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LucasThil
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nasa_turbofan_degradation_FD004

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unit_number
int64
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13.61
333.13
2,323.69
8,713.43
1.07
44.08
313.51
2,387.8
8,052.98
9.189
0.02
362
2,324
100
24.42
14.5716
265
1
57
0.0015
0.0008
100
518.67
642.24
1,572.87
1,401.95
14.62
21.58
551.39
2,387.33
9,034.22
1.3
47.08
518.82
2,387.35
8,121.79
8.4091
0.03
391
2,388
100
38.76
23.2879
264
1
58
42.0047
0.84
100
445
549.06
1,341.57
1,106.69
3.91
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138.78
2,211.87
8,305.27
1.02
41.75
130.18
2,387.96
8,076.8
9.3639
0.02
327
2,212
100
10.54
6.275
263
1
59
24.9987
0.6209
60
462.54
536.57
1,251.72
1,035.54
7.05
9.01
174.73
1,915.23
8,003.35
0.93
36.48
163.88
2,028.13
7,868.12
10.8975
0.02
305
1,915
84.93
14.34
8.5356
262
1
60
20.0033
0.7007
100
491.19
606.79
1,476.45
1,236.52
9.35
13.62
333.23
2,323.68
8,711.42
1.07
44.15
313.04
2,387.8
8,056.63
9.2197
0.02
362
2,324
100
24.26
14.7787
261
1
61
35.0027
0.84
100
449.44
555.26
1,358.23
1,112.98
5.48
7.97
194.11
2,222.82
8,338.06
1.02
41.44
182.03
2,387.88
8,060.79
9.2936
0.02
333
2,223
100
14.68
9.0174
260
1
62
42.0028
0.841
100
445
549.01
1,344.57
1,111.48
3.91
5.7
137.91
2,211.9
8,312.01
1.01
41.7
129.38
2,387.95
8,078.08
9.3956
0.02
329
2,212
100
10.59
6.3125
259
1
63
0.0026
0
100
518.67
642.41
1,574.98
1,388.29
14.62
21.57
550.74
2,387.57
9,037.5
1.3
46.95
519.63
2,387.56
8,120.54
8.4093
0.03
390
2,388
100
38.83
23.3222
258
1
64
9.9987
0.25
100
489.05
603.91
1,492.47
1,295.89
10.52
15.47
392.92
2,318.69
8,768.53
1.26
45.03
370.33
2,387.88
8,116.15
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0.03
370
2,319
100
28.66
17.2008
257
1
65
0.0002
0.001
100
518.67
641.68
1,576.52
1,391.43
14.62
21.58
552.7
2,387.96
9,047.17
1.3
46.91
521.18
2,387.92
8,126.44
8.3885
0.03
389
2,388
100
39.06
23.4061
256
1
66
42.0043
0.84
100
445
549.25
1,338.23
1,115.55
3.91
5.69
137.76
2,211.91
8,309.32
1.01
41.64
129.91
2,388
8,070.94
9.3859
0.02
327
2,212
100
10.65
6.303
255
1
67
35.0054
0.84
100
449.44
555.43
1,351.45
1,109.9
5.48
7.98
193.43
2,222.81
8,339.26
1.02
41.55
182.41
2,387.89
8,062.45
9.3215
0.02
333
2,223
100
14.9
9.0315
254
1
68
0.0001
0
100
518.67
641.78
1,581.16
1,390.67
14.62
21.58
552.27
2,387.91
9,044.67
1.3
46.91
520.44
2,387.95
8,130.78
8.4128
0.03
392
2,388
100
39.14
23.4225
253
1
69
0.0008
0
100
518.67
641.46
1,579.82
1,390.55
14.62
21.59
553.15
2,387.96
9,053.86
1.3
47.14
520.54
2,387.93
8,129.57
8.4031
0.03
391
2,388
100
39.06
23.3688
252
1
70
41.9999
0.8414
100
445
548.58
1,344.66
1,117.54
3.91
5.7
137.96
2,211.94
8,311.46
1.02
41.72
130.09
2,388.03
8,078.86
9.3526
0.02
329
2,212
100
10.57
6.3225
251
1
71
10.0061
0.25
100
489.05
603.79
1,491.5
1,300.18
10.52
15.46
393.13
2,318.68
8,762.49
1.26
44.93
370.13
2,387.85
8,123.16
8.6166
0.03
367
2,319
100
28.65
17.2694
250
1
72
42.0007
0.84
100
445
548.97
1,351.21
1,112.23
3.91
5.7
138.63
2,211.95
8,308.92
1.02
41.76
129.71
2,387.99
8,078.28
9.3343
0.02
328
2,212
100
10.68
6.431
249
1
73
34.9996
0.8401
100
449.44
554.68
1,354.64
1,124.58
5.48
7.98
193.48
2,222.83
8,334.68
1.02
41.52
182.67
2,387.85
8,058.77
9.3464
0.02
331
2,223
100
14.88
8.9067
248
1
74
19.9997
0.7002
100
491.19
606.46
1,481.83
1,239
9.35
13.61
332.58
2,323.72
8,709.37
1.07
44.19
312.94
2,387.8
8,053.3
9.2153
0.02
363
2,324
100
24.38
14.725
247
1
75
10.0057
0.25
100
489.05
604.12
1,497.28
1,290.6
10.52
15.46
394.29
2,318.67
8,772.98
1.26
44.66
370.84
2,387.85
8,120.32
8.6157
0.03
367
2,319
100
28.58
17.2542
246
1
76
20.0005
0.7007
100
491.19
606.66
1,474.37
1,230.09
9.35
13.61
332.67
2,323.7
8,724.32
1.07
43.85
312.88
2,387.89
8,053.53
9.1911
0.02
363
2,324
100
24.48
14.7474
245
1
77
41.9999
0.8409
100
445
548.65
1,341.13
1,109.07
3.91
5.69
138.25
2,211.9
8,301.9
1.01
41.76
129.83
2,387.96
8,072.08
9.3752
0.02
330
2,212
100
10.5
6.3132
244
1
78
42.0033
0.8413
100
445
