Influence of complex LCF and dwell load regimes on fatigue of Ti–6Al–4V
Real components are usually subjected to variable amplitude fatigue, and yet the deformation micromechanisms that occur due to such load changes have barely been the subject of study. Here, unidirectionally rolled equiaxed Ti–6Al–4V plate was subjected to mixed dwell and variable amplitude low cycle...
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| Published in | Acta materialia Vol. 103; pp. 77 - 88 |
|---|---|
| Main Authors | , , , , |
| Format | Journal Article |
| Language | English |
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Elsevier Ltd
15.01.2016
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| Abstract | Real components are usually subjected to variable amplitude fatigue, and yet the deformation micromechanisms that occur due to such load changes have barely been the subject of study. Here, unidirectionally rolled equiaxed Ti–6Al–4V plate was subjected to mixed dwell and variable amplitude low cycle fatigue (LCF), with the finding that overloads near the yield stress were found to retard subsequent fatigue crack growth, whilst elastic underloads were found to accelerate subsequent growth. Dwell intervals were found to be especially damaging, to a far greater extent than either dwell or LCF alone. Dwell facets were found to initiate subsurface and to be smoother than LCF facets, but were otherwise similar in orientation (∼30° to the loading axis) and crystallographic plane, 2–13° from (0002). However, no alteration of the slip bands underlying striations was observed at the point of load changes using TEM. In failure investigation, striation counting is an important tool; the loading changes used were not found to affect the number of striations formed. Dislocation networks were found between similarly oriented grains in the as-received material, which disintegrated under dwell loading and at high stresses.
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| AbstractList | Real components are usually subjected to variable amplitude fatigue, and yet the deformation micromechanisms that occur due to such load changes have barely been the subject of study. Here, unidirectionally rolled equiaxed Ti-6Al-4V plate was subjected to mixed dwell and variable amplitude low cycle fatigue (LCF), with the finding that overloads near the yield stress were found to retard subsequent fatigue crack growth, whilst elastic underloads were found to accelerate subsequent growth. Dwell intervals were found to be especially damaging, to a far greater extent than either dwell or LCF alone. Dwell facets were found to initiate subsurface and to be smoother than LCF facets, but were otherwise similar in orientation (30 degree to the loading axis) and crystallographic plane, 2-13 degree from (0002). However, no alteration of the slip bands underlying striations was observed at the point of load changes using TEM. In failure investigation, striation counting is an important tool; the loading changes used were not found to affect the number of striations formed. Dislocation networks were found between similarly oriented grains in the as-received material, which disintegrated under dwell loading and at high stresses. Real components are usually subjected to variable amplitude fatigue, and yet the deformation micromechanisms that occur due to such load changes have barely been the subject of study. Here, unidirectionally rolled equiaxed Ti–6Al–4V plate was subjected to mixed dwell and variable amplitude low cycle fatigue (LCF), with the finding that overloads near the yield stress were found to retard subsequent fatigue crack growth, whilst elastic underloads were found to accelerate subsequent growth. Dwell intervals were found to be especially damaging, to a far greater extent than either dwell or LCF alone. Dwell facets were found to initiate subsurface and to be smoother than LCF facets, but were otherwise similar in orientation (∼30° to the loading axis) and crystallographic plane, 2–13° from (0002). However, no alteration of the slip bands underlying striations was observed at the point of load changes using TEM. In failure investigation, striation counting is an important tool; the loading changes used were not found to affect the number of striations formed. Dislocation networks were found between similarly oriented grains in the as-received material, which disintegrated under dwell loading and at high stresses. [Display omitted] |
| Author | Lindley, T.C. Dye, D. Tympel, P.O. Saunders, E.A. Dixon, M. |
| Author_xml | – sequence: 1 givenname: P.O. surname: Tympel fullname: Tympel, P.O. email: peter.tympel10@imperial.ac.uk organization: Department of Materials, Royal School of Mines, Imperial College London, Prince Consort Road, London SW7 2BP, UK – sequence: 2 givenname: T.C. surname: Lindley fullname: Lindley, T.C. organization: Department of Materials, Royal School of Mines, Imperial College London, Prince Consort Road, London SW7 2BP, UK – sequence: 3 givenname: E.A. orcidid: 0000-0002-8340-0530 surname: Saunders fullname: Saunders, E.A. organization: Rolls Royce plc, Materials – Failure Investigation, Bristol BS34 7QE, UK – sequence: 4 givenname: M. surname: Dixon fullname: Dixon, M. organization: Rolls Royce plc, Elton Road, Derby DE24 8BJ, UK – sequence: 5 givenname: D. orcidid: 0000-0002-8756-3513 surname: Dye fullname: Dye, D. email: david.dye@imperial.ac.uk organization: Department of Materials, Royal School of Mines, Imperial College London, Prince Consort Road, London SW7 2BP, UK |
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| SubjectTerms | Amplitudes Crack propagation Dislocation structures Dwell Facets Fatigue Fatigue (materials) Fatigue failure Low cycle fatigue Striations TEM Titanium alloys Titanium base alloys |
| Title | Influence of complex LCF and dwell load regimes on fatigue of Ti–6Al–4V |
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