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Automatic loading method for parachute gas gun test missiles

An automatic loading and gas cannon technology, applied in ammunition supply, weapon accessories, offensive equipment, etc., can solve the problems of unable to test the launch mode of the ammunition, test failure, burning, etc., and achieve the effects of saving manpower, facilitating operation, and improving the degree of automation

Active Publication Date: 2018-04-20
AEROSPACE LIFE SUPPORT IND LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

If the propellant of the artillery is fired, the gunpowder gas produced will burn the textile material of the canopy used for the test and cause the test to fail, so the traditional test projectile launch mode cannot be used

Method used

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  • Automatic loading method for parachute gas gun test missiles
  • Automatic loading method for parachute gas gun test missiles
  • Automatic loading method for parachute gas gun test missiles

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0015] The present invention will be further described in detail below in conjunction with the accompanying drawings.

[0016] exist figure 1 , figure 2 Among them, the test bomb is placed on the support tray 2, and the breech block and the plug are connected with the bomb delivery vehicle 3. like image 3 As shown in the bomb delivery vehicle, the claw hook on the bomb delivery vehicle hooks the edge of the latch body, and the two pillars on the swivel sleeve 10 cooperate with the holes on the latch body to control the rotation of the latch body.

[0017] After the test bomb and the latch body are installed, the electrical control system gives a signal, the motor 7 drives the reducer 8, the reducer 8 drives the sprocket 6, the sprocket 6 drives the chain 5, the chain drives the bomb transporter 3, and the bomb transporter 3 Drive the latch body and the test bomb to move along the track on the bracket 1 to the direction of the gun bore. When the bomb delivery vehicle 3 mov...

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PUM

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Abstract

The invention discloses an automatic loading method for parachute gas gun test missiles and belongs to the technical field of gas gun testing. According to the technical scheme, on the technology of manual loading of test missiles of an existing gas gun, it is designed that a support (1), missile trays (2), a missile conveying trolley (3), swinging disk oil cylinders (4), a chain (5), a chain wheel (6), a motor (7), a speed reducer (8), a claw hook (9), a rotating sleeve (10), a rotating oil cylinder (11) and other structures are included, and are assembled into the automatic loading method for the gas gun test missiles. The automatic loading method for the parachute gas gun test missiles has the beneficial effects that automatic loading of the test missiles is achieved, practicability isgood, operation is convenient and fast, and the testing efficiency is greatly improved.

Description

technical field [0001] The invention relates to an automatic loading method for a parachute gas cannon test bomb, which belongs to the technical field of automatic loading of a parachute gas cannon platform. Background technique [0002] In order to verify the performance of parachute types such as recovery parachute, aerial bomb parachute, seat stabilizer parachute, resistance parachute, etc., such as: parachute opening procedure, speed and strength when opening parachute, etc., it is necessary to have a parachute that can shoot in the range of 18°~60° It can provide a launcher with a speed of 15-250m / s and a maximum ballistic height of more than 200m to meet the airborne time of the test carrier. If it is launched with the propellant of the artillery, the gunpowder gas produced will burn the textile material of the canopy used in the test and cause the test to fail, so the traditional test projectile launch mode cannot be used. In order to realize the degree of automation...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41A9/38
Inventor 高春鹏季享文高峰周峰马坤昌赵鸽荣阔许奇亮韩志华
Owner AEROSPACE LIFE SUPPORT IND LTD
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