APPARATUS AND SYSTEM FOR THIN RIM PLANET GEAR FOR AIRCRAFT ENGINE POWER GEARBOX

• US 20170191548A1
• Filed: 12/30/2015
• Published: 07/06/2017
• Est. Priority Date: 12/30/2015
• Status: Active Application

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Hallman, Darren Lee, Ligata, Haris, Hasting, William Howard, Fang, Ning, van der Merwe, Gert Johannes, Rhoads, Mark Alan, Ertas, Bugra Han, Bradley, Donald Albert, Fisher, Kenneth Lee
• Application Number:
  US14/984,472
• Publication Number:
  US 20170191548A1
• Time in Patent Office: Days
• 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: F02K 3/06 with front fan
• CPC Class Codes: F05D 2260/40311 of the epicyclical, planetary or differential type
• CPC Class Codes: F16H 57/08 of gearings with members having orbital motion

Abstract

A planet gear includes an annular planet gear ring including an annular planet gear rim. The annular planet gear rim has an inner radius and an outer radius. The inner radius and the outer radius define a rim thickness therebetween. The annular planet gear rim further has a bending stress neutral axis. The bending stress neutral axis radius and the rim thickness define a ratio including values in a range from and including about 3 to and including about 10.

Claims

1. A planet gear comprising:

an annular planet gear ring comprising an annular planet gear rim, said annular planet gear rim having an inner radius and an outer radius, the inner radius and the outer radius defining a rim thickness therebetween, said annular planet gear rim further having a bending stress neutral axis, the bending stress neutral axis radius and the rim thickness define a ratio including values in a range from and including about 3 to and including about 10.

2. The planet gear of claim 1 further comprising a bearing, wherein said annular planetary gear ring disposed circumferentially about said bearing.

3. The planet gear of claim 2, wherein said bearing comprises a rolling element bearing.

4. The planet gear of claim 3, wherein said rolling element bearing comprises an annular inner bearing ring and a plurality of rolling elements, said plurality of rolling elements disposed circumferentially about said annular inner bearing ring, said annular planetary gear ring disposed circumferentially about said plurality of rolling elements.

5. A gear assembly comprising:

a sun gear;

a ring gear; and

a plurality of planet gears coupled to said ring gear and said sun gear, wherein each planet gear of said plurality of planet gears comprising an annular planet gear ring comprising an annular planet gear rim, said annular planet gear rim having an inner radius and an outer radius, the inner radius and the outer radius defining a rim thickness therebetween, said annular planet gear rim further having a bending stress neutral axis, the bending stress neutral axis radius and the rim thickness define a ratio including values in a range from and including about 3 to and including about 10.

6. The gear assembly of claim 5 further comprising a bearing, wherein said annular planetary gear ring disposed circumferentially about said bearing.

7. The gear assembly of claim 6, wherein said bearing comprises a rolling element bearing.

8. The gear assembly of claim 7, wherein said rolling element bearing comprises an annular inner bearing ring and a plurality of rolling elements, said plurality of rolling elements disposed circumferentially about said annular inner bearing ring, said annular planetary gear ring disposed circumferentially about said plurality of rolling elements.

9. The gear assembly of claim 8, wherein said sun gear, said plurality of planet gears, said ring gear, and said carrier configured in a planetary configuration.

10. The gear assembly of claim 8, wherein said sun gear, said plurality of planet gears, said ring gear, and said carrier configured in a star configuration.

11. The gear assembly of claim 8, wherein said sun gear, said plurality of planet gears, said ring gear, and said carrier configured in a solar configuration.

12. The gear assembly of claim 11 further comprising a power shaft coupled to said carrier.

13. The gear assembly of claim 11 further comprising a power shaft coupled to said ring gear.

14. A turbomachine comprising:

a power shaft and a gear assembly, said power shaft rotationally coupled to said gear assembly;

said gear assembly comprising;

a sun gear;

a ring gear; and

a plurality of planet gears coupled to said ring gear and said sun gear, wherein each planet gear of said plurality of planet gears comprising an annular planet gear ring comprising an annular planet gear rim, said annular planet gear rim having an inner radius and an outer radius, the inner radius and the outer radius defining a rim thickness therebetween, said annular planet gear rim further having a bending stress neutral axis, wherein the bending stress neutral axis radius and the rim thickness define a ratio including values in a range from and including about 3 to and including about 10.

15. The turbomachine of claim 14 further comprising a bearing, wherein said annular planetary gear ring disposed circumferentially about said bearing.

16. The turbomachine of claim 15, wherein said bearing comprises a rolling element bearing.

17. The turbomachine of claim 16, wherein said rolling element bearing comprises an annular inner bearing ring and a plurality of rolling elements, said plurality of rolling elements disposed circumferentially about said annular inner bearing ring, said annular planetary gear ring disposed circumferentially about said plurality of rolling elements.

18. The turbomachine of claim 17, wherein said sun gear, said plurality of planet gears, said ring gear, and said carrier configured in a planetary configuration.

19. The turbomachine of claim 17, wherein said sun gear, said plurality of planet gears, said ring gear, and said carrier configured in a star configuration.

20. The turbomachine of claim 17, wherein said sun gear, said plurality of planet gears, said ring gear, and said carrier configured in a solar configuration.