RU2466342C1 - Missile launching plant - Google Patents

Abstract

FIELD: weapons and ammunition.

SUBSTANCE: launching plant includes base, movable pack of fan-like launching tubes, which has the possibility of being oriented as to elevation angle and as to azimuth. Launching tubes are located like a fan along generatrixes of hyperboloid of rotation and hinged to two equally spaced discs kinematically connected to drives.

EFFECT: wide capture zone at relatively high reponse speeds of the plant.

8 dwg

Description

The invention relates to the field of weapons, in particular to launchers for launching missiles.

Known launcher for launching missiles (US Pat. RU 2207481), containing a base, movable with the possibility of orientation in elevation and azimuth, a package of launch tubes and a drive unit, made in the form of a drive-hinge with two degrees of mobility.

A disadvantage of the known design is the limited affected area with the drives stopped.

Known launcher for launching rockets (US Pat. RU 2238505), containing a base, movable with the possibility of orientation in elevation and azimuth, a package of launch tubes arranged in the form of a cone fan-shaped converging their axes in the center of the drive unit.

A disadvantage of the known design are significant overall dimensions.

The technical result achieved by the invention is to reduce the overall dimensions of the launcher.

The specified technical result is achieved in that the launcher for launching missiles contains a base, movable with the possibility of orientation in elevation and azimuth, a package of launch tubes arranged fan-shaped, and two drives, while launch tubes are fan-shaped along the generators of the hyperboloid of rotation and pivotally connected to two spaced disks kinematically connected to the drives.

Distinctive features in the claimed invention in comparison with the prototype is that the launch tubes are fan-shaped along the generators of the hyperboloid of rotation and are pivotally connected to two spaced disks kinematically connected to the drives.

The design of the launcher is illustrated by drawings, where:

figure 1 shows the launcher, General view;

figure 2 is a kinematic diagram of the launcher;

figure 3 - launcher, side view;

figure 4 - launcher, top view;

5 is a launcher, side view with launcher tubes rotated in the opposite direction;

figure 6 - launcher, top view of figure 5;

figure 7 - launcher in the initial state, side view;

on Fig - launcher in the initial state, top view.

The missile launcher comprises a base 1, launch tubes 2, fan-shaped in hinges 3 and 4 mounted in disks 5 and 6, respectively, while disk 5 is connected to drive 7 via shaft 8, and disk 6 is connected to drive 9 by a hollow shaft 10 through a gear 11, wherein the launch tubes 2 are movable relative to the hinges 3 and stationary relative to the hinges 4.

Guidance on the launcher target is carried out by the relative rotation of the plates 5 and 6 by the actuators 7 and 9, which provide, through the control system, the necessary direction to the launch tubes 2.

This launcher has a relatively small overall dimensions and provides a large capture area at relatively high reaction rates.

Claims (1)

A launcher for launching missiles, comprising a base movable with the possibility of orientation along the elevation angle and in azimuth, a package of launch tubes arranged fan-shaped, and two actuators, characterized in that the launch tubes are fan-shaped along the generators of the hyperboloid of rotation and pivotally connected to two spaced apart disks, kinematically connected to drives.

Images