Skip Nav Destination
Close Modal
Search Results for
nozzles
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 171 Search Results for
nozzles
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
Series: ASM Failure Analysis Case Histories
Volume: 2
Publisher: ASM International
Published: 01 December 1993
DOI: 10.31399/asm.fach.v02.c9001281
EISBN: 978-1-62708-215-0
... Abstract The first-stage nozzles of a high-pressure turbine section of an industrial gas turbine exhibited leading and trailing-edge deterioration. The nozzles were made of X-40, a cobalt-base alloy, and were aluminide coated. Failure analysis determined that the deterioration was the result...
Abstract
The first-stage nozzles of a high-pressure turbine section of an industrial gas turbine exhibited leading and trailing-edge deterioration. The nozzles were made of X-40, a cobalt-base alloy, and were aluminide coated. Failure analysis determined that the deterioration was the result of hot corrosion caused by a combination of contaminants, cooling-hole blockage, and coating loss.
Image
in Hot Corrosion of Stage 1 Nozzles in an Industrial Gas Turbine
> Handbook of Case Histories in Failure Analysis
Published: 01 December 1993
Fig. 2 Representative leading (a) and trailing (b) edges of the nozzles.
More
Image
in Fatigue Failure at Fillet-Welded Nozzle Joints in a Type 316L Stainless Steel Tank
> Handbook of Case Histories in Failure Analysis
Published: 01 December 1993
Fig. 1 Diagram of the cylindrical tank. Double-wall nozzles 1 and 2 were not supported at their ends inside the vessel. The other two nozzle, which were single walled, were supported as shown.
More
Image
in Fatigue Failure at Fillet-Welded Nozzle Joints in a Type 316L Stainless Steel Tank
> Handbook of Case Histories in Failure Analysis
Published: 01 December 1993
Fig. 3 Fillet weld joint between the shell and double-wall nozzles. The hatched portion in the weld was removed by lathe machining.
More
Image
in Failure Analysis of Gas Turbine Engine Fuel Nozzle Heat Shields
> ASM Failure Analysis Case Histories: Improper Maintenance, Repair, and Operating Conditions
Published: 01 June 2019
Fig. 1 Overall Location of Fuel Nozzles in J52 Series Engines
More
Image
in Failure Analysis of Gas Turbine Engine Fuel Nozzle Heat Shields
> ASM Failure Analysis Case Histories: Improper Maintenance, Repair, and Operating Conditions
Published: 01 June 2019
Fig. 3 Location of Fuel Nozzles in Half Engine Cross Section
More
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.aero.c9001491
EISBN: 978-1-62708-217-4
... Abstract Two silica phenolic nozzle liners cracked during proof testing. The test consisted of pressuring the nozzles to 14.1 MPa (2050 psia) for 5 to 20 s. It was concluded that the failure was due to longitudinal cracking in the convergent exhaust-nozzle insulators, stemming from the use...
Abstract
Two silica phenolic nozzle liners cracked during proof testing. The test consisted of pressuring the nozzles to 14.1 MPa (2050 psia) for 5 to 20 s. It was concluded that the failure was due to longitudinal cracking in the convergent exhaust-nozzle insulators, stemming from the use of silica phenolic tape produced from flawed materials that went undetected by the quality control tests, which at the time, assessed tape strength properties in the warp rather than the bias direction. Once the nozzle manufacturer and its suppliers identified the problem, they changed their quality control procedures and resumed production of nozzle liners with more tightly controlled fiber/fabric materials.
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.power.c0091655
EISBN: 978-1-62708-229-7
... Abstract Cracking occurred in an ASME SB166 Inconel 600 safe-end forging on a nuclear reactor coolant water recirculation nozzle while it was in service. The safe-end was welded to a stainless-steel-clad carbon steel nozzle and a type 316 stainless steel transition metal pipe segment...
