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contributor authorRongqiao Wang
contributor authorJingxu Nie
date accessioned2017-05-08T23:53:20Z
date available2017-05-08T23:53:20Z
date copyrightOctober, 1997
date issued1997
identifier issn1528-8919
identifier otherJETPEZ-26771#969_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/118636
description abstractThis paper presents a new experimental system to study the L-HCCF of an actual turbine disk mortise teeth at elevated temperature, using an actual disk as experimental component. This system ingeniously achieves combined loading (simulating low cycle radial centrifugal force and high cycle crosswise vibration of blade), high-frequency induction local heating (550°C constant temperature), control of high cycle vibrating frequency and amplitude, and crack real-time detection. The experimental result is identical with the practical flight failure. This method can be easily popularized to study the L-HCCF of many components.
publisherThe American Society of Mechanical Engineers (ASME)
titleA New Experimental Method to Study Combined Fatigue of Actual Turbine Disk Mortise Teeth at Elevated Temperatures
typeJournal Paper
journal volume119
journal issue4
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2817084
journal fristpage969
journal lastpage972
identifier eissn0742-4795
keywordsFatigue
keywordsTemperature
keywordsTurbines
keywordsDisks
keywordsCycles
keywordsFailure
keywordsFlight
keywordsHeating
keywordsBlades
keywordsVibration
keywordsElectromagnetic induction
keywordsCentrifugal force AND Fracture (Materials)
treeJournal of Engineering for Gas Turbines and Power:;1997:;volume( 119 ):;issue: 004
contenttypeFulltext


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