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Grain size effects in a Ni-based turbine disc alloy in the time and cycle dependent crack growth regimes

Grain size effects in a Ni-based turbine disc alloy in the time and cycle dependent crack growth regimes
Grain size effects in a Ni-based turbine disc alloy in the time and cycle dependent crack growth regimes
The fatigue crack growth (FCG) behaviour in a Ni-based turbine disc alloy with two grain sized variants, in a low solvus high refractory (LSHR) superalloy has been investigated under a range of temperatures (650–725 °C) and environments (air and vacuum) with trapezoidal waveforms of 1:1:1:1 and 1:20:1:1 durations at an R = 0.1. The results indicate that a coarse grained structure possesses better FCG resistance due to the enhanced slip reversibility promoted by planar slip as well as the reduction in grain boundary area. The fatigue performance of the LSHR superalloy is significantly degraded by the synergistic oxidation effect brought about by high temperature, oxidising environment and dwell at the peak load, associated with increasingly intergranular fracture features and secondary grain boundary cracking. Secondary cracks are observed to be blocked or deflected around primary c0, carbides and borides, and their occurrence closely relates to the roughness of the fracture surface, FCG rate and grain boundary oxidation. The apparent activation energy technique provides a further insight into the underlying mechanism of the FCG under oxidation–creep–fatigue testing conditions, and confirms that oxidation fatigue is the dominant process contributing to the intergranular failure process. At high enough crack growth rates, at lower temperatures, cycle dependent crack growth processes can outstrip crack-tip oxidation processes.
Ni-based superalloy, fatigue crack growth, grain boundary oxidation, secondary cracking, apparent activation energy
0142-1123
217-227
Jiang, R.
b78f0919-0168-43cd-9cda-dd922d8776bf
Everitt, S.
6fbb5641-5cb6-4fd9-97c5-7bc43a67ee74
Lewandowski, M.
4e42c302-1cfd-438b-9ed4-dc0f5b9af9fe
Gao, N.
9c1370f7-f4a9-4109-8a3a-4089b3baec21
Reed, P.A.S.
8b79d87f-3288-4167-bcfc-c1de4b93ce17
Jiang, R.
b78f0919-0168-43cd-9cda-dd922d8776bf
Everitt, S.
6fbb5641-5cb6-4fd9-97c5-7bc43a67ee74
Lewandowski, M.
4e42c302-1cfd-438b-9ed4-dc0f5b9af9fe
Gao, N.
9c1370f7-f4a9-4109-8a3a-4089b3baec21
Reed, P.A.S.
8b79d87f-3288-4167-bcfc-c1de4b93ce17

Jiang, R., Everitt, S. and Lewandowski, M. et al. (2014) Grain size effects in a Ni-based turbine disc alloy in the time and cycle dependent crack growth regimes. International Journal of Fatigue, 62, 217-227. (doi:10.1016/j.ijfatigue.2013.07.014).

Record type: Article

Abstract

The fatigue crack growth (FCG) behaviour in a Ni-based turbine disc alloy with two grain sized variants, in a low solvus high refractory (LSHR) superalloy has been investigated under a range of temperatures (650–725 °C) and environments (air and vacuum) with trapezoidal waveforms of 1:1:1:1 and 1:20:1:1 durations at an R = 0.1. The results indicate that a coarse grained structure possesses better FCG resistance due to the enhanced slip reversibility promoted by planar slip as well as the reduction in grain boundary area. The fatigue performance of the LSHR superalloy is significantly degraded by the synergistic oxidation effect brought about by high temperature, oxidising environment and dwell at the peak load, associated with increasingly intergranular fracture features and secondary grain boundary cracking. Secondary cracks are observed to be blocked or deflected around primary c0, carbides and borides, and their occurrence closely relates to the roughness of the fracture surface, FCG rate and grain boundary oxidation. The apparent activation energy technique provides a further insight into the underlying mechanism of the FCG under oxidation–creep–fatigue testing conditions, and confirms that oxidation fatigue is the dominant process contributing to the intergranular failure process. At high enough crack growth rates, at lower temperatures, cycle dependent crack growth processes can outstrip crack-tip oxidation processes.

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More information

e-pub ahead of print date: 3 August 2013
Published date: May 2014
Keywords: Ni-based superalloy, fatigue crack growth, grain boundary oxidation, secondary cracking, apparent activation energy
Organisations: Engineering Mats & Surface Engineerg Gp

Identifiers

Local EPrints ID: 356189
URI: http://eprints.soton.ac.uk/id/eprint/356189
ISSN: 0142-1123
PURE UUID: 91c87112-8d60-4abe-9694-08a71681ec8a
ORCID for N. Gao: ORCID iD orcid.org/0000-0002-7430-0319
ORCID for P.A.S. Reed: ORCID iD orcid.org/0000-0002-2258-0347

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Date deposited: 11 Sep 2013 12:31
Last modified: 15 Mar 2024 03:10

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Contributors

Author: R. Jiang
Author: S. Everitt
Author: M. Lewandowski
Author: N. Gao ORCID iD
Author: P.A.S. Reed ORCID iD

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