Weld stub arrangement and a method of using the arrangement to make an article

Patent metadata

Field	Value
Publication number	US-10384302-B2
Application number	US-201815903087-A
Country	US
Kind code	B2
Filing date	Feb 23, 2018
Priority date	Feb 24, 2017
Publication date	Aug 20, 2019
Grant date	Aug 20, 2019

Abstract

A workpiece for use with a flash producing welding process comprises a revolute body, a plurality of first attachment portions, a plurality of second attachment portions. The revolute body has an axis of rotation.
Each of the first attachment portions has a first radially outer weld joint surface, and each of the second attachment portions has a second radially outer weld joint surface. The revolute body comprises a plurality of first and second stub portions, with each of the first stub portions having a first radially inner weld joint surface, and each of the second stub portions having a second radially inner weld joint surface.

First claim

What is claimed is:

1. A workpiece for use with a flash producing welding process, the workpiece comprising:
a revolute body comprising an axis of rotation;
a plurality of first attachment portions, each of the first attachment portions comprising a first radially outer weld joint surface; and
a plurality of second attachment portions, each of the second attachment portions comprising a second radially outer weld joint surface;

wherein the revolute body comprises a plurality of first and second stub portions, each of the first stub portions having a first radially inner weld joint surface, each of the second stub portions having a second radially inner weld joint surface, and respective ones of the first stub portions and second stub portions are arranged in an alternating sequence circumferentially around the axis of rotation, each of the first radially outer weld joint surfaces is joined to a corresponding one of the first radially inner weld joint surfaces by a flash producing welding process at a first weld joint plane, each of the second radially outer weld joint surfaces is joined to a corresponding one of the second radially inner weld joint surfaces by a flash producing welding process at a second weld joint plane,
wherein each first weld joint plane is positioned at a first radius from the axis of rotation, each second weld joint plane is positioned at a second radius from the axis of rotation, the first radius is different to the second radius, and the difference between the first radius and the second radius is a radial offset from the axis of rotation.

2. The workpiece as claimed in claim 1 , wherein the radial offset is between 5 and 20 mm.

3. The workpiece as claimed in claim 1 , wherein each of the first attachment portions has a first attachment tip, each of the second attachment portions has second attachment tip, and the plurality of first attachment tips and second attachment tips together define a tip circumference.

4. The workpiece as claimed in claim 1 , wherein the revolute body is a rotor, and the first and second attachment portions are aerofoils.

5. The workpiece as claimed in claim 1 , wherein the flash producing welding process is selected from the group consisting of linear friction welding, orbital welding, and forge welding.

6. A method for forming a workpiece, the method comprising the steps of: providing a revolute body having an axis of rotation, and a plurality of first and second stub portions arranged in an alternating circumferential array around the axis of rotation, each first stub portion having a first radially inner weld joint surface, and each second stub portion having a second radially inner weld joint surface; providing a first attachment portion corresponding to each first stub portion, and a second attachment portion corresponding to each second stub portion, each first attachment portion comprising a first radially outer weld joint surface, and each second attachment portion comprising a second radially outer weld joint surface; and using a flash producing welding process to weld each first radially outer weld joint surface to a corresponding first radially inner weld joint surface at a first weld joint plane, and each second radially outer weld joint surface to a corresponding second radially inner weld joint surface at a second weld joint plane to form the workpiece,
wherein each first weld joint plane is positioned at a first radius from the axis of rotation, each second weld joint plane is positioned at a second radius from the axis of rotation, the first radius being different to the second radius, and the difference between the first radius and the second radius is a radial offset from the axis of rotation.

7. The method as claimed in claim 6 , wherein the radial offset is between 5 and 20 mm.

8. The method as claimed in claim 6 , wherein the revolute body is a rotor, and the first and second attachment portions are aerofoils.

9. The method as claimed in claim 6 , wherein the flash producing welding process is selected from the group consisting of linear friction welding, orbital welding, and forge welding.

10. A computer program that, when read by a computer, causes performance of the method as claimed in claim 6 .

11. A non-transitory computer readable storage medium comprising computer readable instructions that, when read by a computer, cause performance of the friction welding process as claimed in claim 6 .

Assignees

• Rolls Royce Plc

Inventors

• March Richard N

Classifications

• B23K20/1245 Primary

  characterised by the apparatus · CPC title

• F01D5/02

  Blade-carrying members, e.g. rotors (rotors of non-bladed type F01D1/34; stators F01D9/00 {; selecting particular materials F01D5/28}) · CPC title

• B23K2101/001

  Turbines · CPC title

• F01D5/147

  Construction, i.e. structural features, e.g. of weight-saving hollow blades (F01D5/148, F01D5/16 and F01D5/20 take precedence; blade shape F01D5/141; blades with cooling or heating channels or cavities F01D5/18; heating, heat-insulating or cooling means on blades F01D5/18) · CPC title

• F01D5/005

  Repairing methods or devices · CPC title