Measurement Uncertainties Encountered During Gas Turbine Driven Compressor Field Testing

Author:

Brun Klaus1,Kurz Rainer1

Affiliation:

1. Solar Turbines Incorporated, San Diego, CA

Abstract

Field testing of gas turbine compressor packages requires the accurate determination of efficiency, capacity, head, power and fuel flow in sometimes less than ideal working environments. Nonetheless, field test results have significant implication for the compressor and gas turbine manufacturers and their customers. Economic considerations demand that the performance and efficiency of an installation are verified to assure a project’s return on investment. Thus, for the compressor and gas turbine manufacturers, as well as for the end-user, an accurate determination of the field performance is of vital interest. This paper describes an analytic method to predict the measurement uncertainty and, thus, the accuracy, of field test results for gas turbine driven compressors. Namely, a method is presented which can be employed to verify the validity of field test performance results. The equations governing the compressor and gas turbine performance uncertainties are rigorously derived and results are numerically compared to actual field test data. Typical field test measurement uncertainties are presented for different sets of instrumentation. Test parameters that correlate to the most significant influence on the performance uncertainties are identified and suggestions are provided on how to minimize their measurement errors. The effect of different equations of state on the calculated performance is also discussed. Results show that compressor efficiency uncertainties can be unacceptably high when some basic rules for accurate testing are violated. However, by following some simple measurement rules and maintaining commonality of the gas equations of state, the overall compressor package performance measurement uncertainty can be limited and meaningful results can be achieved.

Publisher

American Society of Mechanical Engineers

Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Accurate measurement and evaluation method of axial compressor efficiency under the influence of multiple factors;International Journal of Turbo & Jet-Engines;2022-12-26

2. An enhanced aircraft engine gas path diagnostic method based on upper and lower singleton type-2 fuzzy logic system;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2019-01-12

3. Degradation in Gas Turbine Systems;Journal of Engineering for Gas Turbines and Power;2000-11-01

4. Gas Turbine Field Performance Determination: Sources of Uncertainties;Journal of Engineering for Gas Turbines and Power;2000-02-01

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