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nickel-base alloys

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Series: ASM Technical Books
Publisher: ASM International
Published: 01 January 2017
DOI: 10.31399/asm.tb.sccmpe2.t55090135
EISBN: 978-1-62708-266-2
...Abstract Abstract Nickel and nickel-base alloys are specified for many applications, such as oil and gas production, power generation, and chemical processing, because of their resistance to stress-corrosion cracking (SCC). Under certain conditions, however, SCC can be a concern. This chapter...
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Published: 01 November 2007
Fig. 6.45 Weight change as a function of exposure time for nickel-base alloys (alloys 625, 600, and 825) and iron-base alloys (alloy 800HT, 316SS, and 347SS) in N 2 -4O 2 -12CO 2 -1HCl-500 ppm SO 2 . Testing was initially performed at 649 °C, then increased to 704 °C, and finally to 760 °C More
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Published: 01 November 2007
Fig. 6.46 Weight change as a function of exposure time for nickel-base alloys (alloys 625, 600, and 825) and iron-base alloys (alloy 800HT, 316SS, and 347SS) in N 2 -9O 2 -12CO 2 -1HCl-500 ppm SO 2 . Testing was initially performed at 649 °C, then increased to 704 °C, and finally to 760 °C More
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Published: 01 November 2007
Fig. 6.47 Weight change as a function of exposure time for nickel-base alloys (alloys 625, 600, and 825) and iron-base alloys (alloys 800HT, 316SS, and 347SS) in N 2 -9O 2 -12CO 2 -4HCl-100 ppm SO 2 . Testing was initially performed at 593 °C, then increased to 704 °C, and to 816 °C, and finally More
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Published: 01 November 2007
Fig. 6.48 The metal loss and internal penetration for nickel-base alloys (alloys 214, 600, and 601) and cobalt-base alloys (alloys 25 and 188) along with Fe-Ni-Co-Cr alloy (alloy 556), Fe-Ni-Cr alloy (alloy 800H), and Type 310SS tested in Ar-5.5O 2 -1HCl-1SO 2 at 900 °C (1650 °F) for 800 h More
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Published: 01 January 2000
Fig. 21 Comparative behavior of several nickel-base alloys in pure sulfuric acid (H 2 SO 4 ). The isocorrosion lines indicate a corrosion rate of 0.5 mm/year (20 mils/year). More
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Published: 01 December 2008
Fig. 16 Corrosion rates for various stainless steels and nickel base alloys. Source: Ref 20 More
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Published: 01 July 2000
Fig. 5.33 Anodic polarization curves for three nickel-base alloys in 1 N HCl at 25 °C. Alloy F, 22.34 Cr, 7.07 Mo, 0.07 C (wt%); alloy C, 54 Ni, 2.5 Co, 15.5 Cr, 16 Mo, 4W, 5.4 Fe, 0.08 C (wt%); alloy B, 26.5 Mo, 0.75 Cr, 5.2 Fe, 0.02 C (wt%). Redrawn from Ref 29 More
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Published: 01 December 2006
Fig. 1 Compositional and property linkages for nickel-base alloys More
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Published: 01 November 2007
Fig. 6.23 Corrosion of several aluminum-containing nickel-base alloys with and without molybdenum in Ar-20O 2 -0.25Cl 2 at 900 °C (1650 °F). Source: Ref 39 More
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Published: 01 November 2007
Fig. 6.25 Corrosion of several iron- and nickel-base alloys in air-2Cl 2 at 900 and 1000 °C (1650 and 1830 °F) for 50 h. Source: Ref 40 More
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Published: 01 November 2007
Fig. 6.26 Loose scales on samples of several nickel-base alloys after testing at 900 °C (1650 °F) in Ar-20O 2 -1Cl 2 for 100 h More
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Published: 01 November 2007
Fig. 6.49 Corrosion rates of several iron- and nickel-base alloys in HCl at 400 to 700 °C (750 to 1290 °F). Source: Ref 54 More
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Published: 01 November 2007
Fig. 6.54 Corrosion of nickel-base alloys in H 2 -10HCl at 850 °C with 24 h cycles. Source: Ref 56 More
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Published: 01 November 2007
Fig. 7.32 Corrosion of stainless steels and nickel-base alloys at 816 °C (1500 °F) for 100 h in the MPC coal gasification atmosphere with 0.1, 0.5, and 1.0% H 2 S. Also included were aluminized Type 310 and alloy 800 [310 (Al) and 800 (Al], and chromized Type 310 and alloy 800 [310 (Cr) and 800 More
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Published: 01 December 2015
Fig. 2 Compositional and property linkages for nickel-base alloys More
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Published: 01 November 2007
Fig. 4.35 Nitridation kinetic data for alloy 214 (nickel-base alloy containing 4.5% Al) and alloy 230 (nickel-base alloy containing little aluminum) after exposure to 100% N 2 at 1090 °C (2000 °F) for 168 h. Source: Ref 50 More
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Published: 30 November 2013
Fig. 9 Hot-corrosion attack of René 77 nickel-base alloy turbine blades. (a) A land-based, first-stage turbine blade. Notice the deposit buildup and flaking and splitting of the leading edge. (b) Stationary vanes. (c) A land-based, first-stage gas turbine blade that had type 2 hot-corrosion More
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Published: 01 January 2017
Fig. 5.19 Recommended region of chromium and molybdenum content of nickel-base alloy with approximately 55 to 60 wt% Ni in H 2 S-CO 2 -Cl − -S environment. Line 1: SCC; 230 °C (450 °F), l MPa H 2 S + 1 MPa CO 2 + 25 wt% NaCl + 1 g/L S 8 , 336 h; four-point bent beam. Line 2: hydrogen More
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Published: 01 March 2002
Fig. 8.3 Oxidized carbide in precipitation-hardened nickel-base alloy More