RU202432U1 - FIGHTING MACHINE - Google Patents

Abstract

The utility model relates to the field of weapons designed to protect military units in all forms of combat and on the march, as well as sedentary and stationary objects from air attack and reconnaissance means, including small-sized ones. chassis, equipment, launcher with cradles for transporting and launching missiles and devices for guiding cradles horizontally and vertically. SAM in TPK are fixed in the cradles of the combat vehicle launcher. The cradles of the launcher of the combat vehicle are made with a two-row placement of the TPK with missiles. This made it possible to position the shaft of the vertical guidance device of the launcher between the rows of the TPK with anti-aircraft guided missiles and connect it to increase the rigidity of the metal structure, both with the inner and outer sides of the cradle. launches of anti-aircraft guided missiles, including when a combat vehicle is moving. At the same time, the double-row placement of the TPK with missiles in the cradles significantly facilitates the process of loading the launcher, reduces the dimensions of the combat vehicle in height, which ensures its transportation by rail and air transport.

Description

The utility model relates to the field of weapons, in particular, to combat vehicles of anti-aircraft missile systems (SAM), which are designed to protect military units in all forms of combat and on the march, as well as sedentary and stationary objects from air attack and reconnaissance, including small.

Known anti-aircraft missile systems, for example, "Pantsir" ("Arms and Technologies of Russia" - Encyclopedia of the XXI century, volume IX, pp. 133-143; magazine "Technics and weapons", No. 04/2016). The complex consists of anti-aircraft guided missiles (SAM) in transport and launch containers (TPK) and a combat vehicle, including a base chassis (wheeled or tracked), complex equipment, a launcher with cradles for transporting and launching missiles and cradle guidance devices horizontally and vertically ... Anti-aircraft guided missiles in transport and launch containers are fixed in the cradles of the launcher of a combat vehicle with a three-row SAM system.

During the launch, the missile launcher leaves the TPK and the stability of the dispersion of the missile defense system should be ensured at the launch site, a decisive influence on which the elastic properties of the metal structure of the launcher of the combat vehicle, in particular, the characteristics of the rigidity of the cradles, have a decisive influence.

The disadvantage of the Pantsir anti-aircraft missile system is that the middle cradle with a three-row SAM arrangement is massive to ensure the required rigidity. This leads to an increase in the mass of the metal structure of the launcher, the use of a base chassis of increased carrying capacity and the inconvenience of loading.

The purpose of the utility model is to eliminate these shortcomings.

The technical result of the proposed utility model is to reduce the mass and increase the rigidity of the launcher metal structure. This significantly increases the reliability of the combat vehicle, improves the convenience of loading, and reduces the height of the combat vehicle to ensure its transportation by rail and air.

The specified technical result is achieved by the fact that the cradles of the launcher of the combat vehicle are made with double-row placement of anti-aircraft guided missiles, which made it possible to locate the shaft of the vertical guidance device of the launcher between the rows of missiles in the TPK and connect it to both the inner and outer sides of the cradle, which increased rigidity of the metal structure of the cradles with the same mass.

The tests carried out have fully confirmed the specified technical result.

The utility model is illustrated by drawings, where:

- in Fig. 1 shows a general view of a combat vehicle;

- in Fig. 2 is a structural diagram of a launcher with two-row placement of missiles.

The combat vehicle (Fig. 1) consists of a base chassis 1, equipment 2 and a launcher 3 with cradles 4 for transporting and launching anti-aircraft guided missiles 5 and cradle guidance devices horizontally and vertically.

The structural diagram of a launcher with double-row placement of anti-aircraft guided missiles in transport and launch containers (Fig. 2) shows the placement of missiles in the TPK of the upper 6 and lower 7 rows in cradle 4 and shaft 8 of the vertical guidance device of the launcher 3, located between the rows of missiles and connecting the inner 9 and outer 10 sides of the cradle.

The use of the proposed utility model increases the efficiency of the combat vehicle with a minimum weight and increased rigidity of the metal structure of the combat vehicle launcher and provides missile launches when the combat vehicle moves.

In addition, the two-row placement of missiles in cradles greatly facilitates the process of loading the launcher, reduces overall dimensions in height, which ensures the movement of the combat vehicle by rail and air transport.

Claims (1)

A combat vehicle containing a base chassis, equipment, a launcher with cradles for transporting and launching anti-aircraft guided missiles, cradle guidance devices horizontally and vertically, characterized in that the cradles of the launcher are made with double-row placement of anti-aircraft guided missiles in transport and launch containers, and the inner and outer sides of the cradle are rigidly connected to the shaft of the vertical guidance device of the launcher, located between the upper and lower rows of anti-aircraft guided missiles in transport-launch containers.

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