Shaft assembly comprising a frangible coupling and a flexible coupling

Patent metadata

Field	Value
Publication number	US-10344806-B2
Application number	US-201615086868-A
Country	US
Kind code	B2
Filing date	Mar 31, 2016
Priority date	Apr 20, 2015
Publication date	Jul 9, 2019
Grant date	Jul 9, 2019

Abstract

A shaft assembly comprises a first shaft portion, connected to a second shaft portion by a flexible coupling. The first shaft portion is further connected to the second shaft portion by a frangible coupling with the frangible coupling being configured to fail if a torsional load through the frangible coupling exceeds a predetermined maximum torsional load. The flexible coupling allows an angular misalignment between the first and second shaft portions not exceeding a maximum angular misalignment.

First claim

The invention claimed is:

1. A shaft assembly comprising:
a first shaft portion connected to a second shaft portion by a flexible coupling, the first shaft portion being further connected to the second shaft portion by a frangible coupling,
the frangible coupling being configured to fail upon a bending load across the frangible coupling exceeding a predetermined maximum bending load, and
the flexible coupling being configured to transmit torque between the first shaft portion and the second shaft portion after failure of the frangible coupling, the failure of the frangible coupling causing the first shaft portion and the second shaft portion to become angularly misaligned with each other, the misalignment not exceeding a maximum angular misalignment.

2. The shaft assembly as claimed in claim 1 , further comprising an axial load carrying element providing an axial connection between the first shaft portion and the second shaft portion.

3. The shaft assembly as claimed in claim 1 , wherein the first and second shaft portions are arranged in axial series and the frangible coupling extends axially between the first and second shaft portions.

4. The shaft assembly as claimed in claim 1 , wherein the first and second shaft portions are arranged concentrically and the frangible coupling extends radially between the first and second shaft portions.

5. The shaft assembly as claimed in claim 1 , wherein the flexible coupling includes an axial load carrying element.

6. The shaft assembly as claimed in claim 1 , wherein the flexible coupling is a membrane coupling.

7. The shaft assembly as claimed in claim 1 , wherein the flexible coupling is a constant velocity joint.

8. The shaft assembly as claimed in claim 7 , wherein the constant velocity joint includes a ratchet assembly, the ratchet assembly restricting angular movement of the constant velocity joint to only one angular direction.

9. The shaft assembly as claimed in claim 1 , further comprising a bump stop, wherein the bump stop limits the angular axial misalignment between the first and second shaft portions.

10. The shaft assembly as claimed in claim 9 , wherein the bump stop includes one or more resilient elements.

11. The shaft assembly as claimed in claim 1 , wherein the frangible coupling is concentric with the flexible coupling.

12. A gas turbine engine comprising the shaft assembly as claimed in claim 1 .

Assignees

• Rolls Royce Plc

Inventors

• Rix Andrew Iain James

Classifications

• F01D21/04

  responsive to undesired position of rotor relative to stator {or to breaking-off of a part of the rotor}, e.g. indicating such position · CPC title

• F16D1/02

  for connecting two abutting shafts or the like · CPC title

• F16D9/00 Primary

  Couplings with safety member for disconnecting, e.g. breaking or melting member · CPC title

• F16D47/02 Primary

  of which at least one is a coupling · CPC title

• F05D2260/311

  of the frangible or shear type · CPC title