DOUBLE ROW CYLINDRICAL ROLLER BEARING WITH HIGH LENGTH TO DIAMETER RATIO ROLLERS

• US 20170089218A1
• Filed: 09/25/2015
• Published: 03/30/2017
• Est. Priority Date: 09/25/2015
• Status: Active Application

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Hasting, William Howard, Fisher, Kenneth Lee, Bradley, Donald Albert, Dickman, Joseph Robert
• Application Number:
  US14/865,239
• Publication Number:
  US 20170089218A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: F01D 15/12 Combinations with mechanical gearing driven by multiple engines F01D13/00
• CPC Class Codes: F01D 25/16 Arrangement of bearings; Supporting or mounting bearings in casings bearings per se F16C
• CPC Class Codes: F01D 5/06 Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections F01D5/022, F01D5/023 take precedence
• CPC Class Codes: F02C 7/36 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 Class Codes: F04D 29/321 for axial flow compressors
• CPC Class Codes: F04D 29/325 for axial flow fans blade mountings F04D29/34, blades F04D29/38
• CPC Class Codes: F05D 2220/32 in gas turbines
• CPC Class Codes: F05D 2240/50 Bearings
• CPC Class Codes: F05D 2260/40311 of the epicyclical, planetary or differential type
• CPC Class Codes: F16C 19/28 with two or more rows of rollers
• CPC Class Codes: F16C 2360/23 Gas turbine engines in general F02C
• CPC Class Codes: F16C 2361/61 Toothed gear systems, e.g. support of pinion shafts in general F16H57/02
• CPC Class Codes: F16C 33/34 Rollers; Needles
• CPC Class Codes: F16H 1/28 with gears having orbital motion
• CPC Class Codes: F16H 2057/085 Bearings for orbital gears
• CPC Class Codes: F16H 57/08 of gearings with members having orbital motion
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A planet gearbox is provided for connection to a carrier of an epicyclic gearing arrangement with a single input and single output and including a sun gear, a ring gear and at least one double helix planet gear rotatable on a cylindrical roller bearing wherein the ratio of each cylindrical roller'"'"'s length to each cylindrical roller'"'"'s diameter exceeds 1.0. A gas turbine engine includes a shaft coupling a compressor of a compressor section to a turbine of a turbine section. An epicyclic gearing arrangement has a single input from the shaft coupled to a sun gear, a single output from the carrier that is coupled to the shaft of a fan and includes a planet gearbox with cylindrical rollers having a length-to-diameter ratio exceeding 1.0.

Claims

1. A planet gearbox for connection to a carrier of an epicyclic gearing arrangement that has only a single input and a single output and that includes a sun gear and a ring gear disposed circumferentially around the planet gearbox and the sun gear, the planet gearbox comprising:

a support pin configured to be fixed to the carrier and defining a cylindrical outer surface that is equidistant from a central axis that extends in an axial direction;

an inner race defining a cylindrical inner surface that is non-rotatably connected to the cylindrical outer surface of the support pin, the inner race defining an outer surface that defines at least one track, each track defined in the outer surface being configured to receive and rotatably guide therein a respective plurality of cylindrical rollers;

a respective plurality of cylindrical rollers rotatably disposed within each respective track of the inner race;

an outer race defining an inner cylindrical surface contacting each respective plurality of cylindrical rollers, the outer race defining an outer cylindrical surface that defines a gearing surface that is configured to mesh with both the sun gear and the ring gear;

wherein each cylindrical roller defines a cylindrical outer surface that is disposed with an axis of rotation that extends in a direction parallel to the axial direction, and the cylindrical outer surface of each cylindrical roller is defined by a diameter that extends through the axis of rotation along a direction that is normal to the axis of rotation; and

wherein the outer cylindrical surface of each cylindrical roller defines a length in the direction parallel to the axis of rotation of the cylindrical roller, and the ratio of each cylindrical roller'"'"'s length to each cylindrical roller'"'"'s diameter is greater than one.

2. The planet gearbox of claim 1, wherein the ratio of each cylindrical roller'"'"'s length to each cylindrical roller'"'"'s diameter is greater than 1.3.

3. The planet gearbox of claim 1, wherein each cylindrical roller has a length-to-diameter ratio that falls within the range from 1.3 to 1.8, inclusive.

4. The planet gearbox of claim 1, wherein at least a central section of the cylindrical outer surface of each cylindrical roller is disposed uniformly equidistant from the axis of rotation along a central section of the axial length of the cylindrical roller.

5. The planet gearbox of claim 1, wherein the gearing surface of the outer race is a double helical gearing surface with the bias of each one of the two double helical gearing surfaces of the outer race being disposed nonparallel with the other one of the two double helical gearing surfaces of the outer race.

6. The planet gearbox of claim 1, further comprising for each respective track a respective roller cage disposed between the inner race and the outer race and configured to maintain in each respective track, a respective separation between each respective cylindrical roller in each pair of adjacent cylindrical rollers in that respective track, wherein each respective track is defined by a pair of guiderails, which are spaced apart from each other in the axial direction and extend circumferentially around the inner race and provide respective guiding surfaces to each respective roller cage.

7. The planet gearbox of claim 6, wherein each respective roller cage defines a circumferential row, each circumferential row of the respective roller cage being disposed above a respective track of the inner race, each circumferential row defining a plurality of generally cylindrical openings, each generally cylindrical opening defining a major axis in the axial direction and a minor axis in the circumferential direction, the openings in each row being spaced equidistantly apart circumferentially around the respective roller cage with the number of openings in each row being equal to the number of cylindrical rollers disposed in the respective track disposed beneath the respective row of the respective roller cage, wherein each respective cylindrical roller is disposed with its cylindrical outer surface extending through a respective opening defined by the respective roller cage.

