1995
DOI: 10.1016/0956-716x(95)00229-o
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The influence of crystallography and creep ductility on thermal fatigue crack initiation in nickel-base superalloys with elongated macrograins

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Cited by 6 publications
(6 citation statements)
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“…It was different from other experimental results [7,8]. Literatures [7,8] showed that propagation rate of crack started to increase and then decrease when the crack length was 5 -6 mm. The reason is that it creates large stress near crack in the course of thermal fatigue experiment.…”
Section: Resultscontrasting
confidence: 68%
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“…It was different from other experimental results [7,8]. Literatures [7,8] showed that propagation rate of crack started to increase and then decrease when the crack length was 5 -6 mm. The reason is that it creates large stress near crack in the course of thermal fatigue experiment.…”
Section: Resultscontrasting
confidence: 68%
“…It is difficult to compare thermal fatigue results by different investigation. Some experiment results [3][4][5][6][7][8][9][10][11][12][13][14][15] show thermal fatigue property of the alloy is greatly affected by different factors such as upper temperature, holding time, specimen shape, notched radius and direction.…”
Section: Introductionmentioning
confidence: 99%
“…15 Several alloys with elongated grains have been investigated including cast and powder metallurgy (mechanically alloyed materials) produced materials. [16][17][18][19][20] Both creep fatigue and TMF experiments have been conducted on as cast or cast and heat treated conditions. TMF experiments were performed on CM 247LC, a directionally solidified alloy, using single wedge specimens and a temperature-time cycle with a minimum temperature of 200uC and a maximum temperature of 1000uC; 16 CM 247LC is a derivative of MAR-M247.…”
Section: Single Crystal and Directionally Oriented Microstructuresmentioning
confidence: 99%
“…[16][17][18][19][20] Both creep fatigue and TMF experiments have been conducted on as cast or cast and heat treated conditions. TMF experiments were performed on CM 247LC, a directionally solidified alloy, using single wedge specimens and a temperature-time cycle with a minimum temperature of 200uC and a maximum temperature of 1000uC; 16 CM 247LC is a derivative of MAR-M247. The maximum tensile stress in the specimens was perpendicular to the elongated macrograins.…”
Section: Single Crystal and Directionally Oriented Microstructuresmentioning
confidence: 99%
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