Lithium propellant supply device used for electric propulsion engine test and supply method thereof

A supply device and propellant technology, applied in the direction of engine testing, measuring devices, machine/structural component testing, etc., can solve problems such as difficulties in lithium MPDT engine test research, public reporting of important details of supply pipelines, etc., and achieve enhanced practicality High performance and ease of operation, simple valve control technology, and easy-to-achieve blow-off cleaning process

Inactive Publication Date: 2013-07-24
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Many foreign institutions and departments have carried out experimental research on lithium MPDT engines, but they have not made public reports on the important details of the supply pipeline in the test
At present, the design of gas pipelines and liquid pipelines has reached a relatively high level in China, but there are still great difficulties in applying the existing devices and methods to the experimental research of lithium MPDT engines

Method used

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  • Lithium propellant supply device used for electric propulsion engine test and supply method thereof
  • Lithium propellant supply device used for electric propulsion engine test and supply method thereof

Examples

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Embodiment Construction

[0033] The lithium propellant supply device and its supply method of the present invention will be further described below in conjunction with the accompanying drawings and examples.

[0034] Such as figure 1 As shown, the lithium propellant supply device of the present invention includes an argon gas path sub-device, a lithium propellant supply sub-device and a cooling water control sub-device. The following is an explanation according to the general use sequence of the set of devices, which is convenient for understanding and use.

[0035] The argon gas distribution device includes an argon gas cylinder 101 , an argon gas cylinder manual stop valve 102 , an argon gas pipeline filter 103 and an argon gas pipeline pressure gauge 104 . The argon cylinder 101 is mainly used to store the inert gas argon. The argon gas cylinder manual stop valve 102 is installed on the outlet pipeline of the argon gas cylinder 101, and is used to control the switch of the argon gas pipeline. Th...

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Abstract

The invention brings forward a lithium propellant supply device used for an electric propulsion engine test and a supply method thereof. The device comprises an argon gas circuit subdevice, a cooling water control subdevice and a lithium propellant supply subdevice that is placed in a vacuum cabin. Heating films are arranged on outer walls of a lithium storage tank, a lithium transfer storage tank and propellant pipelines; and cooling valves are arranged on a propellant pipeline between the lithium storage tank and the lithium transfer storage tank and a propellant pipeline between the lithium transfer storage tank and an engine. Besides, the argon gas circuit subdevice provides gas pressure for the lithium storage tank; and the cooling water control subdevice provides cooling water for the cooling valves. According to the supply method, the heating films are used to carry out liquefaction on solid alkali metal lithium and then extrude the processed lithium into the transfer storage tank; and a motor is used to control a piston to realize controllable supply of a flow of a lithium propellant. According to the invention, high maneuverability and practicality are realized; therefore, the flow of the supplied lithium solid propellant is controlled stably as well as a requirement of a ground test of an engine is met.

Description

technical field [0001] The invention relates to a set of solid propellant supply device suitable for electric propulsion engine test, in particular to the supply technology of lithium (Lithium), a solid alkali metal propellant of a magnetoplasma dynamic engine (MPDT). Background technique [0002] The magnetoplasma dynamic engine (MPDT) is a typical electromagnetic space electric propulsion engine, which has the advantages of high specific impulse, large thrust range, long life, high control precision, and repeatable start. It has broad application prospects in missions such as space exploration and interstellar navigation. [0003] The propellant of the magnetoplasma dynamic engine can use hydrogen, lithium, neon, argon, xenon, etc., and use the interaction between the magnetic field and the current to generate the Lorentz force to accelerate the plasma state propellant to generate thrust, so it is also called the Lorentz force Accelerator (Lorentz Force Accelerator). The...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M15/02
Inventor 王海兴耿金越陈士强
Owner BEIHANG UNIV
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