Optimal design of high-performance aerostatic equipment based on finite difference method with flux error feedback
This paper proposes an aerostatic lubrication model with the use of finite difference method, and the solution of the model is designed with the combination of flux error feedback and grid parameter optimization. The model and solution are validated by the performance test on the slider with the dia...
Main Authors: | Tao Lai, Xiaoqiang Peng, Junfeng Liu |
---|---|
Format: | Article |
Language: | English |
Published: |
SAGE Publishing
2020-11-01
|
Series: | Measurement + Control |
Online Access: | https://doi.org/10.1177/0020294018824124 |
Similar Items
-
Investigation of the performance of an aerostatic precision postitioning stage with aerostatic capstan driven system
by: 游積富
Published: (2004) -
Aerostatic Architecture. Theory of Unsupported Aerostatic Coverings
by: Victor Logvinov
Published: (2011-05-01) -
Characteristics Analysis and Optimization for Aerostatic Bearings
by: Chih-Chi Lu, et al.
Published: (2006) -
An Optimization Method for the Main Influence Factors on the Performance of Aerostatic Spindle
by: Dongju Chen, et al.
Published: (2019-01-01) -
Impact Diagnostic of Aerostatic Spindle Unit with Aerostatic Beaings
by: R. A. Poshekhonov, et al.
Published: (2014-01-01)