首页> 外国专利> Niobium silicide-based turbine components with composition graded portion ; methods of laser cladding of niobium silicide on a turbin component, also used for repairing

Niobium silicide-based turbine components with composition graded portion ; methods of laser cladding of niobium silicide on a turbin component, also used for repairing

机译:成分分级的硅化铌基涡轮组件;涡轮机部件上硅化铌激光熔覆的方法,也用于修复

摘要

A turbine component (10) formed from a niobium silicide-based composition is described. The component (10) can be compositionally-graded through at least a portion of its structure. A turbine blade (10) formed from a composition which includes a niobium silicide alloy is also described. The blade includes an airfoil (12), an airfoil tip region (31), a platform (24) on which the airfoil (12) is mounted and a dovetail root (26) attached to an underside of the platform (24). The niobium silicide alloy in at least one portion of the turbine blade (10) is compositionally different from the niobium silicide alloy in another portion of the turbine blade (10). Processes for fabricating a niobium silicide-based turbine article are also described, using laser cladding techniques. Repair methods are also set forth in the application.
机译:描述了一种由基于硅化铌的组合物形成的涡轮机部件(10)。组分(10)可以通过其结构的至少一部分在组成上分级。还描述了由包括硅化铌合金的组合物形成的涡轮叶片(10)。叶片包括翼型件(12),翼型件尖端区域(31),在其上安装翼型件(12)的平台(24)以及附接到平台(24)下侧的燕尾榫根(26)。涡轮叶片(10)的至少一部分中的硅化铌合金与涡轮叶片(10)的另一部分中的硅化铌合金在成分上不同。还描述了使用激光熔覆技术制造基于硅化铌的涡轮机制品的方法。修复方法也在本申请中提出。

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