Bearing arrangement for turbine engine geartrain

Patent metadata

Field	Value
Publication number	US-12331683-B2
Application number	US-202318375102-A
Country	US
Kind code	B2
Filing date	Sep 29, 2023
Priority date	Sep 29, 2023
Publication date	Jun 17, 2025
Grant date	Jun 17, 2025

Abstract

An engine assembly is provided that includes a sun gear, a ring gear, a plurality of intermediate gears, a carrier, a first rotating structure, a second rotating structure and a first bearing. The ring gear is rotatable about an axis and circumscribes the sun gear. The intermediate gears are arranged circumferentially about the axis in an array. Each of the intermediate gears is radially between and meshed with the sun gear and the ring gear. The carrier is rotatable about the axis. Each of the intermediate gears is rotatably mounted to the carrier. The first rotating structure is configured as or otherwise includes the carrier. The second rotating structure is configured as or otherwise includes the ring gear. The first bearing is radially between and engaged with the first rotating structure and the second rotating structure.

First claim

What is claimed is:

1. An engine assembly, comprising:
a sun gear;
a ring gear rotatable about an axis and circumscribing the sun gear;
a plurality of intermediate gears arranged circumferentially about the axis in an array, each of the plurality of intermediate gears radially between and meshed with the sun gear and the ring gear;
a carrier rotatable about the axis, each of the plurality of intermediate gears rotatably mounted to the carrier;
a first rotating structure comprising the carrier;
a second rotating structure comprising the ring gear;
a first bearing radially between and engaged with the first rotating structure and the second rotating structure;
a stationary structure circumscribing the first rotating structure; and
a second bearing radially between and engaged with the first rotating structure and the stationary structure;
wherein the first bearing and the second bearing are arranged on opposing axial sides of the array of the plurality of intermediate gears.

2. The engine assembly of claim 1 , wherein
the first bearing circumscribes the first rotating structure; and
the second rotating structure circumscribes the first bearing.

3. The engine assembly of claim 1 , wherein the sun gear is rotatable about the axis.

4. The engine assembly of claim 1 , further comprising:
a first propulsor rotor;
a geartrain including the sun gear, the ring gear, the plurality of intermediate gears and the carrier; and
a rotating assembly comprising a turbine rotor, the rotating assembly configured to drive the first propulsor rotor through the geartrain.

5. The engine assembly of claim 4 , further comprising:
a second propulsor rotor;
the rotating assembly configured to drive rotation of the second propulsor rotor.

6. The engine assembly of claim 1 , wherein the first bearing comprises a rolling element bearing.

7. The engine assembly of claim 1 , further comprising a lock device configured to lock rotation of the first rotating structure or the second rotating structure about the axis.

8. The engine assembly of claim 1 , further comprising a brake configured to brake rotation of the first rotating structure or the second rotating structure about the axis.

9. An engine assembly, comprising:
a sun gear;
a ring gear rotatable about an axis and circumscribing the sun gear;
a plurality of intermediate gears arranged circumferentially about the axis in an array, each of the plurality of intermediate gears radially between and meshed with the sun gear and the ring gear;
a carrier rotatable about the axis, each of the plurality of intermediate gears rotatably mounted to the carrier;
a first rotating structure comprising the carrier;
a second rotating structure comprising the ring gear;
a first bearing radially between and engaged with the first rotating structure and the second rotating structure, wherein the first rotating structure is radially inboard of the first bearing and the second rotating structure is radially outboard of the first bearing;
a stationary structure circumscribing the first rotating structure; and
a second bearing radially between and engaged with the first rotating structure and the stationary structure.

10. An engine assembly, comprising:
a sun gear;
a ring gear rotatable about an axis and circumscribing the sun gear;
a plurality of intermediate gears arranged circumferentially about the axis in an array, each of the plurality of intermediate gears radially between and meshed with the sun gear and the ring gear;
a carrier rotatable about the axis, each of the plurality of intermediate gears rotatably mounted to the carrier;
a first rotating structure comprising the carrier;
a second rotating structure comprising the ring gear;
a first bearing radially between and engaged with the first rotating structure and the second rotating structure;
a second sun gear;
a second ring gear circumscribing the second sun gear;
a plurality of second intermediate gears arranged circumferentially about the axis in an array, each of the plurality of second intermediate gears radially between and meshed with the second sun gear and the second ring gear; and
a second carrier rotatable about the axis, each of the plurality of second intermediate gears rotatably mounted to the second carrier;
the second rotating structure further comprising the second carrier.

11. The engine assembly of claim 10 , wherein the second sun gear is rotatable about the axis.

12. The engine assembly of claim 10 , wherein the second ring gear is rotatable about the axis.

13. The engine assembly of claim 10 , further comprising:
a geartrain including the sun gear, the ring gear, the plurality of intermediate gears, the carrier, the second sun gear, the second ring gear, the plurality of second intermediate gears and the second carrier; and
a rotating assembly comprising a turbine rotor, the rotating assembly coupled to the geartrain through at least one of the sun gear or the second sun gear.

14. The engine assembly of claim 13 , further comprising:
a first propulsor rotor coupled to the geartrain through the second ring gear;
the rotating assembly configured to drive the first propulsor rotor through the geartrain.

15. The engine assembly of claim 10 , wherein the first bearing is disposed axially between the array of the plurality of intermediate gears and the array of the plurality of second intermediate gears.

Assignees

• Rtx Corp

Inventors

• Hanrahan Paul R

Classifications

• F16H2057/085

  Bearings for orbital gears · CPC title

• F16H57/08

  of gearings with members having orbital motion · CPC title

• F16H1/28

  with gears having orbital motion · CPC title

• F02C7/36

  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 title

• F16H2057/087

  Arrangement and support of friction devices in planetary gearings, e.g. support of clutch drums, stacked arrangements of friction devices · CPC title