Core aerospace engineering and protocols for Gas Path Analysis & EGT Margin.
Jet engines degrade over time due to turbine blade erosion, thermal barrier coating spallation, and compressor blade fouling. As efficiency drops, the engine burns more fuel and operates hotter, eroding the Exhaust Gas Temperature (EGT) margin toward safety redlines.
AviationTwins models the complete gas turbine thermodynamic cycle: by analyzing pressure ratios and temperatures across every compressor and turbine stage during takeoff and cruise, the platform isolates exactly which component is degrading, scheduling targeted core washes or blade replacements weeks before an in-flight shutdown could occur.