Gear with optimized gear web shape

Patent metadata

Field	Value
Publication number	US-10072732-B2
Application number	US-201414547638-A
Country	US
Kind code	B2
Filing date	Nov 19, 2014
Priority date	Nov 19, 2014
Publication date	Sep 11, 2018
Grant date	Sep 11, 2018

Abstract

A gear comprises gear teeth. An annular web has the gear teeth on an external surface thereof and rotatable about a rotational axis of the gear. The web comprises a wall having at least a first axial surface and a second axial surface on the opposite side of the wall. The web defined by a first web section in which the first axial surface, in an inward direction, inclines away from a radial plane to which the rotational axis is normal, a second web section radially inward of the first web section, and in which the first axial surface, in the inward direction, inclines toward said radial plane.

First claim

The invention claimed is:

1. A gear comprising:
gear teeth, the gear teeth being non-parallel to a rotational axis of the gear, whereby a direction of a load received by the gear is oblique relative to a radial direction of the gear, the gear teeth located between radial planes to which the rotational axis is normal;
an annular web having the gear teeth on an external surface thereof and rotatable about the rotational axis of the gear, the web comprising a wall having at least a first axial surface and a second axial surface on the opposite side of the wall, the web defined by at least:
a first web section in which the first axial surface, in an inward direction, inclines away from the radial planes, the first axial surface being generally aligned with said direction of the load; and
a second web section radially inward of the first web section, and in which the first axial surface, in the inward direction, inclines toward said radial planes,
wherein a transition between the first web section and the second web section is axially spaced from the radial planes.

2. The gear according to claim 1 , wherein the web further comprises another web section between the first web section and the gear teeth, the other web section having a greater thickness in the axial direction than the first web section and the second web section.

3. The gear according to claim 2 , wherein the gear teeth are monolithically integral with the other web section.

4. The gear according to claim 1 , wherein the first surface and the second surface are smooth and continuous at least in the first web section and the second web section.

5. The gear according to claim 1 , wherein the first surface defines a curved concavity with the first web section and the second web section, an intersection between the first web section and the second web section being tangential to the radial plane.

6. The gear according to claim 1 , wherein, in the first web section, the second axial surface inclines away from the radial plane in an inward direction.

7. The gear according to claim 6 , wherein, in the second web section, the second axial surface inclines toward said radial plane in the inward direction.

8. The gear according to claim 7 , further comprising one of a shaft and a hub inward of the web, and a fillet at a junction between the second axial surface and the shaft or hub.

9. The gear according to claim 1 , wherein the gear teeth form a helical gear.

10. The gear according to claim 1 , further comprising one of a shaft and a hub inward of and connected to the second web section, a junction between the second web section and the shaft or hub being axially spaced from the radial planes.

11. A gear set comprising:
A first gear having external gear teeth; and
A second gear in operative meshing engagement with the first gear for transmission of rotational movement from one to another, whereby a load results on the second gear, the second gear comprising:
Gear teeth on an external surface thereof, the gear teeth being non-parallel to the rotational axis of the second gear, a direction of a load received by the second gear being oblique relative to a radial direction of the second gear, the gear teeth located between radial planes to which the rotational axis is normal;
A first web section inclining away, in an inward direction and a first axial direction, the first web section being generally aligned with said load; and
A second web section radially inward of the first web section and inclining in an axial direction opposite to the first axial direction in the inward direction;
Wherein a transition between the first web section and the second web section is axially spaced from the radial planes.

12. The gear set according to claim 11 , wherein the web further comprises another web section between the first web section and the gear teeth, the other web section having a greater thickness in the axial direction than the first web section and the second web section.

13. The gear set according to claim 12 , wherein the gear teeth are monolithically integral with the other web section.

14. The gear set according to claim 11 , wherein surfaces of the first web section and the second web section are smooth and continuous.

15. The gear set according to claim 11 , comprising a curved concavity defined with the first web section and the second web section, an intersection between the first web section and the second web section being tangential to the radial plane.

16. The gear set according to claim 11 , further comprising one of a shaft and a hub inward of the web, and a fillet at a junction between the second axial surface and the shaft or hub.

17. The gear set according to claim 11 , wherein the gear teeth form a helical gear.

18. The gear set according to claim 11 , wherein a rotational axis of the first gear is axially offset relative to the rotational axis of the second gear.

19. A gas turbine engine comprising a gear set according to claim 11 .

20. The gear set according to claim 11 , further comprising one of a shaft and a hub inward of and connected to the second web section, a junction between the second web section and the shaft or hub being axially spaced from the radial planes.

Assignees

• Pratt & Whitney Canada

Inventors

• Carrieres Alain

Classifications

• F01D25/164

  Flexible supports; Vibration damping means associated with the bearing · 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

• F05D2260/4031

  as in toothed gearing · CPC title

• F16H1/08 Primary

  the members having helical, herringbone, or like teeth · CPC title

• F16H55/17

  Toothed wheels (worm wheels F16H55/22; chain wheels F16H55/30) · CPC title