Eureka AIR delivers breakthrough ideas for toughest innovation challenges, trusted by R&D personnel around the world.

Method for designing optimal static parameter of radial static pressure gas bearing of turbine expansion engine

A technology of static pressure gas bearings and turbo expanders, which is applied to bearings, shafts and bearings, mechanical equipment, etc., and can solve problems such as low precision

Inactive Publication Date: 2012-01-04
INST OF PLASMA PHYSICS CHINESE ACAD OF SCI
View PDF0 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The purpose of the present invention is to provide a method for designing the optimal static parameters of a radial static pressure gas bearing of a turbo expander, aiming at the low accuracy of the design method of the radial throttle small hole static pressure gas bearing of a turbo expander, the design method Many factors are ignored in the derivation

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

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

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

The invention relates to a method for designing optimal static parameters of a radial static pressure gas bearing of a turbine expansion engine, comprising the following steps: decomposing a journal bearing into a plurality of equivalent slits, listing a differential equation of gas movement, obtaining an equation about bearing capacity coefficient CW, bearing rigidity coefficient KW, total flow M and the total frictional power loss FT based on the differential equation, and obtaining the optimal static parameters for a radial throttling hole static pressure gas bearing of the turbine expansion engine on the condition of different eccentricity ratios obtained through the equation of the bearing capacity coefficient CW, bearing rigidity coefficient KW, total flow M and the total frictional power loss FT. The invention can obtain four performance parameters reflecting the radial throttling hole static pressure gas bearing realized by calculation of one program, therefore, the determined optimal static parameters has high precision in engineering application and can be used for designing the radial throttling hole static pressure gas bearing of the turbine expansion engine with high rotation speed and special usage.

Description

technical field The invention relates to the field of bearing design, can be used to determine the best static parameters of radial throttle small hole static pressure gas bearings of turbo expanders, and is suitable for radial throttle small hole static pressure of various working gas turbo expanders The static design of the gas bearing can also be used in the performance calculation of the radial throttling small hole static pressure gas bearing. Background technique The gas bearing has the characteristics of high speed, low friction and less pollution. It is the most ideal form for the turbo expander, and it is also its core component. Compared with the dynamic pressure gas bearing, the static pressure gas bearing has the characteristics of high load capacity and stable operation. Restricted by the domestic processing level, there is no application of dynamic pressure gas bearings in China at present. Throttle orifice static pressure gas bearings are currently the most c...

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
Patent Type & Authority Patents(China)
IPC IPC(8): G06F17/50F01D25/16F16C32/06
Inventor 王学敏庄明傅豹丘立龙
Owner INST OF PLASMA PHYSICS CHINESE ACAD OF SCI
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
Eureka Blog
Learn More
PatSnap group products