# US 10,767,753 B2 · Rolling element cage for geared turbofan

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- Number: US 10,767,753 B2
- Document ID: US10767753B2
- Status: Granted
- Kind: B2
- Application number: 15/132,650
- Filed: 2016-04-19
- Published: 2016-12-29
- Granted: 2020-09-08
- Earliest claimed: 2015-06-25
- Assignees: Raytheon Technologies Corporation
- Applicants: United Technologies Corporation
- Inventors: William G. Sheridan
- Web page: https://patentgrep.com/patent/US10767753B2

## CPC

- F16H 57/0479: {Gears or bearings on planet carriers}
- F02C 3/107: with two or more rotors connected by power transmission
- F02K 3/02: in which part of the working fluid by-passes the turbine and combustion chamber
- F16C 33/6677: {from radial inside, e.g. via a passage through the shaft and/or inner ring}
- F16H 1/28: with gears having orbital motion
- F16H 57/0427: {on rotary parts, e.g. using baffles for collecting lubricant by centrifugal force}
- F16H 57/043: {within rotary parts, e.g. axial channels or radial openings in shafts}
- F16H 57/0456: {Lubrication by injection; Injection nozzles or tubes therefor (oil mist or spray lubrication F16H57/0458)}
- F16H 57/0471: {Bearing}
- F16H 57/0486: {with fixed gear ratio (axle or inter-axle differentials F16H57/0483)}
- F16H 57/082: {Planet carriers}
- F05D 2260/40311: of the epicyclical, planetary or differential type
- F05D 2260/98: Lubrication
- F16C 19/26: with a single row of rollers
- F16C 2360/23: Gas turbine engines
- F16H 2057/085: {Bearings for orbital gears}
- F16H: GEARING
- F02C: GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS (construction of turbines F01D; jet-propulsion plants F02K; construction of compressors or fans F04; generating combustion products of high pressure or high velocity F23R; using gas turbines in compression refrigeration plants F25B11/00)
- F02K: JET-PROPULSION PLANTS (features of jet-propulsion plants common to gas-turbine plants, air intakes or fuel supply control of air-breathing jet-propulsion plants F02C7/00, F02C9/00)
- F16C: SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS

## Abstract

A gear system for a turbofan engine assembly includes a sun gear rotatable about an engine centerline, a non-rotatable ring gear, and a rotating carrier that drives a fan. A plurality of planet gears is intermeshed between the sun gear and the ring gear. A rolling element bearing assembly supports rotation of the planet gear on the carrier. The rolling element bearing assembly includes a rolling element between an inner race and an outer race separated by a cage. A first passage for lubricant through the planet gear. A second passage is in communication with the first passage for communicating lubricant through the inner race to an interface between the inner race and the cage. A geared turbofan engine is also disclosed.

## Claims

### Claim 1

A gear system for a turbofan engine assembly comprising:
a sun gear rotatable about an engine centerline;
a non-rotatable ring gear;
a rotating carrier that drives a fan, the rotating carrier having a forward plate attached to an aft plate;
a plurality of planet gears intermeshed between the sun gear and the ring gear;
a rolling element bearing assembly for each of the plurality of planet gears, the rolling element bearing assembly supporting rotation of a corresponding one of the plurality of planet gears on the carrier, the rolling element bearing assembly includes a rolling element between an inner race and an outer race separated by a cage, wherein the inner race is supported on a radially outer surface of a corresponding one of the plurality of planet gears and includes guide rails that provide a surface to surface interface supporting the cage and the outer race is supported on a corresponding one of the forward plate and the aft plate;
a first passage for lubricant through each of the plurality of planet gears; and
a second passage in communication with the first passage, the second passage extending through the inner race to the surface to surface interface between the inner race and the cage.

### Claim 2 (depends on 1)

The gear system as recited in claim 1, wherein each of the plurality of planet gears includes an inner cavity and the first passage is in communication with the inner cavity and each of the plurality of planet gears further includes a third passage through each the plurality of planet gears that directs the lubricant toward the rolling element bearing assembly.

