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Device for balanced discharge of parallel storage tanks

A storage tank and parallel connection technology, which is applied to jet propulsion devices, rocket engine devices, aerospace vehicle propulsion system devices, etc., can solve problems such as unbalanced discharge of parallel storage tanks, achieve improved product reliability, high flow control accuracy, The effect of low flow resistance

Inactive Publication Date: 2020-10-02
SHANGHAI INST OF SPACE PROPULSION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0008] Therefore, it is urgent to develop a device for balanced discharge of parallel storage tanks to solve the problem of unbalanced discharge of parallel storage tanks in the system.

Method used

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  • Device for balanced discharge of parallel storage tanks

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Embodiment Construction

[0032] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several changes and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0033] A device for balanced discharge of parallel storage tanks provided according to the present invention, comprising: a volumetric flowmeter A, a volumetric flowmeter B and a rigid interconnection mechanism;

[0034] The main shaft of the volumetric flowmeter A and the main shaft of the volumetric flowmeter B are connected through a rigid interconnection mechanism and rotate synchronously.

[0035] Specifically, it also includes: tank A, tank B;

[0036] The volumetric flowmeter A is connected to t...

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Abstract

The invention provides a device for balanced discharge of parallel storage tanks. The device comprises a volumetric flow meter A (2), a volumetric flow meter B (4) and a rigid interconnection mechanism (3), whereina main shaft of the volumetric flow meter A (2) is connected with a main shaft of the volumetric flow meter B (4) through the rigid interconnection mechanism (3). The device for balanceddischarge of parallel storage tanks has the advantages of being high in flow control precision, wide in pressure application range and high in viscosity adaptability, flow calibration can be completed in a single-machine state, system pipeline matching and system cold flow testing do not need to be conducted, system testing and structural layout are simplified, and product reliability is greatlyimproved.

Description

technical field [0001] The invention relates to the technical field of space propulsion systems. In particular, it relates to a device for balanced discharge of parallel storage tanks. Background technique [0002] During the working process of the spacecraft, there will be differences in the mass of propellant consumption in the two parallel storage tanks of the same component, and this difference is called the unbalanced discharge amount of the parallel storage tanks. Due to the unbalanced propellant consumption of the symmetrically arranged storage tanks, the center of mass of the spacecraft is constantly shifted during flight, which may cause the spacecraft to deviate from the flight track. In order to correct the flight deviation of the spacecraft, the attitude control engine needs to work continuously, consume too much propellant, so that the propellant is exhausted in advance; if the serious imbalance exceeds the ability of the attitude control engine to adjust the a...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/40F02K9/44F02K9/56
CPCB64G1/402F02K9/44F02K9/56
Inventor 马海涛陈健唐妹芳洪鑫金广明谭郦郦汪俊龙
Owner SHANGHAI INST OF SPACE PROPULSION
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