IP Library Granted Patent US 7,989,733
Granted Patent B2
US 7,989,733 · App. 11/466,998 · Granted Aug 2, 2011

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 7,989,733
App. No.
11/466,998
Granted
Aug 2, 2011
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 (14)

1. A device for heating a cylindrical component in a turbomachine of given diameter, by means of hot gas, comprising:

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 said diameter of the cylindrical component.

2. The heating device as claimed in claim 1 , wherein the heaters are equidistant from one another.

3. The heating device as claimed in claim 1 , wherein the inner cylindrical wall is perforated.

4. The heating device as claimed in claim 1 , wherein the heaters are electrical heaters.

5. The heating device as claimed in claim 1 , wherein the first wall of the annular chamber contacts the cylindrical component.

6. The heating device as claimed in claim 1 , further comprising a thermocouple attached to the first wall of the annular chamber.

7. The heating device as claimed in claim 1 , wherein the first half of the ring is supported by a first slider, the second half is supported by a second slider and the first and second sliders are supported by a support member.

8. The heating device as claimed in claim 7 , wherein the support member is supported by a frame member which slides in a vertical direction.

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 Nov 13, 2006
From: BERGEROT, FRANCOIS PIERRE ANDRE; LEEDER, LAURENT; MALTERRE, JACQUES PIERRE FELIX; SOUART, BERNARD ADRIEN EDMOND; THOMAS, HUBERT
To: SNECMA
Reel/Frame 018595/0707 →