LucasThil/nasa_turbofan_degradation_FD004

NASA的CMAPSS商用模块化航空推进系统仿真喷气发动机模拟数据FD004。该数据集包含了CMAPSS喷气发动机的模拟数据。训练轨迹数为248，测试轨迹数为249，涉及六种条件，有两种故障模式：高压压缩机退化与风扇退化。数据集包含的传感器读数包括风扇入口总温度、低压压缩机出口总温度、高压压缩机出口总温度、低压涡轮出口总温度、风扇入口压力、旁通管道总压力、高压压缩机出口总压力、物理风扇转速、物理核心转速等，以及一些衍生参数如发动机压力比、静压、燃料流量比、校正的风扇和核心转速、旁通比、燃烧器燃料空气比、抽气焓等。

NASAs CMAPSS Jet Engine Simulated Data FD004. This dataset contains simulated data from the CMAPSS (Commercial Modular Aero-Propulsion System Simulation) Jet Engine. There are 248 training trajectories and 249 test trajectories, involving six conditions and two fault modes: HPC Degradation and Fan Degradation. The sensor readings include total temperature at fan inlet, total temperature at LPC outlet, total temperature at HPC outlet, total temperature at LPT outlet, pressure at fan inlet, total pressure in bypass-duct, total pressure at HPC outlet, physical fan speed, physical core speed, engine pressure ratio (P50/P2), static pressure at HPC outlet, ratio of fuel flow to Ps30, corrected fan speed, corrected core speed, bypass ratio, burner fuel-air ratio, bleed enthalpy, demanded fan speed, demanded corrected fan speed, HPT coolant bleed, and LPT coolant bleed.