Patent Document ID: 20110153295
Application ID: 12643579
Patent Flag: 0

Claim One:
1. A method for modeling the performance of a gas turbine engine, comprising the steps of: providing a processor; inputting flight condition parameter data and engine output parameter data into a gas turbine engine model operating on the processor, which model includes a physics-based engine model that uses the flight condition parameter data to produce estimated engine output parameter data, and determines residual data from the engine output parameter data and the estimated engine output parameter data; partitioning the flight condition parameter data and residual data into training data and testing data; performing a correlation reduction on the training data, which analysis produces correlation adjusted training data; performing an orientation reduction on the correlation adjusted training data, which reduction produces orientation adjusted training data; reviewing the orientation adjusted training data relative to at least one predetermined criteria, and iteratively repeating the steps of performing a correlation reduction and an orientation reduction using the orientation adjusted training data, and reviewing if the criteria is not satisfied, and if the criteria is satisfied outputting the orientation adjusted training data; producing estimated corrections to the orientation adjusted training data using one or more neural networks; evaluating the neural adjusted data using the partitioned testing data; and modeling the performance of the gas turbine using the estimated corrections to the orientation adjusted training data.