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?
Close Modal
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...
Image
Published: 01 June 2019
Fig. 1 Overall Location of Fuel Nozzles in J52 Series Engines More
Image
Published: 01 June 2019
Fig. 3 Location of Fuel Nozzles in Half Engine Cross Section More
Image
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
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
Published: 01 December 1993
Fig. 2 Representative leading (a) and trailing (b) edges of the nozzles. 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...
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
Published: 01 June 2019
Fig. 1 Exhaust Nozzle With Insulator S/N 014R. More
Image
Published: 01 June 2019
Fig. 2 Convergent Nozzle Liner S/N 014R. More
Image
Published: 01 June 2019
Fig. 3 Convergent Nozzle Insulator S/N 014R, Portions of Throat and Convergent Sections. More
Image
Published: 01 June 2019
Fig. 4 Nozzle Shell and Insulator Configuration. More
Image
Published: 01 June 2019
Fig. 1 Schematic diagram of the burner nozzle configuration. More
Image
Published: 01 June 2019
Fig. 1 Arrangement of nozzle connecting safety valve line to superheater header, showing cracking. More
Image
Published: 01 June 2019
Fig. 2 Section parallel and close to surface at nozzle connection seen in Fig. 1 , showing cracking. Nital etch. More
Image
Published: 01 June 2019
Fig. 3 Sections through cracks at the nozzle: (a) blunted crack; (b) sharp tip of adjacent crack. Nital etch. More
Image
Published: 01 June 2019
Fig. 1 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 June 2019
Fig. 4 Section parallel to shell surface at safety valve nozzle connection. Nital etch. More
Image
Published: 01 June 2019
Fig. 1 Desuperheater nozzle failed after 9 months service in a high pressure steam line. More