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High-pressure fluid multi-stage pressure reducing device

A technology of depressurizing device and high-pressure fluid, which is applied in the directions of jet propulsion device, rocket engine device, pipe/pipe joint/pipe fitting, etc. It is not conducive to the layout of the depressurization pipeline, etc., to achieve the effect of easy disassembly, good application effect and simple structure

Pending Publication Date: 2022-07-08
XIAN AEROSPACE PROPULSION TESTING TECHN INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to solve the problem of pressure reduction of high-pressure and large-flow fluids, the present invention mostly uses multi-stage orifice plates to reduce pressure. There are large distances between orifice plates at all levels, which is not conducive to the arrangement of pressure-reducing pipelines, and when the working conditions of the engine change, the pressure-reducing method can be adjusted. For the technical problem of large disassembly and assembly of orifice plate size, a high-pressure fluid multi-stage depressurization device is provided

Method used

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  • High-pressure fluid multi-stage pressure reducing device

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Embodiment Construction

[0041] The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments do not limit the present invention.

[0042] In order to solve the many disadvantages of using the multi-stage orifice plate depressurization method at present, the present invention designs a high-pressure fluid multi-stage depressurization device with adjustable flow rate, which can reduce the high-pressure propellant (above 10MPa) after the engine pump through the multi-stage depressurization device. The pressure drop is below 1MPa, and at the same time, it has the advantages of small occupied space and adjustable flow rate, and can realize the rapid recovery of propellant after the rocket engine test pump.

[0043] like figure 1 As shown, a high-pressure fluid multi-stage depressurization device includes a coaxially arranged shel...

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Abstract

The invention belongs to a pressure reducing device and a debugging system, and provides a high-pressure fluid multi-stage pressure reducing device in order to solve the technical problems that a multi-stage pore plate pressure reducing mode is mostly adopted when high-pressure large-flow fluid is subjected to pressure reducing at present, pressure reducing pipeline arrangement is not facilitated, and the dismounting and mounting workload is large, and the high-pressure fluid multi-stage pressure reducing device comprises a shell and an inner core which are coaxially arranged. The shell is of a hollow structure with the two ends open, and the two ends of the shell are used for being connected with external fluid pipelines respectively. The inner core is fixedly arranged in the shell. A first-stage throttling structure, a second-stage throttling structure and a third-stage throttling structure are sequentially arranged in the shell from the fluid inlet end to the fluid outlet end, and the first-stage throttling structure, the second-stage throttling structure and the third-stage throttling structure are coaxially arranged outside the inner core and used for sequentially throttling flowing fluid. Expansion cavities are formed in the positions, between the first-stage throttling structure and the second-stage throttling structure and between the second-stage throttling structure and the third-stage throttling structure, in the shell correspondingly and used for sequentially reducing the pressure of fluid flowing through the expansion cavities.

Description

technical field [0001] The invention belongs to a decompression device, in particular to a high-pressure fluid multistage decompression device. Background technique [0002] In the semi-system test of the pump-pressed liquid rocket engine, the pressure of the propellant after the engine pump can reach more than 10MPa. It is necessary to reduce the pressure of the high-pressure propellant after the engine pump from more than 10MPa to less than 1MPa, and return it to the recovery container. [0003] At present, for the depressurization of high-pressure and large-flow fluids, in order to prevent cavitation of the fluid, most of them use multi-stage orifice plate depressurization. When this method is adopted, the spacing between the orifice plates at all levels needs to be greater than 10 times the diameter of the pipeline, which is not conducive to the arrangement of the depressurization pipeline. At the same time, when the engine operating conditions change, the size of the p...

Claims

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Application Information

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IPC IPC(8): F02K9/96F02K9/56F16L55/027
CPCF02K9/96F02K9/56F16L55/02754Y02B30/70
Inventor 周璟莹丁佳伟李谦张俊锋郭浩路泽鑫薛博凯黄立还朱小江李宗昌王颖
Owner XIAN AEROSPACE PROPULSION TESTING TECHN INST