Patent Application
20200254534
The present disclosure is directed to a tool and, in particular, a tool having a plurality of cutting portions that is capable of performing a combination of cutting operations.
Combination tools are used by a variety of industries during material removal operations where it is desirable for a single tool to perform more than one operation on workpiece. This is especially true of machine shops utilizing interpolated milling methods to consolidate material removal operations. Combination tools may include a variety of different cutting elements to achieve these various cuts. For example, the tool may include a mill portion and a drill portion or may include a mill portion and a bore portion. The cutting elements of a combination tools may be selected based on the tolerances required of the finished workpiece, its surface finish, or various processing parameters.
The combination tool's cutting elements, however, may affect its performance during a material removal operation, as evaluated by heat generated by the combination tool, material removal rates, and surface finish of the workpiece. Some of these effects may adversely impact the material removal operation and/or the finished workpiece. The combination tool may, for example, generate heat when operating on workpieces that require tight tolerances and high quality surface finish, and such heat generation may cause the formation (on the workpieces) of certain undesirable materials or coatings that would later need to be removed via subsequent operations. Such subsequent operations typically require time consuming retooling and/or otherwise result in extra downtown between machining operations, either of which adversely impacts machine shops' efficiencies and bottom lines.
Accordingly, a single tool capable of drilling, milling, and boring may be desired to form high quality cuts in workpieces without excessive heat buildup or other adverse effects.
The present disclosure is directed towards a cutting tool having a combination of cutting portions. The cutting tool may include a drill portion, a mill portion, and/or a bore portion, where a diameter of the mill portion is smaller than a diameter of the drill portion. In some embodiments, the diameter of the bore portion is larger than the diameter of the mill portion and in some of these embodiments, the diameter of the bore portion is greater than the diameter of the drill portion. In some embodiments, the drill portion, the mill portion, and/or the bore portion are each positioned along a central axis of the cutting tool, and in some of these embodiments, the mill portion is between the drill portion and the bore portion. In some of these embodiments, the drill portion is provided at an axial end of the cutting tool. Gaps may be provided between the drill portion and the mill portion and/or between the mill portion and the bore portion.
The cutting tool may also include a chamfer portion. The chamfer portion may be positioned on a side of the bore portion that is opposite from the axial end, and a gap may be provided between the bore portion and the chamfer portion or the chamfer portion may abutt the bore portion. The chamfer portion may instead be positioned between the mill portion and the bore portion, and a gap may be provided between the mill portion and the chamfer portion and/or between the chamfer portion and the bore portion.
The present disclosure is also directed towards method of machining a workpiece using a cutting tool having a drill portion, a mill portion, and/or a bore portion. The method may include the steps of drilling a hole in the workpiece with the drill portion; milling the hole in the workpiece with the mill portion in an interpolated milling operation, wherein the mill portion includes a diameter that is smaller than a diameter of the drill portion; and boring the hole in the work piece with the bore portion. The method may also be utilized with the cutting tool that further includes a chamfer portion, such that the method further includes chamfering the hole in the workpiece with the chamfer portion.
These and additional features provided by the embodiments described herein will be more fully understood in view of the following detailed description, in conjunction with the drawings.
The embodiments set forth in the drawings are illustrative and exemplary in nature and not intended to limit the subject matter defined by the claims. The following detailed description of the illustrative embodiments can be understood when read in conjunction with the following drawings, where like structure is indicated with like reference numerals and in which:
Reference will now be made in detail to embodiments of a tool capable of performing a number of different cutting operations in succession. The tool includes a plurality of cutting portions such as, for example, a drilling portion, a milling portion, and a boring portion. Optionally, the tool may include additional cutting portions such as, for example, a chamfering portion. Inclusion of multiple cutting portions permits a single tool to perform multiple machining operations in quick succession without retooling. For example, the tool according to one or more embodiments disclosed herein may perform a drilling operation, a milling operation, a boring operation and, where included, a chamfering operation, and the tool may perform all of these combination of operations in quick succession and without utilization of other cutting tools. Thus, tools according to the present disclosure may provide improved cycle times.
