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Full-unloading disc type magnetic pole large-drift-diameter two-position three-way electromagnetic valve

A two-position three-way, large-diameter technology, used in multi-way valves, lift valves, valve details, etc., can solve the problems that affect the response performance of high-thrust engines, limit the capacity of intake and exhaust channels, structural size and weight, etc. Achieve the effect of improving magnetic efficiency, light structure and high applicable pressure

Pending Publication Date: 2021-08-24
XIAN AEROSPACE PROPULSION INST
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  • Abstract
  • Description
  • Claims
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AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to solve the slow opening and closing response, large structural size and weight of the existing two-position three-way solenoid valve with no unloading and large diameter design, thereby limiting the capacity of the intake and exhaust passages, and affecting large thrust engines above 3000N Insufficient response performance, and provide a fully unloaded disc magnetic large diameter two-position three-way solenoid valve

Method used

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  • Full-unloading disc type magnetic pole large-drift-diameter two-position three-way electromagnetic valve

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Embodiment Construction

[0024] The present invention will be further described below in conjunction with the accompanying drawings and exemplary embodiments.

[0025] refer to figure 1 , the present invention provides a two-position three-way solenoid valve with a full unloading disc type magnetic maximum diameter, including a valve body 1, an electromagnetic housing 2, an outer lining ring 3, an inner lining ring 4, an exhaust valve seat 5, and an intake valve Seat 6, spool rod 7, return spring 8, magnetic disk 9 and coil 10; Described valve body 1 is docked with electromagnetic housing 2 to form a first chamber, and outer lining ring 3 is arranged in the first chamber, and outer lining ring 3 and A second chamber is formed between the valve body 1, and a third chamber is formed between the outer lining ring 3 and the electromagnetic housing 2; the inner lining ring 4 is arranged in the second chamber, and the inner wall of the inner lining ring 4 is radially An annular protruding exhaust valve sea...

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Abstract

The invention relates to a two-position three-way electromagnetic valve, in particular to a full-unloading disc type magnetic pole large-drift-diameter two-position three-way electromagnetic valve, which is used for solving the problems that when an existing two-position three-way electromagnetic valve is designed in a non-unloading large-drift-diameter mode, the opening and closing response is slow, the structural size and the weight are large, then the capacity of an air inlet channel and an air outlet channel is limited, and the response performance of a high-thrust engine of over 3000N is influenced. The full-unloading disc type magnetic pole large-drift-diameter two-position three-way electromagnetic valve comprises a valve body, an electromagnetic shell, an outer lining ring, an inner lining ring, an exhaust valve seat, an air inlet valve seat, a valve element rod, a reset spring, a magnetic disc and a coil.

Description

technical field [0001] The invention relates to a two-position three-way solenoid valve, in particular to a two-position three-way solenoid valve with a full unloading disc type magnetic maximum diameter. Background technique [0002] In the fast-response high-thrust orbital control engine, the system sometimes requires the control valve to meet the high-flow and high-pressure requirements of the high-thrust engine above 3000N, and at the same time, it should also achieve fast opening and closing response, light structure and valve flow resistance loss low performance. In order to meet the above scheme, an electro-pneumatic valve structure composed of a two-position three-way electromagnetic auxiliary valve and a two-position two-way air-controlled main valve is usually used. The control of inflation pressure build-up and exhaust pressure relief is realized by using the change of the air pressure in the control chamber to realize the opening and closing control of the main ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F16K11/044F16K1/36F16K31/06F16K27/02
CPCF16K11/044F16K1/36F16K31/0627F16K27/0263F16K27/029
Inventor 罗大亮朱建国张思坤魏学峰闫旭宇
Owner XIAN AEROSPACE PROPULSION INST
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