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THE INFLUENCE OF LASER SHOCK PEENING ON THE BEHAVIOR OF Ti6Al4V TITANIUM ALLOY UNDER GIGACYCLE FATIGUE CONDITIONS

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This study investigates the gigacycle fatigue behavior of Ti6Al4V titanium alloy – a critical aerospace material – following laser shock peening (LSP). While prior work by the authors demonstrated LSP enhances fatigue life by up to 8 times in stress-concentrated samples, the present research reveals a paradoxical deterioration under gigacycle conditions ( N =10 10 using ultrasonic testing (Shimadzu USF-2000). Contrary to established LSP benefits, treated specimens exhibited a significant reduction in fatigue limit compared to as-received material. Infrared thermography confirmed substantially higher energy dissipation in LSP-processed specimens, while fractography showed a complete transition in failure origin: cracks invariably initiated centrally in LSP specimens versus near-surface initiation in untreated counterparts. These findings are attributed to tensile residual stresses in the specimen core and microstructural alterations induced by LSP.
Title: THE INFLUENCE OF LASER SHOCK PEENING ON THE BEHAVIOR OF Ti6Al4V TITANIUM ALLOY UNDER GIGACYCLE FATIGUE CONDITIONS
Description:
This study investigates the gigacycle fatigue behavior of Ti6Al4V titanium alloy – a critical aerospace material – following laser shock peening (LSP).
While prior work by the authors demonstrated LSP enhances fatigue life by up to 8 times in stress-concentrated samples, the present research reveals a paradoxical deterioration under gigacycle conditions ( N =10 10 using ultrasonic testing (Shimadzu USF-2000).
Contrary to established LSP benefits, treated specimens exhibited a significant reduction in fatigue limit compared to as-received material.
Infrared thermography confirmed substantially higher energy dissipation in LSP-processed specimens, while fractography showed a complete transition in failure origin: cracks invariably initiated centrally in LSP specimens versus near-surface initiation in untreated counterparts.
These findings are attributed to tensile residual stresses in the specimen core and microstructural alterations induced by LSP.

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