IP Library › Granted Patent US 10,759,122
Granted Patent B2
US 10,759,122 · App. 15/841,987 · Granted Sep 1, 2020

Method and tooling for shaping a fan casing

Inventors: Richard Mathon (Brunoy, FR); Dominique Michel Serge Magnaudeix (Evry-Gregy, FR)
Assignee: SAFRAN AIRCRAFT ENGINES
B29C70/446B29C33/505B29C49/44B29C53/20B29C53/82B29C53/84B29C70/545B29D99/006F01D25/24B29L2031/7504F05D2230/42F05D2240/14F05D2300/44F05D2300/603
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Quick Facts
Patent No.
US 10,759,122
App. No.
15/841,987
Granted
Sep 1, 2020
Kind
B2
Abstract

A method of shaping the profile of a fan casing having an inside surface, the method including placing the casing around a surface of revolution of a drum of shaping tooling; interposing at least one bladder that is inflatable under the action of a fluid under pressure between a portion of the inside surface of the casing and the drum, the bladder extending over all or part of the surface of revolution of the drum; stoving the assembly including the casing, the tooling, and the at least one bladder at a predetermined temperature; and during the stoving, applying isostatic pressure via the at least one bladder so as to impart a cylindrical profile to the portion of the inside surface of the casing facing the at least one bladder.

Claims (14)

1. A method of shaping the profile of a fan casing having an inside surface, the method comprising:

placing the inside surface of the fan casing around a surface of revolution of a drum of shaping tooling;

interposing a plurality of bladders that are inflatable under the action of a fluid under pressure between the inside surface of the casing and the drum of the tooling, the bladders extending over all the surface of revolution of the drum;

stoving the assembly comprising the casing, the tooling, and said plurality of bladders at a predetermined temperature; and

during the stoving, applying isostatic pressure via said plurality of bladders so as to impart a cylindrical profile to the inside surface of the casing facing said plurality of bladders and thus to counter ovalization of the casing.

2. The method according to claim 1 , wherein the casing comprises a band extending axially between two flanges, the band having an intermediate zone situated at a distance from the flanges and two lateral zones on either side of the intermediate zone, the flanges extending radially from the lateral zones, the intermediate zone forming a retention zone of the casing, the isostatic pressure being applied in a bladder placed facing an inside surface of the retention zone and two bladders arranged facing inside surfaces of the two lateral zones of the band.

3. The method according to claim 2 , wherein the isostatic pressure is maintained at least until the casing has cooled.

4. The method according to claim 1 , wherein the stoving step corresponds to a step of adhesively bonding an external element onto the fan casing.

5. The method according to claim 1 , wherein the stoving step is performed while repairing the fan casing.

6. A tooling for shaping the profile of a fan casing having an inside surface, the tooling comprising a drum presenting a surface of revolution and a plurality of bladders that are inflatable under the action of a fluid under pressure and extending over all the surface of revolution of the drum, the bladders being arranged so as to face the inside surface of the fan casing when they are put into place around the surface of revolution, said plurality of bladders being connected to an adjustment system configured to adjust a fluid under pressure and configured to use the fluid under pressure to control the inflation of the bladders so as to impart a cylindrical profile to the inside surface of the fan casing when it is in place around the surface of revolution and thus to counter ovalization of the casing.

7. The tooling according to claim 6 , wherein the drum comprises a first rim, a second rim, and a third rim arranged between the first and second rims, and wherein said plurality of bladders are arranged on an outside surface of the first second and third rims so as to face respectively an inside surface of a first lateral zone, a second lateral zone and a retention zone of the casing when the casing is in place around the surface of revolution.

8. The tooling according to claim 6 , wherein the adjustment system configured to adjust a fluid under pressure is integrated in the tooling.

9. A stove including shaping tooling according to claim 6 .

10. The stove according to claim 9 , wherein the adjustment system configured to adjust a fluid under pressure is integrated in the stove.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 18, 2018
From: MATHON, RICHARD; MAGNAUDEIX, DOMINIQUE MICHEL SERGE
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 045578/0419 →
Priority Claims (1)
FR 16 62542 · Dec 15, 2016 · national
Continuity (1)
Related Publication 20180169972A1 · Jun 21, 2018
Cited By (2)
US 12,325,668 US 12,508,747