Patent Grant
11571759
This application is related to application Ser. No. 16/557,533, filed on Aug. 30, 2019, the entire contents of which are incorporated herein by reference.
In general, the invention relates to cutting tools, and more particularly, to a lightweight cutting tool, such as a reamer, and the like, with a fluid dynamic structure, such as airfoil-shaped arms, that directs the flow of fluid in a desired direction to facilitate chip evacuation during a cutting operation.
During a cutting operation, it is essential to remove chips from the cutting zone. It has been observed that a reamer, for example, may have difficulties evacuating chips from the cutting zone, particularly when machining a blind hole.
The problem of the evacuation of chips from the cutting zone in a cutting tool, such as a reamer, and the like, can be solved by providing one or more arms with a fluid dynamic structure having a cross sectional shape similar to an airfoil, turbine blade, and the like, that facilitates chip evacuation both mechanically and fluid dynamically.
The fluid dynamic structure defined by the one or more arms that support the cutting head can facilitate chip evacuation by multiple methods. First, the arms can mechanically “shovel” the chips away from the cutting edge in a similar fashion to flutes in a drill. Second, the arms function as a fluid dynamic structure similar to an airfoil. The work generated by rotating the tool causes the fluid to exert a downward force on the arms and the arms to exert an equal upward force on the air, which results in fluid flow directed towards the rear machine connection. The efficiency of the fluid flow can be improved when machining blind holes by adding additional spokes that act as a turbine blade. These turbine blades are designed to draw fluid into the hole from the hole entrance (near the machine spindle), which will flow through the center of the tool, to the bottom of the hole (near the front of the tool). When fluid exits the center of the tool at the bottom of the hole, it will be drawn up and out of the hole by the fluid dynamic style arms that support the cutting region. In addition, the fluid dynamic structures in the form of airfoil shaped arms/blades may also be used on the outer diameter of the tool purely to generate fluid flow without being used to support a cutting or guide pad region. Fluid flow can also be directed by closing the exit at the center of the cutting tool and replacing this exit with multiple exits that lead to the cutting edge, thereby using a combination of machine fluid and the airfoil shaped arms/blades to direct the fluid flow to facilitate chip evacuation.
In one aspect, a cutting tool comprises a front cutting ring including a sleeve member and one or more cutting head assemblies. Each cutting head assembly includes a leading support arm extending radially outwardly from the sleeve member, a trailing support arm extending radially outwardly from the sleeve member, and a cutting head supported by the leading support arm and the trailing support arm. At least one of the leading support arm and the trailing support arm of the cutting head assembly comprises a fluid dynamic structure for directing fluid flow in an axially rearward direction along an exterior of the center tube, thereby enhancing chip evacuation during a cutting operation.
In another aspect, a cutting tool comprises a front cutting body; a rear machine connection member; a center tube having a front end and a rear end; a front cutting ring secured to the front end of the center tube and the front cutting body; and a rear cutting ring secured to the rear end of the center tube and the rear machine connection member. The front cutting ring comprises a sleeve member and one or more cutting head assemblies, each cutting head assembly including a leading support arm extending radially outwardly from the sleeve member, a trailing support arm extending radially outwardly from the sleeve member, and a cutting head supported by the leading support arm and the trailing support arm. The rear cutting ring comprises a sleeve member and one or more cutting head assemblies, each cutting head assembly including a leading support arm extending radially outwardly from the sleeve member, a trailing support arm extending radially outwardly from the sleeve member, and a cutting head supported by the leading support arm and the trailing support arm. At least one of the leading support arm and the trailing support arm of the front cutting ring and at least one of the leading support arm and the trailing support arm of the rear cutting ring comprises a fluid dynamic structure for directing fluid flow in an axially rearward direction along an exterior of the center tube, thereby enhancing chip evacuation during a cutting operation.
While various embodiments of the invention are illustrated, the particular embodiments shown should not be construed to limit the claims. It is anticipated that various changes and modifications may be made without departing from the scope of this invention.
Referring now to
Directional phrases used herein, such as, for example, left, right, front, back, top, bottom and derivatives thereof, relate to the orientation of the elements shown in the drawings and are not limiting upon the claims unless expressly recited therein. Identical parts are provided with the same reference number in all drawings.
Approximating language, as used herein throughout the specification and claims, may be applied to modify any quantitative representation that could permissibly vary without resulting in a change in the basic function to which it is related. Accordingly, a value modified by a term or terms, such as “about”, “approximately”, and “substantially”, are not to be limited to the precise value specified. In at least some instances, the approximating language may correspond to the precision of an instrument for measuring the value. Here and throughout the specification and claims, range limitations may be combined and/or interchanged, such ranges are identified and include all the sub-ranges contained therein unless context or language indicates otherwise.
