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nickel aluminides
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Image
Published: 01 November 2007
Fig. 3.76 Nickel-rich oxides formed on nickel aluminide IC-218 after 1008 h at 1150 °C (2100 °F) in air with 168 h cycles. Area 1: 11.7% Al, 80.0% Ni, 8.3% Cr. Area 2: 18.8% Al, 49.0% Ni, 32.2% Cr. Area 3: 22.7% Al, 57.1% Ni, 20.2% Cr. Source: Ref 55
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Image
Published: 01 March 2002
Fig. 13.14 Effect of a nickel-aluminide-type coating on the hot corrosion resistance of an IN-713 nickel-base superalloy turbine blade compared with an uncoated blade. (a) Uncoated blade after 118 test cycles, (b) micrograph showing severe degradation of IN-713 by hot corrosion, (c) aluminide
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Image
Published: 01 October 2012
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2001
DOI: 10.31399/asm.tb.aub.t61170337
EISBN: 978-1-62708-297-6
... Abstract This article discusses the effect of alloying on the composition, structure, properties, and processing characteristics of ordered intermetallic compounds, including nickel aluminides, iron aluminides, and titanium aluminides. It includes several data tables along with a list...
Abstract
This article discusses the effect of alloying on the composition, structure, properties, and processing characteristics of ordered intermetallic compounds, including nickel aluminides, iron aluminides, and titanium aluminides. It includes several data tables along with a list of typical applications.
Image
Published: 30 November 2013
of high-temperature erosion-corrosion. Nickel aluminide coatings are sometimes applied to the nickel-base alloy to improve the life of the blades.
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in Opportunities for Powder-Binder Forming Technologies
> Binder and Polymer Assisted Powder Processing
Published: 30 April 2020
Fig. 11.2 Two examples of alignment in powder-binder systems. (a) Whiskers in a sintered alumina matrix. (b) Fibers in a sintered nickel aluminide matrix
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Image
Published: 01 November 2007
Fig. 9.5 Scanning electron backscattered image showing the cross section of a corroded IC-218 nickel aluminide specimen after hot corrosion burner rig testing at 900 °C (1650 °F) for 200 h with 50 ppm sea salt using No. 2 fuel oil (0.4% S) for combustion at 35:1 air-to-fuel ratio. The results
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Series: ASM Technical Books
Publisher: ASM International
Published: 01 February 2005
DOI: 10.31399/asm.tb.chffa.t51040277
EISBN: 978-1-62708-300-3
... not be subjected to tensile stresses; in addition, they are expensive. Therefore, they are used only in selected applications. 21.2.5 Nickel Aluminides Nickel aluminides are attractive because they derive their strength from their ordered microstructure instead of heat treatments. Their yield strength...
Abstract
This chapter discusses the factors that affect die steel selection for hot forging, including material properties such as hardenability, heat and wear resistance, toughness, and resistance to plastic deformation and mechanical fatigue. It then describes the relative merits of various materials and the basic requirements for cold forging dies. The chapter also covers die manufacturing processes, such as high-speed and hard machining, electrodischarge machining, and hobbing, and the use of surface treatments.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2007
DOI: 10.31399/asm.tb.htcma.t52080249
EISBN: 978-1-62708-304-1
... and nickel aluminides. The combustion gas stream was generated by using No. 2 fuel oil containing about 0.4 wt% S with an air-to-fuel ratio of 35 to 1 and injection of either 5 or 50 ppm sea salt into the combustion gas stream. The specimens were loaded in a carousel, that rotated at 30 rpm during testing...
