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Published: 01 March 2002
Fig. 13.17 Archetypical microstructures of aluminide coatings formed on a typical nickel-base superalloy. (a) Inward diffusion based on Ni 2 Al 3 , (b) same as (a) but heat treated at 1080 °C (1975 °F), (c) outward diffusion of nickel in nickel-rich NiAl, and (d) inward diffusion of aluminum More
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Published: 01 March 2002
Fig. 13.20 Ductility of CoCrAlY overlay and standard diffused aluminide coatings showing ductility improvements possible with appropriate overlay compositions More
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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 More
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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 More
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Published: 01 January 2000
Fig. 10 Corrosion losses of hot-dip coatings in the industrial environment of Bethlehem, PA More
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Published: 01 December 2018
Fig. 8.3 Illustration of wheel mold coatings More
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Published: 01 March 2006
Fig. 11.50 Effect of various coatings on fatigue strength of Ti-6Al-4V alloy. Source: Ref 11.56 More
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Published: 01 October 2011
Fig. 11.10 Hardness of various physical vapor deposition (PVD) coatings and chemical vapor deposition (CVD) coatings used for tooling materials. Source: Ref 11.9 More
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Published: 01 August 2012
Fig. 16.15 Applications of physical vapor deposition (PVD) coatings. (a) PVD TiN used for soda can tab punch. (b) PVD TiCN used for AA battery casing extrusion punch. Source: Ref 16.55 More
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Published: 01 August 2012
Fig. 16.26 Ranking of ten tool materials, treatments, and coatings, using a progressive die. CVD, chemcial vapor deposition; PVD, physical vapor deposition. Source: Ref 16.51 More
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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 More
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Published: 01 June 2016
Fig. 1.6 Schoop patent, “Method of Plating or Coating with Metallic Coatings,” 1915 More
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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 More
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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 More
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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 More
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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. More
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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 More
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Published: 01 June 2016
Fig. 7.5 Thermal cyclic life of thermal barrier coatings (TBCs) with the bond coats deposited by cold spraying (CS-TBC) and low-pressure plasma spray (LPPS-TBC). Source: Ref 7.17 More
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Published: 01 June 2016
Fig. 7.16 Sliding wear test of Al-12Si + 20% B 4 C coatings. MM and CM feedstock show significant benefits over Al-12Si coatings. PGDS, pulsed gas dynamic spray; CGDS, cold gas dynamic spray. Source: Ref 7.53 More
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Published: 01 June 2016
Fig. 10.5 Selected mechanical test results for N 2 -sprayed coatings ( d 50 = 23 μm powder) after annealing at various temperatures. (a) Microhardness as a function of anneal temperature. (b) Stress-strain curves. (c) Photos of bend-test specimens More