Pin for planetary gear system

• US 8,550,955 B2
• Filed: 08/16/2011
• Issued: 10/08/2013
• Est. Priority Date: 08/16/2011
• Status: Active Grant

• Current Assignee: GE Infrastructure Technology, LLC (General Electric Company)
• Original Assignee: General Electric Company
• Inventors: Erno, Daniel Jason, Hallman, Darren Lee, Lopez, Fulton Jose
• Primary Examiner(s): LEWIS, TISHA D
• Application Number:
  US13/210,761
• Publication Number:
  US 20120028755A1
• Time in Patent Office: 784 Days
• Field of Search: 475/331, 475/346, 475/347
• US Class Current: 475/331
• CPC Class Codes: F03D 15/00 Transmission of mechanical power
• CPC Class Codes: F03D 15/10 using gearing not limited to rotary motion, e.g. with oscillating or reciprocating members
• CPC Class Codes: F05B 2260/30 Retaining components in desired mutual position
• CPC Class Codes: F05B 2260/40311 of the epicyclic, planetary or differential type
• CPC Class Codes: F16H 1/2836 by allowing limited movement of the planets relative to the planet carrier or by using free floating planets
• CPC Class Codes: F16H 1/48 Special means compensating for misalignment of axes , e.g. for equalising distribution of load on the face width of the teeth in combination with distribution of load on the planet-wheels F16H1/2809
• CPC Class Codes: F16H 57/082 Planet carriers
• CPC Class Codes: Y02E 10/72 Wind turbines with rotation axis in wind direction

Abstract

A pin for coupling a planet gear to a carrier in a planetary gear system is disclosed. The pin includes a first end, a second end, and an outer surface extending between the first end and the second end. In some embodiments, the pin further includes means for modifying the compliance of the pin at an interface between the pin and the carrier. In other embodiments, the pin further include a compliance feature defined in the outer surface, the compliance feature allowing greater compliance of the pin in the tangential direction than in the radial direction.

Claims

1. A pin for coupling a planet gear to a carrier in a planetary gear system, the pin comprising:

a first end;

a second end;

an outer surface extending between the first end and the second end, wherein the outer surface comprises a first end surface extending from the first end and an intermediate surface extending from the first end surface, the first end surface configured for interfacing with the carrier;

means for modifying the compliance of the pin at an interface between the pin and the carrier; and

a closed bore hole extending through the first end surface generally transverse to a central planet axis of the pin.

2. The pin of claim 1, wherein the outer surface further comprises a second end surface extending between the intermediate surface and the second end, the second end surface configured for interfacing with the carrier.

3. The pin of claim 1, wherein the means comprises a channel defined in the first end surface, the channel extending annularly about at least a portion of a periphery of the first end surface.

4. The pin of claim 3, further comprising a plurality of channels.

5. The pin of claim 3, wherein the channel is open.

6. The pin of claim 3, wherein the channel is closed.

7. The pin of claim 1, wherein the means comprises the first end surface having a reduced cross-sectional profile through at least a portion of an axial length of the first end surface.

8. The pin of claim 7, wherein the first end surface tapers throughout at least a portion of the reduced cross-sectional profile.

9. The pin of claim 1, wherein the pin further defines a bore hole, the bore hole extending from the first end generally along a central planet axis and at least partially through the pin.

10. The pin of claim 1, wherein the means allows greater compliance of the pin in the tangential direction than in the radial direction.

11. A pin for coupling a planet gear to a carrier in a planetary gear system, the pin comprising:

a first end;

a second end;

an outer surface extending between the first end and the second end, wherein the outer surface comprises a first end surface extending from the first end and an intermediate surface extending from the first end surface, the first end surface configured for interfacing with the carrier; and

,

a compliance feature defined in the first end surface, the compliance feature allowing greater compliance of the pin in the tangential direction than in the radial direction, wherein the compliance feature comprises the outer surface having a reduced cross-sectional profile through at least a portion of an axial length of the outer surface.

12. The pin of claim 11, wherein the compliance feature comprises a channel, the channel extending annularly about at least a portion of a periphery of the outer surface.

13. The pin of claim 12, further comprising a plurality of channels.

14. The pin of claim 11, wherein the outer surface tapers throughout at least a portion of the reduced cross-sectional profile.

15. The pin of claim 11, wherein the pin further defines a bore hole, the bore hole extending from the first end generally along a central planet axis and at least partially through the pin.

16. The pin of claim 11, wherein the pin further defines a bore hole, the bore hole extending through the outer surface generally transverse to a central planet axis.

17. A pin for coupling a planet gear to a carrier in a planetary gear system, the pin comprising:

a first end;

a second end;

an outer surface extending between the first end and the second end, the outer surface comprising a first end surface extending from the first end and an intermediate surface extending from the first end surface, the first end surface configured for interfacing with the carrier;

means for modifying the compliance of the pin at an interface between the pin and the carrier, the means comprising an open channel defined in the first end surface, the channel extending annularly about at least a portion of an outer periphery of the first end surface.