Fatigue crack growth mechanisms in superalloys: an overview


Reed, P.A.S. (2009) Fatigue crack growth mechanisms in superalloys: an overview. Materials Science and Technology, 25, (2), 258-270. (doi:10.1179/174328408X361463).

Download

[img] PDF - Publishers print
Restricted to Registered users only

Download (1727Kb) | Request a copy
Original Publication URL: http://dx.doi.org/10.1179/174328408X361463

Description/Abstract

Fatigue studies on disc and blade nickel based superalloys by the author and co-workers are reviewed. Crack initiation in single crystal turbine blade alloys is dominated by interdendritic porosity with oxidation processes affecting initiation position. Lifetime trends can be modelled using a multipart Paris type lifing approach. Orientation, loading state, temperature and environment determine stage I/II crack growth mechanisms and the resulting crack path and should be considered in lifing. Mechanistic insights on how complex stress states, subsurface failures and different temperatures/environments affect fatigue processes can thus improve turbine blade lifing, and direct alloy development programmes. In polycrystalline disc alloys
cracks at high temperature may initiate at oxidised subsurface carbides or porosity. Grain size controls cycle and time dependent crack growth: the benefits of increased grain size in resisting
grain boundary attack mechanisms predominate over those of gamma' distribution variation. Optimising grain boundary character and gamma' distribution should yield the best alloy design strategy for high
temperature fatigue performance in turbine discs.

Item Type: Article
ISSNs: 0267-0836 (print)
Related URLs:
Keywords: Single crystal, Fatigue, Ni based superalloys, Initiation, Grain size, Loading state, Environment, Fatigue crack growth rate
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
ePrint ID: 65062
Date Deposited: 29 Jan 2009
Last Modified: 27 Mar 2014 18:46
Contact Email Address: pasr1@soton.ac.uk
URI: http://eprints.soton.ac.uk/id/eprint/65062

Actions (login required)

View Item View Item