NZ331695A - A method and apparatus for forming metallic parts by forging which includes continuous metal stock - Google Patents

Description

0 New Zealand No. 331695 International No. PCT/ TO BE ENTERED AFTER ACCEPTANCE AND PUBLICATION Priority dates: 30.12.1994;11.08.1995; Complete Specification Filed: 18.12.1995 Classification:^) B21K5/02 Publication date: 29 April 1999 Journal No.: 1439 NEW ZEALAND PATENTS ACT 1953 COMPLETE SPECIFICATION Title of Invention: A method and apparatus for forming metallic parts Name, address and nationality of applicant(s) as in international application form: BLACK & DECKER INC, a Delaware body corporate of Drummond Plaza Office Park, 1423 Kirkwood Highway, Newark, Delaware 19711, United States of America 3316 # Under the provisions of Regulation 23 (1) the - Specification has been ante-dated t0 19 3L. caiikQ Initials Patents Form No. 5 Our Ref: JB210534 Divisional Application Out of NZ 300765 NEW ZEALAND PATENTS ACT 1953 COMPLETE SPECIFICATION A METHOD AND APPARATUS FOR FORMING METALLIC PARTS We, BLACK & DECKER INC, a body corporate under the laws of Delaware, USA of Drummond Plaza Office Park, 1423 Kirkwood Highway, Newark, Delaware 19711, United States Of America, hereby declare the invention, for which We pray that a patent may be granted to us and the method by which it is to be performed, to be particularly described in and by the following statement: (followed by Page 1a) ! I f] 2 or; i «2£££Ived PT0575609 OF N.Z. °FFIC£' 05) -1 a- A METHOD AND APPARATUS FOU FORMING METALLIC PARTS Field of the Invention The present invention relates generally to a method and apparatus for forming metal parts, such as drill bits, and more particularly, to a forging method and apparatus for forming metal parts, such as spade-type boring bits.

This application is a divisional application out of NZ 300765. NZ 300765 is directed to drill bits and in particular to spade-type boring bits. Parts of the following description are directed to the spade-type boring bits of NZ 300765. The description is retained for clarity and completene- NZ 334160 is a divisional application filed from this application and is directed to a method and apparatus for forging a part of a predetermined shape from a workpiece.

Background of the Invention Spade-type boring bits, hereinafter referred to as "spade bits", are commonly employed to drill or bore holes through wood or other materials. A spade bit is typically used to drill holes having a relatively large diameter from which a large amount of wood or other material must be removed. For example, during the construction of a home, spade bits are often utilized to drill a series of aligned holes through adjacent studs through which conduit or wiring will extend.

As illustrated in Figure 1, a conventional spade bit 1 includes an elongate shank 2 which defines a longitudinal axis 3. A blade portion 4 is joined to a forward end 6f the shank and the rear end of the shank, opposite the forward end, is received and held by a drill during drilling operations. The blade portion is generally planar and, as shown in Figure 2, defines a centerline 5 in the plane of the blade portion and extending through the longitudinal axis. The blade portion also includes a pair of side segments 4 extending laterally in opposite directions. See, for example, U.S. Patent No. 2,782,824 to Robinson-issued ^itlLkOlUd. iv.Ufcrtl ,February 26, 1957; U.S. Patent No. 4,682,917 to o|:NZ " 5 MAR 1999 RECEIVED s;jj.gs 5 "Williams, III, issued July 28, 1987; U.S. Patent No. 4,950,111 to Thomas issued August 21, 1990; U.S. Patent No. 5,061,127 to Thomas issued October 29, 1991; U.S. Patent No. 5,286,143 to Schimke issued February 15, 5 1994? and British Patent No. GB 2,130,935A published June 13, 1984. A conventional spade bit also generally includes a generally triangular spur 7 joined to and extending axially from a forward end of the blade portion so as to be coplanar therewith. As known to 10 those skilled in the art, the spur serves to guide and center the spade bit during drilling operations.

The spur 7, as well as each side segment 6, generally includes a cutting edge 8 for removing wood or other material when the spade bit 2 is rotated in a 15 predetermined direction of rotation during drilling operations. In particular, the spur cutting edges extend along opposed sides of the base of the spur at the forward end of the blade portion to the forwardmost portion of the spur, i.e., the spur point. In 20 addition, the cutting edge of each side segment is formed on the forward end of the blade portion such that the side segment cutting edge will engage the workpiece when the spade bit is rotated in the predetermined direction of rotation. 25 In operation, the cutting edges of the spur 7 initially drill a lead hole in the workpiece. Thereafter, the cutting edges of the side segments 6 engage and remove material from the workpiece to drill a hole of a predetermined diameter. Since the spur 7 3 0 of a conventional spade bit 2 is typically coplanar with the generally flat side segments as shown in Figure -2, each cutting edge of the generally triangular spur is contiguous with the cutting edge of the adjacent side segment. Thus, a pair of continuous 35 cutting edges 8 are formed, each including a cutting edge of the triangular spur and the cutting edge of the adjacent side segment. See, for example, U.S. Patent •) '» » £'»c> tr o o .L !•0 No. 2,782,624 to Robinson; U.S. Patent No. 4,682,917 to Williams, III; U.S. Patent No. 5,221,166 to Bothum issued June 22, 1993; U.S. Patent No. 5,28 6,143 to Schimke; and U.S. Patent No. 5,291,806 to Bothum issued 5 March 8, 1994.

