Abstract
By analyzing the features of the three-dimensional numerical simulation results for the design scheme of a helium compressor, given were the design direction and guiding principle for its three-dimensional optimized modification design. By employing such methods as adjusting the distribution of blade thickness and the curvature of blade trailing edge profile as well as terminal-bend technology etc., a full three-dimensional optimization design was performed of the aerodynamic design version of the prototype helium compressor. A contrast analysis was conducted of the numerical simulation results before and after the three-dimensional optimized design. The efficiency of the compressor after the three-dimensional optimized design has been increased by 2 percent, effectively limiting the further development of secondary flows.
| Original language | English |
|---|---|
| Pages (from-to) | 504-511 |
| Number of pages | 8 |
| Journal | Reneng Dongli Gongcheng/Journal of Engineering for Thermal Energy and Power |
| Volume | 22 |
| Issue number | 5 |
| State | Published - Sep 2007 |
Keywords
- Blade modeling
- Controllable diffusion blade profile
- Helium compressor
- Three-dimensional optimization
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