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1-20 of 1838
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in Nickel and Nickel Alloys
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Fig. 5 Nickel-base alloy chart showing alloys containing varying amounts of nickel and iron. Chromium contents are constant at approximately 18 to 20%.
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Published: 01 December 2004
Fig. 19 B-1900 nickel-base alloy, as-cast. (a) Structure consists of nickel-rich γ solid-solution matrix containing a few light-etching carbide particles and dispersed γ′. Kalling's reagent. Original magnification 100× (b) Higher magnification. The light-etching carbide particles are dispersed
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Published: 01 January 2002
Fig. 3 SEM image of fracture surface of nickel-base alloy (Inconel 751, annealed and aged) after stress rupture (730 °C, or 1350 °F; 380 MPa, or 55 ksi; 125 h). (a) Low-magnification view, with picture width shown at approximately 0.35 mm (0.0138 in.) from original magnification of 250×. (b
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in Elevated-Temperature Life Assessment for Turbine Components, Piping, and Tubing
> Failure Analysis and Prevention
Published: 01 January 2002
Fig. 9 Gamma-prime overaging in a nickel-base alloy turbine blade material. (a) SEM micrograph of the blade material, showing the breakdown of the eutectic gamma prime (5) and the spreading of the coarse gamma prime. Smaller particles of fine aging gamma prime (4), which would appear between
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in Elevated-Temperature Life Assessment for Turbine Components, Piping, and Tubing
> Failure Analysis and Prevention
Published: 01 January 2002
Fig. 11 Hot corrosion attack of René 77 nickel-base alloy turbine blades. (a) Land-based, first-stage turbine blade. Notice deposit buildup, flaking, and splitting of leading edge. (b) Stationary vanes. (c) A land-based, first-stage gas turbine blade that had type 2 hot corrosion attack. (d
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in X-Ray Diffraction Residual Stress Measurement in Failure Analysis
> Failure Analysis and Prevention
Published: 01 January 2002
Fig. 19 Observation of failed nickel-base alloy (Waspaloy) specimen after rotating bend fatigue. (a) Macro view. (b) Micrograph. Source: Ref 43
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Published: 01 January 2006
Fig. 11 Microstructures of nickel-base Alloy 713C turbine blades. (a) Original structure prior to service. (b) Coarsening of γ' precipitates and elimination of secondary γ' caused by 5000 h of service
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Published: 01 December 2008
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Published: 01 August 2013
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Published: 01 August 2013
Fig. 6 Thin section of a vacuum-plasma-sprayed nickel-base alloy coating (Metco 700) as observed by transmission electron microscopy. The microstructure displays fine, equiaxed, recrystallized grains. RG, recrystallized grains; AT, annealing twins
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Published: 01 June 2016
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Published: 01 December 2004
Fig. 5 Cast dendritic structure of Russian nickel-base alloy CNK7 revealed using (a) glyceregia, (b) Kalling's No. 2, (c) the Lucas electrolytic reagent (2 V dc, 10 s), and (d) Beraha's tint etch (50 mL HCl, 50 mL water, 0.8 g K 2 S 2 O 5 , 4 g NH 4 F·HF, 1 g FeCl 3
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Published: 15 January 2021
Fig. 3 Scanning electron microscopy image of fracture surface of nickel-base alloy (Inconel 751, annealed and aged) after stress rupture (730 °C, or 1350 °F; 380 MPa, or 55 ksi; 125 h). (a) Low-magnification view, with picture width shown at approximately 0.35 mm (0.0138 in.) from original
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Published: 15 January 2021
Fig. 7 Sulfidation and chloridation attack on IN-601 nickel-base alloy of charcoal-regeneration kiln (see also Fig. 8 ). Region 1 is an area of chromium sulfide islands (dark phase) interspersed in a chromium-depleted region (bright phase). Region 2 has an angular phase (consisting mostly
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Published: 15 January 2021
Fig. 8 Sulfidation and chloridation attack on IN-601 nickel-base alloy of charcoal-regeneration kiln at higher magnification (~44×). Lower right is region of chromium sulfide islands (dark phase) interspersed in chromium-depleted region (bright phase). Middle region has an angular phase
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Published: 01 January 2003
Fig. 5 Corrosion attack in a nickel-base alloy after two months at 870 °C (1600 °F) in a molten BaCl 2 salt bath. Source: Ref 2
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Published: 01 December 1998
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Published: 01 January 1993
Fig. 5 Liquation of a niobium carbide stringer in a nickel-base alloy 718 wire. (a) Stringer before onset of liquation. (b) Stringer in initial stage of liquation as it is heated by welding thermal cycle. (c) Movement of stringer liquation into grain boundaries of alloy. 500×
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in X-Ray Diffraction Residual-Stress Measurement in Failure Analysis
> Failure Analysis and Prevention
Published: 15 January 2021
Fig. 19 Observation of failed nickel-base alloy (Waspaloy) specimen after rotating-bend fatigue. (a) Macro view. (b) Micrograph. Source: Ref 53
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Published: 15 December 2019
Fig. 8 Particle size analysis of nickel-base alloy powder. (a) Optical microscopy. (b) Scanning electron microscopy
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