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Device and method for filling solid lithium propellant pipeline

A filling device and propellant technology, which is applied in the field of solid propellant pipeline filling device to achieve the effects of improving efficiency and reliability, and enhancing practicability and ease of operation

Inactive Publication Date: 2013-11-13
BEIHANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In view of the strong reducibility of lithium, it reacts violently with water, and is solid at room temperature, so the filling method of liquid pipeline and gas pipeline is no longer applicable to the filling of lithium propellant pipeline and device

Method used

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  • Device and method for filling solid lithium propellant pipeline
  • Device and method for filling solid lithium propellant pipeline

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Embodiment Construction

[0031] The lithium propellant filling device and its filling method of the present invention will be further described below in conjunction with the accompanying drawings and examples.

[0032] The filling device of the present invention includes an argon extrusion gas path sub-device, a lithium propellant filling sub-device and a cooling water control sub-device, combined below figure 1 , in accordance with the general use sequence of the set of devices, to facilitate understanding and use.

[0033] Considering the strong reducibility of alkali metal lithium, it may be oxidized by gas or impurities in the gas, so the gas in the extrusion gas path adopts inert gas argon and a filter is designed on the argon gas pipeline. The argon extrusion gas circuit branch device includes an argon cylinder 101 , an argon cylinder manual stop valve 102 , an argon pipeline filter 103 and an argon pipeline pressure gauge 104 . The argon cylinder 101 is mainly used to store the inert gas argon...

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Abstract

The invention provides a device and method for filling a solid lithium propellant pipeline. The device comprises an argon gas circuit sub-device, a cooling water control sub-device and a lithium propellant supply sub-device, wherein the lithium propellant supply sub-device is arranged in a vacuum chamber; outer walls of a lithium storage box, a lithium transfer storage box and a propellant pipeline in the lithium propellant supply sub-device are respectively provided with a heating film; a cooling valve is arranged on the propellant pipe between the lithium transfer storage box and an engine; the argon gas sub-device supplies gas pressure for the lithium storage box; and the cooling water control sub-device supplies cooling water for the cooling valve. According to the method disclosed by the invention, the propellant pipe at the downstream of the lithium transfer storage box is blocked by introducing the cooling water to the cooling valve, and solid alkali metal lithium is liquefied by the heating films and is then extruded into the lithium transfer storage box. The device and method disclosed by the invention has higher operability and practicability, realizes stable filling of the solid alkali metal lithium propellant in the lithium transfer storage box and the propellant pipeline and further provides the stable lithium propellant for an engine ground test.

Description

technical field [0001] The invention relates to a set of solid propellant pipeline filling device and method suitable for electric propulsion engine test, in particular to a pipeline filling technology of solid alkali metal propellant—lithium (Lithium). Background technique [0002] The magnetoplasma dynamic engine (MPDT) is a typical electromagnetic space electric propulsion system, which has the advantages of high specific impulse, large thrust range, long life, high control accuracy, 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). Research on various...

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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