail-end structure, and preferably behind the control surfaces, with a type of propulsion cage so as to, through the intermediary of the gas pressure generated by the propellant charge, faciliate a ballistic firing of the projectile from a weapon barrel or launch tube. The projectile is equipped with a sealing ring, which with a gliding frictional contact, coaxially encompasses an axially-limited region of the tail-end structure of the projectile.
    • 一种可以通过由推进剂装药产生的气体压力的作用,从武器枪管或发射管以旋转稳定的方式起火的射弹,以及哪些射弹在飞行中是可引导的。 射弹在其尾端结构的后部区域中,优选地在控制表面的后面,具有一种推进保持架,以便通过由推进剂装料产生的气体压力的中介,将弹道射击 射弹从武器枪管或发射管。 射弹配备有密封环,其具有滑动的摩擦接触,同轴地包围射弹的尾端结构的轴向受限的区域。