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    Automated Welding of Turbine Blades

    Source: Journal of Engineering for Gas Turbines and Power:;1990:;volume( 112 ):;issue: 004::page 550
    Author:
    J. Liburdi
    ,
    P. Lowden
    ,
    C. Pilcher
    DOI: 10.1115/1.2906203
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The 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.
    keyword(s): Welding , Turbine blades , Base metals , High pressure (Physics) , Disciplines , Fracture (Process) , Shapes , Airfoils , Superalloys , Compressors , Pressure AND Heat ,
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      Automated Welding of Turbine Blades

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/106876
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    • Journal of Engineering for Gas Turbines and Power

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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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