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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 June 1985
DOI: 10.31399/asm.tb.sagf.t63420219
EISBN: 978-1-62708-452-9
... Abstract This chapter provides a detailed discussion on five occasions that require written accounts. They are field report, transmittal report with failed unit, laboratory notes of the analyst, failure analysis report, and letter of transmittal of the report to the customer. failure...
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Published: 01 April 2013
Fig. 4 Example layout report showing all dimensions measured on a single casting, with visual indication of deviations from print mean. Note out-of-tolerance condition indicated by asterisks. Source: Ref 2
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Published: 01 April 2013
Fig. 6 Statistical summary report showing the mean of measured observations; the blueprint specification for the mean; the difference between specified and measured means; the tolerance; the standard deviation of the measured dimensions; and the capability of the process. These calculations
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in Failure Analysis Laboratory Management Principles and Practices
> Microelectronics Failure Analysis: Desk Reference
Published: 01 November 2019
Figure 7 Example of FA Report Quality Customer Feedback
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Published: 01 November 2023
Fig. 7 Failure analysis report, classification, and failure mode prediction assisted by AI ( Ref 5 ).
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Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 2018
DOI: 10.31399/asm.tb.msisep.t59220667
EISBN: 978-1-62708-259-4
... Abstract This chapter provides guidelines for conducting metallographic evaluations and offers suggestions on how to effectively report the results. It explains how the approach depends on the objective of the evaluation, which is usually to measure a structural feature, test a hypothesis...
Abstract
This chapter provides guidelines for conducting metallographic evaluations and offers suggestions on how to effectively report the results. It explains how the approach depends on the objective of the evaluation, which is usually to measure a structural feature, test a hypothesis, or investigate structure-related effects. The chapter addresses each case, tailoring its guidelines and suggestions accordingly.
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in Total Strain-Based Strain-Range Partitioning—Isothermal and Thermomechanical Fatigue
> Fatigue and Durability of Metals at High Temperatures
Published: 01 July 2009
Fig. 6.33 Inelastic strain-rate partitioning life relationships reported in Ref 7.6 for zero mean stress conditions: René 95, 650 °C (1200 °F). Data from Ref 6.22 and 6.23 (a) PP. (b) PC. (c) CC. (d) CP. Source: Ref 6.6
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in Total Strain-Based Strain-Range Partitioning—Isothermal and Thermomechanical Fatigue
> Fatigue and Durability of Metals at High Temperatures
Published: 01 July 2009
Fig. 6.36 Predictability capabilities reported in Ref 6.6 of strain-rate partitioning. Data from Ref 6.22 and 6.23 (a) Total strain-range approach. (b) Inelastic strain-range approach. Source: Ref 6.6
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Published: 01 November 2019
Figure 30 Rowlette reports red shift of PMOS recombination emissions from a 10 micron length transistor. Data given at LEOS, 2003 [8] .
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Published: 01 January 2000
Fig. 23 Alloys with reported corrosion rates of <0.5 mm/year (<20 mils/year) in HCl Zone Metal 1 ACI CN-7M (a) (b) (c) Monel (b) (c) (d) Copper (b) (c) (d) Nickel 200 (b) (c) (d) Silicon bronze (b) (c) (d) Silicon cast iron (b) (e) Tungsten Titanium, grade
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in Life Assessment of Steam-Turbine Components
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Fig. 6.33. Uncertainty in indication size as reported by NDE ( Ref 21 ).
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Image
Published: 01 December 2003
Fig. 3 Specific wear rate for a number of polymers, as reported in the literature. The experimental conditions as reported in the literature are given in the table. pv , pressure × velocity Specimen Material Counterface roughness ( R a ), μm Sliding speed ( v ), m/s 1/ S ε
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Published: 01 October 2012
Fig. 5.9 Comparison of typical tensile strengths reported for various titanium alloys. Source: Ref 5.7
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Published: 01 October 2012
Fig. 5.10 Comparison of typical 150 h, 0.1% creep strengths reported for various titanium alloys. Source: Ref 5.7
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in Mechanical Properties and Testing of Titanium Alloys[1]
> Titanium: Physical Metallurgy, Processing, and Applications
Published: 01 January 2015
Fig. 6.22 Relationship between yield strength and reported plane-strain fracture toughness for titanium alloys
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2005
DOI: 10.31399/asm.tb.faesmch.t51270191
EISBN: 978-1-62708-301-0
... Abstract This report describes the failure of a gas turbine in a combined-cycle power plant and the examination and tests that were conducted to determine the cause. Based on microstructural analysis, hardness measurements, and tensile tests, the failure was attributed to inadequate clearances...
Abstract
This report describes the failure of a gas turbine in a combined-cycle power plant and the examination and tests that were conducted to determine the cause. Based on microstructural analysis, hardness measurements, and tensile tests, the failure was attributed to inadequate clearances in the seal land region between two stages in the compressor section of the rotor. The report also recommends changes to remediate the problem.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2005
DOI: 10.31399/asm.tb.faesmch.t51270019
EISBN: 978-1-62708-301-0
... and collect test specimens for subsequent examination and chemical analysis. It also discusses the role of mechanical property testing, the use of nondestructive evaluation, and the final step of generating a report. failure analysis nondestructive evaluation FAILURE ANALYSIS...
Abstract
This chapter discusses the basic steps of a failure investigation. It explains that the first step is to gather and document information about the failed component and its operating history. It advises investigators to visit the failure site as soon as possible to record damages and collect test specimens for subsequent examination and chemical analysis. It also discusses the role of mechanical property testing, the use of nondestructive evaluation, and the final step of generating a report.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2005
DOI: 10.31399/asm.tb.faesmch.t51270177
EISBN: 978-1-62708-301-0
... at the corner of the inner rim near an inclusion. The report recommends the use of a cleaner material and more carefully controlling case hardening process. aircraft engine energy-dispersive X-ray spectrophotometry fatigue crack initiation fractography gears visual examination Summary...
Abstract
A driven gear in the gear box of an aircraft engine fractured after a 40 h test run. The driving gear and gear shaft were also damaged. Based on the results of fractography, chemical analysis, metallography, and hardness testing, the fracture was caused by a fatigue crack initiating at the corner of the inner rim near an inclusion. The report recommends the use of a cleaner material and more carefully controlling case hardening process.
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