Comparison of low cycle (notch) fatigue behaviour at temperature In single crystal turbine blade materials
Reed, P.A.S. and Miller, M.D. (2008) Comparison of low cycle (notch) fatigue behaviour at temperature In single crystal turbine blade materials. In, Reed, Roger, Green, Kenneth, Caron, Pierre, Gabb, Timothy P. and Fahrmann, Michael G. (eds.) Superalloys 2008: Proceedings of the Eleventh International Symposium on Superalloys. Superalloys 2008: 11th International Symposium on Superalloys Warrendale, USA, Minerals, Metals and Materials Society, 527-533.
Full text not available from this repository.
The scatter in notch fatigue lifetimes of CMSX4 at 650˚C and 725˚C in air and vacuum and with Rene N5 in air at 650˚C is compared under the same (plastic) notch strain range levels. Rene N5 shows shorter lifetimes under equivalent conditions and always exhibits multiple initiation sites. The role of interdendritic porosity in initiating fatigue in both alloys is identified, and the number of initiation sites is found to directly affect fatigue life. In air in CMSX4 and Rene N5, subsurface pores initiate fatigue, and this is believed to be due to the repeated in-filling of surface pores by oxidation product, reducing their associated stress concentration and effectively deactivating them as a fatigue initiation site. Tests in vacuum support this hypothesis as cracks do initiate at surface porosity under vacuum conditions. An
attempt to evaluate initiating porosity distributions, has indicated a correlation between total area of initiating porosity and fatigue lifetime, which to some extent may allow for crack coalescence behaviour. A deterministic fracture mechanics based model has been proposed to allow for the effect of pore shape, size and position in determining subsequent fatigue life (and hence scatter). The predictions of the model have been assessed using full factorial design of experiments, assessing the effects of variability in pore shape, size and distance below the notch root, as well as the materials parameters (crack growth laws and Kmax) used in the lifing calculation. The model successfully explains some, but not all of the observed scatter in lifetimes.
|Item Type:||Book Section|
|Keywords:||notch fatigue, cmsx4, porosity, fatigue initiation, lifing model, scatter|
|Subjects:||T Technology > TJ Mechanical engineering and machinery
T Technology > TN Mining engineering. Metallurgy
T Technology > TL Motor vehicles. Aeronautics. Astronautics
|Divisions:||University Structure - Pre August 2011 > School of Engineering Sciences > Engineering Materials & Surface Engineering
|Date Deposited:||29 Jan 2009|
|Last Modified:||02 Mar 2012 11:33|
|Publisher:||Minerals, Metals and Materials Society|
|RDF:||RDF+N-Triples, RDF+N3, RDF+XML, Browse.|
Actions (login required)