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Small rocket shell launching device

A launcher and rocket technology, applied to rocket launchers, weapon types, offensive equipment, etc., can solve problems such as buffering and protection that are not considered

Inactive Publication Date: 2017-11-24
NORTHWESTERN POLYTECHNICAL UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the design of the launcher did not take into account the cushioning and protection of the launcher when the rocket was launched and returned to its original position

Method used

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Examples

Experimental program
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Effect test

Embodiment Construction

[0026] The present embodiment is a small-sized rocket launcher. The fixed carrier of the launch device is an unmanned aerial vehicle or a ground launch vehicle.

[0027] refer to Figure 1 to Figure 6 The rocket launching device of this embodiment is composed of a launch tube pitching device 1, an attitude sensor 2, a fixing device 3, a sight sensor 4, and an electronic control box 5. The launching tube pitching device 1 is located between the launch tube 35 and the two sides of the fixing device 3. and are connected by bolts respectively. The attitude sensor is fixed on the top of the fixture 3 and is used to measure the attitude of the pitching device of the launch tube. The aiming sensor 4 is installed on the front end of the fixing device 3 for observing the aiming target. The electronic control box 5 is located at the lower part of the fixing device 3 .

[0028]In this embodiment, the launching tube pitching device 1 includes a pitching fixed limiter 6, a pitching out...

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Abstract

The invention discloses a small rocket shell launching device which comprises a launcher canister elevation mount, an attitude sensor, a fixing unit, view sensors and an electronic control box. The launcher canister elevation mount is located on the side face of a launcher canister and the fixing device in a fixed connection manner, the attitude sensor is fixed on a sensor support at the top of the fixing unit, and statuses of the launching device ready for launch, during the launch, post-launch are automatically acquired through the attitude sensor; the view sensors located on the front portion of the electronic control box are connected with a view reduction motor mounted on a main mounting plate and used for viewing targets; the electronic control box is mounted on the lower portion of the fixing unit and is used for fixing a circuit board and a power module of the launching device; integrated viewing and launching of the launching device is guaranteed by equipping the launching device with multiple sensors; the launching device is buffered and protected during launching through buffer springs. The small rocket shell launching device is carried by an unmanned aerial vehicle or a ground vehicle and has the advantages of being downsized and portable and safe.

Description

technical field [0001] The invention relates to the technical field of rocket launching, in particular to a small rocket launching device. Background technique [0002] Rockets launch ammunition propelled by a rocket motor. It is mainly used for killing and suppressing the enemy's vital forces, destroying fortifications and weapons and equipment. The launcher of the rocket includes a bazooka, a rocket launcher, a rocket launcher and a rocket launcher. Because the rocket has a self-propelling device, the force on the launch device is small, so it can be launched by multiple tubes or slide rails. The rockets used by individual soldiers are light and flexible, and are effective short-range anti-tank weapons. [0003] The existing individual or civilian rocket launcher has the advantages of simple and reliable structure, stable launch state, easy operation, and quick location transfer. Such as a traction rocket launcher, the launcher is connected to the vertical plate type u...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41F3/04
CPCF41F3/04
Inventor 王民钢党铁安张韬杨尧张希铭
Owner NORTHWESTERN POLYTECHNICAL UNIV
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