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Series: ASM Failure Analysis Case Histories
Volume: 1
Publisher: ASM International
Published: 01 December 1992
DOI: 10.31399/asm.fach.v01.c9001046
EISBN: 978-1-62708-214-3
... gases to shunt across the preheater/exchanger. Metallographic examination of the plates showed that accelerated internal oxidation had been the cause of failure. Corrosion racks of candidate alloys (types 304, 309, and 316 stainless steels, Inconel 600, Inconel 625, Incoloy 800, Incoloy 825, and Inco...
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Published: 01 January 2002
Fig. 52 Torsion fracture in an aluminum-silicon alloy (alloy 319-T5). Classic brittle torsion fracture on a plane at 45° to the axis of the cylinder. Hardness, 38 HRB; tensile strength, 179 MPa (26 ksi); total elongation, 0.5%. Source: Ref 42 More
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Published: 01 January 2002
Fig. 53 Macroscale brittle torsion fracture in an aluminum-silicon alloy (alloy A356 sand casting). Hardness, 38 HRB; tensile strength, 214 MPa (31 ksi); total elongation, 4%. Source: Ref 42 More
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Published: 15 January 2021
Fig. 52 Torsion fracture in an aluminum-silicon alloy (alloy 319-T5). Classic brittle torsion fracture on a plane at 45° to the axis of the cylinder. Hardness, 38 HRB; tensile strength, 179 MPa (26 ksi); total elongation, 0.5%. Source: Ref 43 More
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Published: 15 January 2021
Fig. 53 Macroscale brittle torsion fracture in an aluminum-silicon alloy (alloy A356 sand casting). Hardness, 38 HRB; tensile strength, 214 MPa (31 ksi); total elongation, 4%. Source: Ref 43 More
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Published: 15 January 2021
Fig. 3 Perforation of alloy 690 incinerator liner near alloy 160 patch, showing that the original 6.35 mm (0.250 in.) wall thickness was reduced to approximately 1.27 mm (0.050 in.) or less in the general area of failure. Courtesy of U.S. Navy More
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Published: 01 January 2002
Fig. 5 Comparison of wear surfaces for low-alloy steel specimens worn in (a) flow-through and (b) recycled slurry tests for 1 h and 1.67 h, respectively. Source: Ref 13 More
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Published: 01 January 2002
Fig. 2 Wear surface by cavitation of copper-base alloy in a lubricated gearbox. Courtesy of CETIM More
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Published: 01 January 2002
Fig. 3 Aluminum alloy 6063-T6 extension-ladder side-rail extrusion that failed by plastic deformation and subsequent buckling. (a) Configuration and dimensions (given in inches). (b) Relation of maximum applied load to the section thickness of the flanges and web of the side-rail extrusion. More
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Published: 01 January 2002
Fig. 7 Micrograph of a section through a copper-lead alloy bearing that failed by deleading. Light area at the upper surface is the copper matrix that remained after the alloy was depleted of lead. As-polished. 100× More
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Published: 01 January 2002
Fig. 7 Low-alloy steel roller bearing from an improperly grounded electric motor that was pitted and etched by electrolytic action of stray electric currents in the presence of moisture. More
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Published: 01 January 2002
Fig. 21 Aluminum alloy lifting sling that fractured because of improper welding of the cross member to the sling body. (a) Configuration and dimensions (given in inches). (b) Fracture surfaces of the sling body (top) and the cross member (bottom). (c) Enlarged view of a fracture surface More
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Published: 01 January 2002
Fig. 3 Cracked HL22-8 aluminum alloy 7075-T6 fasteners. (a) and (b) Typical cracked fastener head. (c) Typical head cracks produced by installing fasteners in misaligned holes during testing More
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Published: 01 January 2002
Fig. 11 Die-cast zinc alloy nuts from a water tap. (a) Nut for the cold-water tap that failed by SCC. (b) Mating nut for the hot-water top that shows only isolated areas of corrosion. (c) Unetched section showing metal in the cold-water tap after corrosion testing. 600× More
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Published: 01 January 2002
Fig. 13 Cadmium-plated alloy steel self-retaining bolts that fractured because of hydrogen damage. (a) Fractured and unused intact bolt. (b) Fractured bolt; brittle fracture surface is indicated by A and B. (c) and (d) Electron fractographs of surfaces A and B, respectively, showing brittle More
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Published: 01 January 2002
Fig. 14 Cadmium-plated AISI 8740 alloy steel fasteners that failed by hydrogen embrittlement. See also Fig. 15 . More
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Published: 01 January 2002
Fig. 20 Alcan aluminum alloy B54S-O rivet that failed by stress corrosion after being heated for 7 days at 100 °C (212 °F). (a) Section through rivet showing shape of fracture surface. 5×. (b) Micrograph showing an intergranular fracture path. 450× More
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Published: 01 January 2002
Fig. 27(a) AISI 4150 alloy steel chuck jaw that broke because of the presence of a brittle white-etching nitride surface layer. The part was hardened and tempered before nitriding. A micrograph of a broken tooth (arrows) of this chuck jaw is shown in Fig. 27(b) . More
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Published: 01 January 2002
Fig. 5 Copper alloy C70600 tube from a hydraulic-oil cooler. The cooler failed from crevice corrosion caused by dirt particles in river water that was used as a coolant. (a) Inner surface of hydraulic-oil cooler tube containing a hole (arrow A) and nodules (one of which is indicated by arrow B More
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Published: 01 January 2002
Fig. 6 Copper alloy C26000 steam-turbine condenser tube that failed by dezincification. (a) Section through condenser tube showing dezincification of inner surface. 3 1 2 ×. (b) Etched specimen from the tube showing corroded porous region at the top and unaffected region below. 100× More