Method and apparatus for segregated oil supply and scavenge in a gas turbine engine

• US 8,904,746 B2
• Filed: 09/05/2011
• Issued: 12/09/2014
• Est. Priority Date: 09/05/2011
• Status: Active Grant

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Fang, Ning, Moscarino, Gary Paul, Record, Adam Mitchell
• Primary Examiner(s): NGUYEN, ANDREW H
• Application Number:
  US13/225,510
• Publication Number:
  US 20130055721A1
• Time in Patent Office: 1,191 Days
• Field of Search: 60/390.8, 607/96, 184/6.11
• US Class Current: 60/39.08
• CPC Class Codes: F01D 25/162 Bearing supports
• CPC Class Codes: F01D 25/18 Lubricating arrangements of machines or engines in general F01M
• CPC Class Codes: F01D 9/065 Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids see also F01D25/16, F01D25/24 and F01D25/26
• CPC Class Codes: F05D 2260/609 Deoiling or demisting
• CPC Class Codes: F05D 2260/98 Lubrication

Abstract

A gas turbine engine oil supply and scavenge apparatus includes: a stationary first frame comprising a first hub and a first outer ring interconnected by an array of radially-extending hollow first struts; a forward wet cavity defined radially inboard of the first frame, having a first rolling element bearing disposed therein; a supply line extending from the first outer ring through one of the first struts and communicating with the forward wet cavity, the supply line adapted to discharge oil to the forward wet cavity; a stationary second frame comprising a second hub and a second outer ring interconnected by an array of radially-extending hollow second struts, the second frame disposed aft of the first frame; and a scavenge path communicating with the forward wet cavity and adapted to remove oil-air mist from the forward wet cavity, the scavenge path defined at least in part by the second frame.

Claims

1. An oil supply and scavenge apparatus for a gas turbine engine, comprising:

a stationary first frame comprising a first hub and a first outer ring interconnected by an array of radially-extending hollow first struts;

a forward wet cavity defined radially inboard of the first frame, having a first rolling element bearing disposed therein;

a supply line extending from the first outer ring through one of the first struts and communicating with the forward wet cavity, the supply line adapted to discharge oil to the forward wet cavity;

a stationary second frame comprising a second hub and a second outer ring interconnected by an array of radially-extending hollow second struts, the second frame disposed aft of the first frame; and

a scavenge path communicating with the forward wet cavity and adapted to remove oil-air mist from the forward wet cavity, the scavenge path defined at least in part by the second frame.

2. The apparatus of claim 1 wherein the second frame includes an annular rear frame arm extending radially inward from the second hub, and the scavenge path passes through the rear frame arm.

3. The apparatus of claim 1 wherein the second frame defines a scavenge plenum communicating with the scavenge path.

4. The apparatus of claim 3 wherein a scavenge tube communicates with the scavenge plenum and an exterior of the second frame.

5. The apparatus of claim 1 wherein the first bearing supports a hollow outer shaft for rotation relative to the first frame.

6. The apparatus of claim 5 wherein an inner shaft is disposed concentrically within the outer shaft and is supported for rotation relative to the second frame by a rolling-element second bearing.

7. The apparatus of claim 6 wherein the second bearing is disposed inside an aft wet cavity defined axially aft of the forward wet cavity.

8. The apparatus of claim 7 wherein the inner shaft includes an annular disk extending radially outward therefrom, the disk defining a boundary between the forward and aft wet cavities.

9. The apparatus of claim 8 wherein at least one transfer port extends through the disk so as to interconnect the forward and aft wet cavities.

10. A method of supplying oil to a bearing in a gas turbine, comprising:

flowing oil through a supply line that extends radially inward through a hollow strut of a stationary first frame, where the first frame comprises a first hub and a first outer ring interconnected by an array of radially-extending hollow first struts, and discharging the oil into a forward wet cavity disposed radially inboard of the first frame which encloses a first rolling element bearing;

using the oil to lubricate the first rolling element bearing, whereby an oil-air mist is generated; and

extracting the oil-air mist through a scavenge path defined at least in part by a stationary second frame that comprises a second hub and a second outer ring interconnected by an array of radially-extending hollow second struts, the second frame disposed aft of the first frame and the rolling element bearing.

11. The method of claim 10 wherein the second frame includes an annular rear frame arm extending radially inward from the second hub, and the scavenge path passes through the rear frame arm.

12. The method of claim 10 wherein the second frame defines a scavenge plenum communicating with the scavenge path.

13. The method of claim 12 wherein a scavenge tube communicates with the scavenge plenum and an exterior of the second frame.

14. The method of claim 10 wherein the first bearing supports a hollow outer shaft for rotation relative to the first frame.

15. The method of claim 14 wherein an inner shaft is disposed concentrically within the outer shaft and is supported for rotation relative to the second frame by a rolling-element second bearing, and the second bearing is disposed inside an aft wet cavity defined axially aft of the forward wet cavity, the method further comprising:

using a second flow of oil to lubricate the second rolling element bearing, whereby a second oil-air mist is generated; and

extracting the second oil-air mist through the scavenge path.

16. The method of claim 15 wherein the inner shaft includes an annular disk extending radially outward therefrom, the disk defining a boundary between the forward and aft wet cavities.

17. The method of claim 16 wherein the oil-air mist is extracted from the forward wet cavity through at least one transfer port extending through the disk, and then through the aft wet cavity.