The tool according to the present disclosure may eliminate the need for a reaming operation, which may not introduce a desired surface finish to the workpiece. The tool herein disclosed may also eliminate the need for subsequent operations, such as a chemical milling operation, in which select material is removed from the workpiece following the operation that forms the hole or recess. For example, excessive heat generation may occur during machining operations on workpieces that require tight tolerances and high qualify surface finish, and this resulting heat buildup may cause formation of certain undesirable materials/coatings that must be subsequently removed by a separate material removal operation (e.g., a chemical milling operation); however, this subsequent material removal operation may be eliminated by utilizing a tool having a plurality of cutting portions as disclosed herein. For example, where the workpiece is a high temperature alloy (e.g., titanium) fan or rotor for a rotating disc (that requires tight tolerances and a high qualify surface finish), alpha case (i.e., a brittle oxide of titanium) may form on the workpiece when temperatures rise above a threshold temperature of about eight hundred degrees Fahrenheit (800° F.), and the tool may include one or more cutting elements (e.g., in a milling portion) that removes the alpha case material without retooling for subsequent material operations.
Tools according to the present disclosure may be made with a variety of conventionally known materials that are suitable for a material removal operation. Such materials include, without limitation, cemented tungsten carbide (including cemented cobalt tungsten carbide) and various grades of tool steel. Moreover, the surfaces of the presently disclosed tools may be coated with dissimilar materials to improve certain properties of the tool, and such coatings include without limitation ceramic coatings, such as TiN, TiC, and TiAlN. In addition, one or more of the cutting portions of the tool may be coated with different coatings that one or more of the other cutting portions.
Because the tool 10 may be utilized in more than one successive material removal operations, or a combination of material removal operations, the tool 10 is sometimes referred to as a combination tool or multi-operation tool. As hereinafter described, the tool illustrated in
The tool 10 extends along a central axis X and includes a proximal end 12 and a distal end 14 (sometimes referred to as an axial end 14). The tool 10 includes a cutting portion 15 that extends proximally from the distal end 14 towards the proximal end 12, and the cutting portion 15 includes an axial cutting face 16 arranged at the distal end 14 for engaging a work piece as the tool 10 is plunged there-into during a drilling operation. The tool 10 may also include a shank portion 18 that extends proximally from (a proximal end of) the cutting portion 15. Here, the shank portion 18 is arranged at the proximal end 12 (of the tool 10). The shank portion 18 may provide the means by which a piece of equipment (not illustrated) may grab (or attach to) the tool 10. In some embodiments, the shank portion 18 includes a uniform shank portion that extends proximally along the central axis X with a uniform diameter and is attached within a piece of equipment; whereas in other embodiments, the shank portion 18 also includes a tapered portion that extends from (a proximal end of) the cutting portion 15, thereby reducing (or increasing) the cutting portion 15 diameter relative to the uniform diameter of the uniform shank portion that extends proximally from the tapered portion.
In the illustrated embodiment, the cutting portion 15 of the tool 10 includes a drilling portion 20, a milling portion 22, and a boring portion 24 that are respectively arranged along the central axis X of the tool 10, from the distal end 14 towards the proximal end 12, as illustrated in
The drilling portion 20 and the milling portion 22 each include a plurality of flutes and respective lands that helically extend, around the tool 10, proximally along the central axis X from the distal end 14. The intersection between the flutes and lands of the drilling portion 20 and the milling portion 22 define respective cutting edges. The drilling portion 20 and the milling portion 22 may have varying numbers of flutes, lands, and cutting edges depending on the end use application. In the illustrated embodiment, the drilling portion 20 and the milling portion 22 have the same number of flutes, such that the flutes of the drilling portion 20 extend into the flutes of the milling portion 22. However, the drilling portion 20 and the milling portion 22 may have different numbers of flutes. In addition, the chamfering portion 26 may include the same or a different number of flutes from either or both of the drilling portion 20 and the milling portion 22. In the illustrated embodiment, the chamfering portion 26 includes less flutes than the drilling portion 20 and the milling portion 22; however, in other embodiments, the chamfering portion 26 may include an equal or greater number of flutes compared to the drilling portion 20 and the milling portion 22. Moreover, the boring portion 24 includes a tooth 25. In the illustrated embodiment, the boring portion 24 is configured as a single point bore having one tooth 25; however, in other embodiments, the boring portion 24 may include one or more additional teeth (not illustrated) that may be aligned with the tooth 25 (along the central axis X) or axially offset along the central axis X relative to the tooth 25, and these one or more additional teeth may be the same as the tooth 25 or any of them may be differently configured than the tooth 25.
