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in Beryllium-Copper and Other Beryllium-Containing Alloys
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Image
Published: 01 June 2016
Fig. 26 Aging response curves for low-beryllium, moderate-strength, and high-thermal-conductivity cast and solution-treated alloy C82000 (97wt%Cu-2.5wt%Co-0.5wt%Be). Source: Ref 11
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Image
Published: 01 June 2016
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in Beryllium-Copper and Other Beryllium-Containing Alloys
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Fig. 4 Age-hardening response curves for the tensile strength, yield strength, and elongation of C17200. (a) Annealed (TB00) temper. (b) Roll-hardened (TD04) temper
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in Beryllium-Copper and Other Beryllium-Containing Alloys
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Image
Published: 01 June 2016
Fig. 23 Age-hardening response curves for tensile strength, yield strength, and elongation of alloy C17200 (Cu-1.8 to 2.2 wt% Be-0.20 wt% min Co plus nickel). (a) Annealed (TB00 temper) and (b) roll-hardened (TD04 temper) conditions. Source: Ref 8
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Image
Published: 01 June 2016
Fig. 24 Age-hardening response curves for tensile strength, yield strength, and elongation of alloy C17510 (Cu-0.2 to 0.6 wt% Be-1.4 to 2.2 wt% Ni). Source: Ref 8
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Book Chapter
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006560
EISBN: 978-1-62708-210-5
... 151 3. Aging Response Curves of Aluminum Casting Alloys , Approved by the ASM Handbook Committee for addition to the ASM Handbook, 2011 4. Kaufman J.G. and Rooy E.L. , Aluminum Alloy Castings: Properties, Processes, and Applications , ASM International , 2004 , p 133 – 173 ...
Abstract
Alloy 296.0 is an aluminum permanent-mold casting alloy with higher silicon than 295.0, which reduces shrinkage and improves fluidity. This datasheet provides information on key alloy metallurgy, fabrication characteristics, processing effects on physical and mechanical properties, and application characteristics of this series alloy. Room-temperature aging characteristics for aluminum alloy 296.0-T4 and 296.0-T6 are also illustrated.
Series: ASM Handbook
Volume: 2
Publisher: ASM International
Published: 01 January 1990
DOI: 10.31399/asm.hb.v02.a0001071
EISBN: 978-1-62708-162-7
... aging response curves for solution-annealed and annealed and cold worked C17200 are shown in Fig. 4 . When age hardened at 315 to 335 °C (600 to 635 °F), strength increases to a plateau in about 3 h for annealed material or about 2 h for cold-worked material and remains essentially constant thereafter...
Abstract
Addition of beryllium, up to about 2 wt″, produces dramatic effects in copper, nickel, aluminum, magnesium, gold, zinc, and other base metal alloys. This article provides information on the chemical composition, microstructure, heat treatment, fabrication characteristics, production steps and physical metallurgy of beryllium-copper, beryllium-nickel, and beryllium-aluminum alloy, and tabulates their mechanical, electrical and physical properties, and temper designations. It describes the important features of this alloy group, including information on safe handling. Additionally, the article presents examples of the beneficial properties of beryllium-copper alloys and quantifies some of the major reasons for their selection for particular applications.
Series: ASM Handbook
Volume: 4E
Publisher: ASM International
Published: 01 June 2016
DOI: 10.31399/asm.hb.v04e.a0006281
EISBN: 978-1-62708-169-6
.... Bronzes originally (from the time of the Bronze Age) referred to alloys in which tin was the major alloying element. Today (2016), however, the term bronze is commonly used for a number of alloys that contain other elements with little, if any, tin. Bronzes can refer to copper alloys with various...
Abstract
Bronzes generally are used to describe many different copper-base alloys in which the major alloying addition is neither zinc nor nickel. They are generally classified by their major alloying elements, for example, tin bronzes with phosphorus used as a deoxidizer, aluminum bronzes, nickel-aluminum bronzes, silicon bronzes, and beryllium bronzes. This article briefly discusses the types, hardening mechanisms, heat treatment processes, applications, and mechanical properties of these bronzes and high-copper alloys.
Series: ASM Handbook
Volume: 4E
Publisher: ASM International
Published: 01 June 2016
DOI: 10.31399/asm.hb.v04e.a0006271
EISBN: 978-1-62708-169-6
... and simulation of age hardening as being the most important heat treatment to strengthen aluminum alloys. It provides information on the heat treatment simulation model, the yield strength model based on the responsible strengthening mechanisms, and the flow curve model based on mechanical tests. The article...