Throughout the text and the claims, use of the word “about” in relation to a range of values (e.g., “about 22 to 35 wt %”) is intended to modify both the high and low values recited, and reflects the penumbra of variation associated with measurement, significant figures, and interchangeability, all as understood by a person having ordinary skill in the art to which this invention pertains.
For purposes of this specification (other than in the operating examples), unless otherwise indicated, all numbers expressing quantities and ranges of ingredients, process conditions, etc., are to be understood as modified in all instances by the term “about”. Accordingly, unless indicated to the contrary, the numerical parameters set forth in this specification and attached claims are approximations that can vary depending upon the desired results sought to be obtained by the present invention. At the very least, and not as an attempt to limit the application of the doctrine of equivalents to the scope of the claims, each numerical parameter should at least be construed in light of the number of reported significant digits and by applying ordinary rounding techniques. Further, as used in this specification and the appended claims, the singular forms “a”, “an” and “the” are intended to include plural referents, unless expressly and unequivocally limited to one referent.
Notwithstanding that the numerical ranges and parameters setting forth the broad scope of the invention are approximations, the numerical values set forth in the specific examples are reported as precisely as possible. Any numerical value, however, inherently contains certain errors necessarily resulting from the standard deviation found in their respective testing measurements including that found in the measuring instrument. Also, it should be understood that any numerical range recited herein is intended to include all sub-ranges subsumed therein. For example, a range of “1 to 10” is intended to include all sub-ranges between and including the recited minimum value of 1 and the recited maximum value of 10, i.e., a range having a minimum value equal to or greater than 1 and a maximum value of equal to or less than 10. Because the disclosed numerical ranges are continuous, they include every value between the minimum and maximum values. Unless expressly indicated otherwise, the various numerical ranges specified in this application are approximations.
In the following specification and the claims, a number of terms are referenced that have the following meanings.
The singular forms “a”, “an”, and “the” include plural references unless the context clearly dictates otherwise.
“Optional” or “optionally” means that the subsequently described event or circumstance may or may not occur, and that the description includes instances where the event occurs and instances where it does not.
As used herein, the term “elongate” is defined as something that is longer than it is wide. In other words, the width is smaller than its length.
As used herein, the term “circular” is defined as an object having a shape of a circle, i.e., an object having a simple closed shape. It is the set of points in a plane that are at a given distance from a given point, the center; equivalently it is the curve traced out by a point that moves in a plane so that its distance from a given point is constant. The distance between any of the points and the center is called the radius.
As used herein, the term “3D printing” is any of various processes in which material is joined or solidified under computer control to create a three-dimensional object, with material being added together, such as liquid molecules or powder grains being fused together, typically layer by layer. In the 1990s, 3D printing techniques were considered suitable only to the production of functional or aesthetical prototypes and, back then, a more comprehensive term for 3D printing was rapid prototyping. Today, the precision, repeatability and material range have increased to the point that 3D printing is considered as an industrial production technology, with the official term of “additive manufacturing”.
As used herein, the term “hole” is defined as an opening trough something; a gap; a cavity or an aperture that can have any cross-sectional shape.
As used herein, the phrase “fluid dynamic structure” is defined as any structure that produces a fluid dynamic force, such as fluid flow, when the structure moves through a fluid. One example of a fluid dynamic structure is an airfoil. Another example of a fluid dynamic structure is a turbine blade.
As used herein, the term “airfoil” is defined as the cross-sectional shape of a fluid dynamic structure, such as a wing, blade, sail, and the like.
As used herein, the term “fluid” is defined as a substance that has no fixed shape and yields easily to external pressure, such as a gas or a liquid.
Referring to
In the illustrated embodiment, an optional fluid conduit 21 extends from the rear machine connection member 20 to the front cutting ring 14, as shown in
Referring now to
It should be noted that the front cutting ring 14 is substantially identical to the rear cutting ring 18, except that the rear cutting ring 18 may have a slightly larger cutting diameter and the guide pad assemblies 26 may be omitted. Therefore, the rear cutting ring 18 will be described only briefly herein, and it will be appreciated that any description herein for the front cutting ring 14 also applies to the rear cutting ring 18.
In general, the front cutting ring 14 includes a sleeve member 22, a plurality of cutting head assemblies 24 and a plurality of guide pad assemblies 26. In the illustrated embodiment, the front cutting ring 14 has a total of six cutting head assemblies 24 and six guide pad assemblies 26, wherein each cutting head assembly 24 is separated by a guide pad assembly 26. It will be appreciated that the invention is not limited by the number of cutting head assemblies 24 and guide pad assemblies 26, and that the invention can be practiced with any desirable number of cutting head assemblies 24 and guide pad assemblies 26, depending on the physical size of the cutting tool 10. In addition, the invention can be practiced with the front cutting ring 14 having only the cutting head assemblies 24 and without the guide pad assemblies 26.
