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300M
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in Engineered Special Bar Quality Steel (Engineering Steels)
> Metallography of Steels: Interpretation of Structure and the Effects of Processing
Published: 01 August 2018
Fig. 15.4 (a) 300M steel quenched at approximately 10 K/s. Bainite, martensite, and areas of ferrite and/or retained austenite. Etchant: nital 2%. (b) 300M steel quenched at approximately 10 K/s in a different region. Bainite, martensite, and ferrite or pearlite are colored by the etchant
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in Overview of the Mechanisms of Failure in Heat Treated Steel Components
> Failure Analysis of Heat Treated Steel Components
Published: 01 September 2008
Fig. 47 Micrograph showing quenched and tempered martensite, typical of 300M heat treated to HRC 54 to 55. Note that the chromium plating is intact.
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Published: 01 June 2008
Fig. 20.9 Comparison of air- and vacuum-melted 300M steel. Source: Ref 12
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Published: 01 November 2012
Fig. 15 Room-temperature S - N curves for a 300M steel with an ultimate tensile strength of 2000 MPa (290 ksi) having various notch severities. Stress ratio R equals 1.0. Source: Ref 6
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Published: 01 November 2013
Fig. 5 Comparison of air- and vacuum-melted 300M steel. Source: Ref 4
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Published: 01 March 2006
Fig. 4.31 Typical constant-life fatigue diagram for low-alloy steel 300M at room temperature. Source: Ref 4.10
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Published: 01 July 1997
Fig. 4 A failed flash-welded joint in a 300M steel arresting-hook stinger. Light-colored radial manganese sulfide inclusions are evident. 0.5x
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in Stress-Corrosion Cracking of High-Strength Steels (Yield Strengths Greater Than 1240 MPa)[1]
> Stress-Corrosion Cracking: Materials Performance and Evaluation
Published: 01 January 2017
Fig. 3.15 Crack growth rates in distilled water plotted as a function of K for three microstructures. The three microstructures are 4340 tempered at 300 °C (570 °F), 300M tempered at 470 °C (880 °F), and 300M isothermally transformed at 250 °C (480 °F) and then tempered at 300 °C. Source
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Published: 01 March 2006
Fig. 4.32 Deduced completely reversed stress amplitude vs. fatigue life relationship for 300M
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Published: 01 March 2006
Fig. 4.34 Comprehensive model for mean stress representation of fatigue results for 300M steel. Q = 4.83; P = –0.139
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in Case Studies of Steel Component Failures in Aerospace Applications
> Failure Analysis of Heat Treated Steel Components
Published: 01 September 2008
Fig. 40 Microstructure and secondary cracking at the discolored region. (a) Normal tempered martensite typical of 300M (25 μm). (b) Secondary cracking apparent on inner diameter surface (100 μm)
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Published: 01 March 2006
Fig. 4.35 Results of applying the comprehensive model for mean stress effects for fatigue behavior of 300M steel assuming zero scatter: (a) Log-log plot of α vs. 2 N f . The number by each data point is the test number in Table 4.1 . (b) Mean stress vs. alternating stress diagram. Q = 4.83
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Published: 01 March 2006
Fig. 4.36 Results of applying the comprehensive model for mean stress effects for fatigue behavior of 300M steel assuming ±1.5× scatter in life. (a) Log-log plot of α versus 2 N f . The number by each data point is the test number in Table 4.1 . (b) Mean stress vs. alternating stress diagram
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Published: 01 March 2006
Fig. 4.37 Results of applying the comprehensive model for mean stress effects for fatigue behavior of 300M steel assuming ±2× scatter in life. (a) Log-log plot of α versus 2 N f . The number by each data point is the test number in Table 4.1 . (b) Mean stress vs. alternating stress diagram
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Series: ASM Technical Books
Publisher: ASM International
Published: 01 September 2008
DOI: 10.31399/asm.tb.fahtsc.t51130351
EISBN: 978-1-62708-284-6
... pins exhibited cracks in the flanges during magnetic particle inspection as part of the manufacturing process. Some parts were returned to the vendor for rework, while others were reworked in-house. The pins were machined from 300M steel. The pins were then heat treated to a strength range of 1930...
