Oil loss protection for a fan drive gear system

Patent metadata

Field	Value
Publication number	US-9879608-B2
Application number	US-201514635524-A
Country	US
Kind code	B2
Filing date	Mar 2, 2015
Priority date	Mar 17, 2014
Publication date	Jan 30, 2018
Grant date	Jan 30, 2018

Abstract

A fan drive gear system includes at least one intermediate gear that includes an axial gear passage for receiving and conveying a fluid suitable for cooling and/or lubricating. At least a first axial end of the intermediate gear includes a first fluid storage trap for capturing fluid entering and/or exiting the gear passage and storing the fluid therein during powered operation of the fan drive gear system. The fluid is capable of being passively supplied to the intermediate gear passage during an interrupted power event.

First claim

The invention claimed is:

1. A fan drive gear system comprising:
at least one gear that includes an axial gear passage for receiving and conveying a fluid suitable for cooling and/or lubricating;
at least a first axial end of gear of said at least one gear includes a first fluid storage trap configured to capture the fluid entering and/or exiting the axial gear passage and configured to store the fluid therein during powered operation of the fan drive gear system, the first fluid storage trap including an opening to said axial gear passage and including a second opening axially opposite the opening to the axial gear passage along a centerline axis of the axial gear passage; and
whereby the first fluid storage trap is configured to passively supply the fluid to the axial gear passage during an interrupted power event via spillover.

2. The fan drive gear system of claim 1 , further comprising;
a sun gear interfaced with the gear of said at least one gear;
a ring gear interfaced with said gear of said at least one gear; and
a carrier body supporting the gear of said at least one gear.

3. The fan drive gear system of claim 2 , wherein the first fluid storage trap comprises a radially outward base portion relative to an axis defined by said carrier body and at least one radially inward base portion relative to said axis defined by said carrier body.

4. The fan drive gear system of claim 3 , wherein said radially outward base portion is defined on a first axial end by a radially aligned wall segment of said carrier body relative to the axis defined by the carrier body and said radially outward base portion is defined on a second axial end by a radially aligned wall of the first fluid storage trap.

5. The fan drive gear system of claim 4 , wherein said radially aligned wall of said first fluid storage trap extends further radially away from said axis defined by the carrier body than said radially aligned wall segment of said carrier body.

6. The fan drive gear system of claim 4 , wherein
said at least one gear includes an axially aligned through hole having an opening at a first end and an opening at a second end opposite the first end; and
said radially aligned wall segment of said carrier body extends to an edge of said opening such that excess fluid in said first fluid storage trap spills from said first fluid storage trap into said gear of the at least one gear.

7. The fan drive gear system of claim 2 , wherein said first fluid storage trap comprises a first fluid storage trap disposed on a first axial end of the gear of said at least one gear and a second fluid storage trap disposed at a second end of said gear of said at least one gear.

8. The fan drive gear system of claim 2 , wherein each fluid storage trap of said at least one fluid storage trap is a passive element.

9. The fan drive gear system of claim 2 , wherein each fluid storage trap of the at least one fluid storage trap is affixed to said carrier body via at least one of a seal element and a bond such that a lubricant does not leak between said fluid storage trap and said carrier body.

10. The fan drive gear system of claim 9 , wherein each fluid storage trap of said at least one fluid storage trap is affixed to said carrier body via at least the bond, and wherein the bond is at least one of a welded bond and an adhesive bond.

11. The fan drive gear system of claim 2 , wherein said gear of said at least one gear further comprises
an axially aligned bore receiving a pin;
at least one roller bearing disposed between a radially outer surface of said pin and a radially outer surface of said gear of said at least one gear;
wherein the pin includes an axially aligned bore defining a radially inner pin surface, and the pin includes at least one through hole connecting the radially inner pin surface to a radially outer pin surface such that fluid in said through hole is passed to an interior of said carrier body.

12. The fan drive gear system of claim 4 , further comprising a powered fluid injection system disposed adjacent at least one opening of said axially aligned bore such that the fluid is injected into an interior of said pin, wherein the powered fluid injection system is distinct from the first fluid trap.

13. The fan drive gear system of claim 1 , wherein the first fluid storage trap is configured to capture the fluid exiting the axial gear passage.

14. The fan drive gear system of claim 1 , wherein the second opening is radially centered relative to the axis defined by the gear, and the second opening does not extend radially beyond the diameter of the axial gear passage.

15. A gas turbine engine comprising
a fan;
a compressor module downstream of the fan;
a combustor downstream of the compressor;
a turbine module downstream of the combustor having at least a fan drive turbine that indirectly drives the fan;
a fan drive gear system mechanically connecting the fan drive turbine and the fan; and
wherein the fan drive gear system comprises:
at least one gear that includes an axial gear passage configured to receive and conveying a fluid suitable for cooling and/or lubricating; and
at least a first axial end of said gear of said at least one gear includes a first fluid storage trap configured to capture the fluid entering and/or exiting the axial gear passage and store the fluid therein during powered operation of the fan drive gear system, the first fluid trap including an opening to said axial gear passage and including a second opening axially opposite the opening to the axial gear passage along a centerline axis of the axial gear passage;
whereby the first fluid trap is configured to passively supply the fluid to the gear passage during an interrupted power event.

16. The gas turbine engine of claim 15 , wherein the fan drive gear system further comprises:
a sun gear interfaced with said gear of said at least one gear;
a ring gear interfaced with said gear of said at least one gear; and
a carrier body supporting the gear of said at least one gear.

17. The gas turbine engine of claim 16 , wherein the first fluid storage trap is operable to retain the fluid injected into said at least one gear, and return said fluid to said gear of said at least one gear.

18. The gas turbine- of claim 12 , wherein said first fluid trap is disposed on a first axial end of said planetary gear and further comprising a second fluid trap disposed at a second axial end of said planetary gear, the second axial end being axially opposite the first axial end.

19. The gas turbine engine of claim 16 , wherein said first fluid storage trap is a passive element.

20. The gas turbine engine of claim 16 , wherein the first fluid storage trap is affixed to said carrier body via at least one of a seal element and a bond such that the fluid does not leak between said first fluid storage trap and said carrier body.

21. The fan drive gear system of claim 20 , wherein said first fluid storage trap is affixed to said carrier body via at least the bond, and wherein said bond is at least one of a welded bond and an adhesive bond.

22. A method for providing fluid to a fan drive gear system during interrupted power comprising:
disposing a first fluid storage trap adjacent an opening in a gear, wherein the gear includes at least a first axial end having a first fluid storage trap configured to capture the fluid entering and/or exiting an axial gear passage and configured to store the fluid therein during powered operation of the fan dri

Assignees

• United Technologies Corp

Inventors

• Sheridan William G

Classifications

• F05D2260/98

  Lubrication · CPC title

• F16H57/082

  Planet carriers · CPC title

• F02C7/36 Primary

  Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user ({F02C3/107 - F02C3/13 and} F02C7/32 take precedence; couplings for transmitting rotation F16D; gearing in general F16H) · CPC title

• F01D25/18

  Lubricating arrangements (of machines or engines in general F01M) · CPC title

• F16H57/043

  within rotary parts, e.g. axial channels or radial openings in shafts · CPC title