As illustrated, the drilling portion 20 may be positioned along the central axis X proximate to the distal end 14 of the tool 10 and may define a drill diameter D1. In addition, the drilling portion 20 may be configured as any number of drills without departing from the present disclosure. The milling portion 22 may be positioned proximal of the drilling portion 20 and may define a mill diameter D2. In the illustrated embodiment, the milling portion 22 is configured as an end mill and abuts (a proximal end of) the drilling portion 20, but in other embodiments, a gap may extend between the milling portion 22 and the drilling portion 20. The boring portion 24 may be positioned proximal of the milling portion 22 and may define a bore diameter D3. In the illustrated embodiment, a gap extending along the central axis X is provided between the boring portion 24 and the milling portion 22; however, in other embodiments, the gap is smaller or larger than that illustrated in
The drill diameter D1, the mill diameter D2, the bore diameter D3, and the chamfer diameter D4 may have varying dimensions depending on the particular end use application, and their values relative to each other may vary. For example, the drill diameter D1, the mill diameter D2, the bore diameter D3, and the chamfer diameter D4 may all have the same value, may all have different values, or two or more of them may have the same value. In the exemplary embodiment of
The milling operation (Op2) may impart lower temperatures to the workpiece 2 than what was imparted during the drilling operation (Op1), but the surface finish of the workpiece 2 (i.e., of the milled hole H2) may nevertheless be unsatisfactory for some end use applications. Moreover, it may be desirable to further enlarge the diameter of the milled hole H2, for example to provide greater accuracy of the diameter, and/or to otherwise further machine the milled hole H2 (e.g., to provide a taper, etc.). Accordingly, the boring portion 24 of the tool 10 may be rotated about the central axis X and brought into engagement with the workpiece 2 to perform a boring operation, which is identified as “Op3” in
After the boring operation (Op3) has been performed for form the bored hole H3, the tool 10 may be configured to perform a chamfering operation identified as “Op4” in
As previously disclosed, the tool 10 may be utilized to provide a plurality of material removal processes in rapid succession, including but not limited to, one or more of the following: the drilling operation (Op1), the milling operation (Op2), the boring operation (Op3), and the chamfering operation (Op4). In some embodiments, one or more of the foregoing are performed sequentially (i.e., the drilling operation (Op1), then the milling operation (Op2), then the boring operation (Op3), and then the chamfering operation (Op4)). In other embodiments, however, they are performed in various other non-sequential orders, and such non-sequential orders of operation may or may not depend on the positioning of the cutting portions (i.e., the drilling portion 20, the milling portion 22, the boring portion 24, and/or the chamfering portion 28) relative to each other along the central axis X. For example, the tool 10 may be provided with the milling portion 22 located at the axial face 16 such that the milling portion 22 is utilized to create the first hole via a plunge milling operation.
First, the workpiece 2 to be machined is placed within a suitable machining tool (not depicted) such as, for example, a computer numerical control (“CNC”) machining center (“Machining Center”). Then the tool 10 is installed and positioned therein so that its distal tip or axial cutting face 16 is spaced above the top surface 4 of the workpiece 2. In this example, the axial cutting face 16 is initially spaced about 1 mm above the top surface 4. Thereafter, a first material removal process commences, which may include utilization of any number of cutting tools. In the present example, the first material removal process is the drilling operation (Op1) utilizing the drilling portion 20 of the tool 10. Here, the drilling operation (Op1) commences with the tool 10 rotating about the central axis X thereof at a speed of about 1,500 revolutions per minute (“RPM”) and being fed in the downward direction Y towards the top surface 4 and into the workpiece 2 at a feedrate of about one hundred and fifty (150) millimeters per minute (“mm/min”), so as to plunge the axial cutting face 16 of the tool 10 into the workpiece 2 to a depth of about seven (7) mm below the top surface 4 of workpiece 2, thereby creating the drill hole H1 having a diameter that is about equal to the drill diameter D1 of drilling portion 20. In other examples, the tool 10 may start and stop at different distances above and below the top surface 4, depending on the end use application and/or the workpiece to be machined. The drilling operation (Op1) causes the drilling portion 20 to engage the workpiece 2 so as to remove the desired portion(s) thereof, which in turn results in the drill hole H1. In some embodiments, the drilling operation (Op1) includes a peck drilling cycle. The drilling operation (Op1) concludes once the drill hole H1 has been suitably formed within the workpiece 2 via the drilling portion 20 and, if no further material removal is needed, the tool 10 may be withdrawn therefrom. If further material removal operations are to be performed, however, the conclusion of the drilling operation (Op1) marks the beginning of at least a second material removal process, for example, the beginning of the milling operation (Op2). However, the boring operation (Op3) or the chamfering operation (Op4) may instead follow the drilling operation (Op1), and one or more material removal operations may subsequently follow thereafter. At the conclusion of the drilling operation (Op1), the tool 10 may cease rotation about the central axis X, or immediately ramp up or down to another rotational speed as specified in a subsequent material removal operation.