### Claim 3 (depends on 2)

The gear system as recited in claim 2, wherein the carrier includes an outer scoop that rotates with the carrier receives the lubricant from an outer fixed lubricant jet, the outer fixed lubricant jet fixed relative to rotation of the carrier and is spaced axially apart from the carrier and feeds the lubricant into the inner cavity and through the first passage, the second passage and the third passage to provide the lubricant to the rolling element bearing assembly.

### Claim 4 (depends on 3)

The gear system as recited in claim 3, wherein the carrier includes an inner scoop that rotates with the carrier and receives the lubricant from an inner fixed lubricant jet, the inner fixed jet is fixed relative to rotation of the carrier, is spaced axially apart from the carrier and feeds the lubricant through the carrier to a spray bar, the spray bar spraying the lubricant into at least one gear interface between each of the plurality of planet gears, the sun gear and the ring gear.

### Claim 5 (depends on 1)

The gear system as recited in claim 1, wherein the rolling element bearing assembly is one of a ball, roller, tapered roller and spherical roller element.

### Claim 6 (depends on 1)

The gear system as recited in claim 1, wherein the cage comprises at least one of a steel and a steel alloy.

### Claim 7 (depends on 1)

The gear system as recited in claim 1, wherein the cage is plated with at least one of silver, nickel and gold.

### Claim 8 (depends on 1)

The gear system as recited in claim 1, wherein the guide rails are coated with at least one of Tungsten Carbide, Titanium Nitride, Chrome and Chrome Carbide alloy.

### Claim 9 (depends on 1)

The gear system as recited in claim 1, wherein surfaces of the surface to surface interface between the guide rails and the cage include a surface finish less than or equal to 16 micro-inches.

### Claim 10

A geared turbofan engine comprising:
a fan configured to drive air along a bypass flow path;
a compressor section configured to communicate compressed air to a combustor section for generating a high energy gas flow for driving a turbine section where energy is extracted and utilized to drive the compressor section and the fan; and
a gear system driven by the turbine section for driving the fan, the gear system including a sun gear rotatable about an engine centerline, a non-rotatable ring gear, a rotating carrier that drives the fan, a plurality of planet gears intermeshed between the sun gear and the ring gear, a rolling element bearing assembly corresponding with each of the plurality of planet gears and supporting rotation of a corresponding one the plurality of planet gears on the carrier,
wherein the rolling element bearing assembly includes a rolling element between an inner race and an outer race separated by a cage, the inner race is disposed on a radially outermost surface of a corresponding one of the plurality of planet gears and includes guide rails that provide a surface to surface interface supporting the cage, the outer race is supported on the rotating carrier, a first passage extends through each of the plurality of planet gears, and a second passage extends through the inner race communicate lubricant to an interface between a surface of the guide rails of the inner race and a surface of the cage.

### Claim 11 (depends on 10)

The geared turbofan engine as recited in claim 10, wherein each of the plurality of planet gears includes an inner cavity with the first passage in communication with the inner cavity and each of the plurality of planet gears further includes a third passage through each of the plurality of planet gears for directing the lubricant toward the rolling element bearing assembly.

### Claim 12 (depends on 11)

The geared turbofan engine as recited in claim 11, wherein the carrier includes an outer scoop that receives the lubricant from an outer fixed lubricant jet and feeds the lubricant into the inner cavity and through the first passage, the second passage and the third passage to provide the lubricant to the rolling element bearing assembly.

### Claim 13 (depends on 12)

The geared turbofan engine as recited in claim 12, wherein the carrier includes an inner scoop that receives the lubricant from an inner fixed lubricant jet and feeds the lubricant through the carrier to a spray bar, the spray bar spraying the lubricant into at least one gear interface between the plurality of planet gears, the sun gear and the ring gear.

### Claim 14 (depends on 10)

The geared turbofan engine as recited in claim 10, wherein the guide rails coated with at least one of Tungsten Carbide, Titanium Nitride, Chrome and Chrome Carbide alloy.

### Claim 15 (depends on 10)

The geared turbofan engine as recited in claim 10, wherein the surface of the guide rails and the surface of the cage includes a surface finish of less than or equal to sixteen (16) micro-inches.