IP Library Granted Patent US 7,718,017
Granted Patent B2
US 7,718,017 · App. 11/691,122 · Granted May 18, 2010

Method for the monobloc sizing for the tempering casings and device for implementing the method

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Quick Facts
Patent No.
US 7,718,017
App. No.
11/691,122
Granted
May 18, 2010
Kind
B2
Abstract

A method of sizing a cylindrical part following shaping, by plastic deformation, of a metallic material that has maximum structural shrinkage at a maximum-shrinkage temperature between a first temperature and a second temperature, which is lower than the first temperature, is disclosed. The method includes placing the part in a shaft furnace, heating the part to the first temperature, lowering and fitting into the part an internal-sizing tool with an outer diameter greater than an inner diameter of the part at maximum structural shrinkage, transporting the assembly formed by the part and the sizing tool to a tempering vessel, cooling the part to a temperature below said second temperature, and extracting the internal-sizing tool. The method applies to the manufacture of turbomachine casings.

Claims (18)

1. A method of sizing a cylindrical part following shaping, by plastic deformation, of a metallic material that has maximum structural shrinkage at a maximum-shrinkage temperature between a first temperature and a second temperature which is lower than the first temperature, the method comprising:

placing the part in a shaft furnace;

positioning an internal-sizing apparatus outside the furnace and in line with the part, the internal-sizing apparatus includes an internal-sizing tool with an outer diameter which is greater than an inner diameter of the part at maximum structural shrinkage;

heating the part to the first temperature;

lowering and fitting the internal-sizing tool into the part;

transporting the assembly formed by the part and the internal-sizing tool to a tempering vessel;

cooling the part to a temperature below said second temperature; and

extracting the internal-sizing tool.

2. The method as claimed in claim 1 , wherein the part is placed in a furnace and heated to the first heat treatment temperature; after treatment, said sizing tool is placed on the part and the assembly is positioned in a tempering tub; the part is cooled to said lower temperature.

3. The method as claimed in claim 1 , wherein the metal is a Z5CNU17 alloy.

4. The method according to claim 1 , wherein the internal-sizing apparatus includes:

a dummy bar attached to a frame;

first and second articulated radial arms attached to the frame at first and second ends of the frame, respectively, which radial arms support the part; and

a catching gripper which attaches to the dummy bar, and

wherein the internal-sizing tool is suspended from the catching gripper by cables.

5. The method as claimed in claim 4 , wherein the catching gripper is movable between a first position where the catching gripper is secured by a rod to the dummy bar and a second position where the dummy bar is suspended from the catching gripper by cables.

6. The method according to claim 1 , wherein the part is a turbomachine casing.

7. The method according to claim 1 , wherein the first temperature is 1000° C., the second temperature is ambient temperature, and the maximum-shrinkage temperature is between 200° C. and 300° C.

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 Mar 26, 2007
From: BRETON, MICHEL; SAGNE, PATRICE RENE
To: SNECMA
Reel/Frame 019065/0025 →