研究目的
Investigating the effects of multiple laser peening (LP) on the vibration fatigue properties and microstructural evolution of TC6 titanium alloy.
研究成果
Multiple LP significantly enhances the vibration fatigue properties of TC6 titanium alloy by inducing compressive residual stress and beneficial microstructural evolution, such as high-density dislocations and deformation twins. The vibration fatigue life increased by 105.2% after 5 times LP, with surface residual stress transforming from tensile to compressive and microhardness increasing by 32.9%. These improvements are attributed to the compressive residual stress and microstructural changes induced by LP.
研究不足
The study focuses on the effects of LP on TC6 titanium alloy under specific conditions. The generalizability of the findings to other materials or under different conditions is not explored. The study also does not address the cost-effectiveness or scalability of the LP process for industrial applications.
1:Experimental Design and Method Selection:
The study involved conducting vibration fatigue experiments on TC6 titanium alloy specimens before and after LP to compare their fatigue life and observe fracture morphologies using SEM. Residual stress and microhardness measurements were also performed. Microstructures were characterized using TEM and EBSD.
2:Sample Selection and Data Sources:
TC6 titanium alloy specimens were used, with their chemical composition and mechanical properties provided.
3:List of Experimental Equipment and Materials:
A Q-switched Nd-YAG laser system for LP, a THV-1 micro Vickers hardness tester for microhardness measurements, an x-350 X-ray diffractometer for residual stress measurements, a DC-300-3 electromagnetic vibration table for vibration fatigue tests, and SEM (Zeiss Sigma 500) and TEM (Tecnai G2 F20) for microstructural observations.
4:Experimental Procedures and Operational Workflow:
LP was applied to both sides of the specimens with specific parameters. Vibration fatigue tests were conducted at the specimens' natural frequency, with the frequency adjusted after every 105 cycles.
5:Data Analysis Methods:
The data were analyzed to compare vibration fatigue life, residual stress, microhardness, and microstructural changes before and after LP.
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TEM
Tecnai G2 F20
American FEI company
Used for microstructural characterization
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Q-switched Nd-YAG laser system
GAIA-1064
Used for laser peening experiments
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THV-1 micro Vickers hardness tester
Used to measure the microhardness at different depths from the top surface
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x-350 X-ray diffractometer
Handan stress technology institute
Used to measure the residual stress of the samples before and after LP
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DC-300-3 electromagnetic vibration table
Suzhou Sushi Test Instrument Co. Ltd
Used to carry out the vibration fatigue experiment
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SEM
Zeiss Sigma 500
Used to observe the vibration fatigue fracture morphologies
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