Rotor blade manufacture
US-2015369051-A1 · Dec 24, 2015 · US
US9102014B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9102014-B2 |
| Application number | US-81740010-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 17, 2010 |
| Priority date | Jun 17, 2010 |
| Publication date | Aug 11, 2015 |
| Grant date | Aug 11, 2015 |
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A method of servicing an airfoil for use in a gas turbine engine. The airfoil assembly is defined by a base material and includes an airfoil and a platform from which the airfoil extends. A predetermined amount of the base material is removed from the airfoil assembly proximate to a fillet area of the airfoil assembly via water jet material removal. The fillet area comprises a junction between the airfoil and the platform and is located at an intersection between the airfoil and the platform. A remainder of the base material comprising base material of the airfoil assembly other than proximate to the fillet area is left intact.
Opening claim text (preview).
What is claimed is: 1. A method of servicing an airfoil assembly for use in a gas turbine engine, the airfoil assembly defined by a base material and comprising an airfoil having a radially inner end which is attached to a platform from which the airfoil extends, the method comprising: removing predetermined amounts of the base material from the airfoil assembly proximate to a fillet area and the radially inner end of the airfoil assembly at leading and trailing edges of the airfo…
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