发明公开
EP1662092A3 Fatigue-resistant gas turbine airfoil and method therefor 有权
耐疲劳燃气轮机叶片及其方法

Fatigue-resistant gas turbine airfoil and method therefor
摘要:
A metallic component is bounded by at least one peripheral edge. The component includes at least one elongated treated zone having a length substantially greater than its width. This treated zone is spaced away from and disposed generally parallel to the peripheral edge of the component and the entire thickness of the component within the treated zone is in a state of residual compressive stress. Crack growth from the edge due to fatigue or damage is resisted.
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