Identifying faults in the variable geometry system of a gas turbine compressor

Journal of Turbomachinery

Volumn 123, Issue 1, 2001, Pages 33-39

  Tsalavoutas, A ^a   Mathioudakis, K ^a   Stamatis, A ^a   Smith, M ^a  

^a NATIONAL TECHNICAL UNIVERSITY OF ATHENS   (Greece)

Author keywords

[No Author keywords available]

Indexed keywords

AXIAL FLOW TURBOMACHINERY; COMPRESSORS; CONDITION MONITORING; FUEL BURNERS; GEOMETRY; STATORS;

AEROTHERMODYNAMIC MEASUREMENTS;

GAS TURBINES;

AXIAL COMPRESSOR; COMPRESSOR; GAS TURBINE; MEASUREMENT METHOD; PERFORMANCE;

EID: 0034891267     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1330267     Document Type: Article

References (14)

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13. Combination of different unsteady quantity measurements for gas turbine blade fault diagnosis