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coatings
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Published: 01 June 2008
Fig. 22.20 Hardness of coatings for tool materials. PVD, physical vapor deposition; CVD, chemical vapor deposition
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Published: 01 June 2008
Fig. 22.21 Physical vapor deposition coatings on cemented carbide substrates. (a) TiN. (b) TiCN. (c) TiAlN. Source: Ref 3
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in Surface Engineering to Add a Surface Layer or Coating
> Surface Engineering for Corrosion and Wear Resistance
Published: 01 March 2001
Fig. 2 Nitride ceramic coatings deposited on cemented carbide substrates by physical vapor deposition. (a) TiN. (b) TiCN. (c) TiAlN
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in Surface Engineering to Add a Surface Layer or Coating
> Surface Engineering for Corrosion and Wear Resistance
Published: 01 March 2001
Fig. 4 Corrosion losses of hot dip coatings in the industrial environment of Bethlehem, PA. Source: Ref 18
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in Surface Engineering to Add a Surface Layer or Coating
> Surface Engineering for Corrosion and Wear Resistance
Published: 01 March 2001
Fig. 8 Volume steady-state erosion rates of weld-overlay coatings at 400 °C (750 °F) as a function of average microhardness at 400 °C (90° impact angle; alumina erodent). Source: Ref 45
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Published: 01 November 2007
Fig. 8.16 Erosion behavior of alloys and coatings under hot, oxidizing combustion gas stream at 815 °C (1500 °F) and 366 m/s (1200 ft/s) with fly-ash as erodent. Source: Ref 25
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in Life-Assessment Techniques for Combustion Turbines
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Fig. 9.31. Ductility/temperature characteristics of (a) MCrAIY coatings ( Ref 58 ) and (6) aluminide coatings ( Ref 59 to 61 ).
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Published: 01 January 1998
Fig. 16-11 Schematic of structural zones in PVD coatings as a function of substrate temperature as proposed by Movchan and Demchishin. Source: Ref 38
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Published: 01 January 1998
Fig. 16-12 Schematic of structural zones in PVD coatings as a function of substrate temperature and argon pressure in sputtering as proposed by Thornton. Source: Ref 39 , 40
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in Accepted Practice for Metallographic Preparation of Thermal Spray Coating Samples
> Thermal Spray Technology: Accepted Practices
Published: 01 June 2022
Figure 4 Typical sectioning orientation for thermal spray coatings
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in Accepted Practice for Metallographic Preparation of Thermal Spray Coating Samples
> Thermal Spray Technology: Accepted Practices
Published: 01 June 2022
Figure 14 Thermally sprayed coatings after polishing steps. (a) Following 3 μm (diamond) polishing. (b) Following 0.05 μm (oxide) polishing
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in Accepted Practice for Metallographic Preparation of Molybdenum Thermal Spray Coatings
> Thermal Spray Technology: Accepted Practices
Published: 01 June 2022
Figure 1 Cutaway view of an AE 3007 engine. Molybdenum coatings are used for a range of applications in the “cold” sections of a gas turbine. Photo courtesy of Rolls-Royce Corporation
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Published: 01 June 2016
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Published: 01 June 2016
Fig. 2.1 Optical micrographs of copper coatings prepared by (a) arc spraying and (b) cold spraying
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Published: 01 June 2016
Fig. 2.9 SEM cross-sectional micrographs of cold-sprayed FeAl coatings on steel 316L substrate. Four layers obtained with fine powder at (a) short, (b) medium, and (c) long spray distances, and obtained with coarse powders at (d) short and (e) medium spray distances. Source: Ref 2.63
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Published: 01 June 2016
Fig. 2.18 Optical micrographs of cold-sprayed copper coatings on thermally sprayed Al 2 O 3 coatings. (a) Copper on a cold-sprayed aluminum bond coat, processed onto a D-gun-sprayed Al 2 O 3 coating using a nonheated substrate. (b) Copper directly cold sprayed onto a suspension high-velocity
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Published: 01 June 2016
Fig. 2.23 Microstructures of commercially pure nickel (Ni-99.7) coatings, cold sprayed with nitrogen as process gas at a process gas pressure of 4 MPa (580 psi) and process gas temperatures of (a) 800 °C (1470 °F) and (b) 1000 °C (1830 °F). Both coatings are dense, showing no internal porosity.
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Published: 01 June 2016
Fig. 5.3 Optical micrographs with etched aluminum coatings as a function of gas temperature at (a) 204 °C (400 °F) and (b) 315 °C (600 °F), revealing the extent of particle deformation. (c) Micrographs used to determine the nature of bonding of the coating. Source: Ref 5.12
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