Gearbox assembly

Patent metadata

Field	Value
Publication number	US-12007011-B2
Application number	US-202318165590-A
Country	US
Kind code	B2
Filing date	Feb 7, 2023
Priority date	Aug 12, 2022
Publication date	Jun 11, 2024
Grant date	Jun 11, 2024

Abstract

A gearbox assembly includes a first gear and a second gear. The first gear includes a plurality of first gear teeth. The second gear includes a plurality of second gear teeth. The plurality of first gear teeth and the plurality of second gear teeth mesh with each other as the first gear and the second gear rotate. A profile shape of at least one first gear tooth of the first gear is characterized by a total profile modification between 66 micrometers and 120 micrometers.

First claim

The invention claimed is:

1. A gearbox assembly comprising:
a first gear comprising a plurality of first gear teeth; and
a second gear comprising a plurality of second gear teeth, the plurality of first gear teeth and the plurality of second gear teeth meshing with each other as the first gear and the second gear rotate,
wherein a profile shape of at least one first gear tooth of the first gear is characterized by a total profile modification between 66 micrometers and 120 micrometers, wherein the total profile modification is a function of a tangential force on the at least one first gear tooth, a stiffness per unit length of the at least one first gear tooth, a mesh contact ratio of the first gear and the second gear, and a unit length of contact between the at least one first gear tooth and a respective second gear tooth.

2. The gearbox assembly of claim 1 , wherein the first gear is a sun gear and the second gear is a plurality of planet gears.

3. The gearbox assembly of claim 1 , wherein the total profile modification is between 68 micrometers and 90 micrometers.

4. The gearbox assembly of claim 1 , wherein the total profile modification is greater than or equal to

F
t

(

3.2

K
max

⁢
ε
⁢
γ
⁢

X
0

)

wherein F t is the tangential force in Newtons, K max is the stiffness per unit length in Newtons per millimeters micrometers, εγ is the mesh contact ratio, and X 0 is the unit length of contact in millimeters.

5. The gearbox assembly of claim 4 , wherein F t is between 42,000 Newtons and 70,000 Newtons.

6. The gearbox assembly of claim 4 , wherein F t is between 47,000 Newtons and 51,000 Newtons.

7. The gearbox assembly of claim 4 , wherein K max is between 13 Newtons per millimeter micrometer and 19 Newtons per millimeter micrometer.

8. The gearbox assembly of claim 4 , wherein K max is between 15 Newtons per millimeter micrometer and 17 Newtons per millimeter micrometer.

9. The gearbox assembly of claim 4 , wherein εγ is between 2.3 and 5.

10. The gearbox assembly of claim 4 , wherein εγ is between 2.6 and 4.2.

11. The gearbox assembly of claim 4 , wherein X 0 is between 2.5 millimeters and 5.5 millimeters.

12. The gearbox assembly of claim 4 , wherein X 0 is between 3.2 millimeters and 4.8 millimeters.

13. The gearbox assembly of claim 4 , wherein the gearbox assembly is coupled to a fan of a turbine engine, and F t is a function of a torque of the fan, a gear ratio of the gearbox assembly, a pitch diameter of the first gear, and a number of meshes of the first gear with the second gear.

14. A turbine engine comprising:
a fan including a fan rotor;
an engine core including a shaft assembly; and
a gearbox assembly comprising:
a first gear coupled to the shaft assembly of the engine core, the first gear comprising a plurality of first gear teeth; and
a second gear coupled to the fan rotor of the fan, the second gear comprising a plurality of second gear teeth, the plurality of first gear teeth and the plurality of second gear teeth meshing with each other as the first gear and the second gear rotate,
wherein a profile shape of at least one first gear tooth of the first gear is characterized by a total profile modification between 66 micrometers and 120 micrometers, wherein the total profile modification is a function of a tangential force on the at least one first gear tooth, a stiffness per unit length of the at least one first gear tooth, a mesh contact ratio of the first gear and the second gear, and a unit length of contact between the at least one first gear tooth and a respective second gear tooth.

15. The turbine engine of claim 14 , wherein the total profile modification is between 68 micrometers and 90 micrometers.

16. The turbine engine of claim 14 , wherein the total profile modification is greater than or equal to

F
t

(

3.2

K
max

⁢
ε
⁢
γ
⁢

X
0

)

wherein F t is the tangential force in Newtons, K max is the stiffness per unit length in Newtons per millimeters micrometers, εγ is the mesh contact ratio, and X 0 is the unit length of contact in millimeters.

17. The turbine engine of claim 16 , wherein F t is between 42,000 Newtons and 70,000 Newtons.

18. The turbine engine of claim 16 , wherein F t is between 47,000 Newtons and 51,000 Newtons.

Assignees

• Gen Electric
• Ge Avio Srl

Inventors

• Piazza Andrea
• Ganiger Ravindra Shankar

Classifications

• F16H55/0886

  with corrections along the width, e.g. flank width crowning for better load distribution · CPC title

• F16H57/02 Primary

  Gearboxes; Mounting gearing therein · CPC title

• F16H2057/02039

  Gearboxes for particular applications · CPC title

• F02K3/06

  with front fan · CPC title

• F05D2260/40311

  of the epicyclical, planetary or differential type · CPC title