Research Article
Vibration Reliability Analysis of Aeroengine Rotor Based on Intelligent Neural Network Modeling Framework
Table 2
The analysis results of R and QAR data.
| GMT/HH:MM:SS | BALT/FEET | CAS/KNOTS | EGT1/DEGC | EGT2/DEGC | FF1/PPH | FF2/PPH | TAT/DEGC | … | R |
| 9:00:01 | 1856 | 188 | 759 | 758 | 7504 | 7344 | 23.75 | … | 0.6941 | 9:00:02 | 1856 | 190 | 758 | 758 | 7504 | 7344 | 23.75 | … | 0.7096 | 9:00:03 | 1888 | 195 | 758 | 757 | 7488 | 7360 | 24 | … | 0.7074 | 9:00:04 | 1888 | 195 | 757 | 750 | 7520 | 7376 | 24 | … | 0.6899 | … | … | … | … | … | … | … | … | … | … | 10:00:01 | 36096 | 252 | 647 | 640 | 2816 | 2816 | −26.75 | … | 0.9188 | 10:00:02 | 36096 | 252 | 647 | 640 | 2816 | 2816 | −26.75 | … | 0.9311 | 10:00:03 | 36096 | 253 | 647 | 640 | 2816 | 2816 | −26.75 | … | 0.9247 | 10:00:04 | 36096 | 253 | 647 | 640 | 2816 | 2816 | −26.75 | … | 0.9053 | … | … | … | … | … | … | … | … | … | … | 12:00:01 | 10944 | 176 | 421 | 410 | 736 | 720 | 2.25 | … | 0.7492 | 12:00:02 | 10912 | 176 | 421 | 410 | 736 | 720 | 2.25 | … | 0.7297 | 12:00:03 | 10912 | 176 | 422 | 411 | 736 | 720 | 2.5 | … | 0.7598 | 12:00:04 | 10880 | 176 | 422 | 411 | 736 | 736 | 2.5 | … | 0.7116 |
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