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An airtight leak detection method for a liquid rocket engine propellant supply pipeline

A technology for supply pipelines and liquid rockets, applied in liquid tightness measurement using liquid/vacuum degree, fluid tightness test, machine/structural component test, etc., can solve long cycle, heavy workload, micro leakage Difficult to check and other problems, to achieve the effect of low cost, rapid response and fast detection

Active Publication Date: 2019-12-24
XIAN AEROSPACE PROPULSION TESTING TECHN INST
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  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to solve the problem that the existing pipeline airtightness detection method has a large workload, a long cycle, and is difficult to check micro-leakage, and provides an airtight leak detection method for a liquid rocket engine propellant supply pipeline, The invention adopts three kinds of detection means to cooperate with each other and complement each other, which can efficiently and reliably complete the airtight inspection of the pressure pipeline

Method used

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  • An airtight leak detection method for a liquid rocket engine propellant supply pipeline
  • An airtight leak detection method for a liquid rocket engine propellant supply pipeline
  • An airtight leak detection method for a liquid rocket engine propellant supply pipeline

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Embodiment Construction

[0057] Below in conjunction with accompanying drawing and specific embodiment the content of the present invention is described in further detail:

[0058] Such as figure 1 , figure 2 As shown, the liquid rocket engine propellant supply pipeline airtight leak detection system of the present invention includes sensors, front-end adapter cabinets, measurement cables, data acquisition modules, data analysis equipment and displays; wherein the sensors are temperature sensors, pressure sensors and acoustic emission The sensor is mainly used to detect the stress wave and temperature change caused by leakage in the pipeline, and is connected to the front-end transfer cabinet through an active cable; the data acquisition module includes a signal conditioning circuit, an amplification circuit, a filter circuit, and an A / D conversion circuit; data analysis The equipment is a computer, and the computer uses the analysis software containing the leak detection algorithm to analyze the si...

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Abstract

The invention relates to a liquid rocket motor propellant supply pipeline airtight leakage detection system and method, and solves the problems that the present pipeline airtightness detection methodhas high workload and long period and has difficulty to detect the micro-leakage. The airtight leakage detection system comprises sensors, a front-end transfer cabinet, a measuring cable, a data acquisition module, data analysis equipment and a displayer. The data acquisition module comprises a signal conditioning circuit, an amplification circuit, a filter circuit and an A / D conversion circuit. The data analysis equipment is the computer. The displayer is connected with the data analysis equipment. The sensors include a temperature sensor, a pressure sensor and an acoustic emission sensor. The signals acquired from the sensors are transmitted to the data acquisition module through the front-end transfer cabinet and the measuring cable, and the signals are transmitted to the data analysisequipment through amplification, filtering and A / D conversion. The airtight leakage detection method based on the airtight leakage detection system comprises the following steps: 1) sensor installation; 2) sensor verification; 3) data acquisition; and 4) data processing.

Description

technical field [0001] The invention relates to the field of fault monitoring, in particular to an airtight leak detection method for a liquid rocket engine propellant supply pipeline. Background technique [0002] The pressure pipeline is the most basic unit for transporting fluid in the field of liquid rocket engine testing. Due to the aging of the pipeline used in the test, changes in geographical and climatic environments, and other reasons, pipeline leakage accidents often occur during thermal tests or propellant filling. , the propellant used in the test has the characteristics of high toxicity, flammability (fuel), and volatile (oxidizer). The high-purity nitrogen used for valve control, pressurization, blowing, etc. If there is a large amount of nitrogen leakage, the consequences will be very serious. In order to ensure the reliability of the test process system and prevent the phenomenon of running, escaping, and dripping of the medium in the pipeline, it is necess...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M3/28G01M3/24
CPCG01M3/24G01M3/2807G01M3/2815
Inventor 左明聪陈海峰刘英元张少博董冬白文义邝奇翟文化耿直刘晓姚羽佳赵纳赵涛
Owner XIAN AEROSPACE PROPULSION TESTING TECHN INST
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