Liquid methane deep supercooling and filling system and method based on anti-freezing control

Abstract

The invention discloses a liquid methane deep supercooling and filling system and method based on anti-freezing control. The system comprises a ground liquid methane storage tank, a vertical liquid nitrogen bath type heat exchanger and an on-rocket liquid methane storage tank; the on-rocket liquid methane storage tank, a filling pipeline, an engine and other parts are pre-cooled by cold nitrogen after liquid nitrogen gasification before filling; during filling, a mode of filling while supercooling is adopted, a vertical liquid nitrogen bath heat exchanger is used for supercooling liquid methane to a 95K temperature zone, then the supercooled liquid methane enters a rocket storage tank, and the flow and the supercooling degree in the filling system are flexibly controlled through compositeadjustment based on pressure control and liquid level control; once it is detected that the liquid methane is frozen, pipelines are switched immediately, and high-pressure nitrogen is adopted for rapid rewarming melting treatment; and meanwhile, the gasified cold nitrogen is used for controlling the pressure of a gas pillow area of the on-rocket liquid methane storage tank and maintaining the supercooling degree of the liquid methane. According to the liquid methane deep supercooling and filling system and method based on anti-freezing control, the functions of liquid methane large supercooling degree acquisition, liquid methane supercooling anti-freezing control, self-adaptive adjustment of the supercooling heat exchanger to different flows and set temperature zones and the like are realized.

Description

technical field [0001] The invention relates to the technical field of acquisition and filling of liquid methane supercooling at a low-temperature rocket launch site, and in particular to a liquid methane deep supercooling and filling system and method based on anti-freezing control. Background technique [0002] With the development of aerospace technology, cryogenic launch vehicles are gradually moving towards commercialization, and cryogenic propellants are transitioning from the most popular combination of liquid hydrogen / liquid oxygen and liquid oxygen / kerosene to the more promising combination of liquid methane / liquid oxygen, so Liquid methane has been paid more and more attention as a new propellant fuel. There are many advantages in using liquid methane / liquid oxygen as low-temperature rocket fuel: 1. The liquefaction temperature (111.7K) is higher than that of hydrogen, which is easy to liquefy, and the production and storage costs are low, and the temperature diffe...

AI Technical Summary

Problems solved by technology

After calculation and analysis, it is concluded that the use of 77K liquid nitrogen heat exchange cooling technology to obtain deep subcooled liquid methane is the most economical, simple and reliable method. However, there are still the following technical difficulties in the application of this method to the filling system of cryogenic rocket launch sites: 1. Anti-freezing problem of deep subcooled liquid methane

When 77K liquid nitrogen is used for cooling, it is easy to solidify liquid methane, because the freezing point of liquid methane is relatively high (90.694K), so when filling at the launch site, if the operation is not performed according to the designed flow rate or the filling is stopped, The liquid methane will freeze in the subcooler, block the filling pipeline, there will be a delay in filling, and the possibility of affecting the launch, and once the subcooler is designed, it will be difficult to adjust the filling flow and liquid methane subcooling degree. Make the

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