Skip Nav Destination
Close Modal
Search Results for
Nickel alloy
Update search
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
Filter
- Title
- Authors
- Author Affiliations
- Full Text
- Abstract
- Keywords
- DOI
- ISBN
- EISBN
- Issue
- ISSN
- EISSN
- Volume
- References
NARROW
Format
Topics
Book Series
Date
Availability
1-20 of 345 Search Results for
Nickel alloy
Follow your search
Access your saved searches in your account
Would you like to receive an alert when new items match your search?
1
Sort by
Image
Published: 01 January 2002
Fig. 7 Copper-nickel alloy heat-exchanger tubes that failed from denickelification due to attack by water and steam. (a) Etched section through a copper alloy C71000 tube showing dealloying (light areas) around the tube surfaces. Etched with NH 4 OH plus H 2 O. 3.7×. (b) Unetched section
More
Image
Published: 01 January 2002
Fig. 7 Sulfidation and chloridation attack on nickel alloy of charcoal-regeneration kiln. See also Fig. 8 . Region 1 is an area of chromium sulfide islands (dark phase) interspersed in chromium-depleted region (bright phase). Region 2 has angular phase (consisting mostly of nickel sulfide
More
Image
Published: 01 January 2002
Fig. 8 Sulfidation and chloridation attack on nickel alloy of charcoal-regeneration kiln, with greater magnification (at ∼44×). Lower right is region of chromium sulfide islands (dark phase) interspersed in chromium-depleted region (bright phase). Middle region has angular phase (consisting
More
Image
in Failure Analysis of Heat Exchangers
> Analysis and Prevention of Component and Equipment Failures
Published: 30 August 2021
Fig. 7 Copper-nickel alloy heat-exchanger tubes that failed from denickelification due to attack by water and steam. (a) Etched section through a copper alloy C71000 tube showing dealloying (light areas) around the tube surfaces. Etched with NH 4 OH plus H 2 O. Original magnification: 3.7×. (b
More
Image
in Perforation of a Nickel-Base Alloy Kiln
> ASM Failure Analysis Case Histories: Steelmaking and Thermal Processing Equipment
Published: 01 June 2019
Fig. 1 Sulfidation and chloridation attack on nickel alloy of charcoal-regeneration kiln. See also Fig. 2 . Region 1 is an area of chromium sulfide islands (dark phase) interspersed in chromium-depleted region (bright phase). Region 2 has angular phase (consisting mostly of nickel sulfide
More
Image
in Perforation of a Nickel-Base Alloy Kiln
> ASM Failure Analysis Case Histories: Steelmaking and Thermal Processing Equipment
Published: 01 June 2019
Fig. 2 Sulfidation and chloridation attack on nickel alloy of charcoal-regeneration kiln, with greater magnification (at ∼44×). Lower right is region of chromium sulfide islands (dark phase) interspersed in chromium-depleted region (bright phase). Middle region has angular phase (consisting
More
Book Chapter
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.steel.c0091757
EISBN: 978-1-62708-232-7
... the chemical makeup of these phases. Fig. 1 Sulfidation and chloridation attack on nickel alloy of charcoal-regeneration kiln. See also Fig. 2 . Region 1 is an area of chromium sulfide islands (dark phase) interspersed in chromium-depleted region (bright phase). Region 2 has angular phase (consisting...
Abstract
A kiln, 7.6 m (25 ft) long with a 1 m (3 ft) internal diameter and a 6.3 mm (0.25 in.) wall thickness, is used to regenerate spent charcoal returned by water utilities. This charcoal contains up to 0.57% S and 2.04% Cl. The kiln is made of Inconel 601 (N06601) welded using Inconel 617 (N06617) as a filler alloy. Wet charcoal is fed in at one end of the kiln and travels while being tumbled within the inclined rotating vessel. Temperatures range from 480 deg C (900 deg F) (Zone 1) to 900 deg C (1650 deg F) (Zones 2 and 3). Steam is introduced at the discharge end at 95 g/s (750 lb/h), 34 to 69 kPa (5 to 10 psi), and 125 deg C (260 deg F). The kiln developed perforations within eight months of operation. Investigation (visual inspection, metallurgical analysis, energy-dispersive spectroscopy, and 44X micrographs) supported the conclusion that the sulfur and chlorine in the charcoal attacked the Inconel 601, forming various sulfides and chlorides. Recommendations included on-site testing, and installation of test coupons of various alloys before fabricating another kiln. The suggested alloys were RA85H, 800HT, HR-120, Haynes 556, and HR-160.
Book Chapter
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.usage.c0091756
EISBN: 978-1-62708-236-5
... Abstract An alloy IN-690 (N06690) incinerator liner approximately 0.8 mm (0.031 in.) thick failed after only 250 h of service burning solid waste. Investigation supported the conclusion that the root cause of the failure was overfiring during startup and sulfidation of the nickel-base alloy...
Abstract
An alloy IN-690 (N06690) incinerator liner approximately 0.8 mm (0.031 in.) thick failed after only 250 h of service burning solid waste. Investigation supported the conclusion that the root cause of the failure was overfiring during startup and sulfidation of the nickel-base alloy. No recommendations were made.
