Abstract
The research progress on partial turbomachinery technology of high-bypass-ratio turbofan engine were reviewed and analyzed in the present study and the partial key technology of turbomachinery required for our country's high-bypass-ratio turbofan engine were also expatiated. The main contents included four aspects: fan/compressor design technique, turbine design technique, flow and noise control and multi-disciplinary coupling technique.
| Original language | English |
|---|---|
| Pages (from-to) | 1504-1518 |
| Number of pages | 15 |
| Journal | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| Volume | 23 |
| Issue number | 8 |
| State | Published - Aug 2008 |
Keywords
- Civil engine
- High-bypass-ratio
- Key turbomachinery technology
- Turbofan
- Turbomachinery
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