IP Library Granted Patent US 8,732,949
Granted Patent B2
US 8,732,949 · App. 12/933,951 · Granted May 27, 2014

Process for manufacturing a single-piece blisk by cutting with an abrasive water jet

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Quick Facts
Patent No.
US 8,732,949
App. No.
12/933,951
Granted
May 27, 2014
Kind
B2
Abstract

A process for manufacturing a single-piece blisk, including: using an abrasive water jet to cut a block of material, so as to create blade preforms extending radially from a disk, then milling the blade preforms.

Claims (22)

1. A process for manufacturing a single-piece blisk, comprising:

using an abrasive water jet to cut out a first piece of material from a block of material;

removing the first piece of material from the block of material;

using the abrasive water jet to cut out a second piece of material from the block of material;

removing the second piece of material from the block of material so as to create blade preforms extending radially outwards from a disk; and

milling the blade preforms,

wherein the first piece of material extends through an entire thickness of the block of material along a central axis of the block of material.

2. The process according to claim 1 , wherein the abrasive water jet cutting removes at least 50% by weight of the block of material.

3. The process according to claim 1 , wherein the milling the blade preforms is done so as to obtain profiled blade blanks, and is followed by a milling to finish the blade blanks, so as to obtain blades to a final profile.

4. The process according to claim 1 , wherein the diameter of the single-piece blisk is greater than or equal to 800 mm.

5. The process according to claim 1 , wherein the thickness of the single-piece blisk is greater than or equal to 100 mm.

6. The process according to claim 1 , wherein the blades of the single-piece blisk are twisted.

7. The process according to claim 1 , wherein the material block used is made of titanium or a titanium alloy.

8. The process according to claim 1 , wherein the single-piece blisk is a single-piece blisk for an aircraft turbine engine.

9. The process according to claim 1 , wherein the single-piece blisk is a single-piece blisk for a turbine or compressor rotor in an aircraft turbine engine.

10. The process according to claim 1 , wherein a water jet cutting machine including a focussing gun is used to cut out the first piece of material and the second piece of material.

11. The process according to claim 10 , wherein an axis of the focussing gun is displaced along a globally U-shaped line beginning at a radial end of the block, extending radially inwards, extending along a circumferential direction, and extending radially outwards to another radial end of the block to cut out the first piece of material.

12. The process according to claim 10 , wherein the focussing gun moves along a radial line to cut out the second piece of material.

13. The process according to claim 1 , wherein the first piece of material is removed manually from the block of material.

14. The process according to claim 1 , wherein the first piece of material includes a twisted shape along the radial direction.

15. The process according to claim 1 , wherein the second piece of material includes a twisted shape along the radial direction.

16. The process according to claim 1 , wherein the second piece of material extends over only a part of the thickness of the block of material.

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 →