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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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