IP Library Granted Patent US 7,788,806
Granted Patent B2
US 7,788,806 · App. 11/776,256 · Granted Sep 7, 2010

Process for manufacturing a blisk and mold for implementing the process

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Quick Facts
Patent No.
US 7,788,806
App. No.
11/776,256
Granted
Sep 7, 2010
Kind
B2
Abstract

A process for manufacturing an integrally bladed disk for a turbomachine rotor by friction welding is disclosed. The manufacturing process includes arranging a plurality of blades in the form of a ring in a mold having symmetry of revolution; casting a degradable material, preheated to a temperature above its melting point, onto the ring of blades in the mold; extracting the molded ring which is obtained after the degradable material has solidified; welding the molded ring onto a disk; and eliminating the degradable material.

Claims (20)

1. A process for manufacturing a blisk, comprising:

arranging a plurality of blades in the form of a ring in a mold with symmetry of revolution, each of the blades including a shroud and a root, the shroud disposed at an upper end of the blade and an airfoil machined with a twist along a radial axis, and the root includes a shoulder disposed at a front end of the root which cooperates with a holding device to prevent the blade from moving radially during welding, and a friction surface which is consumed during welding;

casting a degradable material, preheated to a temperature above its melting point, onto the ring of blades arranged in the mold;

wherein the mold includes a bottom ring, an outer ring, and a top ring, the bottom ring includes an annular wall disposed at an inner periphery of the bottom ring and extends axially toward an inside of the mold, and the plurality of blades are arranged such that the friction surface of each of the blades contact the annular wall, and the top ring is of plane shape and is fastened to the bottom ring;

extracting a molded ring which is obtained after the degradable material has solidified;

welding the molded ring onto a disk;

eliminating the degradable material, wherein the welding is performed by friction welding,

wherein the plurality of blades are arranged such that a lateral edge of the shroud of each of the blades abuts a corresponding lateral edge of the shroud of an adjacent blade and a prestress is exerted on the blades, and

the top ring presses the root of each of the blades to exert the prestress on the blades when the top ring is fastened to the bottom ring.

2. The process for manufacturing a blisk as claimed in claim 1 , wherein the welding is performed by inertial friction welding.

3. The process for manufacturing a blisk as claimed in claim 1 , wherein the friction surfaces of the molded ring and of the disk are beveled and include a complementary frustoconical shape.

4. The process for manufacturing a blisk as claimed in claim 1 , wherein, during the friction welding operation, the disk is pressed axially against the molded ring.

5. The process for manufacturing a blisk as claimed in claim 1 , wherein a melting point of the degradable material is lower than a melting point of the material of the blades or the disk.

6. The process for manufacturing a blisk as claimed in claim 5 , wherein the degradable material is eliminated chemically or thermally.

7. The process for manufacturing a blisk as claimed in claim 6 , wherein the degradable material is a resin.

8. The process for manufacturing a blisk as claimed in claim 7 , wherein the resin is based on a polyurethane or silicone.

9. The process for manufacturing a blisk as claimed in claim 6 , wherein the degradable material is a metal alloy.

10. The process for manufacturing a blisk as claimed in claim 9 , wherein the alloy is based on lead-tin.

11. The process for manufacturing a blisk as claimed in claim 1 , wherein a top of the shroud includes sealing teeth.

12. The process for manufacturing a blisk as claimed in claim 1 , further comprising machining the airfoils and weld zone after eliminating the degradable material.

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 Jul 11, 2007
From: FABRE, ADRIEN; ROUSSELIN, STEPHANE
To: SNECMA
Reel/Frame 019543/0769 →