1999
DOI: 10.1007/s11661-999-0043-7
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Secondary carbide precipitation in a directionally solified cobalt-base superalloy

Abstract: A directionally solidified cobalt-base alloy, DZ40M, was solidified with a columnar grained austenitic matrix with a ͗001͘ preferential orientation and primary carbides of chromium-rich M 7 C 3 and MC at grain boundaries and interdendritically. Secondary carbides in DZ40M alloy are chromium-rich M 23 C 6 and tungsten-rich M 6 C. The M 23 C 6 carbide has a cube-cube orientation relationship with the austenitic matrix. Initial precipitation of secondary carbide, M 23 C 6 , occurred on dislocations in the austeni… Show more

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Cited by 57 publications
(38 citation statements)
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“…On the other hand, this decomposition (M 6 C → M 23 C 6 ) led to precipitation of M 23 C 6 in the matrix. The precipitation of the secondary M 23 C 6 occurs profusely in cobalt-base superalloys with more than 5% chromium from the older X-40 to the newer MM-509 alloy [10,11]. Fig.…”
Section: Microstructure Characterizationmentioning
confidence: 98%
“…On the other hand, this decomposition (M 6 C → M 23 C 6 ) led to precipitation of M 23 C 6 in the matrix. The precipitation of the secondary M 23 C 6 occurs profusely in cobalt-base superalloys with more than 5% chromium from the older X-40 to the newer MM-509 alloy [10,11]. Fig.…”
Section: Microstructure Characterizationmentioning
confidence: 98%
“…The black-coarse M 7 C 3 carbides of the unused stellite are not any more present in the microstructure. Also the light-gray areas of cobalt with a fine dispersion of M 7 C 3 , which were situated between the Co-␥ dendrites, have been replaced by a continuous network of elongated carbides, presumably grown at some preferential crystallographic orientations [17][18][19][20][21][22][23][24], Fig. 6b.…”
Section: Aging Effectmentioning
confidence: 99%
“…Since M 7 C 3 is mainly a chromium carbide, the surrounding matrix should be oversaturated with Cr and as a result the Cr/C ratio will become high. This favors the formation of M 23 C 6 [17] according to reaction (2) [18][19][20][21]:…”
Section: Aging Effectmentioning
confidence: 99%
See 1 more Smart Citation
“…Hence, it is very much essential to modify the surface of the components to improve the service life of the component. Wear, corrosion and tear of the component surface are the main reason for the failure of the engineering materials [1][2][3][4]. It is comprehensively not verbalized in potential wear applications.…”
Section: Introductionmentioning
confidence: 99%