The chip swarf created during the drilling operations is generally directed radially along the cutting surface and toward the outer periphery of the hole being formed, due to the orientation of the 10 cutting edges and the rotation of the spade bit.

However, chip swarf is not as readily removed in the vicinity of the corner formed by the intersection of a spur cutting edge and the cutting edge of an adjacent side segment. Instead, chips accumulate in the corner 15 formed by the spur and adjacent side segment cutting edges since the chips are not directed away from the corner by the intersecting cutting edges. Due to the accumulation of chip swarf, the cutting edge in the vicinity of the corner defined by the spur and the 20 adjacent side segment cutting edges does not readily cut into the workpiece and remove material therefrom. Instead, additional power or torque must be applied to rotate the spade bit and to drill a hole through the workpiece once chip swarf has collected in the corner 25 between the spur and adjacent side segment cutting edges.

A further problem caused by the radially outward movement of the chip swarf along the surfaces of the side segment cutting edges is that the chip 3 0 swarf is forced into the peripheral wall of the hole being formed, and thus binds between the peripheral wall and the outer edge of the rotating^ blade portion. This binding further increases the power consumption of the drill. 3 5 The primary cause of these problems, as shown in Figure 2, is that the cutting edges 8 of each side segment 6 are not aligned with the centerline 5 that 9 • C10 t: A Ij O D passes through the longitudinal axis 3. Instead, each cutting edge is positioned in advance of the centerline in the predetermined direction of rotation of the spade bit l. Since the cutting edges are positioned in 5 advance of the centerline, the chip swarf is not directed solely circumferentially away from the cutting edges. Instead, the rotation of the spade bit also imparts a radial force component to the chip swarf which urges the chip swarf against the peripheral wall. 10 During drilling operations, conventional spade bits can also splinter the workpiece in which the hole is drilled. In particular, conventional spade bits can splinter the workpiece at both the entry and exit points and can produce a hole having relatively 15 rough sidewalls, thereby reducing the quality and cleanliness of the resulting hole. In many instances, clean holes of a relatively high quality are more desirable than holes having rough and splintered sidewalls. For example, wiring can be pulled more 20 readily through clean holes having smooth sidewalls since holes having rough and splintered sidewalls increase the frictional resistance on the wire being pulled therethrough and, in some instances, can cut or otherwise damage the insulation surrounding the wire 25 being pulled through the holes.

Spade bits are typically formed by a hot forging process. According to this process, a coil of wire stock of £ given diameter is cut into segments, each of which is approximately the length of an 30 individual spade bit. Each segment is then headed to form a portion of material with an increased diameter at the first end of the segment, i.e., a bulb of material having an increased diameter over a shorter length at the first end. Thereafter, the segment is 35 heated and forged by compressing the heated bulb of material between a pair of opposed dies. Typically, the pair of opposed dies are closed in a rectilinear O ± *i, b J manner such that the heated bulb of material is subjected to compressive forces which urge the material into the predetermined shape defined by the dies. The forged part can then be trimmed and finished to produce 5 spade bits such as those described above. An identification mark can also be stamped on the spade bit during its processing. , By initially cutting the wire stock, however, the parts must be individually handled and processed throughout the hot forging 10 process. For example, each individual part must be appropriately aligned during each step of the process to ensure that the spade bits formed thereby are within tolerance.

Regardless of the process by which it is 15 formed, the performance of a spade bit is typically measured by several parameters. One such parameter is-the quality of the hole produced by a spade bit as defined by the cleanliness of the hole including the cleanliness of both the entry and exit points and the 20 relative smoothness of the sidewalls of the resulting hole. In addition, a spade bit is measured by the speed at which it cuts a hole of a predetermined diameter as well as the power or torque required to cut the hole of the predetermined diameter. Finally, the 25 longevity or life of the spade bit itself, typically measured by hours of use or service, is a parameter. Therefore, it is desirable to develop long-lasting spade bits which rapidly drill high-quality holes while requiring a minimum amount' of power or torque.

Summary of the Invention In view of the foregoing background, it is therefore an object of the present invention to provide an improved method and apparatus for manufacturing a 35 plurality of metal parts, such as spade bits, which significantly reduces the required handling and processing of individual parts. - 6 o o...

The following description is given firstly with reference to the spade-type boring bit of NZ 300765, secondly with reference to the method and apparatus of the present invention, and finally with reference to the method of NZ 334160 NZ 300765 provides for a spade-type boring bit having an elongate shank defining a central longitudinal axis, and a blade portion joined to one end of the shank and including a pair of generally flat side segments, such as wings, extending laterally in opposite directions from the central longitudinal axis. According to one preferred embodiment, the side segments include respective forward cutting edges which are aligned with each other along a centerline which passes through the central longitudinal axis. This alignment of the forward cutting edges along a centerline which passes through the central longitudinal axis results in the chip swarf being directed perpendicularly away from the cutting edges, with no radially outward component of movement. Thus, the chip swarf is not forced radially into the peripheral wall of the hole being formed, and the resulting binding is significantly alleviated. o •'» t [>oc; o o JL b C* D Therefore, the long-lasting spade bit of nz 300765 efficiently produces high-quality holes. According to one embodiment, the blade portion also includes a generally flat central segment 5 disposed along the central longitudinal axis which defines a central plane. The central segment includes opposite sides which are parallel to the central axis and which are joined to respective side segments. Further, the opposed side segments preferably define 10 respective lateral planes which are parallel to each other and to the central longitudinal axis, but which are oblique to the central plane of the central segment, thereby producing a blade portion having a distinct Z-shaped cross-section. 15 The blade portion of the spade bit of NZ 300765 also includes a spur joined to and extending axially from the forward end of the blade portion. In one embodiment, the spur is threaded such that the spade bit is self-feeding. In other 20 embodiments, the spur is preferably of a triangular shape extending to a spur point on the central longitudinal axis. The spur of these embodiments includes a pair of spur cutting edges extending along opposite sides of the spur between the spur point and 25 the forward end of the blade portion. Each spur cutting edge advantageously extends radially outward of at least an innermost portion of the forward cutting edge of the adjacent side segment. In addition, each spur cutting edge is advantageously angularly offset 3 0 from the forward cutting edge of the adjacent side segment in the predetermined direction of rotation of the spade-type boring bit when viewed along the central longitudinal axis. Thus, each spur cutting edge is both radially and angularly separated from the forward 35 cutting edge of the adjacent side segment.

