System and apparatus for supporting a planetary carrier within a gearbox

Patent metadata

Field	Value
Publication number	US-10221939-B2
Application number	US-201715434609-A
Country	US
Kind code	B2
Filing date	Feb 16, 2017
Priority date	Feb 16, 2016
Publication date	Mar 5, 2019
Grant date	Mar 5, 2019

Abstract

An apparatus and system for supporting a planetary carrier within an aircraft gearbox includes a retainer for engaging a rotor mast and for supporting the planetary carrier.

First claim

The invention claimed is:

1. An aircraft gearbox comprising:
a gearbox housing;
a planetary gear set disposed within the gearbox housing, the planetary gear set comprising:
a sun gear;
a ring gear;
a planetary carrier; and
a plurality of planet gears; and

a retainer configured to be coupled to a mast, the retainer comprising a flange portion, a surface configured to support the planetary carrier being located on the flange portion.

2. The aircraft gearbox according to claim 1 , wherein:
the planetary carrier comprises an overhung planetary carrier, having a plurality of downwardly-extending, cantilevered posts; and
each of the plurality of planet gears is rotatably mounted on one of the posts of the planetary carrier.

3. The aircraft gearbox according to claim 1 , wherein the ring gear is stationary.

4. The aircraft gearbox according to claim 1 , wherein the sun gear is configured to receive rotational energy from an input, and the planetary carrier is configured to transmit rotational energy to the mast.

5. The aircraft gearbox according to claim 4 , wherein the planetary carrier is configured to transmit rotational energy to the mast through a first set of splines provided on the planetary carrier and a second set of splines provided on the mast.

6. The aircraft gearbox according to claim 1 , wherein:
the sun gear, the planetary carrier, and the mast are all configured to rotate about a substantially common axis of rotation, the axis of rotation defining an axial direction; and
the surface configured to support the planetary carrier is configured to support the planetary carrier in the axial direction.

7. The aircraft gearbox according to claim 6 , wherein: the flange portion extends radially with respect to the axis of rotation.

8. The aircraft gearbox according to claim 1 , wherein the retainer is configured to be coupled to the mast through a threaded connection.

9. The aircraft gearbox according to claim 8 , wherein the retainer comprises external threads configured to mate with internal threads provided on the mast.

10. The aircraft gearbox according to claim 1 , wherein the surface configured to support the planetary carrier comprises a continuous circular surface.

11. A retainer for supporting a planetary carrier within a gearbox comprising:
a coupling feature adapted for coupling the retainer to a mast; and
a flange portion, a surface configured to support the planetary carrier being located on the flange portion.

12. The retainer according to claim 11 , wherein:
the planetary carrier is configured to rotate about an axis of rotation, the axis of rotation defining an axial direction; and
the surface configured to support the planetary carrier is configured to support the planetary carrier in the axial direction.

13. The retainer according to claim 12 , wherein the flange portion extends radially with respect to the axis of rotation.

14. The retainer according to claim 11 , wherein the coupling feature comprises a first thread feature configured to mate with a second thread feature provided on the mast.

15. The retainer according to claim 11 , wherein the coupling feature is configured to engage a groove provided on the mast.

16. The retainer according to claim 11 , wherein the surface configured to support the planetary carrier comprises a continuous circular surface.

17. An aircraft gearbox comprising:
a gearbox housing;
a planetary gear set disposed within the gearbox housing, the planetary gear set comprising:
a sun gear;
a ring gear;
a planetary carrier; and
a plurality of planet gears; and

a retainer configured to be coupled to a mast, the retainer comprising:
a surface configured to support the planetary carrier; and
external threads configured to mate with internal threads provided on the mast.

18. The aircraft gearbox according to claim 17 , wherein:
the planetary carrier comprises an overhung planetary carrier, having a plurality of downwardly-extending, cantilevered posts; and
each of the plurality of planet gears is rotatably mounted on one of the posts of the planetary carrier.

19. The aircraft gearbox according to claim 17 , wherein the ring gear is stationary.

20. The aircraft gearbox according to claim 17 , wherein the sun gear is configured to receive rotational energy from an input, and the planetary carrier is configured to transmit rotational energy to the mast.

21. The aircraft gearbox according to claim 20 , wherein the planetary carrier is configured to transmit rotational energy to the mast through a first set of splines provided on the planetary carrier and a second set of splines provided on the mast.

22. The aircraft gearbox according to claim 17 , wherein:
the sun gear, the planetary carrier, and the mast are all configured to rotate about a substantially common axis of rotation, the axis of rotation defining an axial direction; and
the surface configured to support the planetary carrier is configured to support the planetary carrier in the axial direction.

23. The aircraft gearbox according to claim 22 , wherein:
the retainer further comprises a flange portion extending radially with respect to the axis of rotation; and
the surface configured to support the planetary carrier is located on the flange portion.

24. The aircraft gearbox according to claim 17 , wherein the surface configured to support the planetary carrier comprises a continuous circular surface.

25. A retainer for supporting a planetary carrier within a gearbox comprising:
a surface configured to support the planetary carrier; and
external threads configured to mate with internal threads provided on a mast.

26. The retainer according to claim 25 , wherein:
the planetary carrier is configured to rotate about an axis of rotation, the axis of rotation defining an axial direction; and
the surface configured to support the planetary carrier is configured to support the planetary carrier in the axial direction.

27. The retainer according to claim 26 , further comprising a flange portion extending radially with respect to the axis of rotation, the surface configured to support the planetary carrier being located on the flange portion.

28. The retainer according to claim 25 , wherein the retainer comprises a flange portion, the surface configured to support the planetary carrier being located on the flange portion.

29. The retainer according to claim 25 , wherein the surface configured to support the planetary carrier comprises a continuous circular surface.

Assignees

• Bell Helicopter Textron Inc

Inventors

• Poster Scott

Classifications

• F16H57/082 Primary

  Planet carriers · CPC title

• B64D35/00

  Transmitting power from power plants to propellers or rotors; Arrangements of transmissions · CPC title

• F16H57/08

  of gearings with members having orbital motion · CPC title

• B64C27/12

  Rotor drives · CPC title