Superalloys 2000 (Ninth International Symposium) 2000
DOI: 10.7449/2000/superalloys_2000_829_837
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MC-NG: A 4th Generation Single-Crystal Superalloy for Future Aeronautical Turbine Blades and Vanes

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Cited by 33 publications
(23 citation statements)
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“…As a promising alternative to the third-generation superalloys, the fourthgeneration alloys can increase the temperature capability without imposing high density and microstructural instabilities. The alloys, with Ru partially substituting for Re, clearly show better oxidation and corrosion resistance (Argence et al 2000), significantly higher creep strength and less propensity to the precipitation of TCP phases.…”
mentioning
confidence: 98%
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“…As a promising alternative to the third-generation superalloys, the fourthgeneration alloys can increase the temperature capability without imposing high density and microstructural instabilities. The alloys, with Ru partially substituting for Re, clearly show better oxidation and corrosion resistance (Argence et al 2000), significantly higher creep strength and less propensity to the precipitation of TCP phases.…”
mentioning
confidence: 98%
“…In the past few years, the growing demand for increasing inlet temperature in turbine blades has led to the development of a new generation of SC superalloys. It is reported that the so-called fourth or new generation of Ni-based SC superalloys containing both Re and Ru can achieve an excellent balance of properties (Argence et al 2000). As a promising alternative to the third-generation superalloys, the fourthgeneration alloys can increase the temperature capability without imposing high density and microstructural instabilities.…”
mentioning
confidence: 99%
“…It can be concluded that the closure effect of pores relying on the compressive stress caused by laser shock results in the vanishment of shrinkages, and the disappearance of the shrinkages has a inhibitory effect on crack initiation [26].…”
Section: Surface Topography Of the Samples Subjected To Lspmentioning
confidence: 99%
“…In recently developed fourth generation single crystal alloys, such as TMS-138, TMR-139, TMS-162 and MC-NG, the content of Re decreased from 6% which is the usual content in third generation single crystal alloys to 4 ~ 5 wt.%, and added 2 ~ 4 wt.% of Ru to prevent the formation of TCP phase [7,8] . The elemental electron hole numbers, Nv, of these new single crystal alloys were controlled within the values smaller than 2 to increase the microstructure stability for high temperature service of the alloys.…”
Section: Introductionmentioning
confidence: 99%
“…The elemental electron hole numbers, Nv, of these new single crystal alloys were controlled within the values smaller than 2 to increase the microstructure stability for high temperature service of the alloys. There have been quite few reports on the effect of Ru on the microstructure and stress rupture properties of single crystal superalloys [6][7][8][9][10] .…”
Section: Introductionmentioning
confidence: 99%