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cryogenic alloys

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Series: ASM Handbook
Volume: 12
Publisher: ASM International
Published: 01 June 2024
DOI: 10.31399/asm.hb.v12.a0007026
EISBN: 978-1-62708-387-4
... Abstract This article aims to summarize the work on cryogenic strength and toughness and to present the fractography of aluminum alloys. It presents case studies on the importance of understanding the fractography of aluminum alloys and the role of microstructure in the appearance...
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006614
EISBN: 978-1-62708-210-5
... alloys armor plate cryogenic alloys mechanical properties Alloy 2519 ( Table 1 ) is an Al-Cu alloy that was initially developed as a higher strength weldable alloy for armor plate. Aluminum alloys considered for use as armor include alloys 5083, 7039, and 2519. Alloys 7039 and 2519 are weldable...
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Published: 01 January 1990
Fig. 7 Yield strengths of two aluminum-lithium candidate alloys for cryogenic tankage applications. Strain rate, 4 × 10 −4 /s with a 0.5-h hold at temperature More
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Published: 01 June 2024
Fig. 11 Optical micrographs of commercial aluminum alloys for cryogenic applications, showing variation in microstructures from the as-cast stage to the product fabrication stage. (a) AA2219 direct chill (DC) cast microstructure of large-sized ingot. (b) AA2219-T851 ring rolled to 2800 mm (110 More
Series: ASM Handbook
Volume: 6
Publisher: ASM International
Published: 01 January 1993
DOI: 10.31399/asm.hb.v06.a0001464
EISBN: 978-1-62708-173-3
... Abstract Cryogenic temperatures cause many structural alloys to become brittle, which is an unacceptable condition in most structural applications and is rectified by optimizing the weld composition. Although nonmatching weld compositions are most appropriate, differences between the welds...
Series: ASM Handbook
Volume: 4A
Publisher: ASM International
Published: 01 August 2013
DOI: 10.31399/asm.hb.v04a.a0005822
EISBN: 978-1-62708-165-8
.... , Bond R. , and Torres P. , “Effects of Cryogenic Treatment on the Residual Stress and Mechanical Properties of an Aerospace Aluminum Alloy,” NASA , Huntsville, AL , 2002 7. Collins D.N. , Cryogenic Treatment of Tool Steels , Adv. Mater. Process. , 1998 8. Meng F...
Series: ASM Handbook
Volume: 8
Publisher: ASM International
Published: 01 January 2000
DOI: 10.31399/asm.hb.v08.a0003267
EISBN: 978-1-62708-176-4
... that of the yield strength, allowing the alloy to maintain its ductile behavior. The ultimate tensile strengths of the fcc metals have stronger temperature dependence than those of bcc metals. Austenitic stainless steels have fcc structures and are used extensively at cryogenic temperatures because...
Series: ASM Handbook Archive
Volume: 12
Publisher: ASM International
Published: 01 January 1987
DOI: 10.31399/asm.hb.v12.a0000624
EISBN: 978-1-62708-181-8
...-12Ni-0.5Ti alloy intended for use at cryogenic temperatures. The series shows the effect on Charpy impact energy at −196 °C (−321 °F), and on fracture-surface characteristics, of the temperature of aging after austenitizing at 900 °C (1650 °F) for 2 h and air cooling.) Fig. 1208 This SEM...
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Published: 15 June 2019
Fig. 1 Notch-yield ratio versus yield strength at a temperature of 4K of alloy 7005 and other aluminum alloys used at cryogenic temperatures More
Series: ASM Handbook
Volume: 2
Publisher: ASM International
Published: 01 January 1990
DOI: 10.31399/asm.hb.v02.a0001110
EISBN: 978-1-62708-162-7
... Abstract Niobium-titanium alloys (NbTi) became the superconductors of choice in the early 1960s, providing a viable alternative to the A-15 compounds and less ductile alloys of niobium-zirconium. This can be attributed to the relative ease of fabrication, better electrical properties...
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002404
EISBN: 978-1-62708-193-1
... at elevated temperatures. In addition, AISI type 300-series stainless steels are the most widely used structural alloys for cryogenic applications, because they exhibit high strength, ductility, and fracture toughness properties as well as low thermal expansion and low magnetic permeability. Extensive...
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Published: 01 June 2024
Fig. 16 SEM micrographs of fracture surfaces showing the effect of a cold rolling and stretching combination to impart 7% cold work to Al-Cu-Li alloy AA2219 alloy to obtain the peak-aged condition of T87 at ambient and cryogenic temperatures in both longitudinal (L) and transverse (T More
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Published: 01 June 2024
Fig. 14 (a–c) Engineering stress-strain curves and (d–f) true-stress/true-strain curves of various aluminum alloys (AA2219-T851, AA8090-T8771, WL049-T851) developed for cryogenic applications tested at 295, 77, and 4 K. Source: Ref 23 More
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Published: 01 June 2024
Fig. 13 Bright-field transmission electron micrographs of precipitate phases present in commercial aluminum alloys used in cryogenic propellant tanks of launch vehicles. (a) Distribution of θ′ phase. (b) Fine precipitation of T 1 and θ′ phases in the aluminum matrix, with the selected area More
Series: ASM Handbook
Volume: 7
Publisher: ASM International
Published: 30 September 2015
DOI: 10.31399/asm.hb.v07.a0006128
EISBN: 978-1-62708-175-7
... Abstract High-potential high-alloy tool steels (HATS) containing martensitic microstructure with undissolved hard phases are achieved by a number of complex heat treating cycles, predominantly tempering. This article focuses on three tempering treatments, namely, salt bath heat treatment...
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Published: 01 December 2004
Fig. 43 Grain structure of hot-rolled alloy 718 in the solution-annealed condition from: (a) 954 °C (1750 °F), and (b) 1066 °C (1950 °F). Revealed using glyceregia. This reagent is good for revealing the second-phase precipitates but is not suitable for fully revealing the grain structure More
Series: ASM Handbook
Volume: 6
Publisher: ASM International
Published: 01 January 1993
DOI: 10.31399/asm.hb.v06.a0001461
EISBN: 978-1-62708-173-3
... in this Section details some of the requirements involved during the original construction phase or later in-place repairs of large maritime structures; in addition, reference material is provided to point the reader to other sources of information. Application of materials in cryogenic service (where...
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Published: 01 January 1987
of an Fe-12Ni-0.5Ti alloy intended for use at cryogenic temperatures. The series shows the effect on Charpy impact energy at −196 °C (−321 °F), and on fracture-surface characteristics, of the temperature of aging after austenitizing at 900 °C (1650 °F) for 2 h and air cooling.) More
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Published: 01 January 1987
fractograph of specimens of an Fe-12Ni-0.5Ti alloy intended for use at cryogenic temperatures. The series shows the effect on Charpy impact energy at −196 °C (−321 °F), and on fracture-surface characteristics, of the temperature of aging after austenitizing at 900 °C (1650 °F) for 2 h and air cooling.) More
Image
Published: 01 January 1987
of an Fe-12Ni-0.5Ti alloy intended for use at cryogenic temperatures. The series shows the effect on Charpy impact energy at −196 °C (−321 °F), and on fracture-surface characteristics, of the temperature of aging after austenitizing at 900 °C (1650 °F) for 2 h and air cooling.) More