| METALS AND METAL MATRIX COMPOSITES |
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| Research Progress of Nanoindentation Methods for Measuring Residual Stress in Critical Materials of Aero-engine |
| LUO Jun1,2,3,4, LI Nan1,2,3,4, WANG Xi1,2,3,4, LIU Changkui1,2,3,4,*
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1 AECC Beijing Institute of Aeronautical Materials, Beijing 100095, China
2 AVIC Failure Analysis Center, Beijing 100095, China
3 Beijing Key Laboratory of Aeronautical Materials Testing and Evaluation, Beijing 100095, China
4 Key Laboratory of Aeronautical Materials Testing and Evaluation, Aero Engine Corporation of China, Beijing 100095, China |
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Abstract With the increasing demand for aero-engine, higher requirements are put forward for the performance of engine alloys. The residual tensile stress introduced by manufacturing and machining seriously affects the mechanical properties of the alloy and shortens the service life of the aero-engine. Hence, the measurement of residual stress plays a key role in the reliability and safety of aero-engine. In this paper, the nanoindentation measurement of contact depth, contact stiffness, contact area, hardness and elastic modulus are systematically summarized. The analysis process of residual stress calculation model, such as Suresh, David, Lee, Xu, Wang, Kim and Peng models are introduced. Moreover, the advantages and disadvantages of the calculation models are compared. The latest research progress of nanoindentation theory in residual stress measurement in critical materials of aero-engine, such as stainless steel, aluminum alloy, titanium alloy and nickel-base superalloy are reviewed in detail. The shortcomings of residual stress calculation model are also summarized, and the development of nanoindentation method for measuring residual stress is prospected.
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Published:
Online: 2024-06-25
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| Fund:National Key R & D Program of China (2021YFA1600600). |
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2024, Vol. 38 
