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contributor authorD. L. Doel
date accessioned2017-05-09T00:10:06Z
date available2017-05-09T00:10:06Z
date copyrightJuly, 2003
date issued2003
identifier issn1528-8919
identifier otherJETPEZ-26823#624_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/128339
description abstractGas turbine performance analysis programs convert raw measurements (thrust, fuel flow, gas path temperatures, and pressures) into engine and component figures of merit (e.g., specific fuel consumption, component efficiencies). The derived parameters allow a diagnostician to recognize a poorly performing engine and help to identify the root cause for the problem. These goals can be foiled by measurement problems or by analysis assumptions embedded in the programs. A gifted analyst learns to recognize measurement or assumption problems via characteristic “fingerprints” in the program output. The latest data analysis tools tackle the same issues using a weighted-least-squares algorithm which estimates sensor errors at the same time component health is being determined. The weighted-least-squares algorithm modifies the “fingerprint” of a measurement problem and also that of a problem-free solution. To develop intuition for these new programs, the analyst must understand how weighted-least-squares works and how normal and problem situations are reflected in the output. This paper describes the weighted-least-squares algorithm, as implemented in GE’s TEMPER program, with the goal of stimulating a new intuition for interpreting gas path analysis results.
publisherThe American Society of Mechanical Engineers (ASME)
titleInterpretation of Weighted-Least-Squares Gas Path Analysis Results
typeJournal Paper
journal volume125
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.1582492
journal fristpage624
journal lastpage633
identifier eissn0742-4795
keywordsFlow (Dynamics)
keywordsEngines
keywordsErrors
keywordsMeasurement
keywordsAlgorithms
keywordsProbability AND Turbines
treeJournal of Engineering for Gas Turbines and Power:;2003:;volume( 125 ):;issue: 003
contenttypeFulltext


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