Explore the words cloud of the DevTMF project. It provides you a very rough idea of what is the project "DevTMF" about.
The following table provides information about the project.
Coordinator |
LINKOPINGS UNIVERSITET
Organization address contact info |
Coordinator Country | Sweden [SE] |
Project website | http://www.solidmechanics.iei.liu.se/Projects/DevTMF/index.html |
Total cost | 994˙538 € |
EC max contribution | 994˙538 € (100%) |
Programme |
1. H2020-EU.3.4.5.5. (ITD Engines) |
Code Call | H2020-CS2-CFP01-2014-01 |
Funding Scheme | CS2-RIA |
Starting year | 2016 |
Duration (year-month-day) | from 2016-02-01 to 2020-07-31 |
Take a look of project's partnership.
# | ||||
---|---|---|---|---|
1 | LINKOPINGS UNIVERSITET | SE (LINKOPING) | coordinator | 343˙873.00 |
2 | SWANSEA UNIVERSITY | UK (SWANSEA) | participant | 457˙735.00 |
3 | THE UNIVERSITY OF NOTTINGHAM | UK (NOTTINGHAM) | participant | 192˙930.00 |
DevTMF takes the collective technical expertise and experience of working on thermo-mechanical fatigue (TMF) problems related to large aero-engines from three major centres of TMF research, namely Linköping, Swansea and Nottingham Universities in order to perform the activities of this topic. Together, the team will deliver significant technical innovations in following major topics to ensure world-leading competencies in aero engine and aircraft manufacturing sector for Europe:
1. Improvement and development of advanced standard and non-standard cutting-edge TMF experimental methods and harmonisation of the test methods to enable standardisation across the field by performing comprehensive studies into the phenomena for a range of representative parts, 2. Advanced metallurgical assessment of structural disc alloy(s) taking into account the effect of multiple critical variables (e.g. R-ratio, phase, environment, dwell) to determine active damage mechanisms that control the life under TMF operating conditions, and 3. Physically based coupled models, with experimental validation, capable of predicting TMF initiation and propagation lives of components subjected to complex engine cycles and suitable for implementation in the computer programmes used to predict component lives.
The project will take the above-described technologies to TRL5. Two business opportunities are addressed by this work: (i) at the end of the project the materials understanding and lifing models will be used to optimise/uprate the performance of existing individual aero engine components and (ii) over a longer timescale influence the development of new disc alloys and ultra efficient future designs (Advance, Ultrafan). The developed TMF technologies will enable industrial aero gas turbines used for aero engines to be operated at higher temperatures and pressures, improving their efficiency and reducing fuel consumption (by 1%) and CO2 emissions. Hence improved competitiveness and marker share.
Report regarding the effect of static and dynamic crack tip heating in induction field | Documents, reports | 2019-11-15 09:59:30 |
Risk register and management | Documents, reports | 2019-11-15 09:59:30 |
Literature review of state-of-the-art on TMF life and crack propagation modelling | Documents, reports | 2019-11-15 09:59:30 |
Present basis and plans for modelling approaches and development | Documents, reports | 2019-11-15 09:59:30 |
Report regarding the effect of heating methods on TMF CP rates | Documents, reports | 2019-11-15 09:59:30 |
Internal Consortium Agreement | Documents, reports | 2019-11-15 09:59:30 |
Take a look to the deliverables list in detail: detailed list of DevTMF deliverables.
year | authors and title | journal | last update |
---|---|---|---|
2018 |
Daniel Leidermark, Robert Eriksson, James P. Rouse, Christopher J. Hyde, Svjetlana Stekovic Thermomechanical fatigue crack initiation in disc alloys using a damage approach published pages: 19007, ISSN: 2261-236X, DOI: 10.1051/matecconf/201816519007 |
MATEC Web of Conferences 165 | 2019-11-15 |
2018 |
J. P. Rouse, C. J. Hyde, D. Leidermark, S. Stekovic, J. Jones, M. Whittaker, R. Lancaster, S. Pattison and B. Grant The Development of Predictive TMF Material Models for Cyclic Plasticity in a Nickel-based Superalloy published pages: , ISSN: , DOI: |
12th International Fatigue Congress (FATIGUE 2018) 27 May - 1 June 2018 | 2019-11-15 |
2017 |
M. T. Whittaker, J.P. Jones, S. P. Brookes, R. J. Lancaster, A. Dyer, S.J. Williams TESTING METHODOLOGIES FOR THERMO-MECHANICAL FATIGUE EVALUATION IN ADVANCED AEROSPACE ALLOYS published pages: , ISSN: , DOI: |
11th International Conference on Advanced Materials & Processing 7-8 September 2017 | 2019-11-15 |
2018 |
M.T. Whittaker, J.P. Jones, R.J. Lancaster, C.J. Hyde, J. Rouse, S. Pattison, S. Stekovic Thermo-mechanical fatigue crack growth in advanced aerospace alloys published pages: , ISSN: , DOI: |
12th International Conference on Fatigue Damage of Structural Materials 16-21 September 2018 | 2019-11-15 |
2019 |
J. Palmer, J. Jones, A. Dyer, R. Smith, R. Lancaster, M. Whittaker Development of test facilities for thermo-mechanical fatigue testing published pages: 208-218, ISSN: 0142-1123, DOI: 10.1016/j.ijfatigue.2018.12.015 |
International Journal of Fatigue 121 | 2019-11-15 |
2017 |
Mark Whittaker, Jonathan Jones, Ashley Dyer and Jennie Palmer Testing methodologies for thermo-mechanical fatigue evaluation in advanced aerospace materials published pages: 51, ISSN: 2321-6212, DOI: |
Res. Rev. J Mat. Sci. 2017 Volume 5, Issue 5 | 2019-11-15 |
2018 |
Jonathan Jones Enhancing the Accuracy of Advanced High Temperature Mechanical Testing through Thermography published pages: 380, ISSN: 2076-3417, DOI: 10.3390/app8030380 |
Applied Sciences 8/3 | 2019-11-15 |
2018 |
M. Whittaker, J. Jones, R. Lancaster, S. Pattison, S. Stekovic Thermo-mechanical fatigue crack growth in advanced aerospace alloys (Keynote lecture) published pages: , ISSN: , DOI: |
12th International Fatigue Congress (FATIGUE 2018) 27 May - 1 June 2018 | 2019-11-15 |
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