8. The planet gearbox of claim 1, wherein each respective track extends circumferentially around the outer surface of the inner race, each of the pair of tracks being separated in the axial direction from the other of the pair of tracks, each of the pair of tracks being disposed parallel in the circumferential direction with respect to the other of the pair of tracks, each of the pair of tracks defining a raceway surface extending circumferentially and concentrically with respect to the inner cylindrical surface of the inner race and contacting a portion of each of the cylindrical outer surfaces of the cylindrical rollers disposed in the respective track, each of the pair of tracks defining a pair of radially extending sidewalls that are spaced apart in the axial direction from each other.

9. The planet gearbox of claim 1, wherein the inner cylindrical surface of the inner race is press-fitted to the cylindrical outer surface of the support pin.

10. The planet gearbox of claim 1, wherein each of the cylindrical rollers is formed of ceramic material.

11. A gas turbine engine comprising:

a fan including a plurality of blades extending radially from a hub and rotatable about a first axis of rotation defined centrally through the hub;

a compressor section disposed downstream from the fan and including one or more compressors;

a turbine section located downstream of the compressor section, the turbine section including one or more turbines;

a rotatable input shaft mechanically coupling at least one of the one or more compressors of the compressor section to rotate in unison with at least one of the one or more turbines of the turbine section;

an epicyclic gearing arrangement that has only a single input and a single output and that includes a carrier, a sun gear rotatable about a second axis of rotation that is parallel to the first axis of rotation, a ring gear disposed circumferentially around the sun gear, at least one planet gearbox that is carried by the carrier and houses a planet gear rotatable with respect to the carrier about a second axis of rotation that is parallel to the first axis of rotation, the at least one planet gear meshes with both the sun gear and the ring gear; and

an engine envelope surrounding the fan, the compressors, the turbines and the epicyclic gearing arrangement, wherein only one of the ring gear and the carrier is non-rotatably coupled to the engine envelope; and

the planet gearbox further including;

a support pin fixed to the carrier and defining a cylindrical outer surface that is equidistant from a central axis that extends in an axial direction,

an inner race defining an inner cylindrical surface that is non-rotatably connected to the cylindrical outer surface of the support pin, the inner race defining an outer surface that defines a at least one track that is configured to receive and rotatably guide therein a respective plurality of cylindrical rollers,

an outer race defining an inner cylindrical surface and an outer cylindrical surface that defines a gearing surface of the planet gear and that is configured to mesh with both the sun gear and the ring gear,

a plurality of cylindrical rollers wherein the individual cylindrical rollers being distributed between each track of the inner race, each cylindrical roller being free to rotate about a third axis of rotation that is parallel to the second axis of rotation, each cylindrical roller defining a cylindrical outer surface contacting both the inner race and the inner cylindrical surface of the outer race, each cylindrical roller defining a length in the direction parallel to the third axis of rotation and wherein the ratio of each cylindrical roller'"'"'s length to each cylindrical roller'"'"'s diameter is greater than one.

12. The gas turbine engine of claim 11, wherein the one or more compressors of the compressor section includes a low pressure compressor, wherein the one or more turbines of the turbine section includes a low pressure turbine, and wherein the shaft is a low pressure shaft mechanically coupling the low pressure compressor to the low pressure turbine.

13. The planet gearbox of claim 11, wherein the ratio of each cylindrical roller'"'"'s length to each cylindrical roller'"'"'s diameter is greater than 1.3.

14. The planet gearbox of claim 11, wherein each cylindrical roller has a length-to-diameter ratio that falls within the range from 1.3 to 1.8, inclusive.

15. The planet gearbox of claim 11, wherein at least a central section of the cylindrical outer surface of each cylindrical roller is disposed uniformly equidistant from the axis of rotation along a central section of the axial length of the cylindrical roller.

16. The planet gearbox of claim 11, wherein the gearing surface of each cylindrical outer race is a double helical gearing surface with the bias of each one of the two double helical gearing surfaces of the outer race being disposed nonparallel with the other one of the two double helical gearing surfaces of the outer race.

17. The planet gearbox of claim 11, further comprising a respective roller cage disposed between the inner race and the outer race and configured to maintain in each respective track, a respective separation in the circumferential direction between each respective cylindrical roller in each pair of adjacent cylindrical rollers in that respective track, wherein each respective track is defined by a pair of guiderails, which are spaced apart from each other in the axial direction and extend circumferentially around the inner race and provide respective guiding surfaces to each respective roller cage.

18. The planet gearbox of claim 17, wherein the roller cage defines a first circumferential row and a second circumferential row separated in the axial direction from the first circumferential row, each circumferential row of the roller cage being disposed above a respective track of the pair of tracks of the inner race, each circumferential row defining a plurality of generally cylindrical openings, each generally cylindrical opening defining a major axis in the axial direction and a minor axis in the circumferential direction, the openings in each row being spaced equidistantly apart circumferentially around the cage with the number of openings in each row being equal to the number of cylindrical rollers disposed in the respective one of the pair of tracks disposed beneath the respective row of the roller cage, wherein each respective cylindrical roller is disposed with its cylindrical surface extending through a respective opening defined by the roller cage.

19. The planet gearbox of claim 11, wherein the outer surface of the inner race is concentric with the inner cylindrical surface of the inner race, each respective track extending circumferentially around the outer surface of the inner race, each respective track being separated in the axial direction from any other respective track, each respective track being disposed parallel in the circumferential direction with respect to any other respective track.

20. The planet gearbox of claim 11, wherein the inner cylindrical surface of the inner race is press-fitted to the cylindrical outer surface of the support pin.