Turbine blade having material block and related method

Metal working – Method of mechanical manufacture – Impeller making

Reexamination Certificate

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C029S889700, C416S189000, C416S19300A, C416S195000, C416S19600R, C416S24100B

Reexamination Certificate

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08056227

ABSTRACT:
A turbine blade including a root section at an end of the turbine blade, a first airfoil section adjacent to the root section, and a tip section adjacent to the airfoil section and including a material block that is incongruous with the airfoil section. A midspan section may also include a material block. Each material block can be selectively machined to customize the length of the turbine blade and the position of a tip shroud connection or midspan connection. The turbine blade can be sized for retrofitting last stage blades of older turbines. A radial position of the root mounts for the turbine blade may also be adjusted to provide further customization.

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patent: 7448844 (2008-11-01), Johnson
patent: 7836594 (2010-11-01), Rose

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