IP Library Granted Patent US 7,341,380
Granted Patent B2
US 7,341,380 · App. 11/183,767 · Granted Mar 11, 2008

Installation layout for two coaxial shaft lines

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Quick Facts
Patent No.
US 7,341,380
App. No.
11/183,767
Granted
Mar 11, 2008
Kind
B2
Abstract

In an assembly with two concentric shafts, the internal shaft projecting beyond the external shaft, a seal support sleeve placed between the shafts has a conical shape and bears on a spacer mounted on the external shaft between an assembly nut of the forward end of the external shaft and a bearing, so that the nut is accessible to be unscrewed through the space between the two shafts, thus enabling the external shaft to be disassembled. The invention may be applicable to front bearings of gas turbine high pressure shafts and makes it possible to disassemble the high pressure body from the rear, without needing to disassemble equipment, such as a fan on the front of the machine, or hindering the installation of a gear.

Claims (13)

1. An assembly comprising:

an internal shaft and an external shaft, said internal and external shafts being coaxial and a forward part of the internal shaft projecting beyond a forward end of the external shaft;

a sleeve surrounding the shafts and holding first and second seals, the first seal sealing a portion of the internal shaft and the second seal sealing a portion of the external shaft;

a first bearing supporting the forward end of the external shaft;

a nut screwed around said forward end for providing a stop for said first bearing; and

a spacer having a first part adjusted around the external shaft and retained between the nut and the first bearing, and a second part extending around the nut on which the second seal sealing with the external shaft rubs.

2. The assembly according to claim 1 , further comprising:

a gear arranged under the nut, the spacer and the sleeve in a direction substantially perpendicular to both shafts;

a housing surrounding the gear; and

a bearing shell carrying at least one bearing, said at least one bearing being installable around a hub of the gear for bearing the gear, wherein the bearing and the shell can be assembled together with an ascending displacement of the shell.

3. The assembly according to claim 2 , wherein the seal support sleeve is assemblable to the housing after a forward displacement of the sleeve.

4. The assembly according to claim 1 , wherein a diameter of the second seal is larger than a diameter of the first seal.

5. The assembly according to claim 1 , wherein the sleeve is conical.

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 →
CHANGE OF NAME Recorded Feb 20, 2008
From: SNECMA MOTEURS
To: SNECMA
Reel/Frame 020609/0569 →