Compressor Performance Curve Extrapolation Method Based on the Similarity Theory

Article Preview

Abstract:

Due to the fact that the low speed pump similarity theory is only applicable to incompressible fluid, this theory cannot be used for extrapolation of compressor performance curve. Considering the compressibility of working medium; therefore, this paper has modified the similarity theory and put forward a new index relationship equation. The two low speed performance lines which are already known were used to get the similar working points and extrapolate the performance lines through the optimization method. Compared with the existing performance lines, the results show that the method is simple, convenient and qualified with practicability and accuracy. This method plays an important role on studying startup process of a gas turbine and improving the accuracy of the simulation of startup process.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

1545-1549

Citation:

Online since:

October 2014

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2014 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] Songling Wang, Xuelei Zhang. Method Based on Similarity Laws for Extrapolating Generalized Performance Curves of Compressors[J]. Journal of Power Engineering. 2007, 27(2): 169-173.

Google Scholar

[2] Munson B R, Young D F, Theodor H O. Fundamentals of fluid mechanics third edition, 1998[J].

Google Scholar

[3] Lubing Xu, Shangneng Pan, Jingwei Chen. A Simple Exponent Extrapolation Method of Sub-idle Characteristics on Aero-engine[J]. Science Technology and Engineering. 2013 (18): 5404-5408.

Google Scholar

[4] Wayne R Sexton. A Method To Control Turbofan Engine Starting By Varying Compressor Surge Valve Bleed[D]. Virginia Polytechnic Institute and State University, (2001).

Google Scholar

[5] Agrawal R K, Yunis M. A generalized mathematical model to estimate gas turbine starting characteristics. Transactions of the ASME,1982; 104: 194—201.

DOI: 10.1115/1.3227249

Google Scholar

[6] Guang Wang, Jun Li. Exponent Extrapolation Method of Aero-Engine Turbomahinery Low State Characteristics[J]. Journal of Aerospace Power. 2005, 20(6): 1032-1036.

Google Scholar