As shown in
The front cutting ring 14 can be made of any material with suitable strength to withstand cutting forces based on the application, such as tool steel, aluminum, and the like, using an additive manufacturing (i.e., 3D printing) process. In one embodiment, the front cutting ring 14 has a unitary construction in which the plurality of cutting head assemblies 24 and the plurality of guide pad assemblies 26 are integrally formed with the sleeve member 22. In an alternative embodiment, one or all of the cutting head assemblies 24 and guide pad assemblies 26 can be separately attached to the sleeve member 22.
The front cutting ring 14 also includes a central hub 28 with a plurality of spokes 30 extending radially outward from the central hub 28 to the sleeve member 22. Each spoke 30 may comprise a fluid dynamic structure, such as an airfoil, a turbine blade, and the like, to produce a fluid flow in an axially forward direction from the rear of the cutting tool 10 to the front of the cutting tool 10, as indicated by the arrows shown in
Each cutting head assembly 24 includes a leading support arm 34 extending radially outwardly from the rotational axis, RA, a trailing support arm 36 extending radially outwardly from the rotational axis, RA, and a cutting head 38. In the illustrated embodiment, the cutting head 38 includes a cutting insert pocket 40 and a guide pad pocket 42, as shown in
In the illustrated embodiment, the leading support arm 34 and the trailing support arm 36 are secured directly to the sleeve member 22. However, the sleeve member 22 can extend the entire length between the front cutting ring 14 and the rear cutting ring 18 such that the center tube 16 can be eliminated. Oppositely, the sleeve member 22 can be eliminated and the center tube 16 can extend entirely between the front cutting ring 14 and the rear cutting ring 18. In this case, the arms 34, 36 can be directly secured to the center tube 16.
In the illustrated embodiment, a sleeve member 22 includes a flange 32 that extends radially inward. The flange 32 and sleeve member 22 secure and position the front cutting ring 14 axially and radially to the center tube 16. It should be noted that the front cutting body 12 is secured to the central hub 28 of the front cutting ring 14. However, the front cutting body 12 could be secured to the sleeve member 22, depending on the dimensions of the front cutting body 12.
As shown in
In addition, the leading support arm 34 and the trailing support arm 36 sweep along a helical arc, as shown in
As shown in
One aspect of the invention is that the cutting tool 10 provides directed fluid flow to enhance chip evacuation during a cutting operation. This is achieved by one or both of the leading and trailing support arms 34, 36 of the cutting head assembly 24 comprising a fluid dynamic structure. In addition, one or both of the leading and trailing support arms 44, 46 of the guide pad assembly 26 may comprise a fluid dynamic structure. In the illustrated embodiment, the fluid dynamic structure comprises an airfoil, a turbine blade, and the like. However, it will be appreciated that the fluid dynamic structure can be any structure designed that produces a fluid dynamic flow when the structure moves through a fluid, such as machine fluid, air, and the like.
Some basic concepts of an airfoil will now be described. An airfoil has a suction surface (i.e., the upper surface), which is generally associated with higher velocity and lower static pressure. The airfoil produces a fluid dynamic force when the airfoil moves through a fluid, such as air, and the like. It should be understood that the component of this fluid dynamic force that is perpendicular to the direction of motion is called lift, and the component that is parallel to the direction of motion is call drag. In addition, an airfoil has a pressure surface (i.e., the lower surface), which has a comparatively higher static pressure than the suction surface. The pressure gradient between these two surfaces contributes to the lift force generated by the airfoil.
The geometry of the airfoil is described as follows: 1) the leading edge is the point at the front of the airfoil that has maximum curvature (i.e., minimum radius); 2) the trailing edge is defined similarly as the point of maximum curvature at the rear of the airfoil; 3) the chord line is the straight line connecting the leading and trailing edges. The chord length, or simply chord, c, is the length of the chord line. That is the reference dimension of the airfoil section.
The shape of the airfoil is defined using the following geometrical parameters: 1) the mean camber line or mean line is the locus of points midway between the upper and lower surfaces and its shape depends on the thickness distribution along the chord; 2) the thickness of an airfoil varies along the chord and it may be measured in either of two ways: a) thickness measured perpendicular to the camber line, sometimes described as the “American convention”; and b) thickness measured perpendicular to the chord line, sometimes described as the “British convention.”