Further, at least a portion of each spur cutting edge extends axially rearward of the forward ^ rl i JVQ K t * J. O u cutting edge of the adjacent side segment.

Accordingly, each spur cutting edge can also be axially separated from the forward cutting edge of the adjacent side segment. By providing such radial, angular and, 5 in some instances, axial separation between each spur cutting edge and the forward cutting edge of the adjacent side segment, accumulation of chip swarf between the spur cutting edge and the forward cutting edge of the adjacent side segment is significantly 10 reduced, if not eliminated, since no corner is formed therebetween.

According to one preferred embodiment, the side segments include respective chamfered corner portions. The chamfered corner portion of each side 15 segment preferably includes a chamfered edge extending both axially rearward and laterally outward from the respective forward cutting edge so as to more precisely cut or form the peripheral wall of the resulting hole. By extending both axially rearward and laterally 20 outward from the respective forward cutting edge, the chamfered corner portions can repeatedly cut the peripheral wall of the resulting hole as the spade-type boring bit of NZ 300765 is rotatably advanced through the workpiece. Therefore, the spade 25 bit of NZ 300765 efficiently produces high- quality holes having smooth peripheral walls and clean entry and exit points.

More specifically, the chamfered edge of the chamfered corner portion of each side segment 30 preferably extends both axially rearward and laterally outward from an outer portion of the respective forward cutting edge. In addition, a chamfer angle is typically defined between the chamfered edge of each respective side segment and a line parallel to the 35 central longitudinal axis. According to one preferred embodiment, the chamfer angle is between about 30° and about 60°. Each chamfered corner portion also includes Q •"» > i'» t: < * O J. b.? J a chamfer surface extending between the respective chamfered edge and a rear edge and defining a chamfer plane. In order to prevent binding of the spade-type boring bit, the chamfer surface preferably slopes 5 radially inward from the respective chamfered edge to the roar edge. Accordingly, the chamfer plane advantageously intersects a plane perpendicular to the lateral plane defined by the respective side segment to thereby define a chamfer clearance angle, such as 10 between about 10* and about 20* in one exemplary embodiment.

According to another embodiment, each side segment includes a cutting b^ade insert, preferably comprised of a relatively hard material, such as 15 carbide, mounted along the forward end of the respective side segment to thereby define the respective forward edge. In addition, the forward portion of each side segment defines a cutting plane which preferably intersects the lateral plane defined 20 by the respective side segment so that the forward cutting edge of each side segment is disposed angularly in advance of the respective lateral plane in the predetermined direction of rotation of the spade bit. More specifically, the cutting plane and the lateral 25 plane of each respective side segment define a hook angle therebetween of between about 10* and about 20°.

According to another embodiment of NZ 300765, the spade bit is comprised of multiple discrete parts. In this embodiment, the blade 3 0 portion preferably defines an internal cavity opening at the rear end to which a forwardly extending member of the shank is joined. The spade bit preferably includes means for interlocking the forwardly extending member of the shank within the internal cavity of the 35 blade portion, such as by complimentary threaded portions defined within the internal cavity of the 331CS5 blade portion and along the forwardly extending member of the shank.

Each side segment can also include a forward end having a forward end surface extending between the 5 respective forward cutting edge and a rear edge.

According to one embodiment, each forward end surface defines a forward end plane which intersects a plane perpendicular to the central longitudinal axis to thereby define a lip clearance angle of between about 10 10* and about 20* such that the forward end surface slopes rearwardly from the forward cutting edge to the rear edge. According to another embodiment, each forward end surface includes first and second forward end planes which intersect a plane perpendicular to the 15 central longitudinal axis to thereby define first and second lip clearance angles, respectively. Preferably, the second lip clearance angle is greater than the first lip clearance angle such that the forward end surface continues to slope rearwardly from the forward 20 cutting edge to the rear edge.

Each side segment also includes a first side along which the side segment is joined to -he central segment and an opposed second side defining a second side surface. The second side surface is preferably 25 arcuate or curvilinear in transverse cross-section and tapers inwardly when viewed from the forward end of the spade-type boring bit to define a side surface taper angle of about one-half of 1* to reduce binding of the spade bit during drilling operations. 30 The present invention provides a method and apparatus for forging a plurality of parts, such as spade-type boring bits, from & continuous length of metal stock, such as a continuous wire stock. The forging method includes the steps of incrementally 35 advancing the continuous metal stock a predetermined linear distance, such as with an indexing means, such that the metal stock advances longitudinally in a downstream direction. A leading portion of the continuous metal stock is clamped following each incremental advance of the metal stock to hold the leading portion in a fixed location. A portion of the. continuous metal stock, upstream of the leading portion, is then forged each time the metal stock is clamped and held at the fixed location. In addition, the longitudinal growth of the continuous metal stock created during the forging step is compensated by permitting upstream longitudinal movement of that portion of the continuous metal stock which is upstream of the fixed location.

