Gas generator propellant grain

A technology of gas generating agent and powder column, which is applied to ammunition, projectiles, cartridge ammunition, etc. It can solve the problems of high temperature of the launch tube, strict thermal design requirements, threat of equipment on the bomb and launch device, etc., and achieve low combustion temperature , compact structure, fast gas production effect

Active Publication Date: 2013-08-28
HUBEI INST OF AEROSPACE CHEMOTECH
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Problems solved by technology

Gas-fired ejection is to directly act on the bottom of weapons such as missiles with gunpowder gas, and convert the chemical energy of gunpowder into kinetic energy to drive missiles. Compared with gas-steam devices, it has large energy, small volume, and relatively simple equipment. However, due to the high temperature of the gas in the general gunpowder, the temperature in the launch tube is too high

Method used

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  • Gas generator propellant grain

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Example Embodiment

[0026] Hereinafter, embodiments of the fuel gas generating agent grains related to the invention will be described with reference to the drawings.

[0027] figure 1 Among them, the present invention is a device that provides energy for power plants, and consists of the following components: a support cylinder 1 made of any one of alloy steel, stainless steel, low carbon steel and other metals, and a gas generating agent fixed in the support cylinder 1 2. The support cylinder 1 is cylindrical and has a plurality of axially parallel combustion-supporting holes 5 on its side. The length of the combustion-supporting hole 5 is the same as the length of the fuel gas generating agent 2. The fuel gas generating agent 2 has a cylindrical axial through hole 6 with holes in the axial direction, and the two ends are covered with a fuel-limited layer 3. The fuel gas generating agent 2 completely covers the combustion-supporting hole 5 of the support cylinder. The fuel gas generating agent...

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Abstract

Provided is a gas generator propellant grain. Gas generator propellant is filled in a supporting barrel, more than one combustion-supporting hole is formed in a position, corresponding to the gas generator propellant, of the circumferential surface of the supporting barrel, an axial through hole is formed in the gas generator propellant, a position, making contact with the supporting barrel, of the side face of the gas generator propellant is provided with a lining, and combustion-limiting layers are installed on two end faces of the gas generator propellant. The gas generator propellant grain starts to burn simultaneously from the axial through hole and the combustion-supporting holes in the side face of the supporting barrel, the combustion face tends to increase, and produced gas flows to an exhaust hole of a gas generator through the inner axial through hole and the surface of the supporting barrel. The gas generator propellant grain used for guided missile ejection power devices has the advantages that the gas is produced rapidly, the combustion temperature is low, the gas producing quantity is gradually increased over time, and the change rule is controllable.

Description

technical field [0001] The invention relates to a gas generating agent grain column which provides working energy for a missile weapon type ejection power device. Background technique [0002] At present, the ejection power forms of domestic and foreign missiles mainly include: compressed air type, steam type, gas type, gas-steam type, and electromagnetic type. Among them, the volume of compressed air, steam and electromagnetic equipment is too large to be convenient for transportation and mobile launch. The volume of the gas-steam type device is much smaller than that of the compressed air type, steam type, and electromagnetic type, and it has a wide range of applications. It is the main power form used by missile launches in various countries. Gas-fired ejection is to directly act on the bottom of weapons such as missiles with gunpowder gas, and convert the chemical energy of gunpowder into kinetic energy to drive missiles. Compared with gas-steam devices, it has large en...

Claims

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Application Information

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IPC IPC(8): F42B5/196F42B15/00F42B33/02
Inventor 乔应克鲁国林王文博吴敏张军民谢杨林信培培李冰
Owner HUBEI INST OF AEROSPACE CHEMOTECH
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