A second material removal process is then performed. The second material removal process may also involve any number of cutting tools and commences following completion of the first material removal process such as, for example, following completion of the drilling operation (Op1). In this example, the second material removal operation is the milling operation (Op2) where the milling portion 22 having the mill diameter D2 is utilized to enlarge the drill hole H1 and/or otherwise remove desired portion(s) of the workpiece 2. The milling operation (Op2) may include a plunge process followed by an interpolated milling process. For example, the milling operation (Op2) may include a first step where the combination tool 10 plunges in the downward direction Y towards the workpiece 2 and into the drill hole H1 until the milling portion 22 is within the drill hole H1 formed in the prior drilling operation (Op1), at which time an interpolated milling process may be utilized to interpolate the drill hole H1 to a desired size. Thus, the tool 10 does not start interpolating until it is already within the drill hole H1 formed in the drilling operation (Op1); however, in other embodiments, the tool 10 begins an interpolating process at a location above the workpiece 2, after which the tool 10 is plunged into the workpiece 2 while interpolating. Various interpolated drilling procedures may be utilized, for example, a circle interpolating process (i.e., orbital drilling) where the tool 10 is operated in a tool path that follows circular interpolation, a helical interpolating process where the tool 10 is operated in a tool path that follows a helical interpolation, etc. It will be appreciated, however, that other tool paths may be followed when utilizing the interpolated drilling process and, moreover, that other drilling processes may be utilized.
The milling operation (Op2) begins with the tool 10 being translated in the downward direction Y such that the boring portion 22 is positioned within drill hole H1. Once the boring portion 22 is in the drill hole H1, the tool 10 may commence rotation about the central axis X; or, if the tool 10 did not cease rotation following culmination of a prior material removal operation, the rotational speed of the tool 10 may be increased or decreased as needed when the boring portion 22 is within the drill hole H1.
Alternatively, the tool 10 may be rotating, at a speed of a prior material removal process or at a speed specified for the milling operation (Op2), before it translates along the central axis X in the downward direction Y to position the boring portion 22 within the drill hole H1. Accordingly, the tool 10 may commence rotation about the central axis X when the axial cutting face 16 of the tool 10 is in the same position as it was at the end of the prior material removal process.
