Rotor blade manufacture

Patent metadata

Field	Value
Publication number	US-9624778-B2
Application number	US-201514725898-A
Country	US
Kind code	B2
Filing date	May 29, 2015
Priority date	Jun 24, 2014
Publication date	Apr 18, 2017
Grant date	Apr 18, 2017

Abstract

A method is provided of processing one or more blades of a row of blades which forms part of a rotor for a gas turbine engine. The method includes: providing a rotor disc having a slot for mounting one or more blades; loading the blades in the slot and loading the wax blocks in or adjacent the slot, the wax blocks being configured and positioned such that, on loading, the blades shear material from the wax blocks, the sheared wax blocks reducing a range of tilt angles which can be adopted by the blades; and performing a processing operation on the loaded blades.

First claim

We claim:

1. A method of processing one or more blades of a row of blades which forms part of a rotor for a gas turbine engine, the method including:
providing a rotor disc having a slot for mounting one or more blades;
loading the blades in the slot and loading pre-formed wax blocks in or adjacent to the slot, the wax blocks being configured and positioned such that, on loading, the blades shear material from the wax blocks, the sheared wax blocks reducing a range of tilt angles which can be adopted by the blades; and
performing a processing operation on the loaded blades.

2. A method according to claim 1 , wherein the processing operation is grinding the blade tips.

3. A method according to claim 1 , wherein the wax blocks reduce the range of tilt angles by at least 50%.

4. A method according to claim 1 , wherein the slot is a circumferential slot for mounting a plurality of blades.

5. A method according to claim 1 , wherein the disc has a plurality of axial slots for mounting respective blades, the blades being loaded in the slots and the wax blocks being loaded in or adjacent the slots.

6. A method according to claim 1 , wherein the blades have laterally-projecting platforms which extend over a rim of the disc or laterally-projecting seal wings, and respective wax blocks are positioned beneath the platforms or seal wings.

7. A method according to claim 1 , wherein respective wax blocks are positioned in the slot beneath the roots of the blades.

8. A method according to claim 1 which further includes balancing the blades before the blades are processed.

9. A method according to claim 1 , which further includes applying a protective coating to the loaded blades to protect the blades from debris generated during the processing operation.

10. A method according to claim 1 , which further includes removing the wax blocks from the rotor.

Assignees

• Rolls Royce Plc

Inventors

• Raven Gemma Alexandra
• Taylor Christopher Jonathan
• May Alexander David
• Baird Andrew Alan Robert

Classifications

• F01D5/20

  Specially-shaped blade tips to seal space between tips and stator {(F01D5/225 takes precedence)} · CPC title

• F05D2240/307

  related to the tip of a rotor blade · CPC title

• Y10T29/49323

  Assembling fluid flow directing devices, e.g., stators, diaphragms, nozzles · CPC title

• F01D25/285

  Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures · CPC title

• F05D2230/64

  using positioning or alignment devices for aligning or centring, e.g. pins · CPC title