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Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.aero.c9001605
EISBN: 978-1-62708-217-4
... at the tips of the cracks were evaluated using electron micrograph stereo image pairs to characterize local fracture toughness. To complete the failure analysis, nondestructive evaluation, metallographic examination, and chemical investigations were carried out. No secondary cracks could be found. Most...
Abstract
After a quick-release fitting of an ejection seat broke, an investigation was performed to determine the manner and cause of crack propagation. Most fractography-based investigations aim to characterize only qualitative characteristics, such as the fracture orientation and origin position, topology, and details of interactions with microstructural features. The aim of this investigation was to use quantitative fractography as a tool to extract information, including striation spacing and size of the stretched zone, in order to make a direct correlation with fracture mechanic concepts. As the crack propagated, striations were created on the fracture surface as a result of service-induced load changes. The size of the striations were measured to estimate crack propagation rate. Remaining lifetime estimates were also made. The dimensions of plastically stretched zones found at the tips of the cracks were evaluated using electron micrograph stereo image pairs to characterize local fracture toughness. To complete the failure analysis, nondestructive evaluation, metallographic examination, and chemical investigations were carried out. No secondary cracks could be found. Most of the broken parts showed that the microstructure, the hardness, and the chemical composition of the Al-alloy were within the specification, but some of the cracked parts were manufactured using a different material than that specified.
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in Mechanisms and Appearances of Ductile and Brittle Fracture in Metals
> Failure Analysis and Prevention
Published: 01 January 2002
Fig. 47 Effect of section thickness on fracture toughness. Source: Ref 65
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Published: 01 January 2002
Fig. 22 Effect of temperature on toughness and ductility of face-centered cubic (fcc), body-centered cubic (bcc), and hexagonal close-packed (hcp) metals
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in Elevated-Temperature Life Assessment for Turbine Components, Piping, and Tubing
> Failure Analysis and Prevention
Published: 01 January 2002
Fig. 7 Plot showing the effect of temper embrittlement on the fracture toughness of a 1CrMoV steel. Source: Ref 8
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in Elevated-Temperature Life Assessment for Turbine Components, Piping, and Tubing
> Failure Analysis and Prevention
Published: 01 January 2002
Fig. 18 Effect of aging in terms of the Larson-Miller parameter on toughness of U-710 tested at 900 °C (1650 °F)
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Published: 01 January 2002
Fig. 23 Effect of thickness on state of stress and fracture toughness at the crack tip. Source: Ref 5
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Published: 01 January 2002
Fig. 28 Correlation between crack-tip opening displacement (CTOD) and toughness. (a) Stretched-zone depth versus CTOD. (b) Stretched-zone width versus CTOD. (c) Stretched-zone width versus depth. Source: Ref 18
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Published: 01 January 2002
Fig. 13 Schematic of variation in fracture toughness and macro-scale features of fracture surfaces for an inherently ductile material. As section thickness ( B ) or preexisting crack length ( a ) increases, plane strain conditions develop first along the centerline and result in a flat
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Published: 01 January 2002
Fig. 55 Correlation of shear lip width with fracture toughness. The depth of the shear lip ( D ) is related to the plane-stress plastic zone size and then to the fracture toughness. See text for discussion Source: Ref 25
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Published: 01 January 2002
Fig. 18 The 260 to 315 °C (500 to 600 °F) impairment in torsion toughness in very hard steels. Note: Reduction in toughness is not detected by hardness measurements. Source: Ref 4
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in Failure Analysis and Life Assessment of Structural Components and Equipment
> Failure Analysis and Prevention
Published: 01 January 2002
Fig. 3 A general plot of the ratios of the toughness and stress showing the relationship between linear elastic fracture mechanics and strength of materials as it relates to fracture and structural integrity ( Ref 18 )
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Published: 01 January 2002
Fig. 9 Crack-tip opening displacement (CTOD) toughness, HSLA 50. δ, CTOD; δ c , CTOD fracture toughness, no significant stable crack extension, unstable fracture; δ e , elastic component of CTOD; δ m , CTOD fracture toughness, significant stable crack extension, plastic collapse; δ p , plastic
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Published: 01 December 1992
Fig. 2 Fracture morphology of fracture toughness specimen (fusion line).
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in Failure Investigation of the Wind Turbine Blade Root Bolt
> Handbook of Case Histories in Failure Analysis
Published: 01 December 2019
Fig. 6 The V-notched impact toughness test specimens
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in Metallurgical Investigation of a Cracked Splice Plate Used in a Power Transmission Line Tower
> Handbook of Case Histories in Failure Analysis
Published: 01 December 2019
Fig. 11 Charpy impact toughness versus temperature plot of the samples taken from heel and edge regions of the plate
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Published: 01 December 2019
Fig. 1 Comparison of impact toughness at typical working hardness (source: Crucible Service Centers)
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Published: 15 January 2021
Fig. 14 Schematic of variation in fracture toughness and macroscale features of fracture surfaces for an inherently ductile material. As section thickness ( B ) or preexisting crack length ( a ) increases, plane-strain conditions develop first along the centerline and result in a flat fracture
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Published: 15 January 2021
Fig. 65 Correlation of shear lip width with fracture toughness. The depth of the shear lip ( D ) is related to the plane-stress plastic zone size and then to the fracture toughness. See text for discussion. Source: Ref 2
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Published: 15 January 2021
Fig. 66 Correlation between stretch-zone width (SZW, or δ) and fracture toughness normalized by the elastic modulus, E . Source: Ref 2
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