In operation, the milling operation (Op2) may commence once the axial cutting face 16 at the distal end 14 of tool 10 is repositioned, for example, to a distance of about 1 mm above the top surface 4 of the workpiece 2. In other examples, the milling operation (Op2) may commence when the tool 10 has been repositioned such that the milling portion 22 is within the drill hole H1. During the milling operation (Op2), the tool 10 begins rotating along its central axis X at a specified RPM and then plunges in the downward direction Y into the drill hole H1 at a specified feedrate. Alternatively, the tool 10 begins rotating after the milling portion 22 has been positioned within the drill hole H1. Once the milling portion 22 is within the drill hole H1 formed in the drilling operation (Op1) at the desired location, it begins operating in a tool path following the circular interpolation R. Accordingly, the milling portion 22, via interpolated milling, enlarges the drill hole H1 into the milled hole H2 having a larger diameter that is defined by a diameter of the circular interpolation R. In one such exemplary milling process (Op2), the tool 10 rotates about the central axis X at a speed of about 3,400 RPM while being fed in the downward direction Y towards and into the workpiece 2 at a feedrate of about 150 mm/min, so as to plunge the axial cutting face 16 of the tool 10 into the workpiece 2 to a depth of about twenty (20) mm below the top surface 4 of the workpiece 2. Once at that depth, the combination tool 10 begins to interpolate following the circular interpolation R (or other tool path) having a tool path diameter of about 7.8 mm. This example of the milling operation (Op2) causes milling portion 22 to engage the drill hole H1 of the workpiece 2 so as to remove (interpolate) additional material therefrom, resulting in the mill hole H2, which has a diameter that is about equal to the tool path following the circular interpolation R. The milling process (Op2) concludes once a larger hole, such as the mill hole H2, has been suitably machined into the workpiece 2 and, as detailed below, a third material removal process may be initiated immediately thereafter.
The third material removal process may involve any number of cutting tools and commences following completion of the second material removal process such as, for example, following completion of the milling process (Op2). In this example, the third material removal process is the boring operation (Op3) where boring portion 24 having the bore diameter D3 is utilized to remove desired portion(s) of the workpiece 2, for example, from within the previously enlarged milled hole H2. The boring operation (Op3) may begin immediately upon completion of the prior material removal process and without withdrawing the tool 10 from the workpiece 2. The boring portion 24 may commence rotation about the central axis X when the axial cutting face 16 of the tool 10 is in the same position as it was at the end of the prior material removal process. In other embodiments, the axial cutting face 16 of the tool 10 is plunged further into the workpiece 2 before commencing rotation, whereas, in even other embodiments the tool 10 is fully with drawn from the workpiece before commencing rotation.
Accordingly, the boring portion 24 may instead commence rotation about the central axis X, for example, at a speed of about 4,000 RPM, after the axial cutting face 16 of the tool 10 translates from a position that is about 20 mm below the top surface 4 of the workpiece 2 to a position that is about 30 mm below the top surface 4 of the workpiece 2. Once rotating, the tool 10 may then continue to be fed into the workpiece 2 in the downward direction Y and at a feedrate of about one hundred (100) mm/min. Alternatively, the boring portion 24 may commence rotation about the central axis X when the axial cutting face 16 is about twenty (20) mm below the top surface 4 and then, while rotating, plunge into the workpiece 2 until the axial cutting face 16 is about thirty (30) mm below the top surface 4 of the workpiece 2. The tool 10 may rotate about the central axis X at various speeds during the boring operation (Op3) and, in the depicted example, the tool 10 rotates at a speed of about 4,000 RPM. The boring operation (Op3) concludes once the boring portion 24 has removed the desired about of material from workpiece 2 such that the milled hole H2 has been enlarged into the bored hole H3 and, at this time, the tool 10 may be fully withdrawn from the workpiece 2 and the workpiece 2 may be removed from the piece of equipment being utilized (e.g., a CNC Machining Center). In some embodiments, before the tool 10 is withdrawn from the bored hole H3 or otherwise fully removed from the workpiece 2, the tool 10 may be first offset in a lateral direction opposite of the boring tooth 25 of the boring portion 24 (i.e., in a direction radial outward from the central axis X), so as to provide clearance for the tool 10 as it is withdrawn such that it doesn't score the bored hole H3 formed into the workpiece 2. In one such example embodiment, the tool 10 is first offset by about 0.1 mm to provide clearance for the boring tooth 25 before the tool 10 is withdrawn from the bore hole H3. This marks the end of the entire material removal operation unless the tool 10 includes an additional Cutting Portion, such as the chamfering portion 26.
However, where the tool 10 includes a fourth Cutting Portion, for example, the chamfering portion 26, conclusion of the third material removal process may instead mark the beginning of an optional, fourth material removal process as discussed below.
