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contributor authorM. R. Dellomo
date accessioned2017-05-09T00:01:22Z
date available2017-05-09T00:01:22Z
date copyrightJuly, 1999
date issued1999
identifier issn1048-9002
identifier otherJVACEK-28848#265_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/123093
description abstractOne of the most dangerous problems that can occur in both military and civilian helicopters is the failure of the main gearbox. Currently, the principal method of controlling gearbox failure is to regularly overhaul the complete system. This paper considers the feasibility of using a neural network to perform fault detection on vibration measurements given by accelerometer data. The details and results obtained from studying the neural network approach are presented. Some of the elementary underlying physics will be discussed along with the preprocessing necessary for analysis. Several networks were investigated for detection and classification of the gearbox faults. The performance of each network will be presented. Finally, the network weights will be related back to the underlying physics of the problem.
publisherThe American Society of Mechanical Engineers (ASME)
titleHelicopter Gearbox Fault Detection: A Neural Network Based Approach
typeJournal Paper
journal volume121
journal issue3
journal titleJournal of Vibration and Acoustics
identifier doi10.1115/1.2893975
journal fristpage265
journal lastpage272
identifier eissn1528-8927
keywordsMechanical drives
keywordsArtificial neural networks
keywordsFlaw detection
keywordsNetworks
keywordsFailure
keywordsPhysics
keywordsAccelerometers
keywordsVibration measurement
keywordsHelicopters AND Military systems
treeJournal of Vibration and Acoustics:;1999:;volume( 121 ):;issue: 003
contenttypeFulltext


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