549.59
1,339.95
1,115.48
3.91
5.69
138.12
2,211.94
8,310.39
1.02
41.64
129.83
2,387.92
8,075.21
9.3775
0.02
328
2,212
100
10.36
6.3782
243
1
79
42.0033
0.84
100
445
549.69
1,346.74
1,108.7
3.91
5.7
138.93
2,211.9
8,302.15
1.02
41.53
129.94
2,387.97
8,069.63
9.3518
0.02
330
2,212
100
10.57
6.3827
242
1
80
10.0077
0.25
100
489.05
604.09
1,488.22
1,293.47
10.52
15.46
393.64
2,318.67
8,772.66
1.26
45.03
369.94
2,387.78
8,119.38
8.6532
0.03
367
2,319
100
28.52
17.1861
241
1
81
20.0068
0.7005
100
491.19
606.94
1,473.75
1,233.96
9.35
13.61
332.48
2,323.7
8,713.87
1.07
43.87
313.92
2,387.85
8,054.25
9.18
0.02
364
2,324
100
24.42
14.6309
240
1
82
35.004
0.8412
100
449.44
555.3
1,360.17
1,118.89
5.48
7.98
193.52
2,222.84
8,337.16
1.02
41.62
182.14
2,387.87
8,061.6
9.3146
0.02
330
2,223
100
14.67
8.9893
239
1
83
25.005
0.621
60
462.54
536.28
1,257.13
1,042
7.05
9
174.94
1,915.19
7,998.88
0.94
36.42
163.75
2,028.11
7,871.52
10.8468
0.02
305
1,915
84.93
14.25
8.5233
238
1
84
20.0031
0.7
100
491.19
606.79
1,469.57
1,238.58
9.35
13.61
332.53
2,323.7
8,702.15
1.07
43.94
313.84
2,387.83
8,055.89
9.1847
0.02
364
2,324
100
24.43
14.7178
237
1
85
42.0007
0.8417
100
445
549.1
1,350.3
1,109.72
3.91
5.7
137.88
2,211.86
8,306.62
1.02
41.71
130.58
2,387.93
8,077.56
9.3514
0.02
329
2,212
100
10.59
6.4113
236
1
86
0.0013
0
100
518.67
642.36
1,578.24
1,386.45
14.62
21.58
552.46
2,387.88
9,047.93
1.3
47.03
520.7
2,387.93
8,136.59
8.3964
0.03
390
2,388
100
38.98
23.3123
235
1
87
35.0073
0.8411
100
449.44
555.32
1,352.58
1,120.51
5.48
7.98
193.76
2,222.79
8,333.99
1.02
41.51
182.26
2,387.86
8,065.45
9.3221
0.02
331
2,223
100
14.79
8.9154
234
1
88
42.0001
0.8408
100
445
549.67
1,341.56
1,115.3
3.91
5.69
137.32
2,211.96
8,306.42
1.02
41.48
130.09
2,387.99
8,070.55
9.357
0.02
329
2,212
100
10.67
6.3949
233
1
89
20.0045
0.7
100
491.19
606.67
1,483
1,246.45
9.35
13.62
333.57
2,323.78
8,711.38
1.07
44.01
313.33
2,387.85
8,053.25
9.1871
0.02
364
2,324
100
24.63
14.7623
232
1
90
0.0021
0.0006
100
518.67
642.07
1,576.06
1,384.53
14.62
21.58
552.98
2,387.94
9,048.04
1.3
47.19
520.69
2,387.94
8,131.56
8.4011
0.03
391
2,388
100
38.95
23.4175
231
1
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9.9992
0.25
100
489.05
604.5
1,495.21
1,297.27
10.52
15.47
394.31
2,318.68
8,770.68
1.26
45.18
370.4
2,387.93
8,125.2
8.6104
0.03
366
2,319
100
28.62
16.9787
230
1
92
25.0046
0.62
60
462.54
536.56
1,249.6
1,040.22
7.05
9
174.66
1,915.25
8,002.67
0.94
36.26
163.55
2,028.15
7,863.43
10.8294
0.02
305
1,915
84.93
14.33
8.6429
229
1
93
20.0071
0.7
100
491.19
606.58
1,473.21
1,232.98
9.35
13.61
332.83
2,323.65
8,705.95
1.07
43.89
312.7
2,387.82
8,045.65
9.1983
0.02
363
2,324
100
24.33
14.6484
228
1
94
9.9987
0.2513
100
489.05
604.23
1,492.53
1,295.91
10.52
15.47
393.14
2,318.68
8,770.96
1.26
44.96
370.77
2,387.92
8,127.89
8.6593
0.03
368
2,319
100
28.64
17.12
227
1
95
25.0055
0.6209
60
462.54
536.4
1,249.04
1,037.81
7.05
9
174.46
1,915.25
8,001.66
0.94
36.29
163.76
2,028.13
7,863.31
10.8898
0.02
305
1,915
84.93
14.41
8.6036
226
1
96
42.0036
0.84
100
445
549.52
1,343.06
1,106.93
3.91
5.69
137.55
2,211.88
8,301.31
1.02
41.71
129.93
2,387.96
8,078.97
9.3636
0.02
328
2,212
100
10.62
6.3795
225
1
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10.0032
0.2518
100
489.05
603.39
1,489.59
1,295.78
10.52
15.47
393.26
2,318.66
8,769.86
1.26
44.92
371.2
2,387.89
8,122.65
8.5626
0.03
368
2,319
100
28.85
17.3044
224
1
98
10.0022
0.2515
100
489.05
604.08
1,495.81
1,303.74
10.52
15.47
393.61
2,318.65
8,755.21
1.26
44.94
370.9
2,387.86
8,129.98
8.6377
0.03
369
2,319
100
28.55
17.1995
223
1
99
41.9985
0.84
100
445
549.42
1,346.47
1,111.37
3.91
5.7
137.6
2,211.91
8,304.08
1.02
41.49
129.92
2,388.06
8,077.4
9.3458
0.02
329
2,212
100
10.71
6.2607
222
1
100
35.0077
0.84
100
449.44
555.41
1,362.76
1,117.42
5.48
7.97
193.17
2,222.83
8,331.29
1.02
41.46
181.85
2,387.9
8,060.14
9.2897
0.02
329
2,223
100
14.87
8.7767
221
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CMAPSS Jet Engine Simulated Data FD004 - NASA

