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contributor authorJ. Liburdi
contributor authorP. Lowden
contributor authorC. Pilcher
date accessioned2017-05-08T23:32:33Z
date available2017-05-08T23:32:33Z
date copyrightOctober, 1990
date issued1990
identifier issn1528-8919
identifier otherJETPEZ-26679#550_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/106876
description abstractThe welding of superalloys has been regarded, generally, as an art requiring the highest degree of welder skill and discipline. These highly alloyed materials are prone to micro-cracking and, in some cases, even the best welders cannot achieve satisfactory results. Now, however, advances in automation technology have made it possible to program precisely the complex airfoil shapes and the welding parameters. Consequently, turbine blades can be welded in a repeatable manner, with a minimum of heat input, resulting in better metallurgical quality both in the base metal and the weld deposit. The application of this technology to the automated welding of high-pressure compressor turbine blade tips and the refurbishment of low-pressure turbine blade shrouds are presented in this paper.
publisherThe American Society of Mechanical Engineers (ASME)
titleAutomated Welding of Turbine Blades
typeJournal Paper
journal volume112
journal issue4
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2906203
journal fristpage550
journal lastpage554
identifier eissn0742-4795
keywordsWelding
keywordsTurbine blades
keywordsBase metals
keywordsHigh pressure (Physics)
keywordsDisciplines
keywordsFracture (Process)
keywordsShapes
keywordsAirfoils
keywordsSuperalloys
keywordsCompressors
keywordsPressure AND Heat
treeJournal of Engineering for Gas Turbines and Power:;1990:;volume( 112 ):;issue: 004
contenttypeFulltext


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