Abstract
Considering the effect of atmospheric temperature, atmospheric humidity and fuel heating value, a corrected standardization model was proposed relating gas path parameter deviation based on third similarity theory, the multivariate nonlinear overdetermined equations were established using the historical data as learning sample, and the unknown parameters were solved using Gauss-Newton iterative method. The deviation was solved using the corrected standardization model proposed, and the result was compared with deviation solved by other models. the conclusion is drawn that the correction model proposed is closer to the original factory model with higher accuracy, and it is more innovative and has practical value.
| Original language | English |
|---|---|
| Pages (from-to) | 2592-2598 |
| Number of pages | 7 |
| Journal | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| Volume | 27 |
| Issue number | 11 |
| State | Published - Nov 2012 |
| Externally published | Yes |
Keywords
- Aero-engine
- Deviation
- Gas path parameter
- Similarity theory
- Standardization
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