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schedule
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Image
Published: 01 December 2006
Fig. 19 Construction of the cross-tee, showing the 2 in. Schedule 80 pipe (A), joined to the 3 in. Schedule 80 pipe (C-D) by a reduction socket (E). The remaining arm of the cross (B) was a flanged nipple welded to the 3 in. pipe. The rupture is at the toe of the weld between the 3 in. pipe
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Image
in Transformation-Induced Plasticity Steels
> Advanced-High Strength Steels: Science, Technology, and Applications
Published: 01 August 2013
Fig. 7.3 Cooling schedule in the production of the TRIP sheet. Source: Ref 7.5
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Image
in Transformation-Induced Plasticity Steels
> Advanced-High Strength Steels: Science, Technology, and Applications
Published: 01 August 2013
Fig. 7.4 Time-temperature schedule for the production of hot rolled TRIP and dual-phase (DP) steels. Source: Ref 7.6
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Image
in Failure Analysis of Stress-Corrosion Cracking[1]
> Stress-Corrosion Cracking: Materials Performance and Evaluation
Published: 01 January 2017
Fig. 18.8 Hydrogen cyanide cracking in a schedule 80 ASTM A53 black pipe steel drain line. (a) Primary crack penetration has advanced toward the outside diameter. 2% nital etch. Original magnification: 50×. (b) The primary crack is intergranular and contains numerous intergranular branches. 2
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in Non-Martensitic Strengthening of Medium-Carbon Steels—Microalloying and Bainitic Strengthening
> Steels: Processing, Structure, and Performance
Published: 01 January 2015
Fig. 14.1 Schematic diagram of the schedule of operations required to harden forged bar steels by quench and tempering heat treatments
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Image
in Non-Martensitic Strengthening of Medium-Carbon Steels—Microalloying and Bainitic Strengthening
> Steels: Processing, Structure, and Performance
Published: 01 January 2015
Fig. 14.2 Left diagram: schedule of operations required to strengthen microalloyed forged bar steels by direct cooling after forging. Right diagram: schedule of operations to produce cold-finished bars
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Image
in Transformation-Induced Plasticity Steels
> Advanced High-Strength Steels: Science, Technology, and Applications, Second Edition
Published: 31 October 2024
Fig. 7.3 Cooling schedule in the production of transformation-induced plasticity sheet. M s , martensite start temperature. Source: Ref 7.7
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Image
in Transformation-Induced Plasticity Steels
> Advanced High-Strength Steels: Science, Technology, and Applications, Second Edition
Published: 31 October 2024
Fig. 7.4 Time-temperature schedule to produce hot rolled transformation-induced plasticity (TRIP) and dual-phase (DP) steels. M s , martensite start temperature. Source: Ref 7.8
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Image
in History and Extractive Metallurgy[1]
> Titanium: Physical Metallurgy, Processing, and Applications
Published: 01 January 2015
Fig. 1.14 Schematic of electrowinning cells as operated by TIMET and the U.S. Bureau of Mines
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Image
Published: 01 December 2000
Fig. 4.6 TIMET’s larger hearth furnaces have dual chambers. Two such units, located at the Morgantown, PA facility, have a combined refining capacity of 40 million lb per year. Courtesy of Titanium Metals Corp. (TIMET)
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in Primary Processing Effects on Steel Microstructure and Properties
> Steels: Processing, Structure, and Performance
Published: 01 January 2015
Fig. 9.1 Schematic diagram of temperature-time schedules for primary processing of steel cast by various technologies
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Image
Published: 01 January 2015
Fig. 12.3 Temperature-time processing schedules for cold-rolled and annealed low-carbon sheet steels. Continuous and batch annealing are schematically compared and intercritical annealing used to produce dual-phase and TRIP steels is indicated.
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Image
Published: 01 January 2015
Fig. 12.13 Schematic of temperature-time schedules for thermomechanical and controlled rolling schedules of low-carbon steels. (a) Normal processing. (b) Controlled rolling of C-Mn steels. (c) Controlled rolling of Nb-containing steels. (d) Controlled rolling of Nb-containing steels
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2000
DOI: 10.31399/asm.tb.ttg2.t61120195
EISBN: 978-1-62708-269-3
..., Ti-17); Ti-6Al-2Sn-4Zr-6Mo (UNS R56260, Ti-6246); Ti-6Al-4V (UNS R56400) and Ti-6Al-4V ELI (UNS R56401); Ti-6Al-6V-2Sn (UNS R56620, Ti-662); Ti-7Al-4Mo (UNS R56740); Ti-6Al-1.7Fe-0.1Si (TiMetal 62S); Ti-4.5Al-3V-2Mo-2Fe (SP-700); Ti-6Al-7Nb (IMI 367); Ti-4Al-4Mo-2Sn-0.5Si (IMI 550); Ti-4Al-4Mo-4Sn...
