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Thin-wall double-eccentric-part spherical shell structure provided with rigid shaft

A spherical shell structure, rigid shaft technology, applied in the cocks, engine components, mechanical equipment and other directions including cut-off devices, can solve the problems of valve seat and ball wear, increase the weight of the engine, reduce the reliability of the engine, etc., and reduce the weight. , The effect of simplifying the composition of the engine system and reducing wear and tear

Pending Publication Date: 2018-04-20
BEIJING AEROSPACE PROPULSION INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In order to avoid the wear of the valve seat and the ball during the action of the ball valve, the traditional engine ball valve design method is to first introduce the control air to separate the ball from the valve seat and then rotate the ball to avoid wear. The single switch action of the ball valve is decomposed into lift-open (Closing) - combined action of seating, the ball valve itself must be equipped with a lifting mechanism, and the engine must also be equipped with related lifting air control and electronic control systems, which will complicate the structure of the engine system and the ball valve itself, increase the weight of the engine, and reduce the reliability of the engine
However, the integral ball structure of traditional ball valves highlights the disadvantage of heavy weight on large-diameter valves.

Method used

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  • Thin-wall double-eccentric-part spherical shell structure provided with rigid shaft
  • Thin-wall double-eccentric-part spherical shell structure provided with rigid shaft
  • Thin-wall double-eccentric-part spherical shell structure provided with rigid shaft

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Embodiment Construction

[0022] The present invention will be described in detail below in conjunction with the accompanying drawings and examples.

[0023] Such as figure 1 As shown, the present invention is a double eccentric thin-walled spherical shell structure with a rigid shaft. The main body shape is a 1 / 4 part of the thin-walled spherical shell 1, and the ratio of the shell thickness to the outer diameter of a large-diameter ball valve with a ball diameter > 250 mm is 1 / 40. ~1 / 50, the advantage of this design is that the circumferential and radial dimensions of the spherical shell are reduced as much as possible under the condition of ensuring the strength, and the light weight of the sphere is realized. The lower end provides radial support for the spherical shell, and the rigid shaft 2 penetrates between the upper and lower end faces, which is connected with the spherical shell 1 through the upper spline 3 and the lower spline 5, so as to realize the overall rotation of the thin-walled spher...

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PUM

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Abstract

A thin-wall double-eccentric-part spherical shell structure provided with a rigid shaft comprises a thin-wall spherical shell (1) and the rigid shaft (2); the thin-wall spherical shell (1) is a spherical-crown-shaped part for realizing a sealing function in a ball valve closed state; the upper end surface and the lower end surface of the spherical-crown-shaped part are sector-shaped surfaces; therigid shaft penetrates through the upper sector-shaped surface and the lower sector-shaped surface and is fixedly connected with the upper sector-shaped surface and the lower sector-shaped surface; eccentric distances exist between the rotating center of the rigid shaft and the geometric center of the spherical-crown-shaped part in the relative radial direction and in the relative axial direction;and the whole spherical shell structure is driven by an external driving mechanism to rotate.

Description

technical field [0001] The invention relates to a thin-walled double eccentric partial spherical shell structure with a rigid shaft suitable for a ball valve of a liquid rocket engine. . Background technique [0002] Ball valves are widely used as propellant supply switches in liquid rocket engines. Ball valves have the characteristics of small flow resistance and are not limited by working pressure and flow size. [0003] In order to avoid the wear of the valve seat and the ball during the action of the ball valve, the traditional engine ball valve design method is to first introduce the control air to separate the ball from the valve seat and then rotate the ball to avoid wear. The single switch action of the ball valve is decomposed into lift-open (Closing)-seat combined action, the ball valve itself must be equipped with a lifting mechanism, and the engine must also be equipped with related lifting air control and electronic control systems, which will complicate the st...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F16K5/06
CPCF16K5/0605F16K5/0647
Inventor 刘博李楚林赵莹向猛周炜孙纪国郑孟伟陶瑞峰许健陈涛张强
Owner BEIJING AEROSPACE PROPULSION INST
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