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Fatigue life research and experimental verification of superalloy thin-walled structures subjected to thermal-acoustic loads
Institution:1. Department of Aircraft Maintenance Engineering, Chengdu Aeronautic Polytechnic, Chengdu 610100, China;2. Liaoning Key Laboratory of Advanced Test Technology for Aeronautical Propulsion System, Shenyang Aerospace University, Shenyang 110136, China
Abstract:Rapid alternating stress is formed in structure subjected to harsh thermal-acoustic loads, which will affect fatigue performance and reduce fatigue life seriously. First, fatigue experiment of superalloy thin-walled structure was carried out to obtain fatigue damage location and failure time of the experiment specimen, and S-N curves of superalloy thin-walled structure at 723 K were fitted. Then, dynamic response simulation of superalloy thin-walled structure under the same load as experiment was implemented, and fatigue life was estimated based on the fatigue life prediction model which mainly included: improved rain-flow counting method, Morrow average stress model and Miner linear cumulative damage theory. Further, comparisons between simulation solutions and experimental results achieved a consistency, which verified the validity of the Fatigue Life Prediction Model (FLPM). Moreover, taking a rectangle plate as the analysis object, the distributions of Fain-low circulation blocks and damage levels of the structure were discussed respectively. Finally, current research indicates that in pre-buckling the structure is in softened area and fatigue life decreases with the increase of temperature; in post-buckling the structure is in hardened area and fatigue life increases with the increase of temperature within a certain range.
Keywords:Experimental verification  Fatigue life  Improved rain-flow counting method  Rain-flow cycle matrix  Rain-flow damage matrix  Thermal-acoustic load  Thin-walled structures
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