Abstract
This chapter examines the hot corrosion resistance of various nickel- and cobalt-base alloys in gas turbines susceptible to high-temperature (Type I) and low-temperature (Type II) hot corrosion. Type I hot corrosion is typically characterized by a thick, porous layer of oxides with the underlying alloy matrix depleted in chromium, followed (below) by internal chromium-rich sulfides. Type II hot corrosion is characterized by pitting with little or no internal attack underneath. As the chapter explains, chromium additions make alloys more resistant to all types of hot corrosion attacks.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2012
DOI: 10.31399/asm.tb.lmub.t53550299
EISBN: 978-1-62708-307-2
.... (b) Long-range ordered crystal structure of an ordered intermetallic compound. Source: Ref 6.1 The search for new high-temperature structural materials has stimulated much interest in ordered intermetallics. Recent interest has focused on nickel aluminides based on Ni 3 Al and NiAl, iron...
Abstract
Titanium aluminides are lightweight materials that have relatively high melting points and good high-temperature strength. They also tend to be stronger and lighter than conventional titanium alloys, but considerably less ductile. This chapter begins with a review of the titanium-aluminum phase diagram, focusing on the properties, compositions, and microstructures of alpha-2 Ti3Al alloys. It then describes the properties, microstructures, and compositions of orthorhombic, gamma, and near-gamma alloys as well as the processing methods and procedures normally used in their production.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 March 2002
DOI: 10.31399/asm.tb.stg2.t61280287
EISBN: 978-1-62708-267-9
... protective coatings, including aluminide diffusion, overlay, and thermal barrier types, and how they perform in different environments based on their ability to tolerate strain. coatings corrosion resistance corrosion testing hot corrosion superalloys Overview Introduction Elevated...
Abstract
Superalloys tend to operate in environments where they are subjected to high-temperature corrosion, oxidation, and the erosive effects of hot gases. This chapter discusses the nature of these attacks and the effectiveness of various protection methods. It describes the primary forms of oxidation, the development of protective oxides, and the conditions associated with mixed gas corrosion and hot corrosion attack. It discusses oxidation and corrosion testing, the equipment used, and various ways to present the associated data. It describes the effect of gaseous oxidation on different alloys, discusses the formation of oxide scale in the presence of mixed gases, and explains how alloy composition contributes to oxide growth. The chapter discusses the underlying chemistry of hot corrosion, how to identify its effects, and how it progresses under various conditions. It also discusses protective coatings, including aluminide diffusion, overlay, and thermal barrier types, and how they perform in different environments based on their ability to tolerate strain.
Image
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
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 June 2008
DOI: 10.31399/asm.tb.emea.t52240563
EISBN: 978-1-62708-251-8
..., and secondary fabrication processes. It also covers coating technology, including aluminide diffusion and overlay coatings, and addresses the advantages and disadvantages of superalloys in various applications. cast nickel-based superalloys wrought nickel alloys wrought cobalt-based superalloys cast...
Abstract
Superalloys are nickel, iron-nickel, and cobalt-base alloys designed for high-temperature applications, generally above 540 deg C. This chapter covers the metallurgy, composition, and properties of cast and wrought superalloys. It provides information on melting, heat treating, and secondary fabrication processes. It also covers coating technology, including aluminide diffusion and overlay coatings, and addresses the advantages and disadvantages of superalloys in various applications.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2000
DOI: 10.31399/asm.tb.ttg2.t61120131
EISBN: 978-1-62708-269-3
... increases the turbine blades become bigger, causing both the disk that holds the blades and the shaft that turns with the disk to become heavier. Replacement of conventional nickel-base superalloys with titanium aluminides would alleviate this engine weight-increase problem. For reasons...
Abstract
This chapter discusses some of the promising developments in the use of titanium, including titanium aluminides, titanium matrix composites, superplastic forming, spray forming, nanotechnology, and rapid solidification rate processing. It also reports on efforts to increase the operating temperature range of conventional titanium alloys and reduce costs.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.sap.t53000001
EISBN: 978-1-62708-313-3
... aluminide compounds, compared to nickel aluminide, caused rapid aluminum depletion in the coating by diffusion of aluminum to the coating/substrate interface ( Ref 9 ). This determined the later development of MCrAlY coatings to be based on cobalt and nickel, such as CoCrAlY ( Ref 13 ), NiCrAlY ( Ref 14...
