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fatigue life
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 March 2006
DOI: 10.31399/asm.tb.fdsm.t69870045
EISBN: 978-1-62708-344-7
... discusses high-cycle, low-cycle, and ultra-high cycle fatigue and presents several models that are useful for fatigue life predictions. fatigue design fatigue life analysis high-cycle fatigue S-N curve Introduction Traditional <italic>S-N</italic> Curve In attempting to introduce some...
Abstract
This chapter familiarizes readers with the methods used to quantify the effects of fatigue on component lifetime and failure. It discusses the development and use of S-N (stress amplitude vs. cycles to failure) curves, the emergence of strain-based approaches to fatigue analysis, and important refinements and modifications. It demonstrates the use of approximate equations, including the method of universal slopes and the four-point correlation technique, which provides reasonable estimates of elastic and plastic lines from information obtained in standard tensile tests. It also discusses high-cycle, low-cycle, and ultra-high cycle fatigue and presents several models that are useful for fatigue life predictions.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 September 2005
DOI: 10.31399/asm.tb.gmpm.t51250293
EISBN: 978-1-62708-345-4
... Abstract This chapter summarizes the various kinds of gear wear and failure and how gear life in service is estimated and discusses the kinds of flaws in material that may lead to premature gear fatigue failure. The topics covered are alignment, gear tooth, surface durability and breakage...
Abstract
This chapter summarizes the various kinds of gear wear and failure and how gear life in service is estimated and discusses the kinds of flaws in material that may lead to premature gear fatigue failure. The topics covered are alignment, gear tooth, surface durability and breakage of gear tooth, life determined by contact stress and bending stress, analysis of gear tooth failure by breakage after pitting, and metallurgical flaws that reduce the life of gears. The chapter briefly reviews some components in the design and structure of each gear and/or gear train that must be considered in conjunction with the teeth to enhance fatigue life.
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Published: 01 March 2006
Fig. 10.34 Relation between percent of life to crack initiation and fatigue life data from Ref 10.32 . Source: Ref 10.32
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in Special Materials: Polymers, Bone, Ceramics, and Composites
> Fatigue and Durability of Structural Materials
Published: 01 March 2006
Fig. 12.20 Relation between percent of life to crack initiation and fatigue life. Source: Ref 12.5
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in Introduction to Fatigue and Fracture
> Fatigue and Fracture<subtitle>Understanding the Basics</subtitle>
Published: 01 November 2012
Fig. 1 The process of fatigue. (a) Cyclic loading. (b) Fatigue life of steel with an endurance limit and aluminum with no endurance limit. Source: Ref 2
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in Fatigue and Fracture of Engineering Alloys
> Fatigue and Fracture<subtitle>Understanding the Basics</subtitle>
Published: 01 November 2012
Fig. 21 Effect of case depth on fatigue life. Fatigue tests on induction-hardened 1038 steel automobile axle shafts 32 mm (1.25 in.) in diameter. Case depth ranges given on the chart are depths to 40 HRC. Shafts with lower fatigue life had a total case depth to 20 HRC of 4.5 to 5.2 mm (0.176
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Published: 01 March 2006
Fig. 4.8 Effect of mean stress on fatigue life. (a) Notched specimen fatigue lives resulting from two types of initial overload; also lives of un-notched specimens subjected to strain histories estimated to occur at notch. (b) Details of load history A. (c) Details of load history B. Source
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in Life-Assessment Techniques for Combustion Turbines
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Fig. 9.18. Fatigue-life data for IN 738 samples tested under thermomechanical fatigue conditions ( Ref 18 and 25 ). (a) Plot using strain-range criterion. (b) Plot using maximum-tensile-stress criterion.
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Published: 01 September 2008
Fig. 94 Comparison of fatigue life of induction surface-hardened transmission shafts with that of through-hardened and carburized shafts. Arrow in lower bar (induction-hardened shafts) indicates that one shaft had not failed after testing for the maximum number of cycles shown. Source: Ref 45
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Published: 01 December 2018
Fig. 3.6 Relationship between fatigue life, pore size, and DAS. Reprinted with permission from Ref 4 .
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Published: 01 December 2015
Fig. 14 Comparison of fatigue life for 4130 steel under fretting and nonfretting conditions. Specimens were water quenched from 900 °C (1650 °F), tempered 1 h at 450 °C (840 °F), and tested in tension-tension fatigue. Normal stress was 48.3 MPa (7 ksi); slip amplitude was 30 to 40 μm.
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Published: 01 November 2012
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Published: 01 November 2012
Fig. 13 Histograms showing fatigue-life distribution for 57 specimens of a 75S-T6 aluminum alloy tested at 207 MPa (30 ksi). Note the influence of a (a) linear or (b) logarithmic plot of cycles to failure N on the shape of the histogram. Source: Ref 9
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Published: 01 November 2012
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Published: 01 November 2012
Fig. 54 Effect of hot isostatic pressing (HIP) on fatigue life of A201.0-T7 aluminum casting. Source: Ref 31
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in Fatigue and Fracture of Engineering Alloys
> Fatigue and Fracture<subtitle>Understanding the Basics</subtitle>
Published: 01 November 2012
Fig. 20 Effect of carburizing and surface hardening on fatigue life. Comparison of carburized, through-hardened, and induction-hardened transmission shafts tested in torsion. Arrow in lower bar on chart indicates that one shaft had not failed after the test was stopped at the number of cycles
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in Metallic Joints: Mechanically Fastened and Welded
> Fatigue and Fracture<subtitle>Understanding the Basics</subtitle>
Published: 01 November 2012
Fig. 3 Fatigue life of riveted joints with different tension (T)/shear (S)/bearing (B) ratios. Source: Ref 3
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in Metallic Joints: Mechanically Fastened and Welded
> Fatigue and Fracture<subtitle>Understanding the Basics</subtitle>
Published: 01 November 2012
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in Metallic Joints: Mechanically Fastened and Welded
> Fatigue and Fracture<subtitle>Understanding the Basics</subtitle>
Published: 01 November 2012
Fig. 24 Range of postweld fatigue life improvement techniques. TIG, tungsten inert gas. Source: Ref 16
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Published: 01 August 2015
Fig. 7.9 Bending fatigue life of actual SE 15B35 induction-hardened spindles vs. the induction power setting. Source: Ref 6
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