The continuous metal stock is preferably forged by radially closing a plurality of dies thereabout. The plurality of closed dies define a cavity of predetermined shape which, in turn, defines the resulting shape of the forged portion of the wire stock. In addition, the plurality of closed dies define entry and exit ports through which the continuous metal stock extends during the forging step.

The plurality of dies are preferably mounted on a carriage which is adapted to move longitudinally. In particular, the carriage is preferably mounted such that the longitudinal growth of the continuous metal stock between the forged portion about which the plurality of dies are radially closed and the leading portion which is clamped causes the carriage to move in the upstream longitudinal direction. Thus, the plurality of dies will remain closed about the same portion of the metal stock during the forging step. The carriage is preferably longitudinally biased to prevent excessive upstream movement of the carriage and to return the carriage to its initial position after each forging step.

After forging a portion of the metal stock, the plurality of dies are radially opened and the leading portion of the metal stock is released such 33 that the continuous metal stock can be incrementally advanced prior to repeating the forging method. Once forged, a portion of the continuous metal stock which extends beyond the clamped leading portion of the metal 5 stock can be cut to separate the forged metal stock into a plurality of discrete parts. In addition, an identification mark can be stamped on a previously forged part during the clamping step.

Accordingly, the forging method of the 10 present invention can produce a plurality of parts, such as the spade bit of the present invention, from a continuous metal stock. The efficiency of the forging process and the quality of the parts formed thereby are enhanced since individual parts need not be handled 15 during the forging operations, since such handling of individual parts generally increase the opportunities for misalignment and contributes to poor tolerance control durincr the manufact\jrincr process.

NZ 334160 provides a method and apparatus for forging a part of a predetermined shape from a workpiece with opposed forging dies which define a cavity of the predetermined shape therebetween. At least one forging die includes a contact surface which defines a portion of the cavity for contacting and shaping the workpiece into the predetermined shape of the resulting part.

The respective contact surface also includes at least one relatively flat portion which defines a contact plane which opposes and is parallel to a relatively flat portion of the other die.

According to NZ 334160, the opposed forging dies are radially closed upon their insertion, such as by a ram, in an internal cavity defined by a die housing. The die housing into 35 which the forging dies are inserted circumferentially encompasses and structurally reinforces the pair of forging dies during the forging process.

OFN.Z. - 5 MAR 1999 RECEIVED ^1 6g The forging dies, typically a pair of forging dies, accordingly move radially inward in a predetermined direction, oblique to the respective contact planes defined by the opposed contact surfaces.

The respective contact surfaces therefore impart both axial and radial forces to at least portions of the workpiece to form the part of predetermined shape within the cavity defined between the pair of opposed forging dies. Due to the shape of the contact surfaces 10 and the resulting orientation of the axial and radial forces applied, favorably oriented stresses are generated within the workpiece which facilitate the efficient formation of the part of predetermined shape.

In order to maintain the predetermined alignment of the forging dies, the forging apparatus of NZ 334160 preferably includes a side die positioned adjacent each of the opposed side surfaces defined by the forging dies.

According to this embodiment, the forging dies and the pair of side dies define a conical die assembly which is received by the internal conical cavity defined by 20 the die housing. The opposed forging dies of NZ 334160 can also define entry and exit ports through which a continuous metal stock extends for forging a plurality of parts.

The forging method and apparatus of NZ 334160 thus employ 25 simultaneous axial and radial forces to deform a workpiece. Accordingly, thin parts which have a relatively large diameter can be readily forged. Further the power required to forge parts of a predetermined size and shape is reduced in comparison to conventional compressive forging processes by imparting forces at desirable locations within the workpiece by rotating the forging dies within the die housing. s ;> ics 5 Brief Description of the Drawings Figure 1 is a front elevation view of a conventional spade-type boring bit.

Figure 2 is an end view of a conventional 5 spade-type boring bit of Figure l during a drilling operation.

Figure 3 is a front elevation view of the spade-type boring bit of NZ 300765.

Figure 4 is a side elevation view of a spade-10 type boring bit of NZ 3007 65.

Figure 5 is an end view of the spade-type boring bit of Figure 3 when viewed along the line 5-5 of Figure 3 which is along the central longitudinal axis, and which illustrates the alignment of the 15 forward cutting edges of the side segments along a centerline passing through the central longitudinal axis.

Figure 5A is a fragmentary side view of a portion of a side segment of the spade-type boring bit 20 of Figure 5 illustrating the hook angle, and taken along the line 5A-5A of Figure 5.

Figure 6 is a fragmentary cross-sectional view of a portion of the spur of the spade-type boring bit of Figure 3 illustrating the spur cutting edge, and 25 taken along the line 6-6 of Figure 3.

Figure 7 is a fragmentary perspective view of a side segment of a spade-type boring bit of NZ 300 765 illustrating the chamfered corner portion.