Abstract
This chapter presents various case histories that illustrate a variety of failure mechanisms experienced by the high-strength steel components in aerospace applications. The components covered are catapult holdback bar, AISI 420 stainless steel roll pin, main landing gear (MLG) lever, inboard flap hinge bolt, nose landing gear piston axle, multiple-leg aircraft-handling sling, aircraft hoist sling, internal spur gear, and MLG axle. In addition, the chapter provides information on full-scale fatigue testing, nondestructive testing, and failure analysis of fin attach bolts.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 March 2006
DOI: 10.31399/asm.tb.fdsm.t69870075
EISBN: 978-1-62708-344-7
... reversed stress amplitude vs. fatigue life relationship for 300M Fig. 4.33 Determination of constants Q and P for 300M steel Fig. 4.34 Comprehensive model for mean stress representation of fatigue results for 300M steel. Q = 4.83; P = –0.139 Fig. 4.29 Extension of data...
Abstract
This chapter discusses the concept of mean stress and explains how it is used in fatigue analysis and design. It begins by examining the stress-strain response of test samples subjected to cyclic forces and strains, noting important features and what they reveal about materials and their fatigue behaviors. It then discusses the challenge of developing hysteresis loops for complex loading patterns and accounting for effects such as ratcheting and stress relaxation. The sections that follow provide a summary of the various ways mean stress is described in the literature and the methods used to calculate or predict its effect on the fatigue life of machine components. The discussion also sheds light on why tensile mean stress is detrimental to both fatigue life and ductility, while compressive mean stress is highly beneficial.
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2019
DOI: 10.31399/asm.tb.mfadr7.t91110499
EISBN: 978-1-62708-247-1
.... Unfortunately, DRAM test systems often use algorithmic pattern generator for test execution and evaluation. Although an executable pattern can be in μs or ms time range, the test evaluation time that is required before the next test is executed (also called test-to-test index time) amounts roughly to 300ms...
Abstract
This article provides an introduction to the dynamic random access memory (DRAM) operation with a focus to localization techniques of the defects combined with some physical failure analysis examples and case studies for memory array failures. It discusses the electrical measurement techniques for array failure analysis. The article then presents know-how-based analysis techniques of array failures by bitmap classification. The limits of bitmapping that lead to well-known localization techniques like thermally induced voltage alteration and optical beam induced resistance change are also discussed. The article concludes by providing information on soft defect localization techniques.
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 2018
DOI: 10.31399/asm.tb.msisep.t59220519
EISBN: 978-1-62708-259-4
... engineering steels. As in the case of multiphase steels ( Chapter 13, “Advanced Steels for Forming Operations,” in this book), the use of different etchants to get complementary information can also be successfully applied to quenched and tempered steels. Figure 15.4 presents a sample of 300M steel cooled...
Abstract
This chapter examines the microstructure of special bar quality (or engineering) steels and how it is influenced by carbon content, tempering temperature, and prior austenitic grain size. It explains how some of the changes are difficult to detect and require special etching and/or measurement techniques. It provides information on many types of engineering steel, including medium and high-carbon steels used in rail applications. It also examines the effect of nickel-phosphorus coatings on stainless steel and phosphate coatings used to reduce friction during thread rolling and other such procedures.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 1999
DOI: 10.31399/asm.tb.cmp.t66770037
EISBN: 978-1-62708-337-9
... ), investigating nitrogen-base atmospheres for the heat-treatment of 4340 and 300M steels, found that the three atmospheres (pure nitrogen, methanol CAP-air, and methanol CAP-CO 2 ) produced some partial decarburization as well as some internal oxidation ( Table 2.1 ). The interesting result of this work...
Abstract
This chapter explains how decarburization can occur during carburizing processes and how to limit the severity of its effects. It describes the reactions and conditions that result in a loss of carbon atoms and how they vary with changes in the physical metallurgy of the affected material and the processing environment. It examines the characteristic features of decarburized microstructures and assesses their influence on hardness, residual stresses, and fatigue and fracture behaviors. It also discusses corrective measures and practical considerations regarding their use.
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