Drainage path for a bearing sump in a vertically oriented turbine engine

Patent metadata

Field	Value
Publication number	US-10851689-B2
Application number	US-201816007679-A
Country	US
Kind code	B2
Filing date	Jun 13, 2018
Priority date	Jun 13, 2018
Publication date	Dec 1, 2020
Grant date	Dec 1, 2020

Abstract

A gas turbine engine in a shutdown mode comprises one or more rotatable shafts, a first oil sump, a second oil sump, and an oil drainage conduit fluidically connecting the first oil sump and the second oil sump. The one or more rotatable shafts are oriented with an axis of rotation less than 90 degrees from vertical. The first oil sump has a selected critical vertical level. The second oil sump is positioned at an elevation lower than the elevation of the first oil sump. The oil drainage conduit effects oil drainage by gravity from the first oil sump to the second oil sump to prevent the level of oil collected in the first oil sump from exceeding the selected critical vertical level.

First claim

What is claimed is:

1. A gas turbine engine in a shutdown mode, said engine comprising:
one or more rotatable shafts oriented with an axis of rotation less than 90 degrees from vertical;
a first oil sump at a first axial position relative to said one or more rotatable shafts, said first oil sump having a selected critical vertical level;
a second oil sump at a second axial position relative to said one or more rotatable shafts such that said second oil sump is positioned at an elevation lower than the elevation of said first oil sump; and
an oil drainage conduit fluidically connecting said first oil sump and said second oil sump, said oil drainage conduit having an inlet positioned in said first oil sump at a vertical level below the selected critical vertical level to thereby effect oil drainage by gravity from said first oil sump to said second oil sump to prevent the level of oil collected in said first oil sump from exceeding the selected critical vertical level.

2. The engine of claim 1 wherein the oil drainage conduit is configured to secure oil drainage when the engine leaves a shutdown mode.

3. The engine of claim 2 further comprising a flow blocking device configured to fluidically isolate the oil drainage conduit from said first oil sump upon rotation of the rotatable shafts.

4. The engine of claim 3 wherein the flow blocking device comprises one or more flaps positioned across the oil drainage conduit and wherein centrifugal forces generated by the rotation of the one or more rotatable shafts sealingly engages the flaps with the oil drainage conduit to fluidically isolate the oil drainage conduit from said first oil sump.

5. The engine of claim 1 further comprising a flow blocking device disposed within the oil drainage conduit and configured to prevent oil flow from the second oil sump to the first oil sump.

6. The engine of claim 1 wherein each of the first oil sump and the second oil sump are disposed about a hollow shaft, and wherein the oil drainage conduit is at least partially disposed within the hollow shaft.

7. The engine of claim 6 wherein the inlet comprises more than one inlet passing through the hollow shaft.

8. The engine of claim 7 wherein said inlet is dimensioned to permit oil drainage at a rate sufficient to prevent the level of oil collected in said first oil sump from exceeding the selected critical vertical level.

9. The engine of claim 8 wherein said more than one inlets are spaced evenly about a circumference of the shaft.

10. A gas turbine engine in a shutdown mode, said engine comprising:
one or more rotatable shafts oriented with an axis of rotation less than 90 degrees from vertical;
a first oil sump at a first axial position relative to said one or more rotatable shafts;
a second oil sump at a second axial position relative to said one or more rotatable shafts such that said second oil sump is positioned at an elevation lower than the elevation of said first oil sump;
a seal positioned proximate said first oil sump such that said seal will be exposed to oil if the level of oil collected in said first oil sump exceeds a selected critical vertical level; and
an oil drainage conduit fluidically connecting said first oil sump and said second oil sump, said oil drainage conduit having an inlet positioned in said first oil sump at a vertical level below the selected critical vertical level to thereby effect oil drainage by gravity from said first oil sump to said second oil sump to prevent the level of oil collected in said first oil sump from exceeding the selected critical vertical level.

11. The engine of claim 10 , wherein the seal is disposed between a first oil sump cover and a first of the rotatable shafts, and wherein the first rotatable shaft is hollow and at least a portion of the oil drainage conduit is disposed within the first rotatable shaft.

12. The engine of claim 10 further comprising a flow blocking device disposed in the drainage path and configured to selectively close the drainage path during shaft rotation.

13. The engine of claim 10 further comprising a flow blocking device disposed in the drainage path and configured to permit flow only from the first oil sump to the second oil sump.

14. The engine of claim 10 further comprising an oil baffle disposed vertically above the seal and configured to direct oil to the oil drainage conduit.

15. The engine of claim 14 wherein the oil baffle extends between a sump cover and an inner member positioned radially inward from the seal.

16. The engine of claim 15 wherein the oil baffle is annular.

17. The engine of claim 10 wherein the inlet comprises more than one inlet passing through the hollow shaft, said inlets spaced evenly about a circumference of the shaft.

18. In gas turbine engine in a shutdown mode having one or more rotatable shafts oriented with an axis of rotation less than 90 degrees from vertical, the engine having first oil sump with a selected critical vertical level and a second oil sump positioned at a lower elevation than the elevation of the first oil sump, a method of preventing a level of oil collected in said first oil sump from exceeding the selected critical vertical level, the method comprising:
providing an oil drainage conduit between the first oil sump and the second oil sump, said oil drainage conduit having an inlet positioned in said first oil sump at a vertical level below the selected critical vertical level to thereby effect oil drainage by gravity from said first oil sump to said second oil sump.

19. The method of claim 18 further comprising preventing flow of oil from the second oil sump to the first oil sump.

20. The method of claim 19 further comprising preventing oil flow through the oil drainage conduit when the one or more shafts are rotating.

Assignees

• Rolls Royce Corp

Inventors

• Engel Chadd D

Classifications

• F01M11/065 Primary

  Position · CPC title

• F16N31/00

  Means for collecting, retaining, or draining-off lubricant in or on machines or apparatus (oil separators for separating oil from exhaust steam F22G) · CPC title

• F01M2011/0466

  Filling or draining during running · CPC title

• F01M2011/068

  with internal reservoir · CPC title

• F01D25/16 Primary

  Arrangement of bearings; Supporting or mounting bearings in casings (bearings per se F16C) · CPC title