IP Library Granted Patent US 9,664,117
Granted Patent B2
US 9,664,117 · App. 14/097,774 · Granted May 30, 2017

Guidance of turbine engine shafts

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Quick Facts
Patent No.
US 9,664,117
App. No.
14/097,774
Granted
May 30, 2017
Kind
B2
Abstract

A turbine engine including a power gear box shaft, a turbine shaft, a connecting part of annular shape by which one end of the power gear box shaft and one end of the turbine shaft are connected in a rotationally fixed manner, a structural housing, and a guide bearing for guiding the connecting part relative to the housing, is provided. The guide bearing is mounted between the connecting part and the housing and includes an external ring mounted on the housing, an internal ring mounted on the connecting part, and at least one rolling element configured to enable the external ring to roll around the internal ring. The guide bearing is configured to form a ball joint link enabling a relative angular displacement of its external ring with respect to its internal ring.

Claims (17)

1. A turbine engine comprising:

a power gear box shaft;

a turbine shaft driven by a turbine of the turbine engine;

a connecting part of annular shape by which only one end of the power gear box shaft and one end of the turbine shaft are connected in a rotationally fixed manner;

a structural housing; and

a guide bearing for guiding the connecting part relative to the housing, the guide bearing being mounted between the connecting part and the housing, and comprising

an external ring mounted on the housing,

an internal ring mounted on the connecting part, and

rolling elements configured to enable the external ring to roll around the internal ring,

wherein the guide bearing is configured to form a ball joint link enabling a relative angular displacement of the external ring with respect to the internal ring,

wherein the power gear box shaft and the turbine shaft are not directly connected to each other,

wherein the connecting part comprises a first plurality of upstream splines disposed at an upstream extremity and a second plurality of downstream splines disposed at a downstream extremity, the end of the power gear box shaft comprising a plurality of downstream splines complementary to the first plurality of upstream splines of the connecting part and the end of the turbine shaft comprising a plurality of upstream splines complementary to the second plurality of downstream splines of the connecting part,

wherein the upstream splines of the connecting part and the downstream splines of the power gear box shaft are located upstream of the rolling elements of the guide bearing, and

wherein the downstream splines of the connecting part and the upstream splines of the turbine shaft are located downstream of the rolling elements of the guide bearing.

2. The turbine engine according to claim 1 , wherein the rolling elements comprise an axial portion of at least partially rounded shape in order to enable an inclination of the internal ring with respect to the external ring.

3. The turbine engine according to claim 1 , wherein the guide bearing comprises first and second pluralities of balls disposed in first and second annular rows.

4. The turbine engine according to claim 1 , wherein at least one of the external ring and the internal ring includes a curved support zone for the rolling elements, such that the curved support zone extends axially from a first axial free end to a second axial free end of the external ring or the internal ring, so as to enable an inclination of the internal ring with respect to the external ring.

Assignments (3)
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 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 3, 2014
From: BELMONTE, OLIVIER; AUSTRUY, JULIEN MICHEL PATRICK CHRISTIAN; PERRIER, MATHIEU
To: SNECMA
Reel/Frame 032115/0372 →