The optional fourth material removal process may involve any number of cutting tools and may commence, if at all, following completion of a third material removal process such as, for example, following completion of the boring operation (Op3). A fourth material removal process may be utilized to remove additional material from the workpiece 2 so as to form, for example, a conical hole or countersink. In this example, the fourth material removal process is a chamfering operation (Op4) where the chamfering portion 26 having the chamfer diameter D4 is plunged into the top surface 4 of the workpiece 2 to form a countersink or chamfer H4 in the bored hole H4 proximate to the top surface 4; however, in other embodiments the chamfering operation (Op4) may be performed via interpolation rather than just plunging. As with the prior third material removal process (i.e., the boring operation (Op3)), the chamfering operation (Op4) may commence immediately upon completion of the prior material removal process without withdrawing the tool 10 from the bored hole H3 previously formed into the workpiece 2. Accordingly, the chamfering portion 26 may commence rotation about the central axis X when the axial cutting face 16 of the tool 10 is in the same position as it was at the end of the prior material removal process. In other embodiments, the axial cutting face 16 of tool 10 is plunged further into the workpiece 2 before commencing rotation, or the tool 10 is fully removed from the workpiece 2 prior to commencing further rotation. Accordingly, the chamfering portion 26 may commence rotation about the central axis X, for example, at a speed of about 4,000 RPM, after the axial cutting face 16 of the tool 10 translates from a position that is about thirty (30) mm below the top surface 4 of the workpiece 2 to a position that is about 36.1 mm below the top surface 4 of workpiece 2. Once the chamfering portion 26 has commenced rotation it may be fed into and withdrawn from the workpiece 2 at a feedrate of, for example, sixty (60) mm/min, thereby forming a countersink. In the illustrated example, following rotation of the chamfering portion 26 the tool 10 is raised approximately two (2) mm from the position where the axial cutting face 16 is about 36.1 mm below the top surface 4, such that the axial cutting face 16 is about 34.1 mm below the top surface 4 of the workpiece 2. Once the countersink H4 has been formed via the chamfering operation (Op4), the material removal process may be deemed complete and the workpiece 2 may be removed from the piece of equipment being utilized (e.g., a CNC Machining Center). As with the boring operation (Op3) detailed above, after conclusion of the chamfering operation (Op4) but before removal of the tool 10 from the hole formed into the workpiece 2, the tool 10 may be first offset in a lateral direction (e.g., in a direction opposite of the boring tooth 25 of the boring portion 24), so as to provide clearance for the tool 10 as it is withdrawn such that the boring tooth 25 doesn't score the hole just formed into the workpiece 2.
In some embodiments, the chamfering operation (Op4) further includes a second chamfering operation. For example, the chamfering portion 26 may be utilized to form a “front chamfer” in a front side (i.e., the top surface 4) of the workpiece 2 and, once that front chamfer has been formed via the chamfering portion 26, but before retracting the tool 10 from the hole formed into the workpiece 2, a back chamfer (not illustrated) may be formed into a rear side (i.e., the bottom surface 6) of the workpiece 2 that is opposite the (front) chamfer H4. In one embodiment, the tool 10 is partially retracted through the hole so that the boring tooth 25 is proximate to the bottom surface 6 of the workpiece 2, and then a back chamfer is milled or formed into the workpiece 2 via the interpolation of the boring tooth 25.
The foregoing material removal operation utilizing combination tool 10 is illustrated in
It should be noted that the configuration of a particular material that an end user will perform a material removal operation on may exhibit different material properties than those of the present experiment. These material properties may govern the formation of the chip. To satisfy the requirements of the end user's material removal operation, various parameters of the tool 10 may be modified to further increase the efficiency of the overall material removal operation.
