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    Current Status of Titanium-Boron Composites for Gas Turbines

    Source: Journal of Engineering for Gas Turbines and Power:;1969:;volume( 091 ):;issue: 004::page 297
    Author:
    A. G. Metcalfe
    ,
    G. K. Schmitz
    DOI: 10.1115/1.3574750
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A process to manufacture titanium-boron composites has been demonstrated with a 30-filament tape in which reaction is controlled to a few hundred Angstroms of boride. This tape has good properties—indicating efficient use of the boron reinforcement—combined with good reproducibility (coefficient of variation of tensile properties approaches 2 percent). Simulated exposures confirm predictions that many thousands of hours of service life are possible at temperatures up to 1200 F. In addition, creep, fatigue, compression, cross tensile, and shear properties are presented. Application of this metal matrix tape to gas turbines is discussed. It is shown that the advantages of boron-reinforced plastic tapes in manufacturing are combined with the advantages of a metal matrix for shear load transfer, cross tensile strength, erosion resistance, and high-temperature performance.
    keyword(s): Composite materials , Gas turbines , Titanium , Metals , Shear (Mechanics) , Erosion , Creep , Fatigue , Temperature , Manufacturing , Electrical resistance , Service life (Equipment) , Stress , High temperature , Compression AND Tensile strength ,
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      Current Status of Titanium-Boron Composites for Gas Turbines

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    https://yetl.yabesh.ir/yetl1/handle/yetl/133179
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorA. G. Metcalfe
    contributor authorG. K. Schmitz
    date accessioned2017-05-09T00:18:54Z
    date available2017-05-09T00:18:54Z
    date copyrightOctober, 1969
    date issued1969
    identifier issn1528-8919
    identifier otherJETPEZ-26681#297_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/133179
    description abstractA process to manufacture titanium-boron composites has been demonstrated with a 30-filament tape in which reaction is controlled to a few hundred Angstroms of boride. This tape has good properties—indicating efficient use of the boron reinforcement—combined with good reproducibility (coefficient of variation of tensile properties approaches 2 percent). Simulated exposures confirm predictions that many thousands of hours of service life are possible at temperatures up to 1200 F. In addition, creep, fatigue, compression, cross tensile, and shear properties are presented. Application of this metal matrix tape to gas turbines is discussed. It is shown that the advantages of boron-reinforced plastic tapes in manufacturing are combined with the advantages of a metal matrix for shear load transfer, cross tensile strength, erosion resistance, and high-temperature performance.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleCurrent Status of Titanium-Boron Composites for Gas Turbines
    typeJournal Paper
    journal volume91
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3574750
    journal fristpage297
    journal lastpage303
    identifier eissn0742-4795
    keywordsComposite materials
    keywordsGas turbines
    keywordsTitanium
    keywordsMetals
    keywordsShear (Mechanics)
    keywordsErosion
    keywordsCreep
    keywordsFatigue
    keywordsTemperature
    keywordsManufacturing
    keywordsElectrical resistance
    keywordsService life (Equipment)
    keywordsStress
    keywordsHigh temperature
    keywordsCompression AND Tensile strength
    treeJournal of Engineering for Gas Turbines and Power:;1969:;volume( 091 ):;issue: 004
    contenttypeFulltext
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