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Scrapped propellant destroying heat energy utilization system and method and application

A propellant and power generation system technology, which is applied in the field of waste propellant destruction heat energy utilization system, can solve the problems of resource waste and utilization, and achieve the effect of avoiding the waste of resources

Pending Publication Date: 2020-10-16
中国人民解放军32181部队 +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Its advantage is that it can completely incinerate scrap propellants without leaving hidden dangers, and can control the entire incineration process. Its disadvantage is that the current furnace incineration method does not release a large amount of heat energy during the combustion process, resulting in waste of resources.

Method used

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  • Scrapped propellant destroying heat energy utilization system and method and application

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Embodiment Construction

[0037] The following specific embodiments may be combined with each other, and the same or similar concepts or processes may not be repeated in some embodiments. Embodiments of the present invention will be described below with reference to the accompanying drawings.

[0038] Such as figure 1 As shown, the invention discloses a waste propellant charge destruction heat energy utilization system, method and application. Propellant is a compound or mixture containing oxidant and combustible, which can independently carry out chemical reaction and output energy. Its combustion process is accompanied by a large amount of gas and releases a large amount of heat. Therefore, the heat generated by the destruction and combustion of scrap propellant can be used as a heat source. For power generation and / or heating for heat users, specifically, including:

[0039]The waste propellant charge combustion system, the waste propellant charge combustion system is used to convert the chemical ...

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PUM

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Abstract

The invention discloses a scrapped propellant destroying heat energy utilization system and method and application. The heat energy utilization system comprises a scrapped propellant combustion systemwhich is used for converting the chemical energy of scrapped propellant into heat energy, a steam-water system which is connected with the scrapped propellant combustion system and used for transferring heat energy to a power generation system, the power generation system which communicates with the steam-water system and used for converting heat energy into electric energy and communicates withthe steam-water system to form circulation, and a heat energy utilization system which communicates with the power generation system and is used for converting heat energy and communicating with the steam-water system to form circulation. According to the scrapped propellant destroying heat energy utilization system, a large amount of heat energy released in the destroying and burning process of the scrapped propellant powder can be utilized, and resource waste is avoided.

Description

technical field [0001] The invention relates to the technical field of destroying scrapped propellants, in particular to a heat energy utilization system, method and application for destroying scrapped propellants. Background technique [0002] Propellant is a compound or mixture containing oxidant and combustible, which can independently carry out chemical reaction and output energy. The combustion process is accompanied by a large amount of gas and releases a large amount of heat. Propellant combustion is a self-sustaining combustion that releases energy, that is, after ignition, the scrapped propellant can automatically maintain the combustion process until it is completely burned. Different types of projectiles require propellant with different properties, so there are many types of propellant. When the scrapped ammunition of the army is destroyed and processed, the amount of scrapped propellants that can be used for civilian use is very small, and there is a large backl...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F22B33/18F22B31/00F22B31/08F22G7/12F22D11/06F24D3/02F24D3/10F01D15/10F01K11/02F42D5/04
CPCF01D15/10F01K11/02F22B31/00F22B31/08F22B33/18F22D11/06F22G7/12F24D3/02F24D3/10F42D5/04
Inventor 闫媛媛宋佳飞姜志保王韶光贾昊楠邵先军陈明华
Owner 中国人民解放军32181部队
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