Crack growth threshold analysis in TiAl alloys

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(JTI-CS2-2014-CFP01-ENG-03-04) - CRACK GROWTH THRESHOLD ANALYSIS IN TIAL ALLOYS

Programme: Horizon 2020 Framework Programme
Call: Clean Sky 2 Call for Proposals 01 EU

Topic description

Scope:

This programme will investigate the fatigue crack growth threshold of second generation TiAl alloys suitable for use in the IP turbine of the UltraFan engine. The alloy will be defined by Rolls-Royce. This package of work will determine the fatigue crack growth threshold and crack growth rates, evaluate the effects of temperature and also the effects of the variation in properties within the designated heat treatment window. The influence of original defect size and morphology is also within scope.  Please refer for the full and formal topic description to Annex III of the Clean Sky 2 Work Plan 2014-2015 Amendment nr. 1  Version 3 (see under the tab "Topic Conditions and Documents")

Keywords

MMP Metallic Materials & basic processes SAD Structural Analysis and Design API Aeronautical Propulsion Integration

Tags

Crack propagation Engine Tit Al Alloys Fatigue Fan Turbines

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