Bladed rotor arrangement and a lock plate for a bladed rotor arrangement

Patent metadata

Field	Value
Publication number	US-2016273370-A1
Application number	US-201615052386-A
Country	US
Kind code	A1
Filing date	Feb 24, 2016
Priority date	Mar 20, 2015
Publication date	Sep 22, 2016
Grant date	—

Abstract

A lock plate of a bladed rotor arrangement is hollow. The bladed rotor arrangement comprises is a bladed turbine rotor of a gas turbine engine. The hollow lock plate has reduced weight compared to a solid lock plate and reduces the centrifugal load on the rim of the rotor and reduces the stresses in the lock plate groove on the rotor blade and hence increases the working life of the rotor and the working life of the rotor blade respectively. The lock plate may have radially extending chambers and openings to provide a flow of coolant onto the rotor posts of the rotor).

First claim

1 . A lock plate for a bladed rotor arrangement, wherein the lock plate is hollow, the lock plate comprises a first planar wall, a second planar wall spaced from the first planar wall and a peripheral wall extending around the periphery of the lock plate from the periphery of the first planar wall to the periphery of the second planar wall.

2 . A lock plate as claimed in claim 1 wherein the lock plate comprises a plurality of walls arranged between and secured to the first planar wall and the second planar wall to stiffen the lock plate.

3 . A lock plate as claimed in claim 2 wherein the lock plate comprises a cellular wall structure arranged between and secured to the first planar wall and the second planar wall to stiffen the lock plate.

4 . A lock plate as claimed in claim 3 wherein the cellular wall structure is a honeycomb wall structure.

5 . A lock plate as claimed in claim 2 wherein the lock plate comprises a plurality of radially extending walls to stiffen the lock plate.

6 . A lock plate as claimed in claim 5 wherein the lock plate has a plurality of inlet openings in the second planar wall interconnecting with radially extending passages defined between the radially extending walls and the lock plate having a plurality of outlet openings in the second planar wall interconnecting with the radially extending passages defined between the radially extending walls and the outlet openings in the second planar wall being spaced radially from the inlet openings.

7 . A lock plate as claimed in claim 6 wherein the lock plate has a projection extending away from the second planar wall and the outlet openings extending through the projection.

8 . A bladed rotor arrangement comprising a rotor, a plurality of rotor blades and a plurality of lock plates,
the rotor blades being mounted on the periphery of the rotor, each rotor blade comprising an aerofoil, a platform, a shank and a root, the rotor comprising a plurality of circumferentially spaced axially extending slots, the root of each rotor blade locating in a respective one of the axially extending slots in the periphery of the rotor, a plurality of lock plates being arranged at a first axial end of the rotor, the radially outer ends of the lock plates at the first axial end of the rotor engaging grooves defined by radially inwardly extending flanges on the platforms of the rotor blades, the radially inner ends of the lock plates at the first axial end of the rotor engaging a circumferentially extending groove, wherein at least one of the lock plates being hollow, the at least one plate comprises a first planar wall, a second planar wall spaced from the first planar wall and a peripheral wall extending around the periphery of the lock plate from the periphery of the first planar wall to the periphery of the second planar wall.

9 . A bladed rotor arrangement as claimed in claim 8 wherein each lock plate being hollow.

10 . A bladed rotor arrangement as claimed in claim 9 wherein each lock plate comprises a first planar wall, a second planar wall spaced from the first planar wall and a peripheral wall extending around the periphery of the lock plate from the periphery of the first planar wall to the periphery of the second planar wall.

11 . A bladed rotor arrangement as claimed in claim 10 wherein each lock plate comprises a plurality of walls arranged between and secured to the first planar wall and the second planar wall to stiffen the lock plate.

12 . A bladed rotor arrangement as claimed in claim 11 wherein each lock plate comprises a cellular wall structure arranged between and secured to the first planar wall and the second planar wall to stiffen the lock plate.

13 . A bladed rotor arrangement as claimed in claim 12 wherein each cellular wall structure is a honeycomb wall structure.

14 . A bladed rotor arrangement as claimed in claim 11 wherein each lock plate comprises a plurality of radially extending walls to stiffen the lock plate.

15 . A bladed rotor arrangement as claimed in claim 14 wherein the lock plate has a plurality of inlet openings in the second planar wall interconnecting with radially extending passages defined between the radially extending walls and the lock plate having a plurality of outlet openings in the second planar wall interconnecting with the radially extending passages defined between the radially extending walls and the outlet openings in the second planar wall being spaced radially from the inlet openings.

16 . A bladed rotor arrangement as claimed in claim 15 wherein the lock plate has a projection extending away from the second planar wall and the outlet openings extending through the projection.

17 . A bladed rotor arrangement as claimed in claim 8 wherein at least one seal plate being arranged at the first axial end of the rotor, the radially inner ends of the lock plates at the first axial end of the rotor engaging a circumferentially extending groove at least partially defined by the at least one seal plate at the first axial end of the rotor.

18 . A method of manufacturing a lock plate for a bladed rotor arrangement, wherein the lock plate is hollow, the lock plate comprises a first planar wall, a second planar wall spaced from the first planar wall and a peripheral wall extending around the periphery of the lock plate from the periphery of the first planar wall to the periphery of the second planar wall, the method comprising manufacturing the lock plate by a method selected from the group consisting of metal injection moulding and additive layer manufacturing.

Assignees

• Rolls Royce Plc

Inventors

• Belshaw David

Classifications

• F01D11/006

  Sealing the gap between rotor blades or blades and rotor · CPC title

• F05D2250/283

  honeycomb · CPC title

• F05D2230/31

  Layer deposition · CPC title

• F05D2220/32

  in gas turbines · CPC title

• F01D5/3015 Primary

  with side plates · CPC title