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creep crack growth
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Image
Published: 01 December 1989
Image
Published: 01 December 1989
Fig. 3.29. Effect of environment on creep-crack growth in Inconel 718 at 540 °C (1000 °F) ( Ref 157 ). ○ 20 kN in vacuum. Δ 24.4 kN in vacuum. ∇ 27.8 kN in vacuum. • 20 kN in air.
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Image
in Life Assessment of Steam-Turbine Components
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Fig. 6.15. Creep-crack-growth-rate behavior of type A470, class 8 steel at 538 °C (1000 °F) in air ( Ref 26 ).
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Image
in Petroleum Reactor Pressure-Vessel Materials for Hydrogen Service
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Fig. 7.31. Creep-crack-growth rates for HAZ materials in l¼Cr-½lMo and 2¼Cr-1Mo steels ( Ref 14 ).
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Image
in Life-Assessment Techniques for Combustion Turbines
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Fig. 9.54. Creep-crack-growth rates as a function of stress-intensity factor for IN 738 LC and IN 939 at 850 °C (1560 °F) in air ( Ref 9 and 84 ).
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Image
in Properties and Performance of Aluminum Castings
> Aluminum Alloy Castings: Properties, Processes, and Applications
Published: 01 December 2004
Fig. 8.29 Creep crack growth as a function of applied stress-intensity factor for selected wrought aluminum alloys
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 2005
DOI: 10.31399/asm.tb.mmfi.t69540281
EISBN: 978-1-62708-309-6
... Abstract Large-scale yielding at the crack tip and time-dependent crack growth mechanisms, such as stress relaxation due to creep, are nonlinear behaviors requiring nonlinear analysis methods. This chapter presents two such methods, one based on elastic-plastic fracture mechanics, the other...
Abstract
Large-scale yielding at the crack tip and time-dependent crack growth mechanisms, such as stress relaxation due to creep, are nonlinear behaviors requiring nonlinear analysis methods. This chapter presents two such methods, one based on elastic-plastic fracture mechanics, the other on time-dependent fracture mechanics. It also introduces two new fracture indices, the J-integral for handling large-scale yielding and the C*-integral for creep crack growth, providing close-form and handbook solutions for each.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 1989
DOI: 10.31399/asm.tb.dmlahtc.t60490059
EISBN: 978-1-62708-340-9
... = 385 kJ/mole. 22 20Cr-25Ni-Nb steel 700-750 n varied from 6 to 8.4 with increasing T. Q varied with σ . At σ = 79 MPa, Q = 678 kJ/mole. ... ... Values of n and Q are only “apparent” unless a back stress due to NbC precipitate is considered. Summary of creep-crack-growth constants b...
Abstract
This chapter provides a detailed overview of the creep behavior of metals and how to account for it when determining the remaining service life of components. It begins with a review of creep curves, explaining how they are plotted and what they reveal about the operating history, damage mechanisms, and structural integrity of the test sample. In the sections that follow, it discusses the effects of stress and temperature on creep rate, the difference between diffusional and dislocation creep, and the use of time-temperature-stress parameters for data extrapolation. It explains how to deal with time dependent deformation in design, how to estimate cumulative damage under changing conditions, and how to assess the effect of multiaxial stress based on uniaxial test data. It also includes information on rupture ductility, creep fracture, and creep-crack growth and their effect on component life and performance.
Image
Published: 01 December 1989
Fig. 3.22. Schematic representation of the levels of creep deformation under which creep-crack growth can occur ( Ref 120 ).
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Image
Published: 01 December 1989
Fig. 3.31. Monkman-Grant-type correlation between time to failure and creep-crack-growth rate for gas-turbine disk alloys ( Ref 8 ).
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Image
Published: 01 December 1989
Fig. 3.26. Effects of material composition (steel A had a lower impurity content than steel D) and simulated postweld heat treatment on creep-crack-growth behavior of 1¼Cr-½Mo steels ( Ref 149 ).
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 July 1997
DOI: 10.31399/asm.tb.wip.t65930163
EISBN: 978-1-62708-359-1
... cracking, hydrogen-induced cracking, and other environmentally assisted failure modes. High-temperature creep includes creep rupture and creep crack growth. This article discusses each of these categories, as well as the benefits of a fitness-for-service approach. Fracture Mechanics...
Abstract
Depending on the operating environment and the nature of the applied loading, a structure can fail by a number of different modes, including brittle fracture, ductile fracture, plastic collapse, fatigue, creep, corrosion, and buckling. These failure modes can be broken down into the categories of fracture, fatigue, environmental cracking, and high-temperature creep. This article discusses each of these categories, as well as the benefits of a fitness-for-service approach.
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 1989
DOI: 10.31399/asm.tb.dmlahtc.t60490329
EISBN: 978-1-62708-340-9
...) Toughness Hydrogen embrittlement Hydrogen embrittlement (shutdown) Sulfide stress cracking Toughness Slow crack growth Environment-assisted crack growth Toughness Flow localization Fatigue-crack-growth rate Corrosion Hydrogen attack Strength and creep resistance...
Abstract
This chapter covers the failure modes and mechanisms of concern in hydroprocessing reactor vessels and the methods used to assess lifetime and performance. It begins with a review of the materials used in the construction of pressure-vessel shells, the challenges they face, and the factors that determine shell integrity. The discussion addresses key properties and design parameters including allowable stress, fracture toughness, the effect of microstructure and composition on embrittlement, high-temperature creep, and subcritical crack growth. The chapter also provides information on the factors that affect cladding integrity and ends with a section on life-assessment techniques.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 1989
DOI: 10.31399/asm.tb.dmlahtc.t60490265
EISBN: 978-1-62708-340-9
... ( Ref 121 ). Fig. 6.3. HP-IP rotor configurations and cracking locations. (a) Radial-axial bore crack. (b) Transverse crack in heat groove. (c) Creep cracking in blade-attachment area. Fig. 6.40. Effect of hold time on fatigue-crack-growth-rate properties of 2¼Cr-1Mo cast steel ( Ref...
