Spline lubrication system

• US 9,353,848 B2
• Filed: 03/13/2013
• Issued: 05/31/2016
• Est. Priority Date: 03/13/2013
• Status: Active Grant

• Current Assignee: Hamilton Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: Hamilton Sundstrand Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Blewett, Michael R., Short, Keith E.
• Primary Examiner(s): Bomberg, Kenneth
• Assistant Examiner(s): Harris, Wesley
• Application Number:
  US13/799,415
• Publication Number:
  US 20140274420A1
• Time in Patent Office: 1,175 Days
• Field of Search: 415/112
• US Class Current: 1/1
• CPC Class Codes: F01D 25/18 Lubricating arrangements of machines or engines in general F01M
• CPC Class Codes: F01D 5/026 Shaft to shaft connections
• CPC Class Codes: F02C 7/32 Arrangement, mounting, or driving, of auxiliaries
• CPC Class Codes: F04C 15/0088 Lubrication of machines or engines in general F01M
• CPC Class Codes: F05D 2260/4031 as in toothed gearing
• CPC Class Codes: F05D 2260/98 Lubrication
• CPC Class Codes: F16H 57/0421 on or within the casing, e.g. shields or baffles for collecting lubricant, tubes, pipes, grooves, channels or the like
• CPC Class Codes: F16H 57/0424 Lubricant guiding means in the wall of or integrated with the casing, e.g. grooves, channels, holes means for guiding lubricant into an axial channel of a shaft F16H57/0426
• CPC Class Codes: F16H 57/0426 Means for guiding lubricant into an axial channel of a shaft
• CPC Class Codes: F16H 57/043 within rotary parts, e.g. axial channels or radial openings in shafts
• CPC Class Codes: F16H 57/0486 with fixed gear ratio differentials F16H57/0483
• CPC Class Codes: F16N 21/00 Conduits; Junctions in general F16L; Fittings for lubrication apertures

Abstract

A gearbox assembly for use in a gas turbine engine includes a gearbox housing and first and second shafts. The first shaft is rotatably mounted in the gearbox housing. The first shaft has a first set of splines and defines a central cavity. The second shaft has a second set of splines engaged with the first set of splines. A scupper is positioned on an inner surface of the gearbox housing proximate the first shaft so as to direct liquid from the scupper through the central cavity of the first shaft to the first and second sets of splines.

Claims

1. A gearbox assembly for use in a gas turbine engine, the gearbox assembly comprising:

a gearbox housing;

a first shaft rotatably mounted in the gearbox housing, having a first set of splines, and defining a central cavity;

a second shaft having a second set of splines engaged with the first set of splines;

a scupper positioned on an inner surface of the gearbox housing proximate the first shaft so as to direct liquid from the scupper through the central cavity of the first shaft to the first and second sets of splines, wherein the first shaft has a plurality of entry holes positioned with respect to the scupper for receiving liquid from the scupper; and

an oil catch pan mounted to the gearbox housing and positioned inside the first shaft and axially aligned with the entry holes.

2. The gearbox assembly of claim 1, wherein the first shaft has an annular dam extending radially inward from first shaft, wherein the annular dam is axially positioned between the entry holes and the first set of splines, and wherein the oil catch pan extends through a hole in the annular dam.

3. The gearbox assembly of claim 2, wherein the oil catch pan comprises:

a collection area axially aligned with the entry holes; and

a drip ledge positioned on an opposite side of the annular dam from the collection area.

4. The gearbox assembly of claim 1, wherein the first shaft has an annular dam extending radially inward from first shaft and wherein the annular dam is axially positioned between the entry holes and the first set of splines.

5. The gearbox assembly of claim 1, and further comprising:

a rotatable accessory connected to and driven by the second shaft, wherein the first shaft is a gear shaft and the second shaft is an accessory shaft.

6. The gearbox assembly of claim 1, wherein the scupper comprises:

first and second walls extending substantially perpendicularly from the inner surface; and

a third wall extending from the first wall to the second wall such that the scupper has an open top.

7. The gearbox assembly of claim 1, wherein a hollow passage extends from a bottom of the scupper through the gearbox housing to fluidically connect the scupper to the central cavity.

8. A gas turbine engine comprising:

the gearbox assembly of claim 1;

a spool, wherein the spool comprises;

a compressor;

a turbine; and

a spool shaft connecting the compressor to the turbine;

a third shaft extending from the spool to the gearbox assembly; and

gearing connecting the third shaft to the spool and to the first shaft.

9. A method comprising:

rotating first and second shafts interconnected by splines and mounted to a gearbox;

collecting lubricating liquid in a scupper positioned on an inner surface of the gearbox;

flowing lubricating liquid from the scupper through the first shaft to the splines when the first and second shafts stop rotating, wherein the lubricating liquid flows from the scupper through entry holes positioned circumferentially around the first shaft; and

flowing lubricating liquid from the entry holes across an annular dam to the splines via an oil catch pan.

10. The method of claim 9, and further comprising:

limiting flow from the scupper to the first shaft when the first and second shafts are rotating at normal operating speed.

11. The method of claim 9, and further comprising:

driving rotation of the first and second shafts via a spool of a gas turbine engine.

12. A method comprising:

rotating first and second shafts interconnected by splines and mounted to a gearbox;

collecting lubricating liquid in a scupper positioned on an inner surface of the gearbox;

flowing lubricating liquid from the scupper through entry holes in the first shaft to an oil catch pan when the first and second shafts stop rotating

flowing lubricating liquid from the entry holes across an annular dam to the splines via the oil catch pan; and

flowing no additional lubricating liquid to the splines when the first and second shafts start rotating again.

13. The method of claim 12, and further comprising:

collecting the lubricating liquid between the splines and the annular dam, wherein the annular dam extends radially inward on an inner surface of the first shaft.