Supersonic nozzle of supersonic speed rotational flow natural gas separator

A supersonic, natural gas technology, applied in the fields of processing and processing, natural gas gathering and transportation, can solve the problems of reduced nozzle efficiency, low uniformity and stability of supersonic gas flow velocity, and can not be well satisfied.

Inactive Publication Date: 2009-03-18
曹学文
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The nozzle can produce droplets with a particle size of 0.1 microns to 2.5 microns, but the nozzle does not consider the influence of factors such as flow velocity uniformity and pressure loss on the supersonic cyclone natural gas separator
The supersonic gas flow in the supersonic nozzle tends to form a self-excited oscillation phenomenon, which leads to a large energy loss and reduces the efficiency of the nozzle. Nozzle Performance Requirements

Method used

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  • Supersonic nozzle of supersonic speed rotational flow natural gas separator
  • Supersonic nozzle of supersonic speed rotational flow natural gas separator
  • Supersonic nozzle of supersonic speed rotational flow natural gas separator

Examples

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Embodiment Construction

[0011] The accompanying drawing is an example of a typical supersonic nozzle designed and processed according to the purpose of the present invention. The supersonic nozzle is a cylindrical shell. figure 1 It is a sectional view of a supersonic nozzle, which is composed of a contraction pipe section (1), an expansion pipe section (2) and a rectification pipe section (3).

[0012] figure 2 It is a sectional view of the shrinkage section of the supersonic nozzle, and the shrinkage section of this example is composed of the shrinkage pipe (4) and the straight pipe (5). The surface curve of the shrink tube is a cubic polynomial, the diameter of the inlet is 100mm, the diameter of the outlet is 12.4mm, the length of the shrink tube is 186mm, the shrinkage angle is 15°, and the tangent of the inlet and outlet ends of the shrink tube is parallel to the axial direction. The length of the straight pipe at the end of the shrinkage pipe is 1.0 mm. This straight pipe is the throat of t...

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Abstract

The invention provides a supersonic jet tube used for a supersonic cyclone natural gas separator, which is a key part of the separator, and consists of a contraction tube section, an extension tube section and a rectifying tube section. A moulding surface curve of the contraction tube section is higher-order polynomial, and natural gas airflow is expanded and accelerated in the section to achieve sonic velocity so as to form a straight sonic flow. The moulding surface curve of the extension tube section consists of a plurality of sections of curve, and the sections are smoothly connected to reduce disturbance to the airflow. The moulding surface curve of the supersonic jet tube at inlet and outlet changes flatly, has small curvature change, and has weak influence on the flowing of fluid upstream and downstream without obvious inlet and outlet effect. The extension tube has smooth inlet transition with small disturbance to the fluid. The extension tube section has flat change of moulding surface curve, small airflow expansion rate and good flow speed evenness, thereby helping droplet condensation nucleus grow larger grain diameter for separating. The supersonic jet tube not only evenly accelerates the airflow, improves evenness and stability of flow field, and reduces turbulivity, so that outlet airflow has better airflow quality, and can form droplets with larger grain diameter to improve the separation efficiency of the supersonic cyclone natural gas separator.

Description

Technical field [0001] The invention relates to a supersonic nozzle, which is a key component of a supersonic cyclone natural gas separator and belongs to the technical field of natural gas gathering, transportation, processing and treatment. Background technique [0002] The supersonic cyclone natural gas separator developed by supersonic cyclone separation technology is composed of Laval nozzle, supersonic rectifier, supersonic wing, diffuser and other components. It combines the theories of gas dynamics, thermodynamics and fluid mechanics, and integrates expansion and cooling, cyclone gas / liquid separation, recompression and other processes in a closed and compact device. The gas flow passes through the Laval nozzle and expands adiabatically to supersonic speed, forming a low temperature and low pressure. The low temperature causes the heavy hydrocarbons and water in the natural gas to condense into nuclei and grow into small droplets, forming a gas-liquid mixed flow. T...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F25J3/06B01D45/16
Inventor 曹学文杜永军陈丽
Owner 曹学文
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