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Hastelloy X
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Image
Published: 01 June 2016
Fig. 19 Hastelloy X solution annealed at 1175 °C (2150 °F). (a) Aged at 760 °C (1400 °F) for 25 h. Particles of M 6 C, M 6 C prime, and M 23 C 6 in gamma matrix. (b) Aged at 870 °C (1600 °F) for 25 h. The structure is particles of M 6 C and M 6 C prime (by extraction analysis) in gamma matrix
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Published: 01 August 2013
Fig. 1 Example of grains in a wrought superalloy material. Hastelloy X is shown with frequent twinning due to imparted strains.
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in Wrought and P/M Superalloys
> Properties and Selection: Irons, Steels, and High-Performance Alloys
Published: 01 January 1990
Fig. 14 Oxidation resistance. (a) In dry air for Haynes 188 versus Hastelloy X and L-605 alloys showing continuous penetration from original thickness. (b) Static values at 1100 °C (2010 °F) in air with 5% water vapor
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Published: 01 January 1996
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Published: 01 January 1996
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Published: 01 December 1998
Fig. 3 Long-term creep behavior of various refractory metal alloys compared to that of type 316 stainless steel, a nickel-base superalloy (Hastelloy X), and a cobalt base superalloy (HS-188)
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Published: 01 January 1996
Fig. 21 High-temperature fatigue crack growth of two nickel-base superalloys. (a) Hastelloy X at 760 °C (1400 °F) with R = 0.05. (b) NASA 11B-7 at 650 °C (1200 °F) with R = 0.05.
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in Ordered Intermetallics
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Fig. 29 Variation of yield strength with test temperature for cubic ordered alloys (LRO-1, LRO-15, and LRO-16) and commercial solid-solution alloys Hastelloy X and type 316 stainless steel. T c , critical ordering temperature. Source: Ref 17
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Image
Published: 01 January 2000
Fig. 15 Temperature versus tensile, yield, and rupture strengths of iron-nickel-chromium-molybdenum and nickel-base alloys Alloy Heat treatment 19-9 DL-DX Air cooled from 1010 °C (1850 °F), hot worked at 650 °C (1200 °F), air cooled Hastelloy X Water quenched from 1175 °C
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Series: ASM Handbook
Volume: 24
Publisher: ASM International
Published: 15 June 2020
DOI: 10.31399/asm.hb.v24.a0006582
EISBN: 978-1-62708-290-7
... references Alloy Alloy class (a) Process (b) References Inconel 625 SS BJAM, DED, EBM, SLM 8 – 10 Hastelloy X SS EBM, SLM 11, 12 Inconel 718 PS BJAM, DED, EBM, SLM 13 – 17 Haynes 282 PS DED, EBM 18 , 19 Inconel 738 PS SLM, EBM 3 , 20 , 21 Mar...
Abstract
This article covers the current state of materials development of nickel-base superalloys for additive manufacturing (AM) processes and the associated challenges. The discussion focuses on nickel-base superalloy fusion AM processes, providing information on typically encountered cracking mechanisms in AM nickel-base superalloys, such as solid-solution-strengthened nickel-base superalloys and precipitate-strengthened nickel-base superalloys. The mechanisms include solidification cracking, strain-age cracking, liquation cracking, and ductility-dip cracking. The article also provides a short discussion on binder jet AM and powder recyclability.
Book Chapter
Series: ASM Handbook
Volume: 22A
Publisher: ASM International
Published: 01 December 2009
DOI: 10.31399/asm.hb.v22a.a0005443
EISBN: 978-1-62708-196-2
... 11.5 Ni-o-nel 27 to 93 12.9 Hastelloy B 0 to 100 10.0 Hastelloy C 0 to 100 11.3 Hastelloy D 0 to 100 11.0 Hastelloy F 20 to 100 14.2 Hastelloy N 21 to 204 10.4 Hastelloy W 23 to 100 11.3 Hastelloy X 26 to 100 13.8 Illium G 0 to 100 12.19 Illium R 0...
