Planetary gear sets for power transmissions

Patent metadata

Field	Value
Publication number	US-10233997-B2
Application number	US-201615221179-A
Country	US
Kind code	B2
Filing date	Jul 27, 2016
Priority date	Jul 29, 2015
Publication date	Mar 19, 2019
Grant date	Mar 19, 2019

Abstract

A planetary gear arrangement includes a planet carrier assembly defining a sun gear rotation axis for rotatably supporting a plurality of planetary gears about the sun gear rotation axis and a positioning element coupling a first of the planetary gears to the planet carrier. The planetary gear is movable between first and second positions for displacing a rotation axis of the first of the planetary gears relative to the sun gear rotation axis to change load share among the plurality of planetary gears.

First claim

What is claimed is:

1. A planetary gear carrier assembly to support first and second planetary gears, the planetary gear carrier assembly, comprising:
a planet carrier defining a sun gear rotation axis and having apertures to rotatably support the first and second planetary gears for rotation about planetary gear rotation axis, wherein at least one of the first and second planetary gear has first and second positions, the second position being offset from the first position relative to the sun gear rotation axis; and
an actively controlled positioning element coupled to the at least one of the first and second planetary gears and configured to move the at least one of the first and second planetary gears between the first position and the second position for to reduce a load share imbalance between the first and second planetary gears intermeshed between a sun gear and a ring gear of the planetary gear set.

2. A planetary gear carrier assembly set as recited in claim 1 , wherein the second position has a radial offset relative to the sun gear rotation axis that is different than a radial offset of the first position relative to the sun gear rotation axis.

3. A planetary gear carrier assembly as recited in claim 1 , wherein the second position has a circumferential offset about the sun gear rotation axis that is different than a circumferential offset of the first position relative to the sun gear rotation axis.

4. A planetary gear carrier assembly as recited in claim 1 , wherein the second position is offset both radially and circumferentially from the first position relative to the sun gear rotation axis.

5. A planetary gear carrier assembly as recited in claim 1 , wherein the positioning element comprises (a) a first eccentric coupling rotatably seated in the planet carrier, and (b) a second eccentric coupling rotatably seated in the first eccentric coupling.

6. A planetary gear carrier assembly as recited in claim 1 , wherein the positioning element comprises a single eccentric coupling seated in the planet carrier.

7. A planetary gear carrier assembly as recited in claim 1 , wherein the positioning element comprises an eccentric bearing race.

8. A planetary gear carrier assembly as recited in claim 1 , wherein the positioning element comprises an eccentric bearing liner.

9. A planetary gear carrier assembly as recited in claim 1 , further including a linear actuator operably connected to the positioning element to drive the eccentric coupling between the first and second positions.

10. A rotorcraft transmission having a planetary gear carrier assembly as recited in claim 1 .

11. A method of adjusting a planetary gear arrangement, comprising:
determining load share among a plurality of planetary gears intermeshed between a sun gear and a ring gear;
calculating a position change for a first planetary gear relative to a rotation axis of the sun gear based on the load share among the plurality of planetary gears; and
reducing load share imbalance among the plurality of planetary gears by changing position of the first planetary gear relative to the rotation axis of the sun gear.

12. A method as recited in claim 11 , wherein reducing load share imbalance includes displacing the planetary gear radially relative to the rotation axis of the sun gear.

13. A method as recited in claim 11 , wherein reducing load share imbalance includes displacing the planetary gear circumferentially relative to the rotation axis of the sun gear.

14. A method as recited in claim 11 , wherein changing position of the first of the plurality or planetary gears includes changing the position real-time, while transferring rotational power through the planetary gear set.

15. A method as recited in claim 11 , wherein determining load share among the plurality of planetary gears includes determining load share using data indicative of at least one of force, acceleration, backlash, noise, and temperature within the planetary gear set.

Assignees

• Sikorsky Aircraft Corp

Inventors

• Howard Bertrand J
• Binney David A
• Silva Vinicius

Classifications

• F16H1/2836 Primary

  by allowing limited movement of the planet gears relative to the planet carrier or by using free floating planet gears · CPC title

• F16H57/082

  Planet carriers · CPC title

• F16H2057/085

  Bearings for orbital gears · CPC title

• F16H1/2863

  Arrangements for adjusting or for taking-up backlash · CPC title