Device and method for testing PVT properties of high-purity xenon gas in a closed container

A technology of airtight container and testing device, which is applied in the field of high-purity xenon gas physical property test, to achieve the effects of stable air flow, easy replacement, and comprehensive and complete measurement data

Active Publication Date: 2016-03-30
BEIJING INST OF CONTROL ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0006] Since the application field of high-purity xenon is the aerospace and military industry, the testing technology and related experimental verification of its physical properties involve national security. Countries that have mastered this technology often impose technical blockades. The foreign information that can be found only provides xenon physics. Some parameters of the property, the principle of the physical property test method and the specific steps of implementation are not mentioned

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  • Device and method for testing PVT properties of high-purity xenon gas in a closed container
  • Device and method for testing PVT properties of high-purity xenon gas in a closed container
  • Device and method for testing PVT properties of high-purity xenon gas in a closed container

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Embodiment Construction

[0053] The present invention will be further described below with reference to the accompanying drawings and embodiments.

[0054] like figure 1 As shown, the device of the present invention includes a helium cylinder 1, a helium valve 2, a xenon storage tank 3, a gas source valve 4, a vacuum valve 5, a vacuum pump 6, a transfer valve 7, a transfer gas cylinder 8, a transfer gas cylinder electronic scale 9, Data acquisition system 10 , purity analyzer 11 , filling valve 12 , temperature control device 13 , recovery valve 14 , recovery module 15 , liquid nitrogen valve 16 , liquid nitrogen tank 17 and air release valve 18 .

[0055] The pipeline between the recovery module 15 and the liquid nitrogen tank 17 is a dedicated pipeline for liquid nitrogen, and the rest of the pipelines used for the connection of the device are high-polished stainless steel high-pressure pipelines. The specific connection method is as follows: Helium cylinder 1 passes through the helium valve 2 and th...

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Abstract

The invention provides a device and a method for testing PVT (pressure volume temperature) properties of high-purity xenon gas in a closed container. The device comprises a helium tank, a helium valve, a xenon gas storage tank, an air source valve, a vacuum valve, a vacuum pump, a transfer valve, a transfer air cylinder, a transfer air cylinder electronic scale, a data acquisition system, a purity analyzer, a filling valve, a temperature-control device, a recycle valve, a recycle module, a liquid nitrogen valve, a liquid nitrogen tank and an air vent valve. The invention provides a method for testing the PVT properties of the high-purity xenon gas in the closed container through research. By utilizing the method, a verification test for the PVT properties of the high-purity xenon gas is finished, so that the method is reasonable and feasible. When the PVT properties of xenon gas in the closed container is obtained and physical property test data of xenon gas is accumulated, an excellent foundation is laid for following xenon gas engineering application.

Description

technical field [0001] The invention relates to a PVT property testing device and method for high-purity xenon gas used in a satellite electric propulsion system, and belongs to the technical field of high-purity xenon gas physical characteristic testing. Background technique [0002] At present, there are many types of propulsion systems for in-orbit flight. Among them, the electric propulsion system has developed rapidly in recent years due to its high specific impulse, especially the Hall electric propulsion system and ion electric propulsion system, which are often used in geostationary orbits The satellite platform performs tasks such as north-south position keeping, attitude control (momentum wheel unloading), orbit control, and even synchronous orbit transfer. In addition, electric propulsion systems can accomplish tasks that conventional propulsion systems cannot, such as deep space exploration, interstellar travel and other tasks that require large Δy, as well as ta...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01N33/00
Inventor 宋飞孙水生武葱茏刘国西刘涛翟阔阔刘学毕强宰守刚赵振平宇文雷韩飞龙
Owner BEIJING INST OF CONTROL ENG
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