IP Library › Granted Patent US 9,695,710
Granted Patent B2
US 9,695,710 · App. 14/831,963 · Granted Jul 4, 2017

Oil transfer bearing

Inventors: Michael E. McCune (Colchester, CT); Marc J. Muldoon (Marlborough, CT)
Assignee: UNITED TECHNOLOGIES CORPORATION
F01D25/18F01D25/16F16C33/106F16C33/1045F16H57/043F16H57/0479F16H57/0482F02C7/06F05D2220/32F05D2240/50F05D2260/40311F05D2260/98
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Quick Facts
Patent No.
US 9,695,710
App. No.
14/831,963
Granted
Jul 4, 2017
Kind
B2
Abstract

A transfer bearing assembly includes a transfer bearing shaft. An oil transfer bearing surrounds the transfer bearing shaft. A radially extending tube is attached to the transfer bearing shaft and is configured to engage a carrier on a speed reduction device.

Claims (27)

1. A transfer bearing assembly including:

a transfer bearing shaft;

an oil transfer bearing surrounding the transfer bearing shaft, wherein the oil transfer bearing includes a stationary outer bearing and a rotating inner bearing attached to the transfer bearing shaft; and

a radially extending tube attached to the transfer bearing shaft configured to engage a carrier on a speed reduction device.

2. The assembly of claim 1 , wherein the stationary outer bearing includes at least one race aligned with at least one opening in the rotating inner bearing configured to transfer oil from the stationary bearing to the transfer bearing shaft through the rotating inner bearing.

3. The assembly of claim 2 , wherein the transfer bearing shaft includes at least one axially extending passage in communication with one of the at least one opening in the rotating inner bearing.

4. The assembly of claim 3 , wherein a radially inner end of the tube engages the transfer bearing shaft and a radially outer end of the tube engages a carrier.

5. The assembly of claim 4 , wherein the tube is configured to move in a radial direction relative to the transfer bearing shaft.

6. The assembly of claim 4 , wherein the transfer bearing shaft includes at least one radially extending opening in communication with the axially extending passage and the tube is located within the radially extending opening.

7. A gas turbine engine section including:

a planetary gear set including a rotating carrier; and

a transfer bearing assembly including:

a transfer bearing shaft;

an oil transfer bearing surrounding the transfer bearing shaft, wherein the oil transfer bearing includes a stationary outer bearing and a rotating inner bearing attached to the transfer bearing shaft; and

a radially extending tube attached to the transfer bearing shaft configured to engage the rotating carrier on a speed reduction device.

8. The gas turbine engine section of claim 7 , wherein the stationary outer bearing includes at least one race aligned with at least one opening in the rotating inner bearing configured to transfer oil from the stationary bearing to the transfer bearing shaft through the rotating inner bearing.

9. The gas turbine engine section of claim 8 , wherein the transfer bearing shaft includes at least one axially extending passage in communication with one of the at least one opening in the rotating inner bearing.

10. The gas turbine engine section of claim 9 , wherein a radially inner end of the tube engages the transfer bearing shaft and a radially outer end of the tube engages the carrier.

11. The gas turbine engine section of claim 9 , wherein the transfer bearing shaft includes at least one radially extending opening in communication with the axially extending passage and the tube is located within the radially extending opening.

12. The gas turbine engine section of claim 7 , wherein the tube is configured to move in a radial direction relative to the transfer bearing shaft.

13. The gas turbine engine section of claim 7 , wherein the transfer bearing shaft is attached to the carrier with a flexible member.

14. The gas turbine engine section of claim 7 , wherein the transfer bearing shaft is attached to the carrier with a sliding fit pin connection.

15. The gas turbine engine section of claim 7 , wherein the transfer bearing shaft includes a carrier attachment flange having a plurality of openings for receiving fasteners to attach the transfer bearing shaft to the carrier.

16. A method of lubricating a component on a gas turbine engine comprising:

directing a lubricant through an oil transfer bearing toward at least one axially extending passage in a transfer bearing shaft, wherein the at least one axially extending passage is in communication with a radially extending passage and a tube is located within the radially extending passage; and

directing the lubricant to a carrier from the axially extending passage through a tube capable of moving relative to the transfer bearing shaft in a radially direction.

17. The method of claim 16 , wherein a radially inner end of the tube engages the transfer bearing shaft and a radially outer end of the tube engages the carrier.

Assignments (3)
CHANGE OF NAME Recorded Jul 27, 2023
From: RAYTHEON TECHNOLOGIES CORPORATION
To: RTX CORPORATION
Reel/Frame 064714/0001 →
CORRECTIVE ASSIGNMENT TO CORRECT THE AND REMOVE PATENT APPLICATION NUMBER 11886281 AND ADD PATENT APPLICATION NUMBER 14846874. TO CORRECT THE RECEIVING PARTY ADDRESS PREVIOUSLY RECORDED AT REEL: 054062 FRAME: 0001. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF ADDRESS. Recorded Mar 4, 2021
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 055659/0001 →
CHANGE OF NAME Recorded Sep 4, 2020
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 054062/0001 →
Continuity (2)
Provisional Application 62047086 · Sep 8, 2014
Related Publication 20160069212A1 · Mar 10, 2016