IP Library Granted Patent US 7,029,367
Granted Patent B2
US 7,029,367 · App. 10/963,571 · Granted Apr 18, 2006

Automated polishing process for mechanical parts in titanium or titanium alloy

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Quick Facts
Patent No.
US 7,029,367
App. No.
10/963,571
Granted
Apr 18, 2006
Kind
B2
Abstract

The present invention pertains to an automated polishing process for semi-finished mechanical parts in titanium or titanium alloy, using a machine with abrasive belt mounted on a tangential contact wheel driven in rotation at a determined speed and applied at a determined pressure, the wheel travelling with respect to the part's surface at a determined rate, characterized by the fact that the abrasive belt consists of superabrasive grains in industrial diamond or cubic boron nitride. The process is applied to geometric conforming of jet engine fan or compressor blades.

Claims (23)

1. A process of manufacturing a mechanical part, said process comprising the following steps:

rough-polishing a semi finished part comprising titanium, wherein during said rough polishing, material between 0.1 mm and 0.8 mm thick is removed; and

finish-polishing said rough-polished part, said finish-polishing being performed with an abrasive belt comprising super abrasive grains and mounted on a tangential contact wheel driven in rotation, wherein during said finish-polishing, material between 0.01 mm and 0.2 mm is removed.

2. The process of claim 1 , further comprising a step of manufacturing said semi finished part having an allowance.

3. The process of claim 1 , wherein said semi finished part is made of titanium and said material removed during said steps of rough-polishing and finish-polishing comprises titanium.

4. The process of claim 1 , wherein said semi finished part is made of titanium alloy and said material removed during said steps of rough-polishing and finish-polishing comprises titanium alloy.

5. The process of claim 1 , wherein said mechanical part is a fan blade.

6. The process of claim 5 , wherein said fan blade is a jet engine blade.

7. The process of claim 1 , wherein during said rough-polishing, material between 0.2 mm and 0.4 mm is removed.

8. The process according to claim 1 , wherein the rough-polishing is performed by chemical machining.

9. The process according to claim 1 , wherein the rough-polishing is performed by mechanical polishing with a super abrasive grains belt.

10. The process of claim 2 , wherein said step of manufacturing said semi finished part comprises forging said semi finished part.

11. The process of claim 2 , wherein said allowance is between 2/10 mm and 4/10 mm.

12. The process of claim 1 , wherein said super abrasive grains comprise diamond.

13. The process of claim 1 , wherein said super abrasive grains comprise cubic boron nitride.

14. The process of claim 1 , wherein said abrasive belt comprises a layer of nickel that backs the super abrasive grains.

15. The process of claim 1 , wherein said process is free of a step of manual adjustment by grinding.

16. The process of claim 1 , wherein said finish-polishing is performed by applying a force on said rough-polished part, said force being between 137 N and 196 N.

17. The process of claim 1 , wherein said finish-polishing is performed by moving said abrasive belt at a speed between 4.6 m/s and 18.6 m/s.

18. The process of claim 1 , wherein said finish-polishing is performed by moving said wheel at a speed between 3.4 m/min and 6.7 m/mm.

19. The process of claim 1 , wherein during said finish-polishing, material of 0.1 mm +/−0.01 mm is removed.

20. The process of claim 1 , wherein during said rough-polishing, material of 0.3 mm +/−0.05 mm is removed.

21. The process of claim 1 , wherein said super abrasive grains have a grain size of 220.

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 →