Turbojet injecting incineration device and incineration method

Abstract

The invention relates to a turbojet injecting incineration device and an incineration method. The incineration device comprises a turbojet engine, a suction component used for sucking polluted gas, an oil supply device and a control device, wherein the oil supply device supplies oil to the turbojet engine; the control device controls the turbojet engine to work; and the suction component is communicated with the turbojet engine. The incineration method comprises the steps of: generating high-temperature fuel gas, absorbing the polluted gas, incinerating the polluted gas and discharging the polluted gas. According to the turbojet injecting incineration device and the incineration method, disclosed by the invention, the technical problems of poorer cleaning effect of the traditional blowing method, low efficiency of the traditional neutralization processing method and various types of used devices of the traditional incineration method are solved, the equipment scale is small, high processing efficiency is obtained, and cleaning and detoxifying treatment on toxic propellants remained in a propelling system can be carried out.

Description

technical field [0001] The invention belongs to the field of propulsion system ground service system, and relates to a conventional propellant exhaust gas and waste liquid treatment device, in particular to a turbojet ejection incineration device, which can suck and incinerate the residual propellant in the cavity of the propulsion system after operation , It can also be used for non-toxic treatment of propellant waste gas and waste liquid generated during the ground filling and blowing process of the propulsion system. Background technique [0002] At present, most propulsion systems use conventional propellants, mainly hydrazine fuels and nitro oxidizers. When the propulsion system is filled with propellant and cleaned and maintained on the ground, it will produce toxic waste liquid and gas, which will pollute the environment and products. [0003] A certain propulsion system uses conventional propellants. After a test run or flight, the propulsion system needs to be clea...

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Problems solved by technology

[0007] In order to solve the disadvantages of poor cleaning effect of the traditional blowing method, low efficiency of the neutralization treatment method, and the technical problems of various types of equipment used in the incineration method, the present invention provides a turbojet ejection incineration device and incineration method, which has a scale of equipment Small size, high treatment efficiency, can remove and detoxify the toxic propellant remaining in the propulsion system

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