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Ground direct and quantitative filling system and method

A quantitative filling and direct technology, applied in pipeline system, gas/liquid distribution and storage, jet propulsion device, etc. The effect of time

Active Publication Date: 2015-07-15
BEIJING INST OF SPACE LAUNCH TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Since the direct quantitative method on the ground is difficult to achieve the required filling accuracy, it is rarely used except for final repair and attitude control propellant filling, and there are no reports at home and abroad.

Method used

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  • Ground direct and quantitative filling system and method
  • Ground direct and quantitative filling system and method
  • Ground direct and quantitative filling system and method

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Experimental program
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Effect test

Embodiment Construction

[0062] The structural principle and working principle of the present invention will be described in detail below in conjunction with the accompanying drawings:

[0063] See figure 1 , figure 1 It is a schematic diagram of a filling system according to an embodiment of the present invention. The ground direct quantitative filling system of the present invention includes a stand 1 and a gas circuit system 2, a liquid circuit system 3, an electric control system 4, a filling tank 5, an overflow tank 6 and a filling and draining connector 8 arranged on the stand 1. , The fluid path system 3, the gas path system 2 and the electronic control system 4 are located in the platform, and are used to start the process, manipulate the valve, monitor and display, control the filling amount and filling accuracy, and adjust the filling The injection speed, the liquid system 3 is connected to the gas system 2, and the electronic control system 4 is connected to the liquid system 3, the gas system...

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PUM

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Abstract

The invention relates to a ground direct and quantitative filling system and a ground direct and quantitative filling method, which are used for filling an end correction storage container. The ground direct and quantitative filling system comprises a rack, an air channel system, a liquid path system, an electronic control system, a filling tank, an overflow tank, a waste gas treatment device, a filling and draining connector and an electronic scale, wherein the liquid path system, the air channel system and the electronic control system are positioned in the rack and are used for starting working procedures, controlling a valve, monitoring display, controlling a filling amount and filling accuracy and regulating filling speed. The filling method comprises the following steps of: controlling the filling accuracy, controlling filling flow, controlling the filling process, controlling filling time and controlling filling counter pressure. In the ground direct and quantitative filling system and the ground direct and quantitative filling method, the filling accuracy is close to the filling accuracy reached in a quantitative mode of the storage container on a rocket by utilizing technologies of controlling the filling accuracy, the filling flow, the filling process, the filling time and the like, 'one-button' type filling is realized, and the requirement of filling accuracy of the end correction storage container is met.

Description

Technical field [0001] The invention relates to a filling technology, in particular to a ground direct quantitative filling system and method that meets the filling accuracy requirements of a final repair level tank. Background technique [0002] The propellant filling technology of carrier rockets at home and abroad usually adopts the quantitative method of the tank on the arrow to achieve the required high filling accuracy. However, due to the structural limitations of some types of final repair tanks, there is no quantitative device inside, and the ground direct quantitative method must be used to achieve the required filling accuracy, and the filling process, filling speed and filling back pressure must be carried out. Automatic control. Since it is difficult to achieve the required filling accuracy with the direct quantitative method on the ground, it is rarely used except for terminal repair and attitude control propellant filling, and there is no report at home and abroad...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F02K9/50B67D7/08F17D1/08
Inventor 罗强
Owner BEIJING INST OF SPACE LAUNCH TECH