Stub shaft

Patent metadata

Field	Value
Publication number	US-9938830-B2
Application number	US-201514688521-A
Country	US
Kind code	B2
Filing date	Apr 16, 2015
Priority date	May 8, 2014
Publication date	Apr 10, 2018
Grant date	Apr 10, 2018

Abstract

A controlled collapse stub shaft is provided for allowing controlled axial movement of a mainline shaft which joins a fan or compressor to a turbine of a gas turbine engine. A first end of the stub shaft is adapted to be joined to the mainline shaft. A second end of the stub shaft is adapted to be joined to a part of the engine which is axially stationary relative to the controlled axial movement of the mainline shaft. The stub shaft further has an annular body between the first and second ends. The body contains a plurality of axially-spaced circumferential rows of circumferentially-extending slots, inter-slot ligaments being formed between the slots of each row. Successive rows are offset. In this way, the ligaments of the axially forwardmost and rearwardmost rows excepted, each ligament is sandwiched between a forward slot and a rearward slot of its neighboring rows. Further, each ligament is joined to adjacent ligaments of its neighboring rows by circumferentially-extending bars having a thickness in the axial direction corresponding to the axial spacing between the rows. The bars are axially deflectable to allow the axial distance between the first and second ends of the stub shaft to decrease.

First claim

The invention claimed is:

1. A controlled collapse stub shaft for allowing controlled axial movement of a mainline shaft which joins a fan or compressor to a turbine of a gas turbine engine, a first end of the stub shaft being adapted to be joined to the mainline shaft, a second end of the stub shaft being adapted to be joined to a part of the engine which is axially stationary relative to the controlled axial movement of the mainline shaft, and the stub shaft further having a first annular body between the first and second ends, the annular body containing a plurality of axially-spaced circumferential rows of circumferentially-extending slots, inter-slot ligaments being formed between the slots of each row, and successive axially-spaced rows being offset, whereby, the ligaments of the axially forwardmost and rearwardmost rows excepted, each ligament is sandwiched between a forward slot and a rearward slot of its neighbouring rows, and each ligament is joined to adjacent ligaments of its neighbouring rows by circumferentially-extending bars having a thickness in the axial direction corresponding to the axial spacing between the rows, wherein the bars are axially deflectable to allow the axial distance between the first and second ends of the stub shaft to decrease; and a second annular body coaxial with the first annular body, the second annular body providing the first end of the stub shaft adapted to be joined to the mainline shaft, and the first annular body providing the second end of the stub shaft adapted to be joined to the axially stationary part of the engine.

2. The stub shaft according to claim 1 , wherein the ratio of the length to the width of the slots is at least 3:1.

3. The stub shaft according to claim 2 , wherein a radial clearance is formed between the first and the second annular bodies.

4. The stub shaft according to claim 1 , wherein the ratio of the length of the slots to the thickness in the circumferential direction of the ligaments is at least 3:1.

5. The stub shaft according to claim 1 , wherein the thickness in the axial direction of the bars is less than the width of the slots.

6. The stub shaft according to claim 1 , wherein the thickness in the axial direction of the bars is less than the thickness in the circumferential direction of the ligaments.

7. The stub shaft according to claim 1 , wherein every other row is aligned such that the ligaments of these rows are at the same angular positions.

8. The stub shaft according to claim 1 , wherein each ligament is sandwiched between the mid-points of the forward and rearward slots of its neighbouring rows.

9. The stub shaft according to claim 1 , further comprising a first annular flange at the first end for joining to the mainline shaft.

10. The stub shaft according to claim 9 , further comprising a second annular flange at the second end for joining to the axially stationary part of the engine.

11. The stub shaft according to claim 1 , further comprising one or more shear formations at the second end of the stub shaft, the shear formations forming a load path for transmitting axial loads between the axially stationary part of the engine and the mainline shaft.

12. The stub shaft according to claim 1 , wherein the first annular body is rotationally fixed relative to the second annular body.

13. A gas turbine engine having a mainline shaft which joins a fan or compressor of the engine to a turbine of the engine, and a stub shaft for allowing controlled axial movement of the mainline shaft, the stub shaft having a first end and a second end, the first end of the stub shaft joining to the mainline shaft, and the second end of the stub shaft joining to a part of the engine which is axially stationary relative to the controlled axial movement of the mainline shaft, a first end of the stub shaft being adapted to be joined to the mainline shaft, a second end of the stub shaft being adapted to be joined to a part of the engine which is axially stationary relative to the controlled axial movement of the mainline shaft, and the stub shaft further having a first annular body between the first and second ends, the annular body containing a plurality of axially-spaced circumferential rows of circumferentially-extending slots, inter-slot ligaments being formed between the slots of each row, and successive axially-spaced rows being offset, whereby, the ligaments of the axially forwardmost and rearwardmost rows excepted, each ligament is sandwiched between a forward slot and a rearward slot of its neighbouring rows, and each ligament is joined to adjacent ligaments of its neighbouring rows by circumferentially-extending bars having a thickness in the axial direction corresponding to the axial spacing between the rows, wherein the bars are axially deflectable to allow the axial distance between the first and second ends of the stub shaft to decrease; and a second annular body coaxial with the first annular body, the second annular body providing the first end of the stub shaft adapted to be joined to the mainline shaft, and the first annular body providing the second end of the stub shaft adapted to be joined to the axially stationary part of the engine.

Assignees

• Rolls Royce Plc

Inventors

• Harper Callum

Classifications

• F16F15/10

  Suppression of vibrations in rotating systems by making use of members moving with the system (by balancing F16F15/22 {; yielding couplings F16D3/00} ; with flywheels acting variably or intermittently F16H {; construction providing resilience or vibration-damping for gear elements F16H55/14}) · CPC title

• F05D2240/62

  Flexible · CPC title

• F01D1/02

  with stationary working-fluid guiding means and bladed or like rotor, {e.g. multi-bladed impulse steam turbines}(F01D1/24 takes precedence; without stationary working-fluid guiding means F01D1/18) · CPC title

• F05D2260/15

  Load balancing · CPC title

• F05D2260/30

  Retaining components in desired mutual position · CPC title