TURBINE BLADES AND VANES FOR GAS TURBINE ENGINE
A method of forming a turbine blade or vane is provided and includes forming a wax pattern in a turbine blade or vane shape and additively forming a positive witness band around a tip portion of the wax pattern. 提供了一种形成涡轮叶片或轮叶的方法,并且所述方法包括将蜡模成型为涡轮叶片或轮叶形状,以及在所述蜡模的尖端部分周围增材地形成凸标示带。...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | A method of forming a turbine blade or vane is provided and includes forming a wax pattern in a turbine blade or vane shape and additively forming a positive witness band around a tip portion of the wax pattern.
提供了一种形成涡轮叶片或轮叶的方法,并且所述方法包括将蜡模成型为涡轮叶片或轮叶形状,以及在所述蜡模的尖端部分周围增材地形成凸标示带。 |
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