Abstract
This chapter covers the failure modes and mechanisms of concern in steam turbines and the methods used to assess remaining component life. It provides a detailed overview of the design considerations, material requirements, damage mechanisms, and remaining-life-assessment methods for the most-failure prone components beginning with rotors and continuing on to casings, blades, nozzles, and high-temperature bolts. The chapter makes extensive use of images, diagrams, data plots, and tables and includes step-by-step instructions where relevant.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 1989
DOI: 10.31399/asm.tb.dmlahtc.t60490183
EISBN: 978-1-62708-340-9
... of material constants at 540 °C (1000 °F) needed for prediction of remaining creep-crack-growth life (<xref ref-type="bibr" rid="t60490183-ref73">Ref 73</xref>) Table 5.8. Summary of material constants at 540 °C (1000 °F) needed for prediction of remaining creep-crack-growth life ( Ref 73 ) Material...
Abstract
This chapter covers the failure modes and mechanisms associated with boiler components and the tools and techniques used to assess damages and predict remaining component life. It begins with a review of the design and operation of a utility boiler and the materials used in construction. It then describes the various causes of failure in boiler tubes, headers, and steam pipes, explaining how and why they occur, how they are diagnosed, and how to mitigate their effects. The final and by far largest section in the chapter is a tutorial on damage and life assessment techniques for boiler components and assemblies. It demonstrates the use of various methods, including analytical techniques that estimate life expenditure based on operating history, component geometry, and material properties; predictive methods based on the extrapolation of failure statistics; methods that predict life based on dimensional measurements; methods based on metallographic studies; methods based on temperature estimates; and a method for estimating remaining life under creep conditions based on stress-rupture testing of service-exposed material samples. The chapter also discusses the use of fracture mechanics and presents a number of cases in which life assessments are made based on the integration of several methods.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 1989
DOI: 10.31399/asm.tb.dmlahtc.t60490111
EISBN: 978-1-62708-340-9
... steels ( Ref 20 ). Fig. 4.27. Comparison of crack-growth behavior of Fe-Ni alloy A-286 in air and vacuum at 595 °C (1100 °F) ( Ref 69 ). Fig. 4.28. Creep-rupture/low-cycle-fatigue damage interaction curve for 1Cr-Mo-V rotor steel at 540 °C (1000 °F) (after Ref 82 ). Fig. 4.29...
Abstract
This chapter describes the phenomenological aspects of fatigue and how to assess its effect on the life of components operating in high-temperature environments. It explains how fatigue is measured and expressed and how it is affected by loading conditions (stress cycles, amplitude, and frequency) and factors such as temperature, material defects, component geometry, and processing history. It provides a detailed overview of the damage mechanisms associated with high-cycle and low-cycle fatigue as well as thermal fatigue, creep-fatigue, and fatigue-crack growth. It also demonstrates the use of tools and techniques that have been developed to quantify fatigue-related damage and its effect on the remaining life of components.
Image
Published: 01 October 2011
Fig. 16.25 Schematic of cracking mechanisms with creep-fatigue interaction. (a) Fatigue cracking dominant. (b) Creep cracking dominant. (c) Creep damage influences fatigue crack growth. (d) Creep cracking and fatigue crack occur simultaneously.
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Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 1989
DOI: 10.31399/asm.tb.dmlahtc.9781627083409
EISBN: 978-1-62708-340-9
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 July 2009
DOI: 10.31399/asm.tb.fdmht.t52060173
EISBN: 978-1-62708-343-0
... 8.114 G CPE Creep-plastic exhaustion 8.115 G MDE Modified ductility exhaustion model 8.116 H: Crack growth H CGM Crack-growth model 8.117 H HCG High-temperature crack growth 8.118 H CGA Crack-growth approach 8.119 H CPM Crack-propagation model 8.120...
Abstract
This chapter provides a detailed review of creep-fatigue analysis techniques, including the 10% rule, strain-range partitioning, several variants of the frequency-modified life equation, damage assessment based on tensile hysteresis energy, the OCTF (oxidation, creep, and thermomechanical fatigue) damage model, and numerous methods that make use of creep-rupture, crack-growth, and void-growth data. It also discusses the use of continuum damage mechanics and includes examples demonstrating the accuracy of each method as well as the procedures involved.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 1989
DOI: 10.31399/asm.tb.dmlahtc.t60490001
EISBN: 978-1-62708-340-9
...- and crack-propagation-controlled failures Component Circumstances Initiation-controlled failures HP/IP rotor bores (1950’s) Very brittle (small a c ); highly stressed Rotor dovetails Highly stressed; thin section Rotor grooves Rapid crack growth (large da/dn) Blades Highly...
Abstract
The ability to accurately assess the remaining life of components is essential to the operation of plants and equipment, particularly those in service beyond their design life. This, in turn, requires a knowledge of material failure modes and a proficiency for predicting the near and long term effects of mechanical, chemical, and thermal stressors. This chapter presents a broad overview of the types of damage to which materials are exposed at high temperatures and the approaches used to estimate remaining service life. It explains how operating conditions in power plants and oil refineries can cause material-related problems such as embrittlement, creep, thermal fatigue, hot corrosion, and oxidation. It also discusses the factors and considerations involved in determining design life, defining failure criteria, and implementing remaining-life-assessment procedures.
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