IP Library Granted Patent US 9,803,556
Granted Patent B2
US 9,803,556 · App. 14/423,801 · Granted Oct 31, 2017

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

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Quick Facts
Patent No.
US 9,803,556
App. No.
14/423,801
Granted
Oct 31, 2017
Kind
B2
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.

Claims (12)

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.

Assignments (5)
CORRECTIVE ASSIGNMENT TO CORRECT THE INCORRECT NUMBERS 14766300 AND 14402794 PREVIOUSLY RECORDED AT REEL: 045791 FRAME: 0361. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 26, 2018
From: HISPANO-SUIZA
To: SAFRAN TRANSMISSION SYSTEMS
Reel/Frame 046946/0458 →
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
CHANGE OF NAME Recorded May 13, 2018
From: HISPANO-SUIZA
To: SAFRAN TRANSMISSION SYSTEMS
Reel/Frame 045791/0361 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 25, 2015
From: PELTIER, JORDANE; ARMANGE, FRANTZ; DEMOULIN, LAMBERT OLIVIER MARIE; GARASSINO, ALAIN PIERRE; LLAMAS CASTRO, NURIA; PRUNERA-USACH, STEPHANE; WAISSI, BELLAL
To: SNECMA; HISPANO SUIZA
Reel/Frame 035026/0361 →