Method of removing weld flash

Patent metadata

Field	Value
Publication number	US-10005159-B2
Application number	US-201514803700-A
Country	US
Kind code	B2
Filing date	Jul 20, 2015
Priority date	Aug 15, 2014
Publication date	Jun 26, 2018
Grant date	Jun 26, 2018

Abstract

Method of trimming weld flash from a weld joint formed between a first component and a second component. The method provides a rotary shear tool having a rotary blade and a second blade. The second blade may be a fixed blade. The method further includes shearing the weld flash from the weld joint by passing the weld flash between the rotary blade and second blade of the rotary shear tool. Also provides a rotary shear tool for trimming weld flash from a weld joint formed between a first component and a second component. The rotary shear tool includes: a rotary blade; a second blade; and a mounting portion for mounting the rotary shear tool on a robotic arm.

First claim

The invention claimed is:

1. A method of trimming weld flash from a weld joint formed between a first component and a second component, said method comprising:
providing a rotary shear tool having a rotary blade and a second blade; and
shearing the weld flash from the weld joint by passing the weld flash between the rotary blade and second blade of the rotary shear tool,
wherein the first component is an aerofoil blade and the second component is an annular support and the method comprises passing the weld flash from the weld joint between the rotary blade and second blade of the rotary shear tool with the second blade proximal the annular support.

2. A method according to claim 1 wherein the method comprises mounting the rotary shear tool on a robotic arm and moving the rotary shear tool using the robotic arm such that the weld flash passes between the blades of the rotary shear tool.

3. A method according to claim 1 wherein the rotary shear tool comprises a power source and the method comprises rotating the rotary blade using the power source whilst passing the weld flash between the blades of the rotary shear tool.

4. A method according to claim 1 wherein the second blade is a fixed blade having an upper surface and a lower surface with transverse edge surfaces extending between the upper and lower surfaces, and the method comprises passing the weld flash between the rotary blade and upper surface of the fixed blade of the rotary shear tool.

5. A method according to claim 4 comprising passing the weld flash between the rotary blade and upper surface of the fixed blade of the rotary shear tool at the edge between the upper surface and one of the transverse edge surfaces.

6. A method according to claim 4 wherein the spacing between the upper and lower surfaces of the fixed blade is less than around 5 mm.

7. A method according to claim 4 wherein the fixed blade comprises a chamfered, bevelled or rounded leading edge surface extending between the upper and lower surfaces perpendicular to the transverse edge surfaces and the method comprises feeding the weld flash between the blades of the rotary shear tool over the leading edge surface.

8. A method of making a bladed disc for a gas turbine engine comprising:
joining an aerofoil blade to an annular support at a weld joint using linear friction welding; and
trimming weld flash from the weld joint by the method of claim 1 .

Assignees

• Rolls Royce Plc

Inventors

• Sweeting Paul Philip

Classifications

• F01D5/3061

  by welding, brazing · CPC title

• B23D19/02

  having both a fixed shearing blade and a rotary shearing disc · CPC title

• B25J11/006

  Deburring or trimming · CPC title

• B23K37/08 Primary

  for flash removal · CPC title

• B23P15/006

  turbine wheels · CPC title