Optimization of Aero Gas Turbine Maintenance Using Advanced Simulation and Diagnostic Methods

Engine maintenance costs are a major contributor to the direct operating costs of aircraft. Therefore, the minimization of engine maintenance costs per flight-hour is a key aspect for airlines to operate successfully under challenging market conditions. Minimization can be achieved by increasing the on-wing time or by reducing the shop-visit costs. Combining both provides optimum results and can only be achieved by thorough understanding of the engine. In the past, maintenance optimization was mainly an experience-based process. In this work, a novel analytical approach is presented to optimize the maintenance of commercial turbofan engines. A real engine fleet of more than 100 long-haul engines is used to demonstrate the application. The combination of advanced diagnostic and simulation methods with classical hardware-based failure analysis enables linking of overall engine performance with detailed hardware condition and, thus, an effective optimization of the overall maintenance process.

[1]  John A. Reed,et al.  Multi-Fidelity Simulation of a Turbofan Engine with Results Zoomed Into Mini-Maps for a Zero-D Cycle Simulation , 2013 .

[2]  A Generic Approach for Gas Turbine Adaptive Modeling , 2006 .

[3]  J. Dunham,et al.  Improvements to the Ainley-Mathieson Method of Turbine Performance Prediction , 1970 .

[4]  C. C. Koch,et al.  Stalling Pressure Rise Capability of Axial Flow Compressor Stages , 1981 .

[5]  Pericles Pilidis,et al.  A comparison of component zooming simulation strategies using streamline curvature , 2007 .

[6]  P. Pilidis,et al.  Towards a full two dimensional gas turbine performance simulator , 2007, The Aeronautical Journal (1968).

[7]  Joachim Kurzke HOW TO CREATE A PERFORMANCE MODEL OF A GAS TURBINE FROM A LIMITED AMOUNT OF INFORMATION , 2005 .

[8]  Stephan Staudacher,et al.  Fully Automated Model-Based Performance Analysis Procedure for On-Line and Off-Line Applications , 2008 .

[9]  C. C. Koch,et al.  Loss Sources and Magnitudes in Axial-Flow Compressors , 1976 .

[10]  Vassilios Pachidis,et al.  Multiple-Point Adaptive Performance Simulation Tuned to Aeroengine Test-Bed Data , 2009 .

[11]  U. Okapuu,et al.  A Mean Line Prediction Method for Axial Flow Turbine Efficiency , 1982 .

[12]  Anestis I. Kalfas,et al.  A Partially Integrated Approach to Component Zooming Using Computational Fluid Dynamics , 2005 .

[13]  Yi-Guang Li,et al.  Performance-analysis-based gas turbine diagnostics: A review , 2002 .

[14]  Anestis I. Kalfas,et al.  A Fully Integrated Approach to Component Zooming Using Computational Fluid Dynamics , 2006 .

[15]  Michel L. Verbist,et al.  Gas Path Analysis on KLM In-Flight Engine Data , 2011 .