Figure 7A is a fragmentary cross-sectional view of a portion of the side segment of the spade-type boring bit of NZ 30 0765 illustrating the chamfer clearance angle defined by the chamfered corner portion, and taken along line 7A-7A of Figure 7. 35 Figure 8 is a greatly enlarged fragmentary front elevation view of the blade portion of a spade-type boring bit of NZ 30076 5. ^ l 1 r\ uu _L L" <J 'J Figure 9 is a cross-sectional end view of the blade portion of the spade-type boring bit of Figure 8 during a drilling operation illustrating its distinct Z-shaped cross-section, and taken along the line 9-9 of 5 Figure 8.

Figure 10, taken along the line 10-10 of Figure 9, is a lateral cross-sectional view of a portion of a side segment of the spade-type boring bit during drilling operations to illustrate the resulting 10 chip removal.

Figure 11 is a front elevation view of one embodiment of a spade-type boring bit of NZ 300765 in which the elongate shaft and the blade portion are threadably interlocked. 15 Figure 12 is a lateral cross-sectional view of the embodiment of the spade-type boring bit of Figure 11 illustrating the threaded connection of the elongate shaft to the blade portion, and taken along the line 12-12 of Figure 11.

Figure 13 is a cross-sectional end view of the embodiment of the spade-type boring bit of Figure 11, taken along the line 13-13 of Figure 11, and illustrating the rotation of the blade portion.

Figure 14 is a fragmentary lateral cross-25 sectional view of a portion of a side segment of the • blade portion of the embodiment of the spade-type boring bit of Figure 11 illustrating a cutting blade insert, and taken along the line 14-14 of Figure 13.

Figure 15 is a perspective view of a self-30 feeding embodiment of the spade-type boring bit of ".•JZ 30 0765 which includes a threaded spur.

Figure 16 is "an exploded view of the component parts of the self-feeding embodiment of the spade-type boring bit of Figure 15. 35 Figure 17 is a block diagram of a hot forging process for fabricating the spade-type boring bits of the present invention. 33 -£ 6 ;1 Figure 18 is a representative block diagram of an exemplary forging process of the present invention for fabricating a plurality of parts, such as the spade-type boring bit of the present invention, 5 from a continuous metal stock.

Figure 1 9 is a schematic representation of one embodiment of the die assembly for applying compressive forces during a forging operation.

Figure 20 is a schematic representation of the die assembly and an associated die housing for applying both axial and radial forces which, in turn, generate compressive, tensile and shear stresses within the workpiece during a forging operation. 15 Figure 21 is a schematic representation of an end view of a die assembly and an associated die housing for applying both compressive and shear forces during a forging operation.

Detailed Description of the Preferred Embodiments The present invention will now be described more fully hereinafter with reference to the accompanying drawings, in which a preferred embodiment of the invention is shown. This invention may, 25 however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein? rather, this embodiment is provided so that this disclosure will be thorough and complete and will fully convey the scope of the invention to those 30 skilled in the art. Like numbers refer to like elements throughout.

As illustrated in Figures 3 and 4, a spade-type boring bit 10 of nz 300765, hereinafter referred to as a "spade bit", includes an 35 elongate shank 12 defining a central longitudinal axis 14 therethrough. The rear portion 16 of the shank is adapted to be received and held by a drill (not INTELLECTUAL PROPERTY OFFICE OF N.Z. 1 2 FEB 1999 *2 ► t* O ^ C» O _L t- b -J illustrated). For example, the elongate shank typically includes a cylindrical forward portion and a rear portion 16 that is hexagonal in transverse cross-section so as to be securely received and held by the 5 chuck of a drill (not illustrated) .

The spade bit 10 also includes a blade portion 18 joined to a forward end of the elongate shank 12, and which is integrally formed with the shank 12 in the illustrated embodiment. The blade portion 10 includes a pair of generally flat side segments 20 which extend laterally in opposite directions from the central longitudinal axis 14. As shown in Figure 5, the side segments preferably define respective lateral planes 22 which are parallel to each other and the 15 central longitudinal axis. According to this embodiment of NZ 300765, the blade portion also includes a generally flat central segment 24 disposed along the central longitudinal axis and defining a central plane 26. More particularly, the 20 central segment includes opposite sides 28 which are parallel to the central longitudinal axis, a rear end which is joined to the forward end of the shank and an opposite forward end. According to this embodiment, the pair of side segments are joined to the central 25 segment along respective sides of the central segment.

In particular, the pair of side segments are joined to respective sides of the central segment such that lateral planes 22 defined by the respective side segments 20 intersect the central plane 26 defined by 30 the central segment 24 at an oblique angle 29.

The blade portion 18 also includes a spur 30 joined to and extending axially from the forward end of the blade portion to center and to guide the spade bit 10 during drilling operations. As best illustrated in 35 Figures 3 and 8, the spur of this embodiment is of a generally triangular shape and extends to a spur point on the central longitudinal axis 14. The spur also *2 •"} 1 i^C r-» o O _t Kj b O includes a pair of spur cutting edges 32, shown in cross-section in Figure 6, extending along opposite sides of the spur between the spur point and a base of the spur at the forward end of the blade portion. The 5 spur cutting edges are positioned to initially contact the workpiece during rotation of the spade bit in the predetermined direction of rotation as indicated by the counterclockwise arrows in Figure 5.

Each side segment 20 also includes a 10 respective forward cutting edge 34. Each forward cutting edge is defined along the leading edge of the forward end of the respective side segment to.initially contact and remove material as the spade bit 10 rotates in a predetermined direction of rotation during 15 drilling operations. As illustrated by the arrows in Figure 5, the spade bit is adapted to rotate counterclockwise when viewed along the central longitudinal axis 14 from the forward end toward the rear end.

