Drive gearbox on a turbomachine, consisting of a drive train with gear lines extending into non-parallel planes

Patent metadata

Field	Value
Publication number	US-9803556-B2
Application number	US-201314423801-A
Country	US
Kind code	B2
Filing date	Sep 3, 2013
Priority date	Sep 3, 2012
Publication date	Oct 31, 2017
Grant date	Oct 31, 2017

Abstract

A gearbox to be mounted on a turbomachine and driven by a radial drive shaft of the latter. The gearbox has a three-dimensional or sinuous shape, which can house a large quantity of equipment to be driven, without occupying a large amount of space in any dimension, since the gearbox remains close to the turbomachine and the equipment can be distributed over a large surface. The drive train of gears successively extends into several non-parallel planes and comprises an axial branch on the turbomachine and a branch forming an arc of circle around the turbomachine.

First claim

The invention claimed is:

1. A gearbox to be fixed to a turbomachine in order to drive at least one piece of equipment annexed to the turbomachine, comprising a casing, a drive train internal to the casing and comprising a series of gears, as well as a drive member intended to mesh with a transmission shaft of the turbomachine, with the casing comprising fastening points to the turbomachine and to the equipment, wherein the drive train comprises at least two gear lines located in non-parallel planes and connected together by a junction gear to a junction interface, comprised of a pair of gear wheels with non-parallel axes, of which, at least one end line housed in an end casing branch that has a main extension in a substantially axial direction of the turbomachine when the box is fixed to the turbomachine, and another line, housed in an intermediate casing branch, the intermediate casing branch being curved in a portion of a circle, substantially perpendicular to the end branch and which surrounds a portion of circumference of the turbomachine when the box is fixed to the turbomachine, wherein said another line belongs to an essential transversal plane of the turbomachine.

2. The gearbox according to claim 1 , comprising two said end lines, that have directions of extension that are substantially parallel between them and substantially perpendicular to said other branch.

3. The gearbox according to claim 2 , wherein the end lines extend to diametrically opposite generatrices of the turbomachine.

4. The gearbox as claimed in claim 1 , wherein the drive train is continuous and comprises a gear wheel meshing with a drive pinion that belongs to the transmission shaft, with the drive pinion being adjacent to the drive train.

5. The gearbox as claimed in claim 4 , wherein the drive pinion belongs to the drive train.

6. The gearbox as claimed in claim 1 , wherein the junction gears with non-parallel axes are comprised of conical pinions that are coaxial with other gear wheels of the drive train.

7. A gearbox to be fixed to a turbomachine in order to drive at least one piece of equipment annexed to the turbomachine, comprising a casing, a drive train internal to the casing and comprising a series of gears, as well as a drive member intended to mesh with a transmission shaft of the turbomachine, with the casing comprising fastening points to the turbomachine and to the equipment, wherein the drive train comprises at least two gear lines located in non-parallel planes and connected together by a junction gear to a junction interface, comprised of a pair of gear wheels with non-parallel axes, of which, at least one end line housed in an end casing branch that has a main extension in a substantially axial direction of the turbomachine when the box is fixed to the turbomachine, and another line, housed in an intermediate casing branch, the intermediate casing branch being curved, substantially perpendicular to the end branch and which surrounds a portion of circumference of the turbomachine when the box is fixed to the turbomachine,
wherein said another line belongs to an essential transversal plane of the turbomachine, and
wherein the end lines extend to diametrically opposite generatrices of the turbomachine.

8. The gearbox as claimed in claim 7 , wherein the drive train is continuous and comprises a gear wheel meshing with a drive pinion that belongs to the transmission shaft, with the drive pinion being adjacent to the drive train.

9. The gearbox as claimed in claim 8 , wherein the drive pinion belongs to the drive train.

10. The gearbox as claimed in claim 7 , wherein the junction gears with non-parallel axes are comprised of conical pinions that are coaxial with other gear wheels of the drive train.

Assignees

• Snecma
• Hispano Suiza Sa

Inventors

• Peltier Jordane
• Armange Frantz
• Demoulin Lambert Olivier Marie
• Garassino Alain Pierre
• Llamas Castro Nuria
• Prunera-Usach Stephane
• Waissi Bellal

Classifications

• Y10T74/1966

  Intersecting axes · CPC title

• F16H1/203

  with non-parallel axes (F16H1/22 takes precedence) · CPC title

• F02C7/32 Primary

  Arrangement, mounting, or driving, of auxiliaries · CPC title

• F05D2260/4031

  as in toothed gearing · CPC title

• F05D2250/38

  angled, e.g. sweep angle · CPC title