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LucasThil/nasa_turbofan_degradation_FD003

CMAPSS Jet Engine Simulated Data FD003 - NASA This dataset contains simulated data from the CMAPSS (Commercial Modular Aero-Propulsion System Simulation) Jet Engine by NASA, FD003. Train trjectories: 100 Test trajectories: 100 Conditions: ONE (Sea Level) 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… See the full description on the dataset page: https://huggingface.co/datasets/LucasThil/nasa_turbofan_degradation_FD003.

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Dataset Card

CMAPSS Jet Engine Simulated Data FD003 - NASA

This dataset contains simulated data from the CMAPSS (Commercial Modular Aero-Propulsion System Simulation) Jet Engine by NASA, FD003.

Train trjectories: 100 Test trajectories: 100 Conditions: ONE (Sea Level) Fault Modes: TWO (HPC Degradation, Fan Degradation)

Sensor Descriptions

Sensor IDDescriptionUnits
s_1Total temperature at fan inlet◦R
s_2Total temperature at LPC outlet◦R
s_3Total temperature at HPC outlet◦R
s_4Total temperature at LPT outlet◦R
s_5Pressure at fan inletpsia
s_6Total pressure in bypass-ductpsia
s_7Total pressure at HPC outletpsia
s_8Physical fan speedrpm
s_9Physical core speedrpm
s_10Engine pressure ratio (P50/P2)-
s_11Static pressure at HPC outletpsia
s_12Ratio of fuel flow to Ps30pps/psia
s_13Corrected fan speedrpm
s_14Corrected core speedrpm
s_15Bypass Ratio-
s_16Burner fuel-air ratio-
s_17Bleed Enthalpy-
s_18Demanded fan speedrpm
s_19Demanded corrected fan speedrpm
s_20HPT coolant bleedlbm/s
s_21LPT coolant bleedlbm/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

bibtex
@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}
}