The respective forward cutting edges 34 of the side segments 20 are preferably aligned with each other along a centerline 36 that prsses through the central longitudinal axis 14 of the elongate shaft 12 as shown in Figure 5. By being aligned along the 25 centerline that passes through the central longitudinal axis of the elongate shaft, the forward cutting edges remove material during drilling operations more efficiently th'an conventional spade bits in which the forward cutting edges of the respective side segments 30 are not aligned with each other, but are instead positioned in advance of a centerline that passes through the central longitudinal axis 14. See,-for example, Figure 2.

More specifically, the power or torque 35 supplied to the spade bit 10 of the present invention during drilling operations is more efficiently transferred, via the aligned forward cutting edges 34, *2 - ' ; s'.Q.S > O -L o «J to the workpiece. For a given size of spade bit, the power supplied to the spade bit of nz 30 0765 is more efficiently transferred to the workpiece since the moment arm of the spade bit of 5 nz 300765 is shorter than the moment arm of a conventional spade bit, such as that illustrated in Figures 1 and 2, due, at least in part, to the distinct Z-shaped cross-section of the spade bit of nz 300765. In addition, the power supplied to the 10 spade bit of nz 300 765 is also more efficiently transferred to the workpiece since the total length of the spur cutting edges 32 and the forward cutting edges of the spade bit of nz 300765 of a given diameter is less than the total 15 length of the spur cutting edges and the forward cutting edges of a conventional spade bit of the same diameter. Due to the more efficient power transfer, the spade bit of nz 300765 rotates more rapidly to produce holes of a relatively high quality. 20 The alignment of the forward cutting edges of the side segments 20 along a centerline 36 that passes through the central longitudinal axis 14 further improves the performance of the spade bit by directing the removed chip swarf perpendicularly from the cutting 25 edge and upwardly, and not radially outwardly, as illustrated in Figures 9 and 10. By urging the chip swarf in the indicated direction, and not radially outward as urged by conventional spado bits, the chip swarf does not hinder subsequent rotation of the spade 30 bit by binding between the spade bit and the sidewalls of the hole formed thereby. Accordingly, the longevity of the spade bit is "increased by reducing the wear on the spade bit and the efficiency with which the spade bit drills a hole of a predetermined diameter is 35 enhanced.

As best illustrated in Figures 8 and 9, each spur cutting edge 32 preferably extends radially 8311)85 outward of at least an innermost portion of the forward cutting edge 34 of the adjacent side segment 20. Thus, each spur cutting edge is radially separated from the forward cutting edge of the adjacent side segment, in 5 addition, the spur 30 preferably defines a spur plane which is oblique to the respective lateral planes defined by said side segments such that each spur cutting edge is also preferably angularly offset from the forward cutting edge of the adjacent side segment 10 in the predetermined direction of rotation of the spade bit 10 when viewed along the central longitudinal axis 14. In particular, each spur cutting edge is positioned angularly rearward of the forward cutting edge of the adjacent side segment in the predetermined 15 direction of rotation. Thus, each spur cutting edge is also angularly separated from the forward cutting edge of the adjacent side segment. Further, at least a portion of each spur cutting edge 32 extends axially rearward of the forward cutting edge 34 of the adjacent 20 side segment in the longitudinal direction so that each spur cutting edge is also axially separated from the forward cutting edge of the adjacent side segment.

Due to the separation of each spur cutting edge 32 from the forward cutting edge 34 of the 25 adjacent side segment 20, the spade-type boring bit 10 of NZ 300765 more efficiently removes material during drilling operations. In particular, material is removed by either a spur cutting edge or a forward cutting edge of a side segment and is directed 30 generally rearward from the cutting surface by the respective cutting edge. Due to the separation of the spur cutting edge from the forward cutting edge of the adjacent side segment, little, if any, chip swarf is accumulated therebetween as described above in 35 conjunction with conventional spade bits. Instead, the chip swarf is directed generally rearward from the cutting surface so that the spade bit can continue to n •"» > t1 o c. o o .L b b 0 cut into the workpiece with both the spur cutting edge and the adjacent forward cutting edge, thereby further improving the efficiency of the drilling operation.

According to one embodiment of NZ 300765, 5 each side segment 20 can also include a respective chamfered corner portion 35. As shown in Figures 3 and 8, each chamfered corner portion includes a chamfered edge which extends both axially rearward and laterally outward from the respective forward 10 cutting edge 34. In particular, the forward cutting edge of each side segment typically extends laterally outward from an inner portion to an outer portion. Accordingly, the chamfered edge of each chamfered corner portion preferably extends both axially rearward 15 and laterally outward from the outer portion of the respective forward cutting edge.

By extending both axially rearward and laterally outward from the respective forward cutting edge 34, the chamfered corner portions 35 can 20 repeatedly cut the peripheral wall of the resulting hole as the spade bit 10 of NZ 300765 is rotatably advanced through the workpiece. Therefore, the spade bit of NZ 300765 can efficiently produce high-quality holes having smooth peripheral 25 walls and relatively clean entry and exit points.

