Rotor support structures for rotating drum rotors of gas turbine engines

Patent metadata

Field	Value
Publication number	US-11280219-B2
Application number	US-201916697350-A
Country	US
Kind code	B2
Filing date	Nov 27, 2019
Priority date	Nov 27, 2019
Publication date	Mar 22, 2022
Grant date	Mar 22, 2022

Abstract

A rotor support system for a gas turbine engine includes a rotatable drum rotor and a non-rotatable support casing. The rotor support system includes a bearing assembly configured for positioning between the rotatable drum rotor and the non-rotatable support casing. The bearing assembly includes, at least, a stationary support frame and a rotatable race. Further, the rotatable race is configured to engage the rotatable drum rotor at separate and discrete locations that are circumferentially spaced apart around the rotatable drum rotor.

First claim

What is claimed is:

1. A gas turbine engine, comprising:
a rotatable drum rotor comprising a plurality of blades secured thereto, the plurality of blades extending radially inward from the rotatable drum rotor;
a non-rotatable support casing mounted radially outward of the rotatable drum rotor;
a rotor support system comprising a bearing assembly connected to the the non-rotatable support casing, the bearing assembly comprising, at least, an annular stationary support frame and a rotatable race, the rotatable race comprising a plurality of rotatable roller bearings circumferentially spaced apart about the rotatable rotor drum, each of the plurality of roller bearings comprising an inner race, an outer race, and a plurality of rolling elements arranged between the inner and outer races, wherein the inner race of each of the plurality of roller bearings is fixed to the annular stationary support frame such that the inner races do not rotate with the rotatable drum rotor, the rotatable race engaging the rotatable drum rotor at separate and discrete locations that are circumferentially spaced apart around the rotatable drum rotor.

2. The gas turbine engine of claim 1 , wherein the bearing assembly is positioned at one or more axial locations along the rotatable drum rotor.

3. The gas turbine engine of claim 1 , wherein the annular stationary support frame is mounted radially exterior to the rotatable drum rotor.

4. The gas turbine engine of claim 1 , wherein the annular stationary support frame is mounted radially internal of the rotatable drum rotor.

5. The gas turbine engine of claim 1 , wherein the outer races of the plurality of roller bearings define the rotatable race of the bearing assembly that rotates with the rotatable drum rotor.

6. The gas turbine engine of claim 1 , wherein the plurality of rolling elements comprises at least one of ball rollers or cylindrical rollers.

7. The gas turbine engine of claim 1 , wherein the plurality of rolling elements are constructed, at least in part, of ceramic.

8. The gas turbine engine of claim 1 , wherein the rotatable drum rotor is part of a compressor section, a turbine section, or a combustion section of the gas turbine engine.

9. A rotor support system for a gas turbine engine, the gas turbine engine comprising a rotatable drum rotor and a non-rotatable support casing, the rotor support system comprising:
a bearing assembly configured for positioning between the rotatable drum rotor and the non-rotatable support casing, the bearing assembly comprising, at least, an annular stationary support frame and a rotatable race, the rotatable race comprising a plurality of rotatable roller bearings circumferentially spaced apart about the rotatable rotor drum, each of the plurality of roller bearings comprising an inner race, an outer race, and a plurality of rolling elements arranged between the inner and outer races, wherein the inner races of each of the plurality of roller bearings are fixed to the annular stationary support frame such that the inner races do not rotate with the rotatable drum rotor, the rotatable race configured to engage the rotatable drum rotor at separate and discrete locations that are circumferentially spaced apart around the rotatable drum rotor.

10. The rotor support system of claim 9 , wherein the annular stationary support frame forms an inner race of the bearing assembly, and wherein the rotatable race is an outer race of the bearing assembly.

11. The rotor support system of claim 9 , wherein the outer races of the plurality of roller bearings define the rotatable race of the bearing assembly that rotates with the rotatable drum rotor.

12. The rotor support system of claim 9 , wherein the plurality of rolling elements comprise at least one of ball rollers or cylindrical rollers.

13. The rotor support system of claim 9 , wherein the plurality of rolling elements are constructed, at least in part, of ceramic.

14. The rotor support system of claim 9 , wherein the rotatable drum rotor is part of a compressor section, a turbine section, or a combustion section of the gas turbine engine.

Assignees

• Gen Electric

Inventors

• Puranik Shashank Suresh
• Mondal Bhaskar Nanda
• Schmidt Richard
• Pankaj Peeyush
• Payyoor Narayanan

Classifications

• F16C13/04

  Bearings with only partial enclosure of the member to be borne; Bearings with local support at two or more points · CPC title

• F04D19/024

  with contrarotating parts · CPC title

• F16C13/022

  supporting a hollow roll mantle rotating with respect to a yoke or axle · CPC title

• F16C2360/23

  Gas turbine engines · CPC title

• F01D5/03

  Annular blade-carrying members having blades on the inner periphery of the annulus and extending inwardly radially, i.e. inverted rotors · CPC title