IP Library Granted Patent US 9,180,531
Granted Patent B2
US 9,180,531 · App. 12/318,249 · Granted Nov 10, 2015

Drill and drilling method for workpiece

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Quick Facts
Patent No.
US 9,180,531
App. No.
12/318,249
Granted
Nov 10, 2015
Kind
B2
Abstract

A drill includes a cutting edge. The cutting edge has a point angle which is continuously decreased from a center-position point angle A (herein, 0°<A<180°) at a center position to a maximum-diameter-position point angle of 0° at a maximum diameter position. The cutting edge has a relief angle which is continuously decreased from the center position to the maximum diameter position. The cutting edge of the drill has a relief angle at the maximum diameter position. Hence, the cutting edge also serves as a cutting edge for reaming. The ridgeline and relief face of the cutting edge have no corner, thereby providing good wear resistance.

Claims (40)

1. A drill comprising:

a cutting edge,

wherein the cutting edge has a point angle which is continuously decreased from a center-position point angle A at a center position to a maximum-diameter-position point angle of 0° at a maximum diameter position,

wherein the cutting edge has a radial relief angle which is continuously decreased from the center position to the maximum diameter position,

wherein the point angle A at the center position satisfies the condition 0°<A<180°, and

wherein an axial relief angle at the center position is δ, and the center-position point angle A and the center-position axial relief angle δ satisfy a relationship of δ>(180°−A)/2.

2. The drill according to claim 1 , wherein a ridgeline of the cutting edge is a parabolic ridgeline formed of a part of a parabola.

3. The drill according to claim 1 , wherein a ridgeline of the cutting edge is an arcuate ridgeline formed of a single arc.

4. The drill according to claim 1 , wherein the cutting edge has a rake angle.

5. The drill according to claim 1 , wherein the cutting edge has no rake angle.

6. The drill according to claim 1 , further comprising:

two helical flutes;

lands formed between the helical flutes;

and margins at edges of the lands along the helical flutes.

7. The drill according to claim 1 , wherein a length of the cutting edge along an axis of the drill is at least 1.6 times a maximum diameter of the drill.

8. A drilling method for a workpiece, comprising:

a first step of drilling a hole in the workpiece by using a drill including a cutting edge, the cutting edge having a point angle which is continuously decreased from a center-position point angle A at a center position to a maximum-diameter-position point angle of 0° at a maximum diameter position, the cutting edge having a radial relief angle which is continuously decreased from the center position to the maximum diameter position, and by cutting the workpiece by the cutting edge at the center-position; and

a second step of reaming by cutting the drilled hole formed in the first step, by the cutting edge at the maximum-diameter-position while gradually shifting from the first step,

wherein the point angle A at the center position satisfies the condition 0°<A<180°, and

wherein an axial relief angle at the center position is δ, the center-position point angle A and the center-position axial relief angle δ satisfy a relationship of δ>(180°−A)/2.

9. The drilling method of claim 8 , wherein the drilled a hole is formed in a multilayer component member comprising a reinforced composite material layer.

10. The drilling method of claim 9 , wherein

the step of reaming includes removing delaminated portions of the multilayer component member.

11. The drilling method of claim 10 , wherein the drilled hole is formed in the multilayer component member such that the hole is substantially free of burrs and substantially free of delamination between layers of the multilayer component member.

12. A drill comprising:

a cutting edge,

wherein the cutting edge has a point angle which is continuously decreased from a center-position point angle A at a center position to a maximum-diameter-position point angle of 0° at a maximum diameter position,

wherein the cutting edge has a radial relief angle which is continuously decreased from the center position to the maximum diameter position,

wherein the cutting edge has the radial relief angle at the maximum diameter position,

wherein the point angle A at the center position satisfies a condition 0°<A<180°, and

wherein an axial relief angle at the center position is δ, and the center-position point angle A and the center-position relief angle δ satisfy a relationship of δ>(180°−A)/2.

13. A drilling method for a workpiece, comprising:

a first step of drilling a hole in the workpiece by using a drill including a cutting edge, the cutting edge having a point angle which is continuously decreased from a center-position point angle A at a center position to a maximum-diameter-position point angle of 0° at a maximum diameter position, the cutting edge having a radial relief angle which is continuously decreased from the center position to the maximum diameter position, and by cutting the workpiece by the cutting edge at the center-position; and

a second step of reaming by cutting the drilled hole formed in the first step, by the cutting edge at the maximum-diameter-position while gradually shifting from the first step,

wherein the cutting edge has the radial relief angle at the maximum diameter position,

wherein the point angle A at the center position satisfies the condition 0°<A<180°, and

wherein an axial relief angle at the center position is δ, and the center-position point angle A and the center-position relief angle δ satisfy the relationship of δ>(180°−A)/2.

14. The drilling method of claim 13 , further comprising: wherein the drilled a hole is formed in a multilayer component member comprising a reinforced composite material layer.

15. The drilling method of claim 14 , wherein the step of reaming includes removing delaminated portions of the multilayer component member.

16. The drilling method of claim 15 , wherein the drilled hole is formed in the multilayer component member such that the hole is substantially free of burrs and substantially free of delamination between layers of the multilayer component member.

Assignments (2)
CHANGE OF NAME Recorded May 12, 2017
From: FUJI JUKOGYO KABUSHIKI KAISHA
To: SUBARU CORPORATION
Reel/Frame 042624/0886 →
CHANGE OF ADDRESS Recorded Oct 31, 2014
From: FUJI JUKOGYO KABUSHIKI KAISHA
To: FUJI JUKOGYO KABUSHIKI KAISHA
Reel/Frame 034114/0841 →