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Thermal cycling damage accumulation processes in an advanced metal-matrix composite

Thesis/Dissertation ·
OSTI ID:5700220
The response to thermal cycling of a set of W-1% ThO{sub 2} reinforced Fe-25Cr-8Al-.50Y superalloy matrix composites was studied. During this research, unique composite materials were produced by powder-metallurgical processing. These materials were three aligned composites of differing reinforcement aspect ratio, and a hierarchic composite that included fine-diameter Al{sub 2}O{sub 3} fibers. After HIP processing, specimen blanks were cut from the HIP billets by abrasive water-jet after which specimens were turned using a conventional engine lathe. The specimens were then thermal sprayed with an oxidation resistant FeCrAlY coating identical to the matrix material. The specimens were then thermal cycled between 1,100 C and 352 C and between 1,100 C and 534 C for 100, 500, or 750 cycles on a specially built thermal cycling machine. It was found that the initial longitudinal growth per thermal cycle was small. After many thermal cycles, however, the longitudinal growth per thermal cycle became much larger. The experimental results were analyzed using a new micro-mechanics model. It was found that the predictions of the model agreed with experimental data from the W-FeCrAlY, the W-Cu, and the SiC-Al composite systems.
Research Organization:
Washington Univ., Seattle, WA (United States)
OSTI ID:
5700220
Country of Publication:
United States
Language:
English