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Hydrazine propellant waste liquid degradation device and system

A propellant and waste liquid technology, applied in water/sewage treatment, electrochemical water/sewage treatment, water/sludge/sewage treatment, etc., can solve problems such as incomplete degradation, secondary pollution, and large energy consumption. Achieve the effects of flexible use, lower requirements for installation technology, and low energy consumption

Active Publication Date: 2020-01-10
PLA PEOPLES LIBERATION ARMY OF CHINA STRATEGIC SUPPORT FORCE AEROSPACE ENG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The object of the present invention is to provide a hydrazine propellant waste liquid degradation device, which utilizes the characteristics of high chemical activity and strong degradation ability of plasma to solve the existing problems in the treatment of hydrazine propellant waste liquid in the prior art Technical problems such as incomplete degradation, high energy consumption, and easy to cause secondary pollution

Method used

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  • Hydrazine propellant waste liquid degradation device and system
  • Hydrazine propellant waste liquid degradation device and system
  • Hydrazine propellant waste liquid degradation device and system

Examples

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Embodiment 1

[0037] Such as figure 1 As shown, the hydrazine propellant waste liquid degradation device provided by the present invention includes a high-voltage electrode 1, a low-voltage electrode 3 and a high-voltage pulse power supply 6;

[0038] The high-voltage pulse power supply 6 is connected to the high-voltage electrode 1;

[0039] The low-voltage electrode 3 is grounded;

[0040] The plasma generated in the gap between the low-voltage electrode 3 and the high-voltage electrode 1 degrades the waste liquid of the hydrazine propellant. In order to adjust the output voltage of the high-voltage pulse power supply 6 conveniently, a transformer 7 is provided, and the transformer 7 is electrically connected with the high-voltage pulse power supply 6 .

[0041] Wherein, the gap between the low-voltage electrode 3 and the high-voltage electrode 1 is 0.5cm˜1.5cm. If the gap exceeds 1.5cm, no plasma will be generated between the high-voltage electrode 1 and the low-voltage electrode 3. I...

Embodiment 2

[0045] This embodiment is a further improvement made on the basis of Embodiment 1, and its structural schematic diagram is shown in figure 2 .

[0046] In Embodiment 2, the same components as those in Embodiment 1 are given the same reference numerals, which will not be repeated here, and only the differences between Embodiment 2 and Embodiment 1 will be described.

[0047] In order to further reduce energy consumption and increase the electric field strength at the gap, an insulating layer 2 is provided outside the high-voltage electrode 1, see figure 2 . The insulating layer 2 is one of insulating materials such as glass, quartz, ceramics, resin, etc. The function of the insulating layer 2 is: on the one hand, it avoids short circuit caused by direct contact between the high-voltage electrode 1 and the waste liquid; on the other hand, the insulating material acts as an insulating layer to improve The electric field strength in the discharge area. The shape of the low-volt...

Embodiment 3

[0049] This embodiment is a further improvement made on the basis of Embodiment 2, and its structural schematic diagram is shown in

[0050] image 3 .

[0051] In Embodiment 3, the same components as those in Embodiment 2 are given the same reference numerals, which will not be repeated here, and only the differences between Embodiment 3 and Embodiment 2 will be described.

[0052] In this implementation, the high-voltage electrode 1, the low-voltage electrode 3 and the insulating layer 2 form a dielectric barrier discharge unit, and there are multiple dielectric barrier discharge units, and a plurality of dielectric barrier discharge units are connected in series to form a dielectric barrier discharge module 4. The dielectric barrier discharge modules 4 are connected in parallel to form a dielectric barrier discharge array 5 . In actual use, one of the dielectric barrier discharge unit, dielectric barrier discharge module 4 and dielectric barrier discharge array 5 can be u...

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Abstract

The application discloses a hydrazine propellant waste liquid degradation device and a system. The device comprises a high-voltage electrode, a low-voltage electrode and a high-voltage pulse power supply. The high-voltage pulse power supply is connected with the high-voltage electrode; the low voltage electrode is grounded; plasma generated by the gap between the low-voltage electrode and the high-voltage electrode degrades hydrazine propellant waste liquid, and also discloses the system comprising the device. According to the device and the system disclosed by the invention, the hydrazine propellant waste liquid is degraded by utilizing the characteristic of strong plasma degradation capability, so that high-efficiency degradation can be realized; since the energy required to generate plasma is only electric energy, the energy consumption is low. Since no chemical substances are used in the degradation process, no secondary pollution is caused to the environment.

Description

technical field [0001] The application relates to a hydrazine propellant waste liquid degradation device and system, belonging to the technical field of waste liquid treatment. Background technique [0002] Hydrazine propellants are currently and for a long time to come, one of the main fuel types for my country's main liquid rockets and satellites. Hydrazine propellants include hydrazine, unsymmetrical dimethyl hydrazine, methyl hydrazine, etc., which are highly toxic. After cleaning the rocket transport tanker and the filling pipeline, a large amount of hydrazine propellant waste liquid will be formed. If it is not treated in a timely and effective manner, it will cause immeasurable damage to the environment, crops, groundwater sources, and the safety of personnel and equipment. It has become a major safety hazard that threatens the sustainable development of the space launch site. [0003] In the prior art, the treatment methods for hydrazine propellant waste liquid incl...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C02F1/46
CPCC02F1/4608
Inventor 王殿恺赵文涛卿泽旭叶继飞李南雷石继林饶伟宋俊玲周伟静
Owner PLA PEOPLES LIBERATION ARMY OF CHINA STRATEGIC SUPPORT FORCE AEROSPACE ENG UNIV