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A propellant step-by-step neutralization spray spray system and control method

A spray system, step-by-step technology, applied in the control/regulation system, non-electric variable control, simultaneous control of multiple variables, etc., can solve the problems of insufficient absorption capacity, reduce the probability of accidents, etc. The effect of utilization rate and cost reduction

Active Publication Date: 2020-06-30
BEIJING INST OF AEROSPACE TESTING TECH +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the absorption capacity of the traditional spraying method is insufficient in the face of a large amount of propellant leakage caused by accidents, especially when a large amount of propellant gas is produced at high temperature or local combustion occurs, spraying mist absorbing liquid can be more effective reduce the chance of accidents

Method used

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  • A propellant step-by-step neutralization spray spray system and control method
  • A propellant step-by-step neutralization spray spray system and control method

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Embodiment Construction

[0032] Such as figure 1 As shown, a propellant step-by-step neutralization spray spray system of the present invention includes an absorption liquid storage tank 3, and a liquid delivery pipe 4 connected to the absorption liquid storage tank 3, and the upper edge of the liquid delivery pipe 4 The liquid delivery direction is respectively connected with the first water pump 5, the spray pipe 1 and the suction spray pipe 2. It is characterized in that the part of the liquid delivery pipe 4 located between the spray pipe and the spray pipe 2 is provided with a pressure valve 9, so A second liquid delivery pipe 6 is also connected between the absorption liquid storage tank 3 and the liquid delivery pipe 4, the second liquid delivery pipe 6 is provided with a second water pump 7, and the second liquid delivery pipe 6 is provided with Pressure valve 9 along the liquid delivery direction.

[0033] This solution uses the liquid delivery pipeline of the existing spray system, which sa...

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Abstract

The present invention discloses a step-by-step propellant neutralization water-spraying and mist-spraying system, which comprises an absorption liquid tank and a liquid feeding pipe connected with the absorption liquid tank. The liquid feeding pipe is connected respectively with a first water pump, a water spraying pipe and a mist spraying pipe in the liquid feeding direction at the upper edge. The part of the liquid feeding pipe between the water spraying pipe and the mist spraying pipe is provided with a pressure valve. A second liquid feeding pipe also connects the liquid absorption tank with the liquid feeding pipe, and the second liquid feeding pipe is provided with a second water pump. The second liquid feeding pipe is provided with a check valve in the liquid feeding direction. The invention also relates to a control method of a step-by-step propellant neutralization water-spraying and mist-spraying system, which makes different alarms and security actions according to different degrees of leakage of the propellant, and integrates the water-spraying pipe and the mist-spraying pipe, saving the cost of the additional setting of the mist-spraying pipe. With only two pumps, two systems can be controlled to start step by step, greatly simplifying the control flow.

Description

technical field [0001] The invention relates to the field of security spraying, in particular to a propellant step-by-step neutralization spraying system and a control method. Background technique [0002] The commonly used liquid propellants in my country include hydrazine fuel and dinitrogen tetroxide. Hydrazine fuel is a flammable, explosive, toxic and harmful substance, and dinitrogen tetroxide is a strong oxidant and is a highly toxic substance. Accidental leakage of propellant may occur during storage, and a large amount of toxic exhaust gas will be generated during propellant filling and transfer. Safety protection devices are usually designed for the two working conditions of propellant storage and use. [0003] The propellant may leak during the storage process. The absorption treatment of the leaked propellant during storage adopts the form of an absorption liquid supply pipeline and a spray nozzle. The absorption liquid supply device pumps the absorption liquid in...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D27/02
CPCG05D27/02
Inventor 闫子良郑雪玲郝龙徐光孙鹤荆彦文金朝旭许宏刘朝阳
Owner BEIJING INST OF AEROSPACE TESTING TECH
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