PREDICTIVE MODELING OF HIGH-BYPASS TURBOFAN ENGINE DETERIORATION

A method, medium, and system to receive actual operational flight data for an engine of a particular type and configuration; train a neural network to generate an indicator of the health of the engine based on multiple different inputs to the neural network at a time the flight data was acquired; de...

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Bibliographic Details
Main Authors BRASCO CHRISTINA MARIE, EKLUND NEIL HOLGER WHITE, MARTHALER DANIEL EDWARD, SHAH MOHAK
Format Patent
LanguageEnglish
Published 16.04.2015
Subjects
CALCULATING
COMPUTER SYSTEMS BASED ON SPECIFIC COMPUTATIONAL MODELS
COMPUTING
COUNTING
PHYSICS
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Summary:A method, medium, and system to receive actual operational flight data for an engine of a particular type and configuration; train a neural network to generate an indicator of the health of the engine based on multiple different inputs to the neural network at a time the flight data was acquired; determine a deterioration factor for the engine, based at least in part, on an operational climate for the engine; and provide a record of the determined deterioration factor.
Bibliography:Application Number: US201414512159