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contributor authorB. P. Conner
contributor authorT. Nicholas
date accessioned2017-05-09T00:20:03Z
date available2017-05-09T00:20:03Z
date copyrightApril, 2006
date issued2006
identifier issn0094-4289
identifier otherJEMTA8-27082#133_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/133794
description abstractFretting fatigue damage can reduce the service life of engineering components in contact. The attachment between blades and disks in the fan and compressor stages of gas turbine engines is often a dovetail geometry. As a result, normal and tangential cyclic contact loads are present. Results of fretting fatigue tests using a new dovetail fixture are detailed here. Dovetail specimens and three types of contact pads were all machined out of Ti−6A1−4V. Two types of palliatives are also examined: aluminum bronze coatings and low-plasticity burnishing. While the palliatives were effective in increasing the fatigue life, the three pad geometries produced essentially the same fatigue life.
publisherThe American Society of Mechanical Engineers (ASME)
titleUsing a Dovetail Fixture to Study Fretting Fatigue and Fretting Palliatives
typeJournal Paper
journal volume128
journal issue2
journal titleJournal of Engineering Materials and Technology
identifier doi10.1115/1.2172272
journal fristpage133
journal lastpage141
identifier eissn1528-8889
keywordsFatigue
keywordsStress
keywordsJigs and fixtures
keywordsCoatings
keywordsCycles
keywordsGeometry
keywordsFailure
keywordsPlasticity AND Knudsen number
treeJournal of Engineering Materials and Technology:;2006:;volume( 128 ):;issue: 002
contenttypeFulltext


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