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Hastelloy X

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Published: 01 March 2002
Fig. 14.8 Microstructure of Hastelloy X nickel-base superalloy after creep exposure for 2232 h at 760 °C (1400 °F). Etched in 10% chromic acid, 500× More
Image
Published: 01 March 2002
Fig. B.14 Wrought Hastelloy X solid-solution-hardened nickel-base superalloy microstructure; carbide precipitation has been influenced by deformation. Dislocations have formed around a primary M 6 C, and M 23 C 6 have precipitated on some of them. Thin-foil specimen. Original magnification More
Image
Published: 01 November 2010
Fig. 4.8 Examples of carbides in nickel- and cobalt-base superalloys. (a) Hastelloy X. The structure is primary M 6 C and needle-like M 23 C 6 carbides that have precipitated at dislocations generated around primary carbide. The matrix is γ solid solution. (b) Hastelloy X. Mixed carbide More
Image
Published: 01 March 2002
Fig. 14.3 Room-temperature tensile strength vs. exposure times at 1038 °C (1900 °F) in air for Hastelloy X nickel-base solid-solution and carbide-strengthened superalloy More
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Published: 01 April 2013
Fig. 17 Voids resulting from lack of fill between the faying surfaces of a lap joint between two sheets of Hastelloy X brazed with BNi-1 filler metal. Unetched. 16.5 ×. Source: Ref 1 More
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.sap.t53000117
EISBN: 978-1-62708-313-3
... … … … … … … … … Hastelloy X (a) 15.8 1.5 (e) 49 2 … 22 9 0.6 … … … 0.15 … … … … … … … … Haynes 556 (a) 29 20 21 0.3 … 22 3 2.5 0.1 0.5 … 0.1 0.002 0.02 … … … … … … I9-9DL (a) 66.8 … 9 … 0.3 19 1.3 1.3 0.4 … … 0.3 … … … 0.6 1.1 … … … Incoloy 800...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 March 2002
DOI: 10.31399/asm.tb.stg2.t61280323
EISBN: 978-1-62708-267-9
... superalloys (a) Alloy Incipient melting temperature, °F (°C) γ′ solvus, °F (°C) A-286 … 1570 (855) Astroloy LC … 2050 (1120) Rene 95 … 2050–2135 (1120–1160) IN-901 … 1725 (940) U-700 2220 (1215) 2070–2100 (1130–1150) Hastelloy X 2280 (1250) … HA-25 (L-605) 2425...
Book Chapter

Series: ASM Technical Books
Publisher: ASM International
Published: 01 March 2002
DOI: 10.31399/asm.tb.stg2.t61280189
EISBN: 978-1-62708-267-9
... difficult material). In a development program for an aerospace vehicle, simulated service tests were conducted on identical structural parts made from two nickel-base alloys (Hastelloy X and Rene 41) and a cobalt-base alloy (HS-25). Although the production of acceptable parts was the primary concern...
Book Chapter

Series: ASM Technical Books
Publisher: ASM International
Published: 01 March 2002
DOI: 10.31399/asm.tb.stg2.t61280091
EISBN: 978-1-62708-267-9
... was produced for further forging or rolling to shapes such as turbine airfoils. The iron-nickel- and nickel-base precipitation-hardened alloys thrived. Sheet products made from Inconel, Nimonic 75, Inconel X (Inconel X-750), Hastelloy X, and the cobalt alloy Haynes Alloy 25 (also known as L-605) made their way...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.sap.t53000133
EISBN: 978-1-62708-313-3
... 170 25 … … 64 75 … Hastelloy S Bar 845 130 775 112 575 84 455 65 340 49 310 45 49 50 70 Hastelloy X Sheet 785 114 650 94 435 63 360 52 290 42 260 38 43 45 37 Haynes 230 (a) 870 126 720 105 575 84 390 57 275 40 285 41 48 56 46 Inconel...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 March 2002
DOI: 10.31399/asm.tb.stg2.t61280001
EISBN: 978-1-62708-267-9
... max 0.02 La   Hastelloy W 5.0 61.0 2.5 max 24.5 … … … … 5.5 0.12 max 0.6 V   Hastelloy X 22.0 49.0 1.5 max 9.0 0.6 … … 2.0 15.8 0.15 …   Hastelloy C-276 15.5 59.0 … 16.0 3.7 … … … 5.0 0.02 max …   Haynes HR-120 25.0 37.0 3.0 2.5 2.5 0.7 … 0.1 33.0...
Book Chapter

Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2001
DOI: 10.31399/asm.tb.aub.t61170290
EISBN: 978-1-62708-297-6
... Hastelloy X N06002 22.0 49.0 1.5 max 9.0 0.6 … … 2.0 15.8 0.15 … Hastelloy C-276 N10276 15.5 59.0 … 16.0 3.7 … … … 5.0 0.02 max … Haynes HR-120 N08120 25.0 37.0 3.0 2.5 2.5 0.7 … 0.1 33.0 0.05 0.7 Mn, 0.6 Si, 0.2 N, 0.004 B Haynes HR-160 N12160 28.0 37.0 29.0...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2001
DOI: 10.31399/asm.tb.aub.t61170495
EISBN: 978-1-62708-297-6
... 8.0–10.0 1.0 0.5 … … 0.015 1.0 1.0 … 0.5 Cu Hastelloy D-205 … 65.0 20.0 6.0 … 2.5 … … … … 0.03 … 5.0 … 2.0 Cu Hastelloy N N10003 bal 6.0–8.0 5.0 0.2 15.0–18.0 0.5 … … … 0.010 1.0 1.0 0.010 0.50 V, 0.35 Cu Hastelloy X N06002 bal 20.5–23.0 17.0–20.0...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2007
DOI: 10.31399/asm.tb.htcma.t52080445
EISBN: 978-1-62708-304-1
... Bal … … 25.0 … … HAYNES HR-160 N12160 0.05 28.0 Bal 29.0 1.5 … … Si: 2.75, Ti: 0.5, Nb: 1.0 (a) Nicrofer 45TM N06045 0.1 27 Bal … 23 … … Si: 2.5–3.0, Ce: 0.03–0.09 HASTELLOY X N06002 0.1 22.0 Bal 1.5 18.5 9.0 0.6 … HASTELLOY W N10004 0.12 (a) 5.0 Bal...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2015
DOI: 10.31399/asm.tb.cpi2.t55030074
EISBN: 978-1-62708-282-2
... Composition, % Common high-temperature applications Cr Ni Co Mo Nb Ti Al Fe C Other N06002 Hastelloy X 22.0 49.0 1.5 max 9.0 … … 2.0 15.8 0.15 0.6 W Combustion chambers, heat treatment components N06075 Nimonic 75 19.5 75.0 … … … 0.4 0.15 2.5 0.12 0.25 max Cu Gas...
Book Chapter

Series: ASM Technical Books
Publisher: ASM International
Published: 01 March 2002
DOI: 10.31399/asm.tb.stg2.t61280135
EISBN: 978-1-62708-267-9
...) … 1035 1900 1 Nickel-base alloys Astroloy (c) (c) … 1135 2075 4 Hastelloy X (c) (c) … 1175 2150 1 Incoloy 800 870 1600 1½ 980 1800 ¼ Incoloy 800H … … … 1175 2150 … Incoloy 825 … … … 980 1800 … Incoloy 901 (c) (c) … 1095 2000 2...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2007
DOI: 10.31399/asm.tb.htcma.t52080249
EISBN: 978-1-62708-304-1
... resistance to hot corrosion. Alloys with 15% Cr or less are very susceptible to hot corrosion attack. Cobalt-base alloys are generally better than nickel-base alloys. This may simply be due to higher chromium contents in cobalt-base alloys. One nickel-base alloy (Hastelloy X) with a chromium level similar...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 March 2002
DOI: 10.31399/asm.tb.stg2.t61280011
EISBN: 978-1-62708-267-9
... 130 775 112 575 84 455 65 340 49 310 45 49 50 70 Hastelloy X Sheet 785 114 650 94 435 63 360 52 290 42 260 38 43 45 37 Haynes 230 (a) 870 126 720 105 575 84 390 57 275 40 285 41 48 56 46 Inconel 587 Bar 1180 171 1035 150 830 120 705 102...
Book Chapter

Series: ASM Technical Books
Publisher: ASM International
Published: 01 March 2002
DOI: 10.31399/asm.tb.stg2.t61280203
EISBN: 978-1-62708-267-9
... of cleaning and finishing of superalloys. All of the examples described subsequently are drawn from actual production experience. The examples identify cleaning and finishing problems and the procedures used to solve them. Example 1. Turbine Combustion Chambers Made from Hastelloy X Sheet After heat...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.sap.t53000009
EISBN: 978-1-62708-313-3
... solidified and single-crystal superalloys. Some nickel-base alloys do not rely on precipitates for strengthening but rather depend mainly on solid-solution hardening (SSH). Two notable alloys strengthened by SSH are Hastelloy X and alloy 625, but they also derive some hardening through carbide...