1991
DOI: 10.1007/bf00777163
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Structure, mechanical properties, and thermal stability of the high-temperature nickel pelletized alloy �P741NP

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Cited by 3 publications
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“…[11] EP741NP, a P/M superalloy manufactured by direct HIP, is widely used in turbine engines. [7,[12][13][14] The main disadvantage of superalloys made by HIP is the formation of a prior particle boundary (PPB) containing oxides, carbides, and γ 0 , which is detrimental to the material's mechanical properties. [15] The EP741NP superalloy overcomes the PPB problem through a specially tuned composition and a supersolvus HIP process with coarse powder (53-150 μm).…”
Section: Introductionmentioning
confidence: 99%
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“…[11] EP741NP, a P/M superalloy manufactured by direct HIP, is widely used in turbine engines. [7,[12][13][14] The main disadvantage of superalloys made by HIP is the formation of a prior particle boundary (PPB) containing oxides, carbides, and γ 0 , which is detrimental to the material's mechanical properties. [15] The EP741NP superalloy overcomes the PPB problem through a specially tuned composition and a supersolvus HIP process with coarse powder (53-150 μm).…”
Section: Introductionmentioning
confidence: 99%
“…To avoid excessive grain growth, hot deformation is usually operated at the γ þ γ 0 duplex phase field. However, the high Al, Ti, and Nb content (Al þ Ti þ Nb % 9.3 wt%) of EP741NP alloys results in a large volume fraction of γ 0 up to 60%, and high γ 0 solvus temperature up to 1185 C. [13] This can cause rapid age hardening as a result of cooling during processing, and significantly increase resistance to deformation. Several studies have assessed the hot deformation of γ 0 strengthened superalloys, including γ 0 evolution mechanisms, recrystallization mechanisms, and their interactions.…”
Section: Introductionmentioning
confidence: 99%