This paper presents an analysis of the uncertainties in the determination of gas turbine health, which arise by using a method of gas path analysis. This method uses field measurements to estimate, through a mathematical model of the gas turbine thermodynamic cycle, the characteristic geometric and performance parameters, which are indices of gas turbine health. The investigated sources of uncertainties are the influence of measurement accuracy and the a priori selection of the characteristic parameters that have to be considered constant during the calculation. This fact implies that variations occurring on these parameters in the actual gas turbine cause an estimation error on the characteristic parameters used as problem variables. The analysis leads to the selection of the appropriate measurements to be used in the gas turbine health determination and to the identification of both the most critical measurements and parameters.

1.
Madej, J., Longtin, K., and Smith, D. P., 1996, “Monitoring Service Delivery System and Diagnostics,” Proceedings, 39th GE Turbine State-of-the-Art Technology Seminar, General Electric Company, Schenectady, NY, GER-3956.
2.
Urban, L. A., 1972, “Gas Path Analysis Applied to Turbine Engine Condition Monitoring,” AIAA Paper 72-1082, AIAA, New York.
3.
Stamatis
,
A.
,
Mathioudakis
,
K.
, and
Papailiou
,
K. D.
,
1990
, “
Adaptive Simulation of Gas Turbine Performance
,”
ASME J. Eng. Gas Turbines Power
,
112
, pp.
168
175
.
4.
Benvenuti, E., Bettocchi, R., Cantore, G., Negri di Montenegro, G., and Spina, P. R., 1993, “Gas Turbine Cycle Modeling Oriented to Component Performance Evaluation From Limited Design or Test Data,” Proceedings, 7th ASME COGEN—TURBO, Bournemouth, UK, IGTI Vol. 8, ASME, New York, pp. 327–337.
5.
Benvenuti, E., Bettocchi, R., Cantore, G., Negri di Montenegro, G., and Spina, P. R., 1994, “Experimental Validation of a Gas Turbine Cycle Model Based on a Simultaneous Solution Method,” Proceedings, 8th ASME COGEN—TURBO, Portland, OE, IGTI Vol. 9, ASME, New York, pp. 245–255.
6.
Doel
,
D. L.
,
1994a
, “
TEMPER—A Gas-Path Analysis Tool for Commercial Jet Engines
,”
ASME J. Eng. Gas Turbines Power
,
116
, pp.
82
89
.
7.
Doel
,
D. L.
,
1994b
, “
An Assessment of Weighted-Least-Squares Based Gas Path Analysis
,”
ASME J. Eng. Gas Turbines Power
,
116
, pp.
366
373
.
8.
Bettocchi, R., and Spina, P. R., 1999, “Diagnosis of Gas Turbine Operating Conditions by Means of the Inverse Cycle Calculation,” ASME Paper 99-GT-185.
9.
Stamatis
,
A.
,
Mathioudakis
,
K.
, and
Papailiou
,
K.
,
1992
, “
Optimal Measurement and Health Index selection for Gas Turbine Performance Status and Fault Diagnosis
,”
ASME J. Eng. Gas Turbines Power
,
114
, pp.
209
216
.
10.
ISO 2314, 1989, “Gas Turbine—Acceptance Tests,” International Standard.
11.
Brun, K., and Kurz, R., 1998, “Measurement Uncertainties Encountered During Gas Turbine Driven Compressor Field Testing,” ASME Paper 98-GT-001.
You do not currently have access to this content.