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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...
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Published: 01 December 1993
Fig. 2 Representative leading (a) and trailing (b) edges of the nozzles. More
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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
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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
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Published: 01 June 2019
Fig. 1 Overall Location of Fuel Nozzles in J52 Series Engines More
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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...
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...
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...
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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
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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
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Published: 01 June 2019
Fig. 1 Schematic diagram of the burner nozzle configuration. More
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Published: 30 August 2021
Fig. 10 Crack shown in a typical radiographic testing film taken around a nozzle using cobalt-60 source More
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Published: 30 August 2021
Fig. 11 Nozzle joint with marking to extract a full-thickness specimen More
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Published: 30 August 2021
Fig. 12 (a) Cutout with nozzle. (b) Extracted metal part More
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Published: 30 August 2021
Fig. 40 A 50 mm (2 in.) nozzle on primary cyclone More
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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
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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
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Published: 01 December 1993
Fig. 1 As-received nozzle segments. (a) Leading edges. (b) Trailing edges. More
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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