Method and system for elastic bearing support

Patent metadata

Field	Value
Publication number	US-10274017-B2
Application number	US-201615331121-A
Country	US
Kind code	B2
Filing date	Oct 21, 2016
Priority date	Oct 21, 2016
Publication date	Apr 30, 2019
Grant date	Apr 30, 2019

Abstract

A method of reducing loads in a rotor assembly during an imbalance condition, a shape memory alloy recoupler device, and a hybrid bearing support system are provided. The hybrid bearing support system includes a shaft extension fixedly coupled to a rotatable member at a radially inner end of the shaft extension, a radially outer end of the shaft extension fixedly coupled to a rotatable race of a bearing supporting the rotatable member, and a recoupler device formed of a shape memory alloy (SMA) material coupled in parallel with at least a portion of the shaft extension between the radially inner end and the radially outer end.

First claim

What is claimed is:

1. A hybrid bearing support system for a rotatable member, said system comprising:
a shaft extension fixedly coupled to the rotatable member at a radially inner end of the shaft extension, a radially outer end of said shaft extension fixedly coupled to a rotatable race of a bearing supporting the rotatable member; and
a recoupler device formed of a shape memory alloy (SMA) material coupled in parallel with at least a portion of said shaft extension between the radially inner end and the radially outer end; and
wherein said recoupler device comprises a first crystalline structure having a first stiffness when subjected to a first stress, said recoupler device comprises a second crystalline structure having a second stiffness when subjected to a second stress.

2. The hybrid bearing support system of claim 1 , wherein said shaft extension comprises a conic cross section.

3. The hybrid bearing support system of claim 1 , wherein said recoupler device comprises a conic cross section.

4. The hybrid bearing support system of claim 1 , wherein said recoupler device comprises a radially inner flange, a radially outer flange, and a conic web member extending therebetween.

5. The hybrid bearing support system of claim 1 , wherein said conic web member comprises a single skirt of SMA material.

6. The hybrid bearing support system of claim 4 , wherein said conic web member comprises a plurality of spokes of SMA material.

7. The hybrid bearing support system of claim 4 , wherein at least one of said radially inner flange and said radially outer flange comprise at least one of an SMA material and a steel material.

8. A method of reducing loads in a rotor assembly during an imbalance condition, said method comprising:
supporting the rotor assembly using a load reduction device, the load reduction device including: (i) a shaft extension extending between a bearing assembly and a shaft of the rotor assembly forming a load path therebetween, and (ii) an annular recoupler member extending between the bearing assembly and the shaft forming a second load path parallel to the first load path;
failing the shaft extension when a rotor assembly load through the load reduction device exceeds a predetermined range;
carrying the rotor assembly load through the load reduction device solely through the annular recoupler member; and
wherein the shaft extension includes a first portion coupled to the bearing assembly, a second portion coupled to the shaft of the rotor assembly, and a fusible member positioned between the first portion and the second portion, and wherein failing the shaft extension comprises failing the fusible member of the shaft extension to disconnect the first portion from the second portion during a fan bladeout event.

9. The method of claim 8 , wherein the recoupler member is formed of a shape memory alloy such that the recoupler member is responsive to a change in a stress condition of the load reduction device and configured to change stiffness thereof, thereby regulating an imbalance condition of the shaft of the rotor assembly.

10. The method of claim 8 , wherein carrying the rotor assembly load through the load reduction device solely through the annular recoupler member comprises carrying the rotor assembly load through the load reduction device solely through the annular recoupler member during a post-fan bladeout event windmilling mode of operation.

11. A method of reducing loads in a rotor assembly during an imbalance condition, said method comprising:
supporting the rotor assembly using a load reduction device, the load reduction device including: (i) a shaft extension extending between a bearing assembly and a shaft of the rotor assembly forming a load path therebetween, and (ii) an annular recoupler member extending between the bearing assembly and the shaft forming a second load path parallel to the first load path;
failing the shaft extension when a rotor assembly load through the load reduction device exceeds a predetermined range;
carrying the rotor assembly load through the load reduction device solely through the annular recoupler member; and
wherein supporting the rotor assembly comprises supporting the rotor assembly using both the shaft extension and the recoupler member while a crystal structure of the recoupler member is in a first structure, and wherein failing the shaft extension comprises transitioning the crystal structure of the recoupler member to a second structure.

Assignees

• Gen Electric

Inventors

• Ganiger Ravindra Shankar
• Ghosh Shuvajyoti
• Ac Shivaram
• Joshi Akash
• Shivashankar Vidya Lokammanahalli

Classifications

• F02K3/06

  with front fan · CPC title

• F02C7/06 Primary

  Arrangements of bearings (bearings F16C); Lubricating ({of turbo machines F01D25/18; of machines or} engines in general F01M) · CPC title

• F16C25/083

  with resilient means acting axially on a race ring to preload the bearing · CPC title

• F01D21/045

  special arrangements in stators or in rotors dealing with breaking-off of part of rotor · CPC title

• F01D25/162

  Bearing supports · CPC title