IP Library Granted Patent US 7,780,379
Granted Patent B2
US 7,780,379 · App. 12/355,140 · Granted Aug 24, 2010

Surfacing and contouring cutter for high-speed machining of composite material parts

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Quick Facts
Patent No.
US 7,780,379
App. No.
12/355,140
Granted
Aug 24, 2010
Kind
B2
Abstract

A surfacing and contouring cutter for high-speed machining of parts made of composite material, the cutter having a cut end portion with teeth ( 20 ) that are regularly spaced apart around the axis ( 14 ) of the cutter and that are separated from one another by swarf grooves, the main cutting edge of each tooth being connected to the secondary cutting edge (S 2 ) of the tooth via a corner ( 24 ) of convex rounded shape with a radius of curvature greater than about 1.5 mm, and the secondary cutting angle lying in the range about 5° to 15°.

Claims (16)

1. A surfacing and contouring cutter, in particular for high-speed machining of parts made of composite material, the cutter comprising a body having at least a portion that is made of ceramic, the body extending along the axis of rotation of the cutter and comprising a cut end portion having teeth regularly spaced around the axis of the cutter and separated from one another by swarf grooves, each tooth comprising a front main cutting edge and a side secondary cutting edge, the main cutting edge being formed by an intersection between a main cutting face and a first main flank, and the secondary cutting edge being formed by an intersection between a secondary cutting face and a first secondary flank, the main cutting edge of each tooth being connected to the secondary cutting edge of the tooth via a corner, the corner being of convex rounded shape with a radius of curvature that is greater than about 1.5 mm, the cutter being characterized in that the secondary cutting angle between the secondary cutting face of each tooth and a first reference plane containing the axis of rotation of the cutter and a point under consideration of the secondary cutting edge of the tooth lies in the range about 5° to 15°, said cutting angle being measured in a first working plane perpendicular to the axis of rotation of the cutter and containing the point under consideration of the secondary cutting edge of the tooth, and in that the swarf grooves are formed by front flutes between the teeth, the bottom of each of these flutes being connected to a main cutting face of the tooth by a line that forms an angle lying in the range about 15° to 25° relative to a working plane perpendicular to the axis of the cutter, said angle being measured in a reference plane containing the axis of the cutter.

2. A cutter according to claim 1 , characterized in that the main cutting angle between the main cutting face of each tooth and a second reference plane containing the axis of rotation of the cutter and a point under consideration of the main cutting edge of the tooth lies in the range about 5° to 15°, said cutting angle being measured in a plane towards the rear perpendicular to the second reference plane and to a second working plane perpendicular to the axis of rotation of the cutter and containing the point under consideration of the main cutting edge of the tooth.

3. A cutter according to claim 1 , characterized in that the main cutting angle is about 10°, and/or the secondary cutting angle is about 10°.

4. A cutter according to claim 1 , characterized in that the radius of curvature of the corner is greater than or equal to about 2 mm.

5. A cutter according to claim 1 , characterized in that it has six teeth.

6. A cutter according to claim 1 , characterized in that it has an outside diameter greater than 15 mm, e.g. of about 18 mm.

7. A cutter according to claim 1 , characterized in that the core of the cutter has a diameter greater than 10 mm, e.g. of about 15 mm.

8. A cutter according to claim 1 , characterized in that the main cutting edge of each tooth is rectilinear and extends substantially parallel to a working plane perpendicular to the axis of the cutter.

9. A cutter according to claim 1 , characterized in that the secondary cutting edge of each tooth extends helically around the axis of the cutter and defines a helix angle lying in the range 1° to 40°, and for example equal to about 20°.

10. A cutter according to claim 1 , characterized in that a second main flank extends rearwards from the first main flank, and a second secondary flank extends behind the first secondary flank.

11. A cutter according to claim 1 , characterized in that the first main flank of each tooth has a thickness h lying in the range about 0.5 mm to 1 mm.

12. A cutter according to claim 1 , characterized in that the cumulative thickness k of the first and second secondary flanks of each tooth is greater than about 2 mm.

13. A cutter according to claim 1 , characterized in that two diametrically-opposite teeth have long main cutting edges that are connected to each other at their radially inner ends via at least one central edge.

14. A cutter according to claim 13 , characterized in that the other teeth of the cutter have short main cutting edges with radially inner ends that are spaced apart from the central edge by recesses formed close to said central edge.

15. A cutter according to claim 1 , characterized in that the cut portion of the cutter is substantially cylindrical in shape.

16. A method of machining a part at high speed, in particular a part made of composite material, by means of a cutter according to claim 1 , the method being characterized in that the peripheral cutting speed of the cutter lies in the range 500 m/min to 1000 m/min, and the advance per revolution lies in the range 0.03 mm to 0.12 mm.

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 →