Abstract
Heat treatment simulation helps to predict heat treatment results such as component microstructures, properties, residual stresses, and distortion, and thereby assists in reducing experimental effort in defining heat treatment parameters. This article discusses the modeling and simulation of age hardening as being the most important heat treatment to strengthen aluminum alloys. It provides information on the heat treatment simulation model, the yield strength model based on the responsible strengthening mechanisms, and the flow curve model based on mechanical tests. The article also discusses simulation of the quenching process, and provides examples for aluminum quenching simulation.
Book: Fatigue and Fracture
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002411
EISBN: 978-1-62708-193-1
..., and spinodal alloys. It discusses the fatigue testing of the copper alloys and tabulates the tensile and fatigue strengths of the copper alloys. The article schematically illustrates S-N curves for the solid-solution (non-aging) strengthened alloys. It concludes with a discussion on the role of microstructure...
Abstract
Copper alloys are classified by the International Unified Numbering System designations to identify alloy groups by major alloying element. This article presents the designations and compositions of various copper alloys, such as brasses, nickel silvers, bronzes, beryllium coppers, and spinodal alloys. It discusses the fatigue testing of the copper alloys and tabulates the tensile and fatigue strengths of the copper alloys. The article schematically illustrates S-N curves for the solid-solution (non-aging) strengthened alloys. It concludes with a discussion on the role of microstructure in the fatigue performance of beryllium copper alloys.
Image
in Physical Metallurgy Concepts in Interpretation of Microstructures
> Metallography and Microstructures
Published: 01 December 2004
Fig. 42 Time-temperature diagram of precipitation responses of an aluminum-lithium alloy (alloy 8090) for volume formation of the S phase (Al 2 CuMg). This practical isothermal transformation curve is based on a real commercial-sized component that has been exposed to aging temperatures
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Book: Fatigue and Fracture
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002396
EISBN: 978-1-62708-193-1
... + ( σ a K ′ ) 1 / n ′ where E is the elastic modulus and K ′ and n ′ are cyclic deformation properties. This formulation allows for direct comparison with monotonic tension curves so that cyclic-hardening or cyclic-softening responses can be quickly assessed. Monotonic...
Abstract
This article reviews general trends in the cyclic response for representative commercial alloys to establish the spectrum of cyclic properties attainable through microstructural alteration. Individual alloy classes are examined in detail to assess the understanding of relationships between microstructure and fatigue resistance. These alloys classes include ferritic-pearlitic alloys, martensitic alloys, maraging steels, and metastable austenitic alloys. The article also discusses the role of internal defects and selective surface processing in influencing fatigue performance.
Series: ASM Handbook
Volume: 11B
Publisher: ASM International
Published: 15 May 2022
DOI: 10.31399/asm.hb.v11B.a0006921
EISBN: 978-1-62708-395-9
... several important steps: Define what constitutes a failure Identify the aging mechanism that is likely to be the long-term material behavior response leading to the failure Collect short-term data under test conditions that most closely resemble the use conditions Utilize temperature...
Abstract
The lifetime assessment of polymeric products is complicated, and if the methodology utilized leads to inaccurate predictions, the mistakes could lead to financial loss as well as potential loss of life, depending on the service application of the product. This article provides information on the common aging mechanisms of polymeric materials and the common accelerated testing methods used to obtain relevant data that are used with the prediction models that enable service life assessment. Beginning with a discussion of what constitutes a product failure, this article then reviews four of the eight major aging mechanisms, namely environmental stress cracking, chemical degradation, creep, and fatigue, as well as the methods used in product service lifetime assessment for them. Later, several methods of service lifetime prediction that have gained industry-wide acceptance, namely the hydrostatic design basis approach, Miner's rule, the Arrhenius model, and the Paris Law for fatigue crack propagation, are discussed.
Book: Fatigue and Fracture
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
...) are identical to the semidynamic curves, indicating that the beneficial effects are maintained at very high strain rates ( Ref 94 ). One of the two type 304 heats studied by Marschall ( Ref 96 ) shows a similar response, with J c increasing by 15% under semidynamic conditions. The second heat shows a much...