As best shown in Figures 3 and 8", a chamfer angle 37 is defined between the chamfered edge of each respective chamfered corner portion 35 and a line parallel to the central longitudinal axis 14. The 30 chamfer angle is typically between about 30° and about 60" and, according to one advantageous embodiment, is about 45*. As shown in Figure 8, each chamfered corner portion also has a predetermined width 39 measured along a line colinear with the respective forward 35 cutting edge 34 and which extends between the respective chamfered edge and a line parallel to the central longitudinal axis. o •» » t1 o ^ «■> o jl b O The predetermined width of the chamfered corner portions 35 typically varies directly with the size of spade bit 10 such that larger spade bits have chamfered corner portions with larger widths and 5 smaller spade bits have chamfered corner portions with smaller widths. For example, for a spade bit having a diameter of between 1.5 inches and 0.875 inches, the chamfered corner portions can have a width of. about 0.090 inches. In addition, for a spade bit having a 10 diameter of between 0.8125 inches and 0.75 inches, the chamfered corner portions can have a width of about 0.070 inches. Likewise, for a spade bit having a diameter of between 0.6875 inches and 0.625 inches, the chamfered corner portions can have a width of about 15 0.060 inches. Still further, a spade bit having a diameter of between 0.5625 inches and 0.5 inches can have chamfered corner portions with a width of about 0.050 inches, while a spade bit with a diameter of between about 0.4375 inches and 0.375 inches can have 20 chamfered corner portions with a width of about 0.025 inches. However, the chamfered corner portions of spade bits of NZ 300765 can have any number of widths.

As illustrated in Figure 5A, a forward portion of each side segment also preferably defines a cutting plane 38. The cutting plane intersects the lateral plane"22 defined by the respective side segment 20 to define a hook angle' 40 therebetween. Preferably, 30 the hook angle is between about 10° and about 20° and, more preferably, is about 15°. The forward cutting edges 34 of the illustrated embodiment are disposed angularly in advance of the lateral planes of the respective side segments in the predetermined direction 35 of rotation of the spade bit 10 when viewed along the central longitudinal txis 14. As shown in Figures 9 and 10, chips removed ':rom the workpiece by the forward 1j •'» > i1 n ^ <.> ol> b O cutting edge are thereby directed -upwardly or rearwardly along the spade bit and away from the cutting surface by further rotation of the spade bit, and, in part, by the hook angle defined between the 5 cutting plane and the lateral plane.

Further, each side segment 20 of the spade bit 10 can also include a forward end having a forward end surface 42 extending between the respective forward cutting edge 34 and a rear edge 44. In one embodiment, 10 each forward end surface defines a respective forward end plane which intersects a plane 48 perpendicular to the central longitudinal axis 14 to define a lip clearance angle 50 therebetween. Preferably, the lip clearance angle is between about 10" and about 20° and, 15 more preferably, is about 15*. Advantageously, the forward end surface slopes rearwardly from the forward cutting edge to the rear edge such that only the forward cutting edge contacts the cutting surface during drilling operations. Thus, the drag or other 20 frictional forces generated between the rotating spade bit and the workpiece are reduced,and the efficiency with which the spade bit of NZ 30 0 765 drills is further improved.

More particularly, in the embodiment 25 illustrated in Figure 6, each forward end surface includes first and second forward end planes 46a and 46b, respectively, which intersect a plane 48 perpendicular to the central longitudinal axis 14 to define first and second iip clearance angles 50a and 30 50b, respectively, therebetween. As shown, the second lip clearance angle is typically larger than the first lip clearance angle in order to further reduce drag or other frictional forces generated between the rotating spade bit and the workpiece. For example, in one 35 embodiment, the first and second lip clearance angles are about 5° and 8", respectively. However, the first and second lip clearance angles can be varied• «} • » i , ► p •: t ; O J. t> •? 0 As illustrated in Figures 7 and 7a, the chamfered corner portion 35 of each side segment 20 5 includes a chamfer surface extending between the respective chamfered edge and a rear edge. Each chamfer surface defines a chamfer plane which intersects a plane perpendicular to the lateral plane 22 defined by the respective side segment to thereby 10 define a chamfer clearance angle 41. Advantageously, the chamfer surface slopes radially inward from the chamfered edge to the rear edge to define a chamfer clearance angle of between about 10° and about 20° and, in one preferred embodiment, of about 12°. 15 Still further, each side segment 20 of the illustrated embodiment of the spade bit 10 of nz 300765 includes a first side joined to the central segment 24 along a side 28 thereof, and an opposed second side 52 defining a second or outer side 20 surface. The second or outer side surface extends between respective forward and reir edges and, as shown in Figure 5, preferably follows the arc of a circle in lateral cross-section to furth~*r reduce the drag or other frictional forces generated by the rotation of 25 the spade bit within the hole. Alternatively, the side surface can taper radially inwardly from the forward edge to the rear edge such that only the forward edge of the side surface of the side segment contacts the sidewalls of the hole to thereby further reduce binding 30 of the spade bit.

The second sides 52 of the respective side segments 20 also preferably taper inwardly, axially from the forward end to the rear end of the blade portion 18. Thus, as shown in Figure 3, a side surface 35 taper angle 53, typically, about one-half of 1', or k', is defined between the side surface plane and a line parallel to the central longitudinal axis 14. By *3 •"> » tv p w o a b b O tapering the second sides of the side segments inwardly, the side surfaces preferably only contact the workpiece near the cutting surface such that drag or other frictional forces are still further reduced.

The spade bit 10 of NZ 300765 can be integrally fabricated from a single piece of metal as illustrated in Figures 3 and 4. Alternatively, the spade bit of NZ 300765 can be formed from the combination of several components.

