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in Metallurgical Investigation of a Turbine Blade and a Vane Failure from Two Marine Engines
> ASM Failure Analysis Case Histories: Offshore, Shipbuilding, and Marine Equipment
Published: 01 June 2019
Fig. 16 Coating features of the vane along the airfoil section. (a) Convex side showing intact coating and shrinkage porosity; (b) Coating-matrix interface along convex side; (c) Vane coating and coating-matrix interface along concave side.
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in Metallurgical Investigation of a Turbine Blade and a Vane Failure from Two Marine Engines
> ASM Failure Analysis Case Histories: Offshore, Shipbuilding, and Marine Equipment
Published: 01 June 2019
Fig. 17 Coating degeneration and corrosion attack in MAR-M302 vane along the concave airfoil side. (a) Fine cracking; (b) Subsurface shrinkage porosity; (c) Corrosion product penetration in the subsurface porosity.
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in Metallurgical Investigation of a Turbine Blade and a Vane Failure from Two Marine Engines
> ASM Failure Analysis Case Histories: Offshore, Shipbuilding, and Marine Equipment
Published: 01 June 2019
Fig. 18 EDX analysis of the coating and corroded area of MAR-M302 vane. (a) Al and S peaks observed in the coating; (b) Corroded fracture region showing Na, S, Al and Si peaks.
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Image
in Premature Failure of Turbine Blades by Corrosion
> ASM Failure Analysis Case Histories: Offshore, Shipbuilding, and Marine Equipment
Published: 01 June 2019
Fig. 1 Uncoated and aluminide-coated IN-713 turbine blades that failed by hot corrosion in a marine environment. (a) An uncoated blade showing splitting along the leading edge and swelling on the surface of the airfoil. 2.7x. (b) Section taken through the leading edge of an uncoated blade
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in Wear and Failure of Babbit Bushes in Steam Turbine Sliding Bearings
> ASM Failure Analysis Case Histories: Mechanical and Machine Components
Published: 01 June 2019
Fig. 6 Plasma-spray-coated babbit microstructure. (a) Optical micrograph. (b) Scanning electron micrograph of α phase
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in Analysis of Hot Rolled Steel Transit Damage
> ASM Failure Analysis Case Histories: Improper Maintenance, Repair, and Operating Conditions
Published: 01 June 2019
Fig. 2 (a) A magnetite coating on hot rolled sheet, with fresh rust breaking through; (b) Hot rolled surface, about 60% covered with fresh rust; (c) Hot rolled steel, with all the original magnetite lost. Rust is beginning to darken where arrowed, to form hematite.
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in Liquid Metal Embrittlement of Flange Connector Studs in Contact With Cadmium
> Handbook of Case Histories in Failure Analysis
Published: 01 December 1992
Fig. 10 EDS graph of fracture surface coating.
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in Failure of the Bond Between a Cobalt Alloy Prosthetic Casting and a Sintered Porous Coating
> Handbook of Case Histories in Failure Analysis
Published: 01 December 1992
Fig. 1 Porous, coated knee implant, as received. Insufficient bonding occurred at the tip of the patella flange.
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Published: 01 December 2019
Fig. 12 Cage section showing general microstructure and silver coating
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in Stress-Rupture Characterization in Nickel-Based Superalloy Gas Turbine Engine Components
> Handbook of Case Histories in Failure Analysis
Published: 01 December 2019
Fig. 6 Trailing edge yielding and aluminide coating wrinkling associated with stress-rupture cracking on turbine airfoils
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Published: 01 December 2019
Fig. 5 A micrograph of the fracture surface (gold coated) of Fig. 4 revealing multiple crack origins, a smooth morphology, and arrest marks
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Published: 01 December 2019
Fig. 6 Cross-section showing electroless nickel coating delamination and cracking
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in Degradation of Thermal Barrier Coated Superalloy Component During Service
> Handbook of Case Histories in Failure Analysis
Published: 01 December 2019
Fig. 4 XRD patterns of bond coat before and after spallation
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Published: 01 December 2019
Fig. 6 Chromium-nickel coating layer on the marriage bolt surface. 1000×
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in Fatigue Fracture of Titanium Alloy Knee Prostheses
> Handbook of Case Histories in Failure Analysis
Published: 01 December 1993
Fig. 3 Underside of porous-coated implant that failed by fatigue. Two fatigue cracks are present: the failure and a secondary crack parallel to the fracture surface. Porous beads fractured in the region adjacent to each fracture and migrated into the joint cavity.
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in Brittle Failure of a Titanium Nitride-Coated High Speed Steel Hob
> Handbook of Case Histories in Failure Analysis
Published: 01 December 1993
Fig. 1 Overall view of titanium nitride-coated hob. Approximately.1×
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in Hot Corrosion of Stage 1 Nozzles in an Industrial Gas Turbine
> Handbook of Case Histories in Failure Analysis
Published: 01 December 1993
Fig. 3 SEM micrograph showing missing coating in a deteriorated area. 12.4×.
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Series: ASM Handbook
Volume: 11
Publisher: ASM International
Published: 15 January 2021
DOI: 10.31399/asm.hb.v11.a0006792
EISBN: 978-1-62708-295-2
.... A brief discussion on coatings to improve surface-initiated fatigue and wear is included, due to the similarity to RCF and the increasing criticality of this failure mode. The article presents a working knowledge of Hertzian contact theory, describes the life prediction of rolling-element bearings...
Abstract
Rolling-contact fatigue (RCF) is a common failure mode in components subjected to rolling or rolling-sliding contact. This article provides a basic understanding of RCF and a broad overview of materials and manufacturing techniques commonly used in industry to improve component life. A brief discussion on coatings to improve surface-initiated fatigue and wear is included, due to the similarity to RCF and the increasing criticality of this failure mode. The article presents a working knowledge of Hertzian contact theory, describes the life prediction of rolling-element bearings, and provides information on physics and testing of rolling-contact fatigue. Processes commonly used to produce bearings for demanding applications are also covered.
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.process.c9001589
EISBN: 978-1-62708-235-8
... Abstract The paper discusses the analysis of a coating defect on a high phosphorus electroless nickel (Ni-11 wt. % P) deposit plated on an aluminum alloy substrate. Preliminary investigations had indicated that the elongated defects were possibly caused by the entrapment of long fibers...
Abstract
The paper discusses the analysis of a coating defect on a high phosphorus electroless nickel (Ni-11 wt. % P) deposit plated on an aluminum alloy substrate. Preliminary investigations had indicated that the elongated defects were possibly caused by the entrapment of long fibers or particles during the plating. The possible sources of fibers were identified. The SEM/EDS analysis of fibers collected from the air duct filters correlated very well with the defect shape and the EDS profile collected from under the defect site. It appears that the fibers from air duct filters directly above the plating line were blown into the plating tank and getting co-deposited. The paper describes the step-by-step analysis of the defect that led to successful identification of the root cause of the defect.
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