IP Library Granted Patent US 10,213,882
Granted Patent B2
US 10,213,882 · App. 15/536,408 · Granted Feb 26, 2019

Method for repairing a fan casing

Inventors: Antoine Patrice Marie Desreumaux (Guignes, FR); Patrick Jean-Louis Reghezza (Vaux le Pénil, FR); Sébastien Marc Jean-Michel Perez (Heyrieux, FR)
Assignee: SAFRAN AIRCRAFT ENGINES
B23P6/002F01D25/24F04D29/526B23P2700/01F02K3/06F04D29/38F05D2220/323F05D2230/80F05D2250/12F05D2250/141F05D2250/21F05D2250/232F05D2300/121F05D2300/133F05D2300/175Y02T50/672
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Quick Facts
Patent No.
US 10,213,882
App. No.
15/536,408
Granted
Feb 26, 2019
Kind
B2
Abstract

A method for repairing a fan casing in which the inner surface is damaged, includes attaching a reinforcement element to the fan casing, the reinforcement element being attached to the outer surface of the fan casing opposite the damage.

Claims (10)

1. A method for repairing a fan casing an inner surface of which is subject to damage, the method comprising attaching a reinforcing member to the fan casing having a damage on the inner surface, wherein the reinforcing member is attached to an outer surface of the fan casing, opposite a location of the damage.

2. The method for repairing a fan casing according to claim 1 , further comprising, prior to said attaching, dimensioning the reinforcing member.

3. The method for repairing a fan casing according to claim 2 , wherein the dimensioning of the reinforcing member is accomplished by estimating a cracking zone originating in the inner surface and on a perimeter of the damage and growing wider as the cracking zone propagates in a direction of the outer surface to create, on the outer surface of the fan casing, an outer cracking area, wherein an area of the reinforcing member which is to be attached to the outer surface of the fan casing is at least equal to the outer cracking area.

4. The method for repairing a fan casing according to claim 2 , wherein the dimensioning of the reinforcing member is accomplished by estimating a cracking zone originating in the inner surface and on a perimeter of the damage and growing wider as the cracking zone propagates in a direction of the outer surface to create, on the outer surface of the fan casing, an outer cracking area; wherein an area of the reinforcing member which is to be attached to the outer surface of the fan casing is equal to the outer cracking area.

5. The method for repairing a fan casing according to claim 3 , wherein the cracking zone originates in the inner surface and on the perimeter of the damage and grows wider as the cracking zone propagates in the direction of the outer surface with a propagation angle of between 40 and 50 degrees.

6. The method for repairing a fan casing according to claim 1 wherein the thickness of the reinforcing member is at least equal to 1.5 times a depth of the damage.

7. The method for repairing a fan casing according to claim 1 wherein the reinforcing member is attached to the outer surface of the fan casing by welding, riveting or bonding.

8. A fan casing subject to damage located on the inner surface of the fan casing and a reinforcing member attached to an outer surface of the fan casing and opposite a location of the damage said reinforcing member being dimensioned according to an estimation of a cracking zone originating in the inner surface and on the perimeter of the damage and growing wider as the cracking zone propagates in the direction of the outer surface to create, on the outer surface of the fan casing, an outer cracking area, wherein the area of the reinforcing member which is attached to the outer surface of the fan casing is at least equal to the outer cracking area.

9. The fan casing according to claim 8 , wherein the reinforcing member is made of aluminum, Inconel, or titanium.

10. The fan casing according to claim 8 , wherein a shape of the reinforcing member is rectangular, circular or elliptical.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 15, 2017
From: DESREUMAUX, ANTOINE PATRICE MARIE; REGHEZZA, PATRICK JEAN-LOUIS; PEREZ, SÉBASTIEN MARC JEAN-MICHEL
To: SNECMA
Reel/Frame 043298/0590 →
CHANGE OF NAME Recorded Aug 15, 2017
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 043559/0771 →
Priority Claims (1)
FR 14 62472 · Dec 16, 2014 · national
Continuity (1)
Related Publication 20170348808A1 · Dec 7, 2017