Catcher ring arrangement

Patent metadata

Field	Value
Publication number	US-9434467-B2
Application number	US-201313914961-A
Country	US
Kind code	B2
Filing date	Jun 11, 2013
Priority date	Jun 22, 2012
Publication date	Sep 6, 2016
Grant date	Sep 6, 2016

Abstract

This invention relates to a blade assembly comprising: a hub which is rotatable about an axis; at least one blade having an aerofoil portion and a root, wherein the root is coupled to the hub using a primary retention device which prevents radial separation of the root and hub in normal use; and, a secondary retention device which comprises an annular catcher having a restriction through which the root portion cannot radially pass, the restriction being located radially outwardly and radially spaced from the root part during use.

First claim

The invention claimed is:

1. A blade assembly comprising:
a hub which is rotatable about an axis;
at least one blade having an aerofoil portion and a root, wherein the root is coupled to the hub using a primary retention device which prevents radial separation of the root and the hub in normal use; and
a secondary retention device which comprises an annular catcher having a restriction aperture through which the root cannot radially pass, the restriction aperture being located radially outwardly and radially spaced from the root during use, wherein
the annular catcher comprises at least two sections that abut one another along a parting line, the parting line passing through the restriction aperture,
the at least two sections are annular rings defining the restriction aperture and at least one additional restriction aperture, and
the parting line passes through each of the at least one additional restriction aperture.

2. The blade assembly as claimed in claim 1 , wherein a portion of the blade passes through the restriction aperture, in use.

3. The blade assembly as claimed in claim 2 , wherein the restriction aperture is axi-symmetric.

4. The blade assembly as claimed in claim 1 , wherein the parting line lies on a circumferential midline of the annular catcher.

5. The blade assembly as claimed in claim 1 , wherein the at least two sections of the annular catcher are attached to one another via a plurality of fasteners.

6. The blade assembly as claimed in claim 1 , wherein the annular catcher is radially located around the hub by three or more locating assemblies.

7. The blade assembly as claimed in claim 6 , wherein the locating assemblies include at least one two part connector having male and female portions.

8. The blade assembly as claimed in claim 7 , wherein at least one part of the locator assemblies is local to the restriction aperture.

9. The blade assembly as claimed in claim 1 , wherein the hub is nested within at least a portion of the annular catcher.

10. The blade assembly as claimed in claim 1 , wherein the annular catcher is fixedly attached to the hub via a flanged portion.

11. The blade assembly as claimed in claim 1 , wherein the annular catcher is generally polygonal.

12. The blade assembly as claimed in claim 1 , wherein the annular catcher includes two side rails which are axially spaced relative the axis.

13. The blade assembly as claimed in claim 12 , further comprising a web portion which extends between side rails.

Assignees

• Rolls Royce Plc

Inventors

• Mackie Kenneth John
• Udall Kenneth Franklin

Classifications

• B64C11/08 Primary

  for non-adjustable blades · CPC title

• Y02T50/66

  Cross-Sectional Technologies · mapped topic

• F01D5/3023

  of radial insertion type, e.g. in individual recesses · CPC title

• B64D2027/005

  Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR] · CPC title

• B64C11/06 Primary

  for variable-pitch blades · CPC title