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contributor authorJ. A. Daleo
contributor authorJ. R. Wilson
date accessioned2017-05-08T23:56:37Z
date available2017-05-08T23:56:37Z
date copyrightApril, 1998
date issued1998
identifier issn1528-8919
identifier otherJETPEZ-26778#375_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/120448
description abstractVery few property data on this common turbine blade alloy have been published. As longer hours of service are accumulated, maintenance considerations such as developing optimum component life strategies and repair processes become important. The lack of specific material data hampers the effort of users and repair facilities to achieve optimum service from this alloy. This study measured some of the basic mechanical and metallurgical characteristics of this polycrystalline nickel base superalloy. Tensile and short-term creep rupture properties as well as microstructural and fracture characteristics are presented. Both the as-heat-treated and thermally exposed characteristics at two different temperatures are examined.
publisherThe American Society of Mechanical Engineers (ASME)
titleGTD111 Alloy Material Study
typeJournal Paper
journal volume120
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2818133
journal fristpage375
journal lastpage382
identifier eissn0742-4795
keywordsAlloys
keywordsMaintenance
keywordsSuperalloys
keywordsTurbine blades
keywordsFracture (Process)
keywordsRupture
keywordsCreep
keywordsHeat
keywordsTemperature AND Nickel
treeJournal of Engineering for Gas Turbines and Power:;1998:;volume( 120 ):;issue: 002
contenttypeFulltext


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