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A Damping Structure to Prevent Oscillation of Reducer

A technology of damping structure and pressure reducer, applied in the field of damping structure, can solve the problems of difficult vibration reduction, over-damping, low damping, etc.

Active Publication Date: 2020-10-23
BEIJING INST OF CONTROL ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The technical problem solved by the present invention is: in view of the problems in the current prior art that the two damping structures tend to cause small damping due to their own structures, difficult vibration reduction or over-damping, and easy to produce large deviations in locking pressure, a new design is proposed. A Damping Structure to Prevent Oscillation of Reducer

Method used

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  • A Damping Structure to Prevent Oscillation of Reducer
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  • A Damping Structure to Prevent Oscillation of Reducer

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Embodiment Construction

[0020] A damping structure to prevent the vibration of the pressure reducer, including the main spring 1, the adjusting gasket 2, the spring seat 3, the damping rubber block 4, the valve body 5, and the diaphragm assembly 6. The working principle of this device is: The spring seat 3 on the surface of the damping rubber block 4 and the spring force after assembling the main spring 1 make the damping rubber block 4 produce radial deformation and contact with the side wall of the valve body 5 . When the pressure reducer vibrates, the generated vibration causes reciprocating friction and tangential deformation on the outer edge of the damping rubber block 4 to damp the vibration of the pressure reducer.

[0021] The following will be further explained in conjunction with specific examples:

[0022] Such as figure 1 with figure 2 As shown, the diaphragm assembly 6 is installed on the bottom of the valve body 5, and its lower end is connected to the valve core. The adjusting gask...

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Abstract

A damping structure capable of preventing oscillation of a pressure reducer comprises a main spring (1), an adjustment gasket (2), a spring seat (3), a damping rubber block (4), a valve body (5) and adiaphragm assembly (6). Under the spring force effect of the main spring (1), the damping rubber block (4) is forced to generate initial deformation and stops till the spring seat (3) presses the adjustment gasket (2), and at the moment, the outer edge of the damping rubber block (4) makes contact with the side wall of the valve body (5). When the pressure reducer is oscillated, the spring seat (3) and the diaphragm assembly (6) axially vibrate relative to the valve body (5), the contact parts of the damping rubber block (4) and the valve body (5) generate reciprocating friction or tangentialdeformation to absorb vibration energy, and thus the effect of preventing oscillation is achieved. The magnitude of damping is controlled by controlling the thickness of the adjustment gasket (2), the damping, with the appropriate magnitude, required by the pressure reducer can be provided, the problem that an existing damping structure is prone to underdamping or over-damping is solved, the structure is stable, and the oscillation reducing effect is good.

Description

technical field [0001] The invention relates to a damping structure for preventing vibration of a pressure reducer, which belongs to the field of damping regulation. Background technique [0002] The pressure reducer is one of the key components of the satellite dual-component propulsion system. Its function is to reduce the high-pressure helium in the upstream high-pressure cylinder to the required low pressure, and provide it to the downstream oxidant storage tank and combustion agent storage tank, so that the storage tank Pressure remains relatively constant during satellite transfer orbits. Oscillation phenomenon is prone to occur during the operation of the pressure reducer. Oscillation will cause damage to the pressure reducer valve port and sensitive components, which may cause the pressure reducer to fail, and the downstream pressure cannot be controlled, resulting in the failure of the entire star propulsion system. In order to ensure that the engine works near th...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F16F15/08
CPCF16F15/085
Inventor 王振兴夏继霞冉荣姜华南柯王兆立曹长新沈岩魏延明张雅斌周磊李胜军刘旭辉张涛李新光谢继香周旭冉李伟
Owner BEIJING INST OF CONTROL ENG