Referring back to
In an alternative embodiment, the opening 31 in the center of the front cutting ring 14 and the rear cutting ring 18 can be closed to prevent the flow of fluid through the center tube 16. However, similar to the earlier embodiment, the leading and trailing support arms 34, 36 of the cutting head assembly 24 produces a flow of fluid that is directed in an axially rearward direction along the outside of the center tube 16. In addition, the guide pad assembly 26 has a single arm 47 with a fluid dynamic structure.
As mentioned earlier, the fluid conduit 21 allows fluid to travel from the rear machine connection member 20 to the front cutting ring 14 of the cutting tool 10, as shown in
As seen in
Referring now to
As mentioned above, the trailing support arm 36 of the cutting head assembly 24 is interconnected with the leading support arm 44 of an adjacent guide pad assembly 26, and the leading support arm 34 of the cutting head assembly 24 is interconnected with the trailing support arm 46 of a different adjacent guide pad assembly 26, as shown in
Referring now to
As mentioned earlier, the leading and trailing support arms 34, 36, of the cutting head assemblies 24 and the single arm 47 of the guide pad assemblies 26 of the front cutting ring 140 produce a flow of fluid directed from the front toward the rear of the cutting tool 10, thereby enhancing the evacuation of chips during a cutting operation. As shown in
In the illustrated embodiment shown in
Referring back to
It is noted that the front cutting ring 14 is attached to a front end 52 of the center tube 16 and the rear cutting ring 18 is attached an opposite, rear end 54 of the center tube 16 (
Referring now to
In general, the rear cutting ring 18 includes a sleeve member 22 and a plurality of cutting head assemblies 24. In the illustrated embodiment, each cutting head assembly 24 is capable of having a guide pad pocket 42 (
As shown in
Similar to the front cutting ring 14, the rear cutting ring 18 can be made of steel material, such as tool steel, using an additive manufacturing (i.e., 3D printing) process. In one embodiment, the rear cutting ring 18 has a unitary construction in which the plurality of cutting head assemblies 24 are integrally formed with the sleeve member 22. In an alternative embodiment, one or all of the cutting head assemblies 24 can be separately attached to the sleeve member 22.
Also similar to the front cutting ring 14, the leading and trailing support arms 34, 36 of each cutting head assembly 24 of the rear cutting ring 18 comprise a fluid dynamic structure, such as an airfoil, turbine blade, and the like. As a result, the leading and trailing support arms 34, 36 of each cutting head assembly 24 produce fluid flow in an axially rearward direction toward the rear machine connection member 20 of the cutting tool 10, as indicated by the arrows in
The rear cutting ring 18 is connected to the rear machine connection member 20 and is also attached to the center tube 16 (
Once the rear machine connection member 20 is in fluid communication with the fluid source, the fluid can be provided throughout the cutting tool 10 of the invention. Specifically, fluid entering the rear machine connection member 20 and can travel directly into the rear cutting ring 18. In addition, fluid can travel past the rear cutting ring 18, through the fluid conduit 21 and directly into the front cutting ring 14, into the cutting head assemblies 24 as described above, and exit proximate the cutting insert pocket 40 and the guide pad pocket 42 of each cutting head assembly 24.
In the embodiments described above, each cutting head assembly 24 of the front cutting ring 14 and the rear cutting ring 18 has a leading support arm 34, 44 and a trailing support arm 36, 46. However, it will be appreciated that the invention can be practiced with the cutting head assembly and/or guide pad assembly having only a single arm for supporting the cutting head and a single arm for supporting the guide pad head.
Referring now to
Referring back to
As described above, the fluid dynamic structure defined by the one or more arms 34, 36, 44, 46, 47, 56, 58 that support the cutting head 38 and the guide pad head 48 can facilitate chip evacuation by multiple methods. First, the arms 34, 36 supporting the cutting head 38 can mechanically “shovel” the chips away from the cutting edge in a similar fashion to flutes in a drill. Second, the arms 34, 36, 44, 46, 47, 56, 58 function as a fluid dynamic structure similar to an airfoil. The work generated by rotating the cutting tool 10 causes the fluid to exert a downward force on the arms 34, 36, 44, 46, 47, 56, 58 and cause the arms 34, 36, 44, 46, 47, 56, 58 to exert an equal upward force on the fluid, which results in fluid flow directed towards the rear machine connection member 20.
The efficiency of the fluid flow can be improved when machining blind holes by adding the spokes 30, 62 that act as a turbine blade. These turbine blades are designed to draw fluid into the machined hole from the hole entrance (near the machine spindle), which will flow through the center tube 16 of the cutting tool 10, to the bottom of the machined hole (near the front of the cutting tool 10). When fluid exits the center of the cutting tool 10 at the bottom of the machined hole, the fluid will be drawn up and out of the machined hole by the airfoil style arms 34, 36, 44, 46, 47, 56, 58 that support the cutting region and guide pad.
