LucasThil/nasa_turbofan_degradation_FD002
CMAPSS Jet Engine Simulated Data FD002 - NASA This dataset contains simulated data from the CMAPSS (Commercial Modular Aero-Propulsion System Simulation) Jet Engine by NASA, FD002. Train trjectories: 260 Test trajectories: 259 Conditions: SIX Fault Modes: ONE (HPC 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… See the full description on the dataset page: https://huggingface.co/datasets/LucasThil/nasa_turbofan_degradation_FD002.
CMAPSS Jet Engine Simulated Data FD002 - NASA
This dataset contains simulated data from the CMAPSS (Commercial Modular Aero-Propulsion System Simulation) Jet Engine by NASA, FD002.
Train trjectories: 260 Test trajectories: 259 Conditions: SIX Fault Modes: ONE (HPC Degradation)
Sensor Descriptions
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}
}