Gas turbine performance and health status estimation using adaptive gas path analysis

Proceedings of the ASME Turbo Expo

Volumn 4, Issue , 2009, Pages 109-121

  Li, Y G ^a  

^a CRANFIELD UNIVERSITY   (United Kingdom)

Author keywords

Adaptive gas path analysis; Adaptive GPA; Gas path diagnostics; Gas turbine engine; Performance adaptation

Indexed keywords

AERO-ENGINE; AIR FLOW-RATE; CALCULATION TIME; COMPONENT LEVELS; COMPRESSOR PRESSURE RATIO; DIAGNOSTIC METHODS; ENGINE OPERATORS; ENGINE PERFORMANCE; FLOW CAPACITY; FUEL FLOW RATES; GAS PATH; GAS PATH ANALYSIS; GAS PATH COMPONENTS; GAS TURBINE ENGINE; GAS TURBINE PERFORMANCE; GAS-PATH MEASUREMENTS; HEALTH INFORMATIONS; HEALTH STATUS; ISENTROPIC EFFICIENCY; MEASUREMENT NOISE; NON-LINEAR; NOVEL APPLICATIONS; ON-LINE APPLICATIONS; PERFORMANCE ADAPTATION; ROLLS-ROYCE; ROTATIONAL SPEED; TEST CASE; TURBINE EFFICIENCY; TURBINE ENTRY TEMPERATURE;

AIRCRAFT ENGINES; AIRCRAFT PROPULSION; COMPRESSORS; DEGRADATION; ENGINES; ESTIMATION; GAS TURBINES; GASES; HEALTH; MACHINE DESIGN; REGRESSION ANALYSIS; TURBOMACHINERY;

GAS FUEL ANALYSIS;

EID: 77953224784     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2009-59168     Document Type: Conference Paper

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