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creep life
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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. 6.20. Evolution of creep-cavitation with creep-life fraction expended for Cr-Mo-V rotor steels ( Ref 46 ).
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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. 9.48. Correlation of degree of creep voiding with percent of creep life consumed. Top left, 40%; top right, 60%; bottom left and right, 80% ( Ref 78 ; courtesy of J. Wortmann, MTU Motoren-und Turbinen-Union, Munich).
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Image
Published: 01 July 1997
Fig. 11 Correlation between damaged classification and expended creep-life fraction for 1 1 4 Cr- 1 2 Mo steels. Source: Ref 22
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Image
in Life Prediction for Boiler Components
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Image
in Life Prediction for Boiler Components
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Fig. 5.23. Correlation between damage classification and expended creep-life fraction for 1¼Cr-½Mo steels ( Ref 41 ).
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Image
Published: 01 March 2002
Fig. 12.15 Rupture life and minimum creep rate (MCR) of Nimonic 80A nickel-base superalloy at 750 °C (1380 °F)/234 MPa (34 ksi) vs. grain diameter of specimen tested
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Image
Published: 01 March 2002
Fig. 12.71 Comparison of creep-rupture life of IN-792 type SCDS alloy with primary orientation deviations (α) of 10° and 25° using Larson-Miller parameter (P LM ). Note: P LM = T (C + log t ) where C = Larson-Miller constant, T = absolute temperature, t = time in h. For this plot, C
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in Partitioning of Hysteresis Loops and Life Relations
> Fatigue and Durability of Metals at High Temperatures
Published: 01 July 2009
Fig. 5.7 Predictability of creep-fatigue life using two techniques for experimentally partitioning creep and plastic strains for the method of strain-range partitioning. Source: Ref 5.15
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Image
Published: 01 August 2005
Fig. 3.43 Creep-fatigue interaction effects on the isothermal cyclic life of AISI type 304 stainless steel tested in air at 650 °C (1200 °F), normal straining rate of 4 × 10 3 /s. Source: Ref 3.38
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Published: 01 December 1989
Fig. 1.8. Uncertainty in creep-rupture life assessment due to scatter in the properties of a Cr-Mo-V steel.
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Image
Published: 01 December 1989
Fig. 4.17. Effects of hold time and prior creep damage (0.2 and 0.6 life fractions) on cyclic endurance of 1Cr-½Mo steel ( Ref 39 ).
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Image
in Life Prediction for Boiler Components
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Fig. 5.21. Evolution of creep-cavitation damage with expended life fraction for ferritic steels ( Ref 12 ).
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Image
in Life Prediction for Boiler Components
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Fig. 5.22. Evolution of creep-cavitation damage with expended life fraction for 1Cr-½Mo steels tested at 550 °C (1020 °F) ( Ref 42 ).
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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. 7.21. Loss in creep-rupture life of ½Mo steel at 540 °C (1000 °F) in 5-MPa (725-psi) hydrogen ( Ref 56 ).
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2012
DOI: 10.31399/asm.tb.ffub.t53610415
EISBN: 978-1-62708-303-4
... Abstract This chapter compares and contrasts the high-temperature behaviors of metals and composites. It describes the use of creep curves and stress-rupture testing along with the underlying mechanisms in creep deformation and elevated-temperature fracture. It also discusses creep-life...
Abstract
This chapter compares and contrasts the high-temperature behaviors of metals and composites. It describes the use of creep curves and stress-rupture testing along with the underlying mechanisms in creep deformation and elevated-temperature fracture. It also discusses creep-life prediction and related design methods and some of the factors involved in high-temperature fatigue, including creep-fatigue interaction and thermomechanical damage.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 June 2008
DOI: 10.31399/asm.tb.emea.t52240265
EISBN: 978-1-62708-251-8
... fracture, namely, rupture, transgranular fracture, and intergranular fracture. The next section focuses on some of the metallurgical instabilities caused by overaging, intermetallic phase precipitation, and carbide reactions. Subsequent sections address creep life prediction and creep-fatigue interaction...
Abstract
Creep occurs in any metal or alloy at a temperature where atoms become sufficiently mobile to allow the time-dependent rearrangement of structure. This chapter begins with a section on creep curves, covering the three distinct stages: primary, secondary, and tertiary. It then provides information on the stress-rupture test used to measure the time it takes for a metal to fail at a given stress at elevated temperature. The major classes of creep mechanism, namely Nabarro-Herring creep and Coble creep, are then covered. The chapter also provides information on three primary modes of elevated fracture, namely, rupture, transgranular fracture, and intergranular fracture. The next section focuses on some of the metallurgical instabilities caused by overaging, intermetallic phase precipitation, and carbide reactions. Subsequent sections address creep life prediction and creep-fatigue interaction and the approaches to design against creep.
Image
in Life-Assessment Techniques for Combustion Turbines
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Fig. 9.40. Gamma-prime overaging and associated loss of creep strength in Udimet 710 tested at 845 °C and 350 MPa (1555 °F and 50 ksi) ( Ref 70 ; courtesy of P. Lowden, Liburdi Engineering, Ltd., Burlington, Canada). Top: New creep life, 140 h. Bottom: Service, 45,000 h; creep life, 10 h.
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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. 6.24. Resistivity technique for estimating life fraction, t/t r , expended in creep ( Ref 46 ). (a) Resistivity ratio as a function of exposure condition. (b) Decrease in resistivity ratio with expended creep life.
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Image
Published: 01 November 2010
Fig. 5.5 Influence of molybdenum in the 982 °C/234 MPa (1800 °F/34,000 psi) (a) creep life and (b) creep rate of an experimental single-crystal superalloy. Source: Ref 23
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2018
DOI: 10.31399/asm.tb.fibtca.t52430409
EISBN: 978-1-62708-253-2
... pathways, and relevant test and measurement procedures. It describes life assessment methods based on hardness, wall thickness, scale formation, microstructure, and creep. It also includes a case study on the determination of the residual life of a secondary superheater tube. boiler tubes remaining...
Abstract
The power generating industry has become proficient at predicting how long a component will last under a given set of operating conditions. This chapter explains how such predictions are made in the case of boiler tubes. It identifies critical damage mechanisms, progressive failure pathways, and relevant test and measurement procedures. It describes life assessment methods based on hardness, wall thickness, scale formation, microstructure, and creep. It also includes a case study on the determination of the residual life of a secondary superheater tube.
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