This dataset contains simulated data from the CMAPSS (Commercial Modular Aero-Propulsion System Simulation) Jet Engine by NASA, FD004.

Train trjectories: 248 Test trajectories: 249 Conditions: SIX Fault Modes: TWO (HPC Degradation, Fan Degradation)

Sensor Descriptions

Sensor ID Description Units
s_1 Total temperature at fan inlet ◦R
s_2 Total temperature at LPC outlet ◦R
s_3 Total temperature at HPC outlet ◦R
s_4 Total temperature at LPT outlet ◦R
s_5 Pressure at fan inlet psia
s_6 Total pressure in bypass-duct psia
s_7 Total pressure at HPC outlet psia
s_8 Physical fan speed rpm
s_9 Physical core speed rpm
s_10 Engine pressure ratio (P50/P2) -
s_11 Static pressure at HPC outlet psia
s_12 Ratio of fuel flow to Ps30 pps/psia
s_13 Corrected fan speed rpm
s_14 Corrected core speed rpm
s_15 Bypass Ratio -
s_16 Burner fuel-air ratio -
s_17 Bleed Enthalpy -
s_18 Demanded fan speed rpm
s_19 Demanded corrected fan speed rpm
s_20 HPT coolant bleed lbm/s
s_21 LPT coolant bleed lbm/s

Units Explanation

  • ◦R: Rankine scale
  • HPT: High Pressure Temperature
  • LPT: Low Pressure Temperature
  • HPC: High Pressure Chamber
  • LPC: Low Pressure Chamber
  • rpm: rotation per minute
  • psia: pound per square inch
  • pps: pulse per second
  • lbm: pound mass

Source

CMAPSS Jet Engine Simulated Data

Citation 

@article{Saxena2008DamagePM,
  title={Damage propagation modeling for aircraft engine run-to-failure simulation},
  author={Abhinav Saxena and Kai Goebel and Donald C. Simon and Neil H. W. Eklund},
  journal={2008 International Conference on Prognostics and Health Management},
  year={2008},
  pages={1-9},
  url={https://api.semanticscholar.org/CorpusID:206508104}
}
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