Rotary cutting tools and applications thereof

Patent metadata

Field	Value
Publication number	US-11420273-B2
Application number	US-201916655803-A
Country	US
Kind code	B2
Filing date	Oct 17, 2019
Priority date	Oct 17, 2019
Publication date	Aug 23, 2022
Grant date	Aug 23, 2022

Abstract

In one aspect, rotary cutting tools are described herein comprising sets of coolant channels having exit aperture in the flutes of the tools for efficient coolant delivery to multiple cutting surfaces. Briefly, a rotary cutting tool comprises a shank portion, and a cutting portion extending from the shank portion along a longitudinal axis, the cutting portion comprising flutes helically extending along the longitudinal axis and internal coolant channels comprising exit apertures in the flutes. A projection of an exit aperture of a first set of internal coolant channels intersects a rake face extending below a corner edge of the rotary cutting tool, and a projection of an exit aperture of a second set of internal coolant channels intersects a rake face below a radial cutting edge of the rotary cutting tool.

First claim

The invention claimed is:

1. A rotary cutting tool comprising:
a shank portion; and
a cutting portion extending from the shank portion along a longitudinal axis, the cutting portion comprising flutes helically extending along the longitudinal axis and internal coolant channels comprising exit apertures in the flutes, wherein a projection of an exit aperture of a first set of internal coolant channels intersects a rake face extending below a corner edge of the rotary cutting tool, and a projection of an exit aperture of a second set of internal coolant channels intersects a rake face adjacent to the corner edge below a radial cutting edge of the rotary cutting tool.

2. The rotary cutting tool of claim 1 further comprising a third set of internal coolant channels, wherein a projection of an exit aperture of the third set of internal coolant channels is parallel or substantially parallel with the longitudinal axis.

3. The rotary cutting tool of claim 2 , wherein the exit apertures of the second set of internal coolant channels reside between the exit apertures of the first and third sets of internal coolant channels along the longitudinal axis.

4. The rotary cutting tool of claim 2 , wherein the exit apertures of the third set of coolant channels are proximate the shank portion.

5. The rotary cutting tool of claim 1 , wherein the exit apertures for the first and second sets of internal coolant channels differ in shape.

6. The rotary cutting tool of claim 2 , wherein the exit apertures for the first, second, and third sets of internal coolant channels differ from one another in shape.

7. The rotary cutting tool of claim 2 , wherein the first, second, and third sets of internal coolant channels extend radially from a central internal coolant channel.

8. The rotary cutting tool of claim 1 , wherein the exit apertures of the first and second sets of internal coolant channels are positioned at a base of the flutes.

9. The rotary cutting tool of claim 2 , wherein the exit apertures of the first, second, and third sets of internal coolant channels are positioned at a base of the flutes.

10. The rotary cutting tool of claim 7 , wherein the central internal coolant channel extends through the shank portion.

11. The rotary cutting tool of claim 7 , wherein the central internal coolant channel comprises one or more tapered sections.

12. The rotary cutting tool of claim 2 , wherein at least one of the first, second, and third sets of internal coolant channels comprise a curved section.

13. The rotary cutting tool of claim 2 , wherein at least one of the first, second, and third sets of internal coolant channels are linear.

14. The rotary cutting tool of claim 1 , wherein the first and second sets of internal coolant channels exhibit differing coolant discharge pressures.

15. The rotary cutting tool of claim 2 , wherein the first, second and third sets of internal coolant channels exhibit differing coolant discharge pressures.

16. The rotary cutting tool of claim 15 , wherein the first set of coolant channels exhibit the highest coolant discharge pressure.

17. The rotary cutting tool of claim 1 , wherein the rotary cutting tool is an end mill.

18. The rotary cutting tool of claim 1 , wherein the rotary cutting tool is fabricated by an additive manufacturing method.

19. The rotary cutting tool of claim 1 , wherein the rotary cutting tool is formed of sintered cemented carbide.

20. A method of cutting a workpiece comprising:
providing a rotary cutting tool comprising a shank portion, and a cutting portion extending from the shank portion along a longitudinal axis, the cutting portion comprising flutes helically extending along the longitudinal axis and internal coolant channels comprising exit apertures in the flutes; wherein a projection of an exit aperture of a first set of internal coolant channels intersects a rake face extending below a corner edge of the rotary cutting tool, and a projection of an exit aperture of a second set of internal coolant channels intersects a rake face below a radial cutting edge of the rotary cutting tool;
contacting the workpiece with the rotary cutting tool, wherein a projection of an exit aperture of a first set of internal coolant channels intersects a rake face extending below a corner edge of the rotary cutting tool, and a projection of an exit aperture of a second set of internal coolant channels intersects a rake face adjacent to the corner edge below a radial cutting edge of the rotary cutting tool;
discharging coolant from a first set of internal coolant channels to strike a rake face below a corner edge of the rotary cutting tool; and
discharging coolant from a second set of internal coolant channels to strike a rake face adjacent to the corner edge below a radial cutting edge of the rotary cutting tool.

21. The method of claim 20 further comprising discharging coolant from a third set of internal coolant channels along the longitudinal axis of the rotary cutting tool.

22. The method of claim 21 , wherein the exit apertures for the first, second, and third sets of internal coolant channels differ from one another.

23. The method of claim 21 , wherein the exit apertures of the first, second, and third sets of internal coolant channels are positioned at a base of the flutes.

24. The method of claim 21 , wherein the coolant is discharged from the first, second and third sets of internal coolant channels at differing pressures.

Assignees

• Kennametal Inc

Inventors

• Fang Xiangdong D
• Prichard Paul D
• Gamble Kevin M
• Wills David
• Lane Jeff

Classifications

• B23C5/282 Primary

  Coolant channel characterised by its cross-sectional shape · CPC title

• B23C5/10

  Shank-type cutters, i.e. with an integral shaft · CPC title

• B22F2005/001

  Cutting tools, earth boring or grinding tool other than table ware · CPC title

• B33Y80/00

  Products made by additive manufacturing · CPC title

• B23Q11/1023

  Tool holders, or tools in general specially adapted for receiving the cutting liquid from the spindle · CPC title