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contributor authorTeuber, Hannes
contributor authorBarnikel, Jochen
contributor authorDankert, Michael
contributor authorDavid, Walter
contributor authorGhicov, Andrei
contributor authorVoss, Simon
date accessioned2019-03-17T09:27:28Z
date available2019-03-17T09:27:28Z
date copyright9/18/2018 12:00:00 AM
date issued2019
identifier issn0742-4795
identifier othergtp_141_01_011021.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4255498
description abstractInfluenced by the growing share of Renewable Energies, higher flexibility and increased efficiency of fossil power plants as well as improved cost efficiency in production of turbine components are evident market trends. Daily cycling in turbine operations leads to advanced requirements for robust design especially of rotating parts. Low pressure (LP) steam turbine end-stage blades with larger exhaust areas are one lever to increase the efficiency of the turbine by reduction of exhaust losses and also to realize cost-efficient single flow exhaust applications. Consequently, blade steels with improved mechanical properties are required. The results of the development of a new high-strength precipitation-hardening (PH) steel for LP end-stage blade application with significantly enhanced material properties are reported. The paper covers the testing strategy applied and information on crucial material parameters like improved low cycle and high cycle fatigue (HCF) behavior while keeping good stress corrosion cracking (SCC) resistance and corrosion fatigue (CF) properties. Furthermore, first manufacturing experiences and validation results from a full-scale component test rig are presented.
publisherThe American Society of Mechanical Engineers (ASME)
titleDevelopment of a New High-Strength Steel for Low Pressure Steam Turbine End-Stage Blades
typeJournal Paper
journal volume141
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4040849
journal fristpage11021
journal lastpage011021-7
treeJournal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 001
contenttypeFulltext


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