Abstract
Cracking occurred in an ASME SB166 Inconel 600 safe-end forging on a nuclear reactor coolant water recirculation nozzle while it was in service. The safe-end was welded to a stainless-steel-clad carbon steel nozzle and a type 316 stainless steel transition metal pipe segment. An Inconel 600 thermal sleeve was welded to the safe-end, and a repair weld had obviously been made on the outside surface of the safe-end to correct a machining error. Initial visual examination of the safe-end disclosed that the cracking extended over approximately 85 deg of the circular circumference of the piece. Investigation (visual inspection, on-site radiographic inspection, limited ultrasonic inspection, chemical analysis, 53x metallographic cross sections and SEM images etched in 8:1 phosphoric acid) supported the conclusion that the cracking mechanism was intergranular SCC. No recommendations were made.
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.usage.c9001508
EISBN: 978-1-62708-236-5
... turbine (turbojet) engines, involves the rework and/or replacement of many components including the fuel nozzle heat shields. These heat shields, which are fabricated by press forming from annealed type 321 corrosion resistant steel (CRES) sheet, are utilized to keep hot combustion gases from affecting...
Abstract
New type 321 corrosion-resistant steel heat shields were cracking during welding operations. A failure analysis was performed. The cause was found to be chloride induced stress-corrosion cracking. Packaging was suspected and confirmed to be the cause of the chloride contamination. A contributing factor was the length of time spent in the packaging, 21 years.
Image
Published: 01 January 2002
Fig. 23 Cross section through recirculation inlet nozzle of reactor vessel. Shown are the nozzle, the safe-end that failed, and the thermal sleeve that created susceptibility to crevice corrosion. Dimensions given in inches
More
Image
Published: 01 January 2002
Fig. 34 Cross section through recirculation inlet nozzle of reactor vessel. Shown are the nozzle, the safe-end that failed, and the thermal sleeve that created susceptibility to crevice corrosion. Dimensions given in inches
More
Image
in A Microstructural Examination of Hot Corrosion of a Co-Cr-Fe Alloy Cast Burner Nozzle from a Coal Gasification Plant
> ASM Failure Analysis Case Histories: Failure Modes and Mechanisms
Published: 01 June 2019
Fig. 1 Schematic diagram of the burner nozzle configuration.
More
Image
in Failures of Pressure Vessels and Process Piping
> Analysis and Prevention of Component and Equipment Failures
Published: 30 August 2021
Fig. 10 Crack shown in a typical radiographic testing film taken around a nozzle using cobalt-60 source
More
Image
in Failures of Pressure Vessels and Process Piping
> Analysis and Prevention of Component and Equipment Failures
Published: 30 August 2021
Fig. 11 Nozzle joint with marking to extract a full-thickness specimen
More
Image
in Failures of Pressure Vessels and Process Piping
> Analysis and Prevention of Component and Equipment Failures
Published: 30 August 2021
Fig. 12 (a) Cutout with nozzle. (b) Extracted metal part
More
Image
in Failures of Pressure Vessels and Process Piping
> Analysis and Prevention of Component and Equipment Failures
Published: 30 August 2021
Fig. 40 A 50 mm (2 in.) nozzle on primary cyclone
More
Image
in Failures of Pressure Vessels and Process Piping
> Analysis and Prevention of Component and Equipment Failures
Published: 30 August 2021
Fig. 77 Cross section through recirculation inlet nozzle of reactor vessel. Shown are the nozzle, the safe-end that failed, and the thermal sleeve that created susceptibility to crevice corrosion (dimensions given in inches)
More
Image
in Failures of Pressure Vessels and Process Piping
> Analysis and Prevention of Component and Equipment Failures
Published: 30 August 2021
Fig. 102 (a) The shell plate runs vertically on the left side. The manway nozzle base metal is on the bottom. The nozzle repad was cut off, but a remnant remained (identified as “pad”). (b) Inside surface of cracked manway-to-shell weld. Note the transverse cracks in the weld and some
More
Image
in Hot Corrosion of Stage 1 Nozzles in an Industrial Gas Turbine
> Handbook of Case Histories in Failure Analysis
Published: 01 December 1993
Fig. 1 As-received nozzle segments. (a) Leading edges. (b) Trailing edges.
More
Image
in Hot Corrosion of Stage 1 Nozzles in an Industrial Gas Turbine
> Handbook of Case Histories in Failure Analysis
Published: 01 December 1993
Fig. 5 Cross section through the deteriorated leading edge of a nozzle, showing cooling-hole blockage. (a) 10.37×. (b) 61×.
More
1