IP Library Granted Patent US 7,749,342
Granted Patent B2
US 7,749,342 · App. 10/522,182 · Granted Jul 6, 2010

Reinforced composite mechanical component, and method for making same

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Quick Facts
Patent No.
US 7,749,342
App. No.
10/522,182
Granted
Jul 6, 2010
Kind
B2
Abstract

A mechanical part presents a main direction along which there extends a central zone forming a core and a peripheral zone forming a casing that surrounds the core. The core and the casing present a metallurgical bond between each other. The core is made of a first material presenting at least a metal matrix, and the casing is made of a second material presenting at least a metal matrix. The metal matrices of the first and second materials are based on the same metal, and at least one of the first and second materials is made of a metal matrix composite containing reinforcing elements dispersed in the metal matrix. The mechanical part can be used as a blade for a fan or a low pressure compressor.

Claims (15)

1. A method of manufacturing a blade, comprising:

a) compressing a core and a casing to make a semi-finished product containing said core and said casing, said core and said casing including a metallurgical bond between each other resulting from said compression, said core including a first material that includes at least an aluminum based metal matrix, and said casing including a second material that includes at least an aluminum based metal matrix, and at least one of said first and second materials being made of a metal matrix composite containing reinforcing elements dispersed in said metal matrix;

b) forging the semi-finished product to obtain a blank with a quasi-final shape of the blade; and

c) machining said blank to provide a finished product forming said blade.

2. A method of manufacture according to claim 1 for obtaining a blade in which said first and second materials include said metal matrix composite containing said reinforcing elements dispersed in said metal matrix, wherein said reinforcing elements represent a percentage by weight of the composition of said metal matrix composite that varies progressively in said first material and in said second material in a direction from a center of said core towards a periphery of said casing, and wherein said compressing said core and said casing includes forming the core and the casing conjointly by a powder metallurgy technique.

3. A method of manufacture according to claim 1 , wherein said compressing said core and said casing includes performing, in succession:

a1) using said first material to make a rod extending in a longitudinal direction, said rod serving to form said core placed in a center of the mechanical part;

a2) using said second material to make a sleeve extending in a longitudinal direction, said sleeve serving to form the casing of the mechanical part by surrounding said core;

a3) inserting the rod into the sleeve to form an assembly; and

a4) passing said assembly through an orifice of small section to reduce at least one dimension of said assembly in a direction perpendicular to said longitudinal direction to create a metallurgical bond between said rod and said sleeve.

4. A method of manufacture according to claim 3 , wherein said passing said assembly through the orifice includes rolling or extrusion.

5. A method of manufacture according to claim 3 , wherein said passing said assembly through the orifice is performed at an elevated temperature.

6. A method of manufacture according to claim 5 , wherein said passing said assembly through the orifice is performed at a temperature of about 400° C.

7. A method of manufacture according to claim 1 , wherein said forging includes die stamping.

8. A method of manufacture according to claim 7 , wherein said die stamping is performed at a temperature of about 430° C. and a pressure of about 100 MPa.

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 →