Abstract
Superalloys, although not strictly defined, are generally regarded as high-performance alloys based on group VIII elements (nickel, cobalt, or iron, with a high percentage of nickel) to which a multiplicity of alloying elements have been added. The defining feature of a superalloy is its combination of relatively high mechanical strength and surface stability at high operating temperatures. This chapter provides a brief history of the development of superalloys and discusses their use in the gas turbine engines.
Image
Published: 01 March 2002
Fig. 12.85 Results of aluminide coated and uncoated stress rupture tests on Rene 120 nickel-base superalloy using Larson-Miller parameter (P LM ). Note: P LM = T (C + log t ) where C = Larson-Miller constant, T = absolute temperature, t = time in h. For this plot, C = undefined
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 September 2022
DOI: 10.31399/asm.tb.dsktmse.t56050001
EISBN: 978-1-62708-432-1
... process temperature can lead to distortions Source: Ref 4 Aluminizing This process involves the diffusion of aluminum atoms into substrates (iron base, nickel base, cobalt base, and titanium base) to form metal aluminides (e.g., Fe-Al, Ni-Al, Co-Al, and Ti-Al phases) up to a certain depth...
Abstract
A working knowledge of diffusion is necessary to understand and predict the behavior of metals and alloys during manufacturing and in certain types of service. This chapter covers the fundamentals of diffusion in solids and some of the applications in which diffusion plays a role. It discusses the mechanisms behind interstitial, substitutional, grain boundary, and surface diffusion, the derivation and use of Fick’s laws, and the basic principles of diffusion coating processes, including carburizing, nitriding, nitrocarburizing, cyaniding, carbonitriding, boriding, aluminizing, siliconizing, chromizing, vanadizing, and titanizing. It also discusses diffusion bonding and presents several approaches for dealing with oxide barrier problems.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 30 April 2020
DOI: 10.31399/asm.tb.bpapp.t59290251
EISBN: 978-1-62708-319-5
...(a) shows graphite fibers aligned in alumina, pictured in the transverse view, and Fig. 11.2(b) shows alumina fibers aligned in nickel aluminide (NiAl), looking in the flow direction. The fiber alignment is not perfect but is sufficient to significantly increase strength. Usually, the fiber diameter...
Abstract
This chapter is intended to identify materials, processes, and designs that will lead to great advances in powder-binder forming technologies. It discusses some of the structures obtained through these advances in powder-binder technologies such as binder jetting and extrusion-based additive manufacturing, including bound-metal deposition and fused-filament fabrication: oxidation-resistant high-temperature alloys, anisotropic structures, submicrometer-scale structures, surface hard materials, and artist metallic clays. Some of the advances discussed include the developments in process involving plastics, emulsions, ceramics, and porous structures and foams. Improvements in the design processes have led to the development of functional structures, controlled porosity, and bioinspired structures.
Book Chapter
Book: Principles of Brazing
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 2005
DOI: 10.31399/asm.tb.pb.t51230207
EISBN: 978-1-62708-351-5
.... [1994] Alumina/kovar Ni/Ti/Ni interlayers 980 1800 984–1310 1805–2390 Zhang, Qiao, and Jin [2002] Cobalt alloys Ni-4B 1175 2145 1475 2685 Duvall, Owczarski, and Paulonis [1974] Nickel alloys Ni-4B 1175 2145 1450 2640 Duvall, Owczarski, and Paulonis [1974] Ni-4.5Si...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2007
DOI: 10.31399/asm.tb.htcma.t52080003
EISBN: 978-1-62708-304-1
... to the specific high-temperature corrosive environment in the end application. This can lead to premature failures. For example, because of their good weldability, high nickel filler metals, such as filler metal alloy 82 (ERNiCr-3), are sometimes used for welding the alloys that are to be in service...
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