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Published: 01 January 1996
Fig. 16 Effect of overaging and copper content on SCC resistance of an Al-Zn-Mg alloy in 3.5% NaCl solution. Source: Ref 33
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Published: 01 January 1996
Fig. 71 Effect of overaging on part through crack growth of aluminum alloy 7475 subject to 500 h block flight-by-flight fighter spectrum loading in sump tank water. Source: Ref 127
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in Heat Treating of Air-Hardening High-Strength Structural Steels
> Heat Treating of Irons and Steels
Published: 01 October 2014
Fig. 6 Yield strength of AF1410 determined by the overaging heat treatment. Larson-Miller parameter is provided with temperature ( T ) in °F and time ( t ) in hours.
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Image
Published: 01 October 2014
Fig. 5 Yield strength of AF 1410 determined by the overaging heat treatment. Larson-Miller parameter is provided with temperature ( T ) in °F and time t ) in hours. Source: Ref 4
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in Elevated-Temperature Life Assessment for Turbine Components, Piping, and Tubing
> Failure Analysis and Prevention
Published: 01 January 2002
Fig. 9 Gamma-prime overaging in a nickel-base alloy turbine blade material. (a) SEM micrograph of the blade material, showing the breakdown of the eutectic gamma prime (5) and the spreading of the coarse gamma prime. Smaller particles of fine aging gamma prime (4), which would appear between
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Image
Published: 31 December 2017
Fig. 13 Effect of overaging on the hardness of A354, C355, and A356 T6 heat treated alloys
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Published: 15 June 2019
Fig. 14 Effect of overaging and copper content on stress-corrosion cracking (SCC) resistance of an Al-Zn-Mg alloy in 3.5% NaCl solution. Source: Ref 47
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Image
Published: 01 January 1996
Fig. 23 Schematic effect of yield strength (peak and overaged tempers) on fatigue crack growth rate under spectrum loading. Source: Ref 60
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Published: 01 January 1996
Fig. 18 Fatigue crack propagation rate of C17200 in the overaged and underaged conditions. Material aged to 760 MPa (110 ksi) yield strength
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Image
Published: 01 June 2016
Fig. 23 Q′-phase in an Al-0.93Si-0.61Mg-0.45Cu(Fe,Mn) alloy overaged for 7 h at 200 °C (390 °F). (a) Bright-field transmission electron microscopy (TEM) image in the ⟨100⟩ α zone axis. Q′ are the small precipitates slightly inclined due to their elongation parallel to ⟨510⟩ α directions. (b
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Image
Published: 01 June 2016
Fig. 3 Micrograph of an α-β alloy. Microstructure of solution-treated and overaged Ti-6Al-4V. Source: Ref 7
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in Metallography and Microstructures of Precious Metals and Precious Metal Alloys
> Metallography and Microstructures
Published: 01 December 2004
Fig. 7 Transmission electron microscope micrograph of an overaged sample of Au-0.2Co-0.3Sb (wt%) alloy showing small antimony-rich precipitates in the matrix. Source: Ref 8 , 9
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Published: 01 December 2004
Fig. 16 Micrographs from solution treated and overaged Ti-6Al-4V plate after etching with Kroll's reagent for (a) 5 s, (b) 15 s, (c) 30 s, and (d) 60 s. All specimens polished for 1 h with vibratory polisher, non-nap polyester cloth and alumina. In the severe etch (d), note that fine detail
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Image
Published: 15 June 2019
Fig. 53 Schematic effect of yield strength (YS, peak and overaged tempers) on fatigue crack growth rate under spectrum loading. Source: Ref 92
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Book Chapter
Series: ASM Handbook
Volume: 4D
Publisher: ASM International
Published: 01 October 2014
DOI: 10.31399/asm.hb.v04d.a0005960
EISBN: 978-1-62708-168-9
... Abstract Hardenable steels with high-alloy content includes a family of nickel-cobalt steels with high strength and high toughness. This article describes various heat treatments, namely, normalizing, annealing, hardening, tempering, stress relieving, overaging, quenching, refrigeration...
Abstract
Hardenable steels with high-alloy content includes a family of nickel-cobalt steels with high strength and high toughness. This article describes various heat treatments, namely, normalizing, annealing, hardening, tempering, stress relieving, overaging, quenching, refrigeration, and straightening treatment, applied to HP9-4-20, HP9-4-25, HP9-4-30, and HP9-4-45 steels. These steels have high fracture toughness when heat treated to very high strength levels. The article also describes heat treatments applied to other alloys such as AF 1410, AerMet 100, AerMet 310, and AerMet 340, which provide a good combination of high strength and toughness that make them attractive for aerospace application. It also presents tables that provide information on the effect of aging temperatures and heat treatment on mechanical properties and impact energy of these steels.
Image
Published: 01 January 1996
Fig. 3 Effect of precipitate and grain size on FCP rates in Inconel 718 tested in air at 425 °C (800 °F), R = 0.05, 0.33 Hz. (a) Fine grain; underaged versus overaged. (b) Coarse grain; underaged versus overaged. (c) Underaged; fine grain versus coarse grain. (d) Overaged; fine grain versus
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Book Chapter
Series: ASM Handbook
Volume: 2A
Publisher: ASM International
Published: 30 November 2018
DOI: 10.31399/asm.hb.v02a.a0006531
EISBN: 978-1-62708-207-5
..., and artificially aged T66 Solution heat treated and artificially aged; mechanical property level higher than T6 achieved through special control of the process (6000-series alloys) T7 Solution heat treated and stabilized T73 Solution heat treated and artificially overaged to achieve the best stress...
Abstract
This article presents a summary of aluminum temper designations, and applicable aluminum alloys and product forms for temper designations used in the United States (ANSI H35.1), Europe (EN 515), and internationally (ISO 2107).
Book Chapter
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006622
EISBN: 978-1-62708-210-5
... treated and artificially overaged/stabilized to control important properties (rarely used without second digit, as below) 7050 Rivets T72 Solution heat treated and artificially aged by user from O or F temper (not available from producer) 2024 Sheet T73 Solution heat treated and fully overaged...
Abstract
This article lists temper designations and their definitions for aluminum alloys along with their product forms used in the United States (ANSI H35.1), Europe (EN 515), and internationally (ISO 2107).
Book Chapter
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006746
EISBN: 978-1-62708-210-5
... in T7651 (peak aged) and T7951 (overaged) tempers. Mechanical properties are given in Tables 2 and 3 . AMS specifications include AMS 4250 (7440-T651) and AMS 4299 (7449-T7951 plate) and MMPDS coverage with A and B-basis values. Alloy T7951 plate is particularly suited for low-to-medium gauge parts like...
Abstract
This datasheet provides information on key alloy metallurgy and processing effects on mechanical and corrosion performance properties of aluminum alloy 7449. A comparison of toughness and stress-corrosion cracking resistance of alloy 7449 with other alloys is also provided.
Image
Published: 01 January 1996
Fig. 21 Effects of superposed pressure on the damage evolution in the MB78/15% SiC p overaged (OA) system.
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