1996
DOI: 10.1179/mst.1996.12.6.469
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Microstructure and properties of alloy HP50–Nb: comparison of as cast and service exposed materials

Abstract: Spun cast alloy HP50-Nb tubing retired from service in a steam reformer after approximately 8 years of service had stress rupture properties suggesting very short remaining life. Microstructural examination, however, indicated little or no creep damage (cavitation) but did reveal extensive microstructural modification. The microstructure, mechanical properties, and stress rupture properties of the ex service material were determined and compared with virgin as cast material. The microstructural changes that oc… Show more

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Cited by 20 publications
(8 citation statements)
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“…Another phase, the diamond cubic g-carbide, has also been identified in ex-service HP-Nb reformer tubes and aged HP-Nb alloy [10,22,[25][26][27]. The typical composition of the transformed phase in the ex-service pyrolysis tube closely resembled the reported compositions.…”
Section: Cr-ni-nb-si Rich Phasesupporting
confidence: 51%
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“…Another phase, the diamond cubic g-carbide, has also been identified in ex-service HP-Nb reformer tubes and aged HP-Nb alloy [10,22,[25][26][27]. The typical composition of the transformed phase in the ex-service pyrolysis tube closely resembled the reported compositions.…”
Section: Cr-ni-nb-si Rich Phasesupporting
confidence: 51%
“…The Cr-Ni-Nb-Si rich phase appeared to be transformed from NbC, and the area covered by this phase appeared to increase as distance from the inner diameter increased. The instability of NbC precipitates at temperatures of 700-1050°C has been well reported in the literature [1,[22][23][24][25][26][27]. The product of the transformation is generally identified as G-phase, which has a commonly reported composition of Ni 16 Nb 6 Si 7 , and an FCC structure with a lattice parameter of 1.12 nm [1,23,24].…”
Section: Cr-ni-nb-si Rich Phasementioning
confidence: 99%
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“…The combination of high temperature, carbon oxide atmosphere and moderate tensile stresses causes that the damage in these components occurs mainly by the presence of creep, microstructural degradation and metal dusting 1 . These components operate at temperatures of approximately 850 °C and internal pressures between 1 and 3.5 MPa, and its service life is expected to be about 100,000 h [2][3][4][5][6] . This type of components is usually fabricated with heat resistant austenitic stainless steel, like the HP40 steel (25Cr-35Ni steel), which has excellent creep strength, and good resistance to carburization and oxidation [1][2][3][4][5][6] .…”
Section: Introductionmentioning
confidence: 99%
“…These components operate at temperatures of approximately 850 °C and internal pressures between 1 and 3.5 MPa, and its service life is expected to be about 100,000 h [2][3][4][5][6] . This type of components is usually fabricated with heat resistant austenitic stainless steel, like the HP40 steel (25Cr-35Ni steel), which has excellent creep strength, and good resistance to carburization and oxidation [1][2][3][4][5][6] .…”
Section: Introductionmentioning
confidence: 99%