Abstract
This article describes the fracture toughness behavior of austenitic stainless steels and their welds at ambient, elevated, and cryogenic temperatures. Minimum expected toughness values are provided for use in fracture mechanics evaluations. The article explains the effect of crack orientation, strain rate, thermal aging, and neutron irradiation on base metal and weld toughness. It discusses the effect of cold-work-induced strengthening on fracture toughness. The article examines the fracture toughness behavior of aged base metal and welding-induced heat-affected zones. It concludes with a discussion on the Charpy energy correlations for aged stainless steels.
Series: ASM Handbook
Volume: 4E
Publisher: ASM International
Published: 01 June 2016
DOI: 10.31399/asm.hb.v04e.a0006261
EISBN: 978-1-62708-169-6
.... The precipitation of γ′ causes strengthening, as shown in Fig. 4 . The aging curve has the shape typical of that associated with precipitation hardening, passing through a maximum with time at the aging temperature. Strengthening occurs from the elastic interface strains with the lattice parameter mismatch...
Abstract
This article provides information on nickel alloying elements, and the heat treatment processes of various nickel alloys for applications requiring corrosion resistance and/or high-temperature strength. These processes are homogenization, annealing, solution annealing, solution treating, stabilization treatment, age hardening, stress relieving, and stress equalizing. Discussion of furnaces, fixtures, and atmospheres is included. Nickel alloys used for the heat treatment processes include corrosion-resistant nickel alloys, heat-resistant nickel alloys, nickel-beryllium alloys, special-purpose alloys such as nitinol shape memory alloys, low-expansion alloys, electrical-resistance alloys and soft magnetic alloys. Finally, the article focuses on heat treatment modeling for selecting the appropriate heat treatment process.
Series: ASM Handbook
Volume: 4E
Publisher: ASM International
Published: 01 June 2016
DOI: 10.31399/asm.hb.v04e.a0006263
EISBN: 978-1-62708-169-6
... response of titanium alloys. This factor is even more critical in weakly β-stabilized systems where transformation of the β phase occurs more readily during a quench. The effect of quench delay is shown in Fig. 22 for Ti-6Al-4V bar that was subsequently aged at 480 °C (900 °F...
Abstract
This article provides a detailed discussion on the heat treatment processes for titanium and titanium alloys. These processes are age hardening, solution treatment, aging, and annealing. The article illustrates the characteristics of equilibrium phase diagrams that are important for understanding the heat treatment of titanium alloys. It explains the types of metastable phases encountered in titanium alloys. The article also provides information on the equilibrium phase relationships and properties of titanium alloys.
Series: ASM Handbook
Volume: 24A
Publisher: ASM International
Published: 30 June 2023
DOI: 10.31399/asm.hb.v24A.a0006952
EISBN: 978-1-62708-439-0
... the correlation between microstructure/texture and dynamic impact response of the as-built and heat treated materials. True stress/true strain curves of dynamically deformed as-built L-PBF maraging steel samples at strain rates of 1500, 2000, 3200, 3500, and 4000 s −1 are presented in Fig. 7(a) . Both...
Abstract
This article provides a detailed discussion on nanoindentation hardness, high-strain-rate behavior and strain-rate sensitivity, and corrosion response of additively manufactured (AM) metals. It summarizes the most commonly used AM alloys for applications in harsh environments and their respective corrosion responses in various service environments. It also provides several case studies on location-dependent properties, microstructural evolution, and indentation strain-rate sensitivity of various additively manufactured alloys.
Series: ASM Handbook
Volume: 14B
Publisher: ASM International
Published: 01 January 2006
DOI: 10.31399/asm.hb.v14b.a0005133
EISBN: 978-1-62708-186-3
... temperatures (120 to 190 °C, or 250 to 375 °F). Because creep is the phenomenon responsible for achieving the part shape, age forming is sometimes referred to as creep forming. The most common application for age forming is the shaping of upper wing skins in the aerospace industry. Recent investigations ( Ref...
Abstract
Compared to cold-formed parts, age-formed parts have lower residual stresses and consequently better stress corrosion resistance. This article addresses the technical issues that arise in the investigations of creep in precipitate-strengthened materials. The issues addressed help in developing alloys and tempers particularly suited for the age-forming process. The different steps involved in the program for predicting the final part shape are discussed. These basic steps involve developing mechanical tests to study creep at low temperatures and low stresses, describing low-temperature creep in terms of a constitutive model, and then using the constitutive model in a process model or finite element analysis to predict the final part shape.
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