Tip Clearance Optimization of High Speed Engine Pump Based on Simulation and Experimental Verification

Author:

Song Ping1,Hao Zhi Yong1,Ye Hui Fei1,Mao Jie1,Zhang Lei1

Affiliation:

1. Zhejiang University

Abstract

An improved program of the tip clearance of a high speed engine pump based on simulation was introduced in this paper. In order to verify its reliability, a device was designed to test the performance of the pump and found that the simulation data was in good agreement with the experiment. Within the scope of work, the improved pump shows excellent performance that the head has an improvement of more than 7m averagely, the efficiency is improved by 10 % to 20 %, and the shaft power has increased about 100Wrespectively.The results confirmed that using this numerical analysis method to optimize the tip clearance of the high speed engine pump was reasonable.

Publisher

Trans Tech Publications, Ltd.

Reference13 articles.

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2. Schaub U W,Vlasic E,Moustapha S H. Effect of Tip Clearance on the Performance of a Highly Loaded turbine Stage. In: Henderson R E. AGARD-CP-537. Technology Requirement for Small Gas Turbines. Montreal, Canada: North Atlantic Treaty Organization, 1993, (10): 29-1-29-11.

3. Xiao X W. Investigation of Tip Clearance Flow Physics in Axial Flow Turbine Rotors[D]. Pennsylvania:Pennsylvania State University, (2001).

4. Dring R P, Johslyn H D, Hardin L. An investigation of axial compressor rotor aerodynamics[J]. ASME Journal of Engineering for Power, 1982, 104 (1): 84~96.

5. Pouagare M, Delaney R A. Study of three-dimensional viscous flows in an axial compressor cascade including tip leakage effects using a SIMPLE-based algorithm[J]. ASME Journal of Turbomachinery, 1986, 108(1): 51~58.

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