Abstract
This appendix provides datasheets describing the chemical composition, processing characteristics, mechanical and fabrication properties, and heat treating of various grades of alpha-beta titanium. Datasheets are provided for the following alloys: Ti-5Al-2Sn-2Zr-4Mo-4Cr (UNS: R58650, Ti-17); Ti-6Al-2Sn-4Zr-6Mo (UNS R56260, Ti-6246); Ti-6Al-4V (UNS R56400) and Ti-6Al-4V ELI (UNS R56401); Ti-6Al-6V-2Sn (UNS R56620, Ti-662); Ti-7Al-4Mo (UNS R56740); Ti-6Al-1.7Fe-0.1Si (TiMetal 62S); Ti-4.5Al-3V-2Mo-2Fe (SP-700); Ti-6Al-7Nb (IMI 367); Ti-4Al-4Mo-2Sn-0.5Si (IMI 550); Ti-4Al-4Mo-4Sn-0.5Si (IMI 551); Ti-6Al-2Sn-2Zr-2Mo-2Cr-0.25Si (Ti-6-22-22S); Ti-5Al-2.5Fe (DIN 3.7110, Tikrutan LT 35); and Ti-5Al-5Sn-2Zr-2Mo-0.25Si (UNS R54560, Ti-5522-S).
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2000
DOI: 10.31399/asm.tb.ttg2.t61120240
EISBN: 978-1-62708-269-3
...); Ti-3Al-8V-6Cr-4Mo-4Zr (UNS R58640, Beta C and 38-6-44); Ti-10V-2Fe-3Al (Ti-10-2-3); Ti-13V-11Cr-3Al (UNS R58010, Ti-13-11-3); Ti-15V-3Al-3Cr-3Sn (Ti-15-3); Ti-15Mo-3Al-2.7Nb-0.25Si (UNS R58210, TiMetal 21S and Beta 21S); Ti-5Al-2Sn-4Zr-4Mo-2Cr-1Fe (Beta CEZ); Ti-8Mo-8V-2Fe-3Al (Ti-8823); Ti-15Mo-5Zr...
Abstract
This appendix provides datasheets describing the chemical composition, processing characteristics, mechanical and fabrication properties, and heat treating of beta and near-beta titanium alloys. Datasheets are provided for the following alloys: Ti-11.5Mo-6Zr-4.5Sn (UNS R58030, Beta III); Ti-3Al-8V-6Cr-4Mo-4Zr (UNS R58640, Beta C and 38-6-44); Ti-10V-2Fe-3Al (Ti-10-2-3); Ti-13V-11Cr-3Al (UNS R58010, Ti-13-11-3); Ti-15V-3Al-3Cr-3Sn (Ti-15-3); Ti-15Mo-3Al-2.7Nb-0.25Si (UNS R58210, TiMetal 21S and Beta 21S); Ti-5Al-2Sn-4Zr-4Mo-2Cr-1Fe (Beta CEZ); Ti-8Mo-8V-2Fe-3Al (Ti-8823); Ti-15Mo-5Zr; Ti-15Mo-5Zr-3Al; Ti-11.5V-2Al-2Sn-11Zr (T129); Ti-12V-2.5Al-2Sn-6Zr (T134); Ti-13V-2.7Al-7Sn-2Zr (T175); Ti-8V-5Fe-1Al; and Ti-16V-2.5Al.
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
..., the machining program afforded an opportunity to compile comparative information on the three alloys. Milling predominated in the machining schedule, but enough drilling, single-point cutting, shaping, and abrasive sawing operations were involved to provide a fair knowledge of the production capabilities...
Abstract
The qualities that make superalloys excellent engineering materials also make them difficult to machine. This chapter discusses the challenges involved in machining superalloys and the factors that determine machinability. It addresses material removal rates, cutting tool materials, tool life, and practical issues such as set up time, tool changes, and production scheduling. It describes several machining processes, including turning, boring, planing, trepanning, shaping, broaching, drilling, tapping, thread milling, and grinding. It also provides information on toolholders, fixturing, cutting and grinding fluids, and tooling modifications.
Image
Published: 01 October 2012
Fig. 11.22 Unidirectional alumina-fiber/glass-matrix composite formed by slurry infiltration followed by hot pressing. (a) Light micrograph of transverse section (some porosity can be seen in this micrograph). (b) Pressure and temperature schedule used during hot pressing of this composite
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Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2005
DOI: 10.31399/asm.tb.faesmch.t51270133
EISBN: 978-1-62708-301-0
.... The other adjoining blades that showed hardness within the specified range showed no such cracking. Conclusion The blade failed due to SCC at the mid-chord region. Recommendation Care should be exercised to follow strictly the heat treatment schedule specified. Failure Analysis...
Abstract
A second-stage compressor blade in an aircraft engine fractured after 21 h of service. The remaining portion of the blade was removed and examined as were several adjacent blades. Based on the results of SEM fractography, microstructural analysis, and hardness testing, the blade failed due to stress-corrosion cracking combined with the effects of inadequate tempering.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 2013
DOI: 10.31399/asm.tb.ahsssta.t53700115
EISBN: 978-1-62708-279-2
... fraction of retained austenite. The retained austenite transforms to martensite during plastic deformation, which also produces mechanical twins. Twin boundaries act as effective barriers to dislocation motion. Fig. 7.3 Cooling schedule in the production of the TRIP sheet. Source: Ref 7.5...
Abstract
Transformation-induced plasticity (TRIP) steels are characterized by their excellent strength and high ductility, which allow the production of more complicated parts for lightweight automotive applications. This chapter provides an overview of the compositions, microstructures, processing, deformation mechanism, mechanical properties, hot forming, tempering, and special attributes of TRIP the steels.
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