In addition, the fluid dynamic structures in the form of airfoil shaped arms/blades 30, 34, 36, 44, 46, 47, 56, 58 may also be used on the outer diameter of the tool purely to generate fluid flow without being used to support a cutting or guide pad region. Fluid flow can also be directed by positioning the exit hole 37 near the cutting edge, using a combination of machine fluid and the airfoil shape arms to manipulate fluid flow to assist in chip evacuation, and using the airfoil arm geometry to create a compressor that will force fluid out of holes near the cutting edge of the cutting tool 10.
The patents and publications referred to herein are hereby incorporated by reference.
Having described presently preferred embodiments the invention may be otherwise embodied within the scope of the appended claims.
| Number | Name | Date | Kind |
|---|---|---|---|
| 5135337 | Adamson | Aug 1992 | A |
| 5152640 | Regis et al. | Oct 1992 | A |
| 5605420 | Feldsine | Feb 1997 | A |
| 5921727 | Depperman | Jul 1999 | A |
| 5934842 | Gupta | Aug 1999 | A |
| 6120218 | Bishop | Sep 2000 | A |
| 6655883 | Maar | Dec 2003 | B2 |
| 6913428 | Kress | Jul 2005 | B2 |
| 8764354 | Schuffenhauer | Jul 2014 | B2 |
| 8950985 | Durand-Terrasson | Feb 2015 | B2 |
| 9056357 | Bozkurt | Jun 2015 | B2 |
| 9216461 | Athad | Dec 2015 | B2 |
| 9283624 | Freyermuth et al. | Mar 2016 | B2 |
| 9623494 | Bozkurt | Apr 2017 | B2 |
| 10464138 | Kozaki et al. | Nov 2019 | B2 |
| 10799960 | Zetek et al. | Oct 2020 | B2 |
| 10940551 | Semnisky | Mar 2021 | B1 |
| 20050019110 | Astrakhan | Jan 2005 | A1 |
| 20110182676 | Frank et al. | Jul 2011 | A1 |
| 20110188954 | Frank | Aug 2011 | A1 |
| 20130136551 | Nisikawa | May 2013 | A1 |
| 20130156520 | Hacker et al. | Jun 2013 | A1 |
| 20140161543 | Francis et al. | Jun 2014 | A1 |
| 20190099816 | Zetek et al. | Apr 2019 | A1 |
| 20190314903 | Haenle et al. | Oct 2019 | A1 |
| 20190314904 | Haenle | Oct 2019 | A1 |
| 20200055129 | Leuze | Feb 2020 | A1 |
| 20220023960 | Ljatifi | Jan 2022 | A1 |
| Number | Date | Country |
|---|---|---|
| 209139934 | Jul 2019 | CN |
| 19934125 | Jan 2001 | DE |
| 10359854 | Jul 2005 | DE |
| 102009022051 | Sep 2010 | DE |
| 0074542 | Mar 1983 | EP |
| 1 984 135 | Oct 2008 | EP |
| 3772384 | Feb 2021 | EP |
| 3819055 | May 2021 | EP |
| 2927555 | Aug 2009 | FR |
| 2967366 | May 2012 | FR |
| 2006015444 | Jan 2006 | JP |
| 4654622 | Mar 2011 | JP |
| 2017030075 | Feb 2017 | JP |
| 2018149655 | Sep 2018 | JP |
| 2018149656 | Sep 2018 | JP |
| WO1987004969 | Aug 1987 | WO |
| 2010020234 | Aug 2009 | WO |
| WO-2010097082 | Sep 2010 | WO |
| WO2012101319 | Aug 2012 | WO |
| WO2019002050 | Jan 2019 | WO |
| WO2020118460 | Jun 2020 | WO |
| WO2021023489 | Feb 2021 | WO |
| Entry |
|---|
| Jan. 29, 2021 Search report EP App. No 20190517.1. |
| Apr. 12, 2022 International Search Report WO App. No. PCT/US2021/062367. |
| Mar. 30, 2022 International Search Report WO App. No. PCT/US2021/062322. |
| Jun. 6, 2022 Office action (3 months) (US Only) U.S. Appl. No. 17/115,997. |
| Nov. 5, 2020 Notice of Allowance—U.S. Appl. No. 16/557,533. |
| Number | Date | Country | |
|---|---|---|---|
| 20220176480 A1 | Jun 2022 | US |