Series: ASM Handbook
Volume: 6
Publisher: ASM International
Published: 01 January 1993
DOI: 10.31399/asm.hb.v06.a0001424
EISBN: 978-1-62708-173-3
... 230 N06230 0.1 22.0 bal … 3.0 (max) 2.0 14.0 0.02 La, 0.015 B (max) Haynes HR-160 … 0.05 28.0 bal 29.0 1.5 … … 2.75 Si Hastelloy X N06002 0.1 22.0 bal 1.5 18.5 9.0 0.6 … Hastelloy W N10004 0.12 (max) 5.0 bal 2.5 6.0 24.0 … … Hastelloy S N06635 0.02...
Book Chapter
Series: ASM Handbook
Volume: 22A
Publisher: ASM International
Published: 01 December 2009
DOI: 10.31399/asm.hb.v22a.a0005442
EISBN: 978-1-62708-196-2
... Nimonic 90 8.27 0.299 M-252 8.27 0.298 Inconel 8.51 0.307 Inconel “X” 550 8.30 0.300 Inconel 700 8.17 0.295 Inconel “713C” 7.913 0.2859 Waspaloy 8.23 0.296 René 41 8.27 0.298 Hastelloy alloy B 9.24 0.334 Hastelloy alloy C 8.94 0.323 Hastelloy alloy X 8.23...
Abstract
This article contains a table that lists the density of metals and alloys. It presents information on aluminum, copper, iron, lead, magnesium, nickel, tin, titanium, and zinc, an their respective alloys. Information on wrought alloys, permanent magnet materials, precious metals, and rare earth metals is also listed.
Series: ASM Handbook
Volume: 24A
Publisher: ASM International
Published: 30 June 2023
DOI: 10.31399/asm.hb.v24A.a0006964
EISBN: 978-1-62708-439-0
... system. For example, IN718 can only be used up to 650 °C (1200 °F), because the main strengthening precipitates, γ″, degrade above this temperature, while the other nickel-base alloys, such as IN738LC (γ′ strengthened) and Hastelloy X (solid-solution strengthened) can be used at a higher temperature...
Abstract
This article briefly introduces the concept of creep properties of additively manufactured (AM) alloys, with a focus on the effects of the characteristic microstructure of AM alloys on creep performance. Relevant post-processing treatment also is discussed, in relation to improved creep performance based on the improvement of AM initial microstructure.
Series: ASM Handbook
Volume: 1
Publisher: ASM International
Published: 01 January 1990
DOI: 10.31399/asm.hb.v01.a0001049
EISBN: 978-1-62708-161-0
... … … 0.3 … 1.0 0.5 0.4 … 0.009 … 0.05 La Hastelloy X 47.0 22.0 1.5 9.0 0.6 … … … 18.5 0.5 0.5 0.10 … … … Haynes 230 57.0 22.0 … 2.0 14.0 … 0.3 … … 0.5 0.4 0.10 … … 0.02 La Inconel 587 (a) bal 28.5 20.0 … … 0.7 1.2 2.3 … … … 0.05 0.003 0.05...
Abstract
This article focuses on the properties of conventional wrought superalloys based on nickel, iron, and cobalt, as well as on the properties of alloys produced from powder. The powder metallurgy (P/M) category includes alloys that were originally developed as casting alloys; new alloy compositions developed specifically to benefit from powder processing; and oxide dispersion strengthened alloys (particularly those produced by mechanical alloying). The article discusses some of the applications of superalloys and emphazises the interplay between chemical composition, microstructure, consolidation method, mechanical properties and surface stability of wrought nickel alloys. Vacuum melting processes are a necessity for many nickel- and iron-nickel-base alloys because of the presence of aluminum and titanium as solutes. Cobalt-base alloys do not usually contain these elements and may be melted in air. An appendix to this article presents the property data and corresponding information on a family of cobalt-chromium-tungsten-carbon alloys that use P/M processing.
Series: ASM Handbook
Volume: 6
Publisher: ASM International
Published: 01 January 1993
DOI: 10.31399/asm.hb.v06.a0001422
EISBN: 978-1-62708-173-3
... La Hastelloy X 49.0 22.0 1.5 max 18.5 9.0 … 0.6 … 2.0 0.15 … Haynes 230 bal 22 0–5 0–3 2 … 14 … 0.3 0.1 0.5 Mn, 0.4 Si, 0.02 La, 0.005 B Inconel 600 76.0 15.5 … 8.0 … … … … … 0.08 0.25 Cu max Inconel 601 60.5 23.0 … 14.1 … … … … 1.35 0.05 0.5 Cu...