Image
Published: 01 January 2002
Fig. 43 SEM view of laboratory fatigue fracture of a 70-30 nickel-copper alloy showing mixed intergranular and transgranular morphology. Source: Ref 24
More
Image
Published: 01 January 2002
Fig. 3 SEM image of fracture surface of nickel-base alloy (Inconel 751, annealed and aged) after stress rupture (730 °C, or 1350 °F; 380 MPa, or 55 ksi; 125 h). (a) Low-magnification view, with picture width shown at approximately 0.35 mm (0.0138 in.) from original magnification of 250×. (b
More
Image
in Elevated-Temperature Life Assessment for Turbine Components, Piping, and Tubing
> Failure Analysis and Prevention
Published: 01 January 2002
Fig. 9 Gamma-prime overaging in a nickel-base alloy turbine blade material. (a) SEM micrograph of the blade material, showing the breakdown of the eutectic gamma prime (5) and the spreading of the coarse gamma prime. Smaller particles of fine aging gamma prime (4), which would appear between
More
Image
in Elevated-Temperature Life Assessment for Turbine Components, Piping, and Tubing
> Failure Analysis and Prevention
Published: 01 January 2002
Fig. 11 Hot corrosion attack of René 77 nickel-base alloy turbine blades. (a) Land-based, first-stage turbine blade. Notice deposit buildup, flaking, and splitting of leading edge. (b) Stationary vanes. (c) A land-based, first-stage gas turbine blade that had type 2 hot corrosion attack. (d
More
Image
in X-Ray Diffraction Residual Stress Measurement in Failure Analysis
> Failure Analysis and Prevention
Published: 01 January 2002
Fig. 19 Observation of failed nickel-base alloy (Waspaloy) specimen after rotating bend fatigue. (a) Macro view. (b) Micrograph. Source: Ref 43
More
Image
in Stress-Corrosion Cracking and Galvanic Corrosion of Internal Bolts from a Multistage Water Injection Pump
> Handbook of Case Histories in Failure Analysis
Published: 01 December 2019
Image
Published: 15 January 2021
Fig. 3 Scanning electron microscopy image of fracture surface of nickel-base alloy (Inconel 751, annealed and aged) after stress rupture (730 °C, or 1350 °F; 380 MPa, or 55 ksi; 125 h). (a) Low-magnification view, with picture width shown at approximately 0.35 mm (0.0138 in.) from original
More
Image
Published: 15 January 2021
Fig. 7 Sulfidation and chloridation attack on IN-601 nickel-base alloy of charcoal-regeneration kiln (see also Fig. 8 ). Region 1 is an area of chromium sulfide islands (dark phase) interspersed in a chromium-depleted region (bright phase). Region 2 has an angular phase (consisting mostly
More
Image
Published: 15 January 2021
Fig. 8 Sulfidation and chloridation attack on IN-601 nickel-base alloy of charcoal-regeneration kiln at higher magnification (~44×). Lower right is region of chromium sulfide islands (dark phase) interspersed in chromium-depleted region (bright phase). Middle region has an angular phase
More
Image
in X-Ray Diffraction Residual-Stress Measurement in Failure Analysis
> Failure Analysis and Prevention
Published: 15 January 2021
Fig. 19 Observation of failed nickel-base alloy (Waspaloy) specimen after rotating-bend fatigue. (a) Macro view. (b) Micrograph. Source: Ref 53
More
Image
in Plating Adherence Problems in Electronic Components
> ASM Failure Analysis Case Histories: Processing Errors and Defects
Published: 01 June 2019
Fig. 1 Electroless nickel underplating and gold plating on a copper alloy CDA175 module retaining clip. (a) shows a good plated clip and (b) shows a bad clip with copper oxide (black layer) at the copper/alloy nickel plating interface, where the separation occurred.
More
Book Chapter
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.process.c9001439
EISBN: 978-1-62708-235-8
..., leaving a weak, porous residual structure. The brazing alloy was of type CP 1 as covered by BS 1845. Header and tube materials were basically copper-nickel alloys for which the use of a phosphorus bearing brazing alloy is not recommended owing to the possibility of forming the brittle intermetallic...
Abstract
Persistent leakage was experienced from copper tube heaters which formed part of dairy equipment. Metallurgical examination of the brazed joints showed them to have suffered a preferential corrosion attack. This resulted in the phosphide phase of the brazing alloy being corroded away, leaving a weak, porous residual structure. The brazing alloy was of type CP 1 as covered by BS 1845. Header and tube materials were basically copper-nickel alloys for which the use of a phosphorus bearing brazing alloy is not recommended owing to the possibility of forming the brittle intermetallic compound, nickel phosphide. The use of a brazing alloy containing phosphorus was unsuitable on two counts and a quaternary alloy containing silver, copper, cadmium and zinc, such as those in group AG1 or AG2 of BS 1845 would be more suitable. However, because corrosive problems experienced in these units indicated severe service conditions, a proprietary alloy similar to AG1, but containing 3% nickel, was recommended.
1