Supersonic wing of supersonic spiral natural-gas separator

A supersonic, separator technology, used in separation methods, dispersed particle separation, and production of fluids, etc., and can solve problems such as airflow disturbance, shock waves, and energy loss.

Inactive Publication Date: 2007-01-17
曹学文 +1
View PDF0 Cites 5 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The supersonic wing is the key component of the supersonic cyclone natural gas separator. It has been reported abroad that a flat triangular wing is used for the supersonic cyclone natural gas separator. Since the gas-liquid mixed flow velocity of the supersonic wing section is su

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Supersonic wing of supersonic spiral natural-gas separator
  • Supersonic wing of supersonic spiral natural-gas separator
  • Supersonic wing of supersonic spiral natural-gas separator

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0017] The accompanying drawing is a typical supersonic airfoil example designed and processed according to the purpose of the present invention. The separation section of the supersonic cyclone natural gas separator where the supersonic airfoil is located is a cylindrical shell with an inner diameter of 8.5 mm. figure 1 and figure 2 is the three-dimensional structure diagram of the supersonic airfoil, where figure 1 is the view from the convex side of the supersonic airfoil, figure 2 is the view from the underside of the supersonic airfoil. The supersonic airfoil is composed of a leading edge 1 , a trailing edge 2 , a bottom surface 3 , a convex side surface 4 , a concave side surface 5 and an apex 6 . The bottom surface of the supersonic airfoil is a cylindrical surface, coincides with the inner wall of the airfoil tube, and is fixed on the inner wall. The arc 7 on the bottom surface is a parabola, the axial length, ie, the chord length, is 42.50-76.50 mm, and the opti...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

No PUM Login to view more

Abstract

A supersonic wing of supersonic cyclone natural-gas separator is the critical part. Bottom of supersonic wing is cylindrical or circular platform face, which fits the internal wall of wing sectional pipe and is fixed on the internal wall. The mean camber line of base is para-curve, wing thickness of bottom varies by three-time polynomial law, cylindrical supersonic-wing bottom shape is determined by bottom mean camber line and bottom wing thickness variation model, top of wing aggregates on one point, which is supersonic wing vertex, two sides are concave and convex faces, which are constituted by vertex and bottom boarder line connection; low-temperature supersonic natural gas homogeneous axial flow formed by thermal-insulating expansion is converted into supersonic cyclone, mixture flow of gas and condensate liquid in supersonic cyclone separating area passes by supersonic tail wing at supersonic speed, to form high-speed cyclone field, and gas-liquid separation is finished through tremendous centrifugal force produced by cyclone.

Description

Technical field [0001] The invention relates to a key component of a supersonic cyclone natural gas separator—a supersonic wing, which 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 tube, supersonic wing, diffuser tube and other components. It combines the theories of gas dynamics, thermodynamics and fluid mechanics. Expansion and cooling, cyclone gas / liquid separation, recompression and other processes are completed 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 and nucleate, and grow into small droplets to form a gas-liquid mixed flow; th...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
IPC IPC(8): C10G5/06B01D53/00B01D45/12E21B43/36F25J3/08
Inventor 曹学文何川陈丽杜永军姚英凤林宗虎
Owner 曹学文
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap