Research Article

Two-Stage Degradation Assessment and Prediction Method for Aircraft Engine Based on Data Fusion

Table 3

Parameter types and description in datasets.

SymbolDescriptionUnits

IdEngine number
CycleCurrent engine cycle
Setting1Operation parameter setting 1
Setting2Operation parameter setting 2
Setting3Operation parameter setting 3
Sensor parameters available for analysis
S1T2Total temperature at fan inlet°R
S2T24Total temperature at LPC outlet°R
S3T30Total temperature at HPC outlet°R
S4T50Total temperature at LPT outlet°R
S5P2Pressure at fan inletPsia
S6P15Total pressure in bypass-ductPsia
S7P30Total pressure at HPC outletPsia
S8NfPhysical fan speed rpmRpm
S9NcPhysical core speed rpmRpm
S10EprEngine pressure ratio (P50/P2)
S11Ps30Static pressure at HPC outletPsia
S12PhiRatio of fuel flow to Ps30Pps/psi
S13NRfCorrected fan speedRpm
S14NRcCorrected core speedRpm
S15BPRBypass ratio
S16farBBurner fuel-air ratio
S17htBleedBleed enthalpy
S18Nf_dmdDemanded fan speedRpm
S19PCNfR_dmdDemanded corrected fan speedRpm
S20W31HPT coolant bleedLbm/s
S21W32LPT coolant bleedLbm/s