Book: Surface Engineering
Series: ASM Handbook
Volume: 5
Publisher: ASM International
Published: 01 January 1994
DOI: 10.31399/asm.hb.v05.a0001307
EISBN: 978-1-62708-170-2
... to obtain the desired surfaces. The examples described below, all of which are drawn from actual production experience, identify cleaning and finishing problems and the procedures used to solve them. Example 1 After heat treatment, turbine combustion chambers made from Hastelloy X sheet exhibited...
Abstract
This article describes the methods for removing metallic contaminants, tarnish, and scale resulting from hot-working or heat-treating operations on nickel-, cobalt-, and iron-base heat-resistant alloys. It provides a brief description of applicable finishing and coating processes, including polishing, electroplating, ceramic coatings, diffusion coatings, and shot-peening. The article presents numerous examples that identify cleaning and finishing problems and the procedures used to solve them.
Series: ASM Handbook
Volume: 13A
Publisher: ASM International
Published: 01 January 2003
DOI: 10.31399/asm.hb.v13a.a0003664
EISBN: 978-1-62708-182-5
... allowable corrosion rate, mm/month (mils/month) S43000 Type 430 None Ferric sulfate (A 763-X) 24 1.14 (45) S44600 Type 446 None Ferric sulfate (A 763-X) 72 0.25 (10) S44625 26-1 None Ferric sulfate (A 763-X) 120 0.05 (2) and no significant grain dropping S44626 26-1S None...
Abstract
Most alloys are susceptible to intergranular corrosion, also known as intergranular attack (IGA), when exposed to specific environments. This article reviews the theory and application of acceptance tests for detecting the susceptibility of stainless steels and nickel-base alloys to IGA. It describes the most serious forms of structure-dependent corrosion, such as stress-corrosion cracking and exfoliation, in aluminum alloys including strain-Hardened 5xxx (Al-Mg) alloys and heat treated high-strength alloys. The article concludes with information on the evaluation tests for other alloys such as magnesium alloys and zinc die casting alloys.
Series: ASM Handbook
Volume: 4E
Publisher: ASM International
Published: 01 June 2016
DOI: 10.31399/asm.hb.v04e.a0006265
EISBN: 978-1-62708-169-6
... 1095–1175 2000–2150 5–10 AC or WQ 1095–1175 2000–2150 1 AC or WQ Hastelloy C-276 1215 2220 5–10 WQ 1215 2220 1 WQ Hastelloy X 1175 2150 1 2 –15 AC or WQ 1175 2150 1 AC or WQ (a) Processing times are shown in minutes. The time should be sufficient to assure...
Abstract
This article describes the heat treatment of wrought solid-solution and precipitation-hardening alloys with a focus on the major families of wrought nickel alloys. It also provides information on the heat treatment of some representative solid-solution alloys in the Monel (Ni-Cu), Inconel (Ni-Cr-Mo), Hastelloy (Ni-Mo-Cr), and Incoloy (Ni-Fe-Cr) families of alloys. The heat treatment processes for gamma prime nickel alloys, gamma prime nickel-iron superalloys, and gamma double-prime nickel-iron superalloys are also included. The article also provides information on age-hardenable alloys, and the effects of cold work on aging response and grain growth with examples.
Book Chapter
Book: Corrosion: Materials
Series: ASM Handbook
Volume: 13B
Publisher: ASM International
Published: 01 January 2005
DOI: 10.31399/asm.hb.v13b.a0006543
EISBN: 978-1-62708-183-2
... S64152 8.27 0.298 Inconel 600 N06600 8.41 0.304 Inconel “X” 550 … 8.30 0.300 Inconel 718 N07718 8.22 0.297 Inconel “713C” … 7.913 0.2859 Waspaloy N07001 8.23 0.296 René 41 N07041 8.27 0.298 Hastelloy alloy B N10001 9.24 0.334 Hastelloy alloy C N30002 8.94...
Abstract
Density allows for the conversion of uniform corrosion rates from units of weight (or mass) loss per unit area per time to thickness per unit time. This article contains a table that lists the density of metals, such as aluminum, copper, iron, stainless steel, magnesium, and lead, and their alloys.
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