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Missile launcher structure for oblique launching

A missile launcher, inclined launch technology, applied in the direction of the launch device, etc., can solve the problems of high system integration, high rigidity requirements, and large volume.

Active Publication Date: 2015-05-20
CNGC INST NO 206 OF CHINA ARMS IND GRP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

It is characterized by large volume, heavy weight, high rigidity requirements, and high system integration

Method used

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  • Missile launcher structure for oblique launching
  • Missile launcher structure for oblique launching
  • Missile launcher structure for oblique launching

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Embodiment Construction

[0019] Now in conjunction with embodiment, accompanying drawing, the present invention will be further described:

[0020] The launcher is formed by welding profiled steel pipes, which can hold 4 cartridges, and the upper and lower layers of the cartridges are symmetrically arranged in a trapezoid. After the launcher is loaded with bullets, it meets the requirements of vehicle driving and transportation. One end of the launching frame is installed on the lug of the azimuth turntable through a coupling shaft, the other end is connected with the extension end of the pitching and pushing cylinder, and the fixed end of the pitching and pushing cylinder is connected with the turntable; The launch frame is pushed to the launch angle by pitching and pushing the cylinder, and the 360-degree follow-up target can be realized through the azimuth turntable. In order to meet the needs of vehicle transportation and loading cartridges, the lower layer is designed with left and right attachm...

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Abstract

The invention relates to a missile launcher structure for oblique launching. The structure is formed by welding and forming section steel pipes, four barrel missiles can be carried, and the barrel missiles are pairwise arranged in an upper layer and a lower layer in a trapezoid shape. After the launcher is loaded with the barrel missiles, the running and transporting requirement of a vehicle is met. One end of the launcher is arranged on an orientation rotary table supporting lug through a connecting shaft, the other end of the launcher is connected with the stretching end of a pitching lifting cylinder, and the fixed end of the pitching lifting cylinder is connected with a rotary table. An integrated mechanism is formed by the launcher, the orientation rotary table and the pitching lifting cylinder, the launcher achieves the launching angle through the pitching lifting cylinder, and 360-degree target follow-up can be achieved through the orientation rotary table.

Description

technical field [0001] The invention belongs to the field of missile launch engineering, and relates to the design and manufacture of a mid-short-range tilt-launch anti-aircraft missile launcher with large volume, heavy weight, high rigidity requirements and high integration. The missile launcher is a vehicle-mounted cross-country transport, and is designed based on the requirements of missile installation accuracy and easy loading. Background technique [0002] The new missile launcher is not only the installation basis for missiles, but also the installation basis for other missile launching subsystems. It is characterized by large volume, heavy weight, high rigidity requirements, and high system integration. As an important basic structure for missile launch, the structural design of the missile launcher is one of the important contents of the structural design of the entire missile launch system. The quality of its design directly affects the quality of the missile laun...

Claims

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Application Information

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IPC IPC(8): F41F1/00
Inventor 李忠于周永卫李智邹玉蓉
Owner CNGC INST NO 206 OF CHINA ARMS IND GRP
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