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首页> 外国专利> CONTROLLED PROJECTILE, STEERING DRIVE GROUP OF CONTROLLED PROJECTILE, PNEUMATIC DISTRIBUTION DEVICE OF STEERING DRIVE OF CONTROLLED PROJECTILE, MECHANISM OF INITIATION OF STEERING DRIVE OF CONTROLLED PROJECTILE

CONTROLLED PROJECTILE, STEERING DRIVE GROUP OF CONTROLLED PROJECTILE, PNEUMATIC DISTRIBUTION DEVICE OF STEERING DRIVE OF CONTROLLED PROJECTILE, MECHANISM OF INITIATION OF STEERING DRIVE OF CONTROLLED PROJECTILE

机译：受控项目，受控项目转向驱动组，受控项目转向驱动的气动分配装置，受控项目转向驱动的初始化机制

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FIELD: weapons and ammunition.;SUBSTANCE: group of inventions refers to the field of precision weapons – guided missiles. Guided projectile contains a body. Steering gear unit and the frame with radial holes are fixed in the body. In these holes are installed shafts that coupled the trunnions. Trunnions are made with lateral levers, kinematically connected rods with output levers of the steering gear unit. In the end grooves of the trunnions, aerodynamic steering wheels are hinged. A that the steering gear unit is an air-dynamic and connected to the frame by pins mounted along the axis of the guided projectile and fixed to the inner ledges of the surface of the shell. Drafts that connect the output arms of the steering gear unit to the pivot arms are arranged to be adjustable and located in a sector between adjacent trunnions. There is a mechanism for initiating an air-dynamic drive between the steering gear unit and the frame. In it between the aerodynamic rudders with the possibility of axial displacement are placed cylindrical air intakes. Opposite the air intakes in the body are holes, sealed with plugs. On the opposite side of the frame is fixed the steering gear control equipment.;EFFECT: increase the range of flight guided missiles.;18 cl, 7 dwg
机译：领域：武器和弹药。;实质：一组发明涉及精密武器领域-制导导弹。制导弹丸包含一个身体。转向齿轮箱和带有径向孔的车架固定在车体内。在这些孔中安装了连接耳轴的轴。耳轴由侧向操纵杆，运动学连接的转向杆和转向器输出杆组成。在耳轴的末端凹槽中，装有空气动力学方向盘。方向盘装置是气动的，并通过沿导向弹丸的轴线安装并固定到壳体表面内壁的销钉连接到车架。将转向齿轮箱的输出臂连接到枢轴臂的吃水深度可调，并位于相邻耳轴之间的一个扇形区域中。在转向器单元和车架之间有一种用于启动气动驱动的机构。在空气动力舵之间有轴向位移的可能性被放置在圆柱状进气口中。主体进气口的对面是孔，并用塞子密封。在车架的另一侧固定了舵机控制设备。效果：增加了飞行制导导弹的射程。18 cl，7 dwg

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