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In-series redundant type device

A redundant, tandem single technology, applied in jet propulsion units, rocket engine units, machines/engines, etc., can solve the problem of undiscovered instructions and reports, the number of times and leak rates of propellant control valves cannot meet such severe requirements, Can not use 150N engine and other problems to achieve the effect of light weight, ingenious design, and many movements

Active Publication Date: 2019-12-03
SHANGHAI INST OF SPACE PROPULSION
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The highly reliable serial redundant device is different from the traditional propellant control valve in that the working frequency and leakage rate of the traditional propellant control valve cannot meet such strict requirements, and cannot be used for the 150N engine of the 921 third phase project
[0006] At present, there is no high-reliability series redundant device in China, and there is no public information on the design scheme of similar principles in foreign countries, and no description and report of similar technology to the present invention have been found. Therefore, the high-reliability series redundant device is a new design. field

Method used

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Embodiment Construction

[0030] 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.

[0031] Such as figure 1 As shown, the embodiment of the present invention provides a highly reliable series redundant device, including two single valve assemblies 1, inlet joint 2, filter screen assembly 4, throttle orifice 5 and outlet joint 3, the two The single valve assembly 1 is used to control the on-off of the propellant, relying on the axial movement of the internal moving parts to realize the function of opening or closing the valve; relying on the internal non-metallic seal to press and fit o...

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PUM

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Abstract

The invention provides a high-reliability in-series redundant type device, which comprises a single valve assembly, an inlet connector, a filter screen assembly, a throttling orifice plate and an outlet connector. The two single valve assemblies are used for controlling on-off of propellant, and the function of opening or closing the valve is achieved through axial movement of the internal movingpart. Reliable sealing when the single valve assembly is closed is achieved by pressing and attaching an internal non-metal sealing piece to the metal base. The two single valve assemblies are connected in series and fixedly welded, and the inlet connector is used for being connected with an upstream pipeline and further used for containing the filter screen assembly. The filter screen assembly isused for preventing excess materials in the working medium from entering the inner cavity of the valve; the outlet connector is used for being connected with a downstream engine. The orifice plate isused for adjusting the flow of the propellant. By means of the structural design, the kinematic pair design, the magnetic circuit design and the sealing pair design, the requirements for high sealingreliability, multiple action times, long service life, light weight and quick response can be met.

Description

technical field [0001] The invention relates to a highly reliable serial redundant device for a core cabin of a space station, in particular to a serial redundant device. Background technique [0002] The high-reliability series redundant device is an important part of the attitude and track control system of the 921 Phase III project. [0003] The 921 Phase III project has greatly improved the index requirements for 150N engines compared with Phase II, and the control valves matched with 150N engines have much stricter working times and life requirements. In order to meet the overall new indicators for 150N engine solenoid valves, According to the requirements of the engine control valve design task book, a series redundant reed solenoid valve is designed, which is used for the propellant supply of the 150N binary engine of the core module propulsion subsystem of the space station, and realizes engine ignition and shutdown. [0004] According to the requirements of the cor...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02K9/58F02K9/60
CPCF02K9/58F02K9/60
Inventor 许闯柳珊尤罡胡施俊黄俊杰黄爱清张宝建
Owner SHANGHAI INST OF SPACE PROPULSION
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