IP Library Granted Patent US 8,476,557
Granted Patent B2
US 8,476,557 · App. 13/170,700 · Granted Jul 2, 2013

Device for heating a cylindrical component and use in assembling an inter-shaft bearing in a turbomachine

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Quick Facts
Patent No.
US 8,476,557
App. No.
13/170,700
Granted
Jul 2, 2013
Kind
B2
Abstract

A device for heating a cylindrical component of given diameter is disclosed. The device includes at least two heaters each delivering a stream of hot gas and emerging in an annular chamber. The inside diameter of the annular chamber is slightly greater than the diameter of the cylindrical component. The device may be used for heating a metal journal in which a bearing ring for an inter-shaft bearing in a double-body turbomachine is mounted.

Claims (18)

1. A method for assembling an inter-shaft bearing in a double-body turbomachine comprising:

placing a rear portion of a metal journal in which a bearing ring for a bearing is mounted in a heating device; and

heating the metal journal using the heating device,

wherein the heating device comprises:

at least two heaters which deliver a stream of hot gas;

an annular chamber defined by an outer cylindrical casing, an inner cylindrical wall and first and second walls perpendicular to an axis of the turbomachine such that the annular chamber presents a ring; and

deflectors disposed inside the annular chamber between the heaters, the deflectors being arched and inclined towards the axis of the turbomachine and guide the stream of hot gas emerging into the annular chamber in rotational movement about the axis of the turbomachine,

wherein the ring comprises a first half and a second half which are separable,

wherein the heaters are disposed circumferentially about the annular chamber and are substantially tangential to the annular chamber, and

wherein a diameter of the inner cylindrical wall is greater than a diameter of the metal journal, and

wherein the annular chamber of the heating device surrounds the rear portion of the metal journal during the heating.

2. The method as claimed in claim 1 , wherein a temperature at a surface of the journal is measured and the supply of hot gas is controlled according to said temperature.

3. The method as claimed in claim 1 , further comprising:

placing the bearing ring inside the metal journal; and

tightening a nut to secure the bearing ring inside the metal journal.

4. The method as claimed in claim 3 , wherein the heating device is retracted from the metal journal such that the first half and the second half of the ring are separated and disposed above the metal journal prior to placing the bearing ring inside the metal journal.

5. The method according to claim 3 , wherein a clearance between the metal journal and the bearing ring is measured using distance measuring instruments of a laser type prior to placing the bearing ring inside the metal journal.

6. The method according to claim 1 , comprising moving the heating device such that a support of the heating device abuts a flange of the turbomachine prior to heating of the metal journal.

Assignments (2)
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 →