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aluminide coatings

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Image
Published: 01 January 1994
Fig. 3 Archetypical microstructures of aluminide coatings on a nickel superalloy. (a) Inward diffusion based on Ni 2 Al 3 (and aluminum-rich NiAl). (b) Same as (a) but heat treated at 1080 °C (1975 °F). (c) Outward diffusion of nickel in nickel-rich NiAl. (d) Inward diffusion of aluminum More
Image
Published: 01 January 2006
Fig. 10 Micrograph of a nickel-aluminide coating. As-polished More
Image
Published: 01 January 1997
Fig. 11 Microstructure of a platinum-modified pack aluminide coating on a single-crystal superalloy after engine exposure. 600× More
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003555
EISBN: 978-1-62708-180-1
... and metal dusting, sulfidation, hot corrosion, chloridation, hydrogen interactions, molten metals, molten salts, and aging reactions including sensitization, stress-corrosion cracking, and corrosion fatigue. It concludes with a discussion on various protective coatings, such as aluminide coatings, overlay...
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Published: 01 January 1997
Fig. 12 Columnar structure of an EB-PVD 7% yttria-zirconia thermal barrier coating on a platinum-aluminide-coated single-crystal superalloy. 250× More
Image
Published: 01 January 2006
Fig. 29 Duplex coating consisting of an overlay coating (O) with an aluminide layer (A) on top. There is an interdiffusion zone with the base metal (B) and another interdiffusion zone between A and O. Lactic acid etch. See the article “Corrosion of Industrial Gas Turbines” in this Volume. More
Image
Published: 01 January 2006
Fig. 11 Duplex coating consisting of an overlay coating (O) with an aluminide layer (A) on top. The interdiffusion zone with the base metal (B) is indicated by the letter I. There is another interdiffusion zone between A and O. Lactic acid etch More
Image
Published: 01 January 2002
Fig. 27 Comparison of calculated and observed aluminum content as a function of one-hour thermal cycles from 25 to 1066 °C (75 to 1950 °F) for aluminide-coated GTD-111 blade More
Image
Published: 01 January 2003
Fig. 20 Low-velocity atmospheric pressure burner rig pins after 1000 h exposure to combustion gases from fuel containing (a) 0.099 wt% C residue and (b) 0.33 wt% C residue. Increased carbon residue has a vast effect on aluminide coating performance. More
Image
Published: 30 August 2021
Fig. 17 (a) Photograph of as-received condition of the blade, with sand buildup (light-tan color) under the blade platform. (b) Photograph of breached cooling holes on the pressure side of the upper airfoil (arrows). (c) Optical micrograph showing the eroded surface (arrow) and the aluminide More
Image
Published: 15 January 2021
backscatter electron image of stress-rupture cracks and wrinkled aluminide coating on concave trailing-edge side of single-crystal turbine blade casting. Source: Ref 20 More
Book Chapter

Series: ASM Handbook
Volume: 5
Publisher: ASM International
Published: 01 January 1994
DOI: 10.31399/asm.hb.v05.a0001293
EISBN: 978-1-62708-170-2
... published in 1951 and 52 ( Ref 7 , 8 ). Aluminide coating of chromized steels to further improve high-temperature oxidation resistance was patented in 1953 ( Ref 9 ). The time of first widespread use of chromide coatings on gas turbine parts is obscure but probably occurred in Europe in the early 1960s...
Series: ASM Handbook
Volume: 13C
Publisher: ASM International
Published: 01 January 2006
DOI: 10.31399/asm.hb.v13c.a0004158
EISBN: 978-1-62708-184-9
... in the coating. If there is free sulfur in the coating, it migrates to the oxide-coating interface, weakening this interface, and increasing the amount of oxide spalling. Diffusion aluminide coatings are nickel aluminide (NiAl) and cobalt aluminide (CoAl). NiAl forms on nickel-base superalloys and CoAl forms...
Series: ASM Handbook
Volume: 5
Publisher: ASM International
Published: 01 January 1994
DOI: 10.31399/asm.hb.v05.a0001313
EISBN: 978-1-62708-170-2
... for aircraft gas turbines. Coatings of aluminum-chromium-silicon, aluminum-silicon, and aluminum-tin systems are indicated in Table 5 . The aluminide coatings are applied as thick overlays, using a variety of spray or dip processes. The aluminide coatings provide good oxidation protection to molybdenum...
Series: ASM Handbook
Volume: 20
Publisher: ASM International
Published: 01 January 1997
DOI: 10.31399/asm.hb.v20.a0002473
EISBN: 978-1-62708-194-8
... be projected without consulting test data of the alloy in question. The preceding is a brief introduction to some general aspects of oxidation that apply to typical high-temperature alloys. They apply equally well to intermetallic compounds, aluminide and MCrAlY coatings, and bond coats for thermal barrier...
Series: ASM Handbook
Volume: 4A
Publisher: ASM International
Published: 01 August 2013
DOI: 10.31399/asm.hb.v04a.a0005775
EISBN: 978-1-62708-165-8
..., steels, and stainless steels. Simple aluminide coatings resist high-temperature oxidation by the formation of an alumina protective layer and can be used up to approximately 1150 °C (2100 °F), but the coating can degrade by spallation of the oxide during thermal cycling. For extended periods of time...
Series: ASM Handbook
Volume: 13B
Publisher: ASM International
Published: 01 January 2005
DOI: 10.31399/asm.hb.v13b.a0003837
EISBN: 978-1-62708-183-2
... the adherence of the alumina scale and to decrease the oxidation rate. The effects of noble metals on the oxidation behavior of nickel aluminide coatings were extensively reported ( Ref 32 , Ref 33 , Ref 34 ). Whether used as an environmental coating ( Ref 35 ) or as a bond coat for thermal barriers ( Ref...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003164
EISBN: 978-1-62708-199-3
... environments (good aqueous corrosion resistance) Tooling (high-temperature strength and wear resistance developed through preoxidation) Permanent molds (the ability to develop a thermal barrier coating by high-temperature oxidation) NiAl Aluminides Nickel-aluminum containing more than...
Image
Published: 01 August 2013
Fig. 5 Micrograph of a typical two-phase NiCoCrAlY low-pressure plasma-sprayed coating after several hours of service. The dark aluminide phase is depleted near the coating surface as the aluminum is consumed to form the thermally grown oxide alumina scale visible under the nickel plating used More
Image
Published: 01 January 2003
Fig. 21 Effects of fuel carbon residue (10% bottoms) on type II hot corrosion of nickel aluminide high-temperature coatings. Source: Ref 135 More