Menu
Search
Filters
Close
Menu

98435 ANALYSIS OF HP2 NOZZLE ASSEMBLY FAILURE OF A GAS TURBINE

Picture for 98435 ANALYSIS OF HP2 NOZZLE ASSEMBLY FAILURE
Available for download
Product Number: 51300-98435-SG
ISBN: 98435 1998 CP
Author: P.F. ANTO, S.K. SINGH
$0.00
$20.00
$20.00
The HP2 nozzle assembly of one of the process platform failed by plastic deformation of the vanes after an operating life of 20,000 hours. The vanes were made of alloy 3 1. The failed vanes were subjected to detailed failure analysis by conducting metallography, hardness testing, energy dispersive spectroscopy, x-ray diffraction and electron probe micro analysis. The phenomenon of sulphidation and catastrophic oxidation was not observed in the material. It was found that the material had undergone high temperature oxidation. The material did not show any signs of creep damage and phase growth Yreferential attack of carbides was identified. The alloy exhibited loss of hardness at the aerofoil surface which aided material erosion and degradation of alloy strength properties. Various thermal barrier coatings to prevent high temperature oxidation were studied. Key words : failure analysis, gas turbine, nozzle vane, plastic deformation, alloy 3 1, high temperature oxidation, material corrosion.
The HP2 nozzle assembly of one of the process platform failed by plastic deformation of the vanes after an operating life of 20,000 hours. The vanes were made of alloy 3 1. The failed vanes were subjected to detailed failure analysis by conducting metallography, hardness testing, energy dispersive spectroscopy, x-ray diffraction and electron probe micro analysis. The phenomenon of sulphidation and catastrophic oxidation was not observed in the material. It was found that the material had undergone high temperature oxidation. The material did not show any signs of creep damage and phase growth Yreferential attack of carbides was identified. The alloy exhibited loss of hardness at the aerofoil surface which aided material erosion and degradation of alloy strength properties. Various thermal barrier coatings to prevent high temperature oxidation were studied. Key words : failure analysis, gas turbine, nozzle vane, plastic deformation, alloy 3 1, high temperature oxidation, material corrosion.
PRICE BREAKS - The more you buy, the more you save
Quantity
1+
5+
Price
$20.00
$20.00
Product tags
Also Purchased
Picture for 98430 COMPARATIVE PERFORMANCE OF SIX CAST TUBE
Available for download

98430 COMPARATIVE PERFORMANCE OF SIX CAST TUBE ALLOYS IN AN ETHYLENE PYROLYSIS TEST HEATER

Product Number: 51300-98430-SG
ISBN: 98430 1998 CP
Author: David E. Hendrix
$20.00
Picture for 98443 REMAINING LIFE ASSESSMENT OF STEAM/
Available for download

98443 REMAINING LIFE ASSESSMENT OF STEAM/METHANE AND HYDROGEN REFORMER FURNACE TUBES

Product Number: 51300-98443-SG
ISBN: 98443 1998 CP
Author: Gordon P. Kallenberg
$20.00
Picture for 98429 MATERIALS EXPERIENCE IN A METHANE
Available for download

98429 MATERIALS EXPERIENCE IN A METHANE REFORMING PLANT

Product Number: 51300-98429-SG
ISBN: 98429 1998 CP
Author: Hendrik J. de Bruyn, Michael L. Holland
$20.00
Categories
Industry
Recently viewed
Popular tags
View all

Association for Materials Protection and Performance

© AMPP All Rights Reserved.
Membership Terms of Content Use
Contact Customer Support