One or more of the cutting operations performed by the tool 10 may result in excessive chip or Swarf generation that may adversely impact operation. For example, utilization of a single point boring tool may cause long, continuous chips, or Swarf, that may wrap around the shank portion 18 or other proximal portions of the tool 10. Swarf wrapping around the tool 10 in this manner may impact tool rotation speed and/or rub against the workpiece 2 and damage the finish. The tool 10 may thus include one or more features that facilitate chip removal. For example, the tool 10 may include one or more features that inhibit Swarf from wrapping around the proximal end 12 of the tool, proximate to the shank portion 18. These Swarf inhibiting features may extend solely along the shank portion 18, but in some embodiments, may extend distally from the shank portion 18 into at least one of the Cutting Portions positioned distal from the shank portion. In the exemplary embodiment illustrated in
The combination tool 10 may also include one or more features that facilitate chip breaking such that otherwise longer chips are broken into smaller discrete chips. Thus, the tool 10 may include chip breaker features. These chip breaker features may be positioned along the cutting edges of one or more of the Cutting Portions. In one example, the milling portion 22 includes chip breaker features positioned along the cutting edges thereof. The chip breaker features may be oriented to be approximately perpendicular to the central axis X, or may be angled (with reference to
Material removal operations using conventional combination tools may involve tool pressures, surface finish conditions, tool wear, heat generation, dimensional inaccuracy, or combinations thereof that are undesirable. Such conditions may be exacerbated as material removal rates are increased to accommodate production volumes. The present disclosure is directed to tools that include a combination of elements that may improve the conditions experienced in material removal operations by modifying the chip creation and chip evacuation methodology as compared to conventional tools. Cutting elements that may be included on the drilling portion 20 of the tool 10 include a contoured drill point and an extended gash contour that is positioned along the lands of the drilling portion 20. By incorporating such elements into the drilling portion 20 of the tool 10, the tool 10 may modify the method of chip generation, such that cutting forces and temperatures at the workpiece 2 are reduced as compared to conventional tools. Further, holes produced by the drilling portions 20 may exhibit improved geometric conditions, positional tolerance, and/or surface condition.
As used herein, the term “about” means plus or minus 15% of the numerical value of the number with which it is being used. Therefore, “about 40” means “in the range of 34 to 46.” It is also noted that the terms “generally” and “substantially” may be used herein to represent the inherent degree of uncertainty that may be attributed to any quantitative comparison, value, measurement, or other representation. These terms are also used herein to represent the degree by which a quantitative representation may vary from a stated reference without resulting in a change in the basic function of the subject matter at issue.
Therefore, the disclosed systems and methods are well adapted to attain the ends and advantages mentioned as well as those that are inherent therein. The particular embodiments disclosed above are illustrative only, as the teachings of the present disclosure may be modified and practiced in different but equivalent manners apparent to those skilled in the art having the benefit of the teachings herein. Furthermore, no limitations are intended to the details of construction or design herein shown, other than as described in the claims below. It is therefore evident that the particular illustrative embodiments disclosed above may be altered, combined, or modified and all such variations are considered within the scope of the present disclosure. The systems and methods illustratively disclosed herein may suitably be practiced in the absence of any element that is not specifically disclosed herein and/or any optional element disclosed herein. While compositions and methods are described in terms of “comprising,” “containing,” or “including” various components or steps, the compositions and methods can also “consist essentially of” or “consist of” the various components and steps. All numbers and ranges disclosed above may vary by some amount. Whenever a numerical range with a lower limit and an upper limit is disclosed, any number and any included range falling within the range is specifically disclosed. In particular, every range of values (of the form, “from about a to about b,” or, equivalently, “from approximately a to b,” or, equivalently, “from approximately a-b”) disclosed herein is to be understood to set forth every number and range encompassed within the broader range of values. Also, the terms in the claims have their plain, ordinary meaning unless otherwise explicitly and clearly defined by the patentee. Moreover, the indefinite articles “a” or “an,” as used in the claims, are defined herein to mean one or more than one of the elements that it introduces. If there is any conflict in the usages of a word or term in this specification and one or more patent or other documents that may be incorporated herein by reference, the definitions that are consistent with this specification should be adopted.
As used herein, the phrase “at least one of” preceding a series of items, with the terms “and” or “or” to separate any of the items, modifies the list as a whole, rather than each member of the list (i.e., each item). The phrase “at least one of” allows a meaning that includes at least one of any one of the items, and/or at least one of any combination of the items, and/or at least one of each of the items. By way of example, the phrases “at least one of A, B, and C” or “at least one of A, B, or C” each refer to only A, only B, or only C; any combination of A, B, and C; and/or at least one of each of A, B, and C.
This application claims priority to and the benefit of pending U.S. Provisional Application No. 62/558,003 filed on Sep. 13, 2017, which is incorporated by reference herein in its entirety.
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/US2018/050685 | 9/12/2018 | WO | 00 |
| Number | Date | Country | |
|---|---|---|---|
| 62558003 | Sep 2017 | US |
