Manufacturers of gas turbines have searched for three decades for a reliable way to use gas path measurements to determine the health of jet engine components. They have been hindered in this pursuit by the quality of the measurements used to carry out the analysis. Engine manufacturers have chosen weighted-least-squares techniques to reduce the inaccuracy caused by sensor error. While these algorithms are clearly an improvement over the previous generation of gas path analysis programs, they still fail in many situations. This paper describes some of the failures and explores their relationship to the underlying analysis technique. It also describes difficulties in implementing a gas path analysis program. The paper concludes with an appraisal of weighted-least-squares based gas path analysis.
Skip Nav Destination
ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition
May 24–27, 1993
Cincinnati, Ohio, USA
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7889-7
PROCEEDINGS PAPER
An Assessment of Weighted-Least-Squares Based Gas Path Analysis
David L. Doel
David L. Doel
GE Aircraft Engines, Evendale, OH
Search for other works by this author on:
David L. Doel
GE Aircraft Engines, Evendale, OH
Paper No:
93-GT-119, V002T13A008; 10 pages
Published Online:
February 25, 2015
Citation
Doel, DL. "An Assessment of Weighted-Least-Squares Based Gas Path Analysis." Proceedings of the ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition. Volume 2: Combustion and Fuels; Oil and Gas Applications; Cycle Innovations; Heat Transfer; Electric Power; Industrial and Cogeneration; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; IGTI Scholar Award. Cincinnati, Ohio, USA. May 24–27, 1993. V002T13A008. ASME. https://doi.org/10.1115/93-GT-119
Download citation file:
422
Views
Related Proceedings Papers
Related Articles
An Assessment of Weighted-Least-Squares-Based Gas Path Analysis
J. Eng. Gas Turbines Power (April,1994)
Component Map Generation of a Gas Turbine Using Genetic Algorithms
J. Eng. Gas Turbines Power (January,2006)
Observer-Based Cylinder Air Charge Estimation for Spark-Ignition Engines
J. Eng. Gas Turbines Power (October,2017)
Related Chapters
Turbojet Engines
Turbo/Supercharger Compressors and Turbines for Aircraft Propulsion in WWII: Theory, History and Practice—Guidance from the Past for Modern Engineers and Students
Introduction
Computer Vision for Structural Dynamics and Health Monitoring
Case Study 10: Data Reconciliation
Engineering Optimization: Applications, Methods, and Analysis