For example, as illustrated in Figures 11 and 12, the elongate shank 12 and the blade portion 18 can be separately formed and subsequently joined to form the spade bit of NZ 300765.

In particular, the blade portion 18 can include an internal cavity 54 which opens at a rear end to which the elongate shaft 12 is joined. Correspondingly, the elongate shaft 12 can include a forwardly extending member 56 adapted to be received within the internal cavity defined by the blade portion.

The spade bit 10 of this embodiment also includes means for interlocking the forwardly extending member of the shank within the internal cavity of the blade portion. For example, the interlocking means can include complimentarily threaded portions defined within the internal cavity of the blade portion and along the forwardly extending member of the shank such that the shank and the blade portion can be threadably connected. As known to those skilled in the art, the threaded connection is preferably self-tightening such that rotation of the spade bit in the predetermined direction of rotation further tightens the threaded connection between the shank and the blade portion. The spade bit can also include other interlocking means.

For example, the blade portion and the ^'t J O J_ «? J shank can be press-fit or joined, such as by brazing, to form a secure interconnection therebetween. In addition, the shank can include the internal cavity and the blade portion can include a corresponding rearwardly extending member for interlocking the pieces - As illustrated in Figures 13 and 14, each side segment 20 of one embodiment of the spade bit 10 of NZ 300765 can include a cutting blade insert 58. Each cutting blade insert is typically comprised of a relatively hard material, such as carbide and is mounted along the forward end of a respective side segment to define the respective forward cutting edge 34 and, in some embodiments, the respective chamfered edge 35. In addition, the forward cutting edges defined by the respective cutting blade inserts of this embodiment can be aligned along the centerline 3 6 that passes through the central longitudinal axis 14 of the elongate shank 12 as described above.

Although a spade bit 10 of NZ 300765 can be comprised of multiple pieces and can also include cutting blade inserts 58 as illustrated in Figures 11-14, a spade bit of NZ 300765 can be comprised of multiple pieces without including cutting blade inserts. Likewise, a spade bit of NZ 300765- can be fabricated as an integral unit, but can still include cutting blade inserts 58. Alternatively, the forward cutting edges 34 and, in some embodiments, the chamfered edges 35 of a spade bit of NZ 300765 can be formed by depositing a layer of a relatively hard material, such as diamond, on a substrate, namely, the leading edge of the forward end of each side segment 20. The relatively hard material is preferably stronger than the underlying side segments. 331GS5 As illustrated in Figure 15, the spade bit of NZ 300765 can also be self-feeding to facilitate entry and advancement of the spade bit through a workpiece. According to this embodiment, the blade portion 18' of the spade bit 10' includes a threaded spur 30' joined to and extending axially from the forward end of the blade portion. As illustrated, the blade portion of the self-feeding embodiment of the spade bit also includes a pair of generally flat side segments 20' that extend laterally in opposite directions from the central longitudinal axis 14' of the spade bit. In the illustrated embodiment, the side segments include respective chamfered corner portions ' and respective forward cutting edges 34' which are aligned with each other along a centerline 36' that passes through the central longitudinal axis. Thus, among the features which the self-feeding embodiment of the spade bit has in common with the other embodiments described above is the Z-shape cross-section of the blade portion, as best illustrated in Figures 5, 13 and , and the chamfered corner portions of the side segments, as best shown in Figures 3, 8 and 15.

Accordingly, the self-feeding embodiment of the spade bit illustrated in Figure 15 also provides the numerous improvements in drilling efficiency described in detail above.

The self-feeding embodiment of the spade bit ' of NZ 300765 can be fabricated according to any method, such as hot forging, known to 30 those skilled in the art .

Alternatively, the self-feeding- embodiment of the spade bit can be formed according to the forging process described below. As shown in Figure 16, however, another method of forming 35 the self-feeding embodiment of the spade bit is to join several pieces to form the spade bit of Figure 15. In particular, the threaded spur 30' is formed at a first 331SS5 end of an elongate shank 12' by any conventional technique. The remainder of the blade portion, including the oppositely extending side segments 20', is formed as a separate piece which includes an 5 internally threaded bore extending axially therethrough. The remainder of the blade portion is mounted on the elongate shank and threadably engaged to the threaded spur. Thereafter, a tubular sleeve 57' can be placed over and swaged to the elongate shank to 10 securely affix the blade portion to the shank and to form the self-feeding embodiment of the spade bit shown in Figure 15.

The spade bit 10 of NZ 300765, and the individual pieces thereof, can be formed from a 15 hot forging process as schematically illustrated in Figure 17. As shown, a continuous length of metal stock 59, such as wire, is initially cut into a plurality of pieces, each piece of which will eventually form a spade bit. Thereafter, the 2 0 individual parts are headed to form a bulb of material at a first end of the part 62. Each headed part is then sequentially heated and forged as illustrated by blocks 64 and 66, respectively. For a workpiece comprised of steel alloy, for example, each headed part 25 is heated to a temperature of between 1200°F and 2200*F. Thereafter, a pair of opposed dies 68 can be closed about the heated part. The opposed dies define a cavity of a'predetermined shape which, in turn, defines the resulting shape of the forged part. Once 3 0 forged, the opposed dies can be opened and the excess flash trimmed from the forged part as shown in block 70. Thereafter, an identification mark, such as the width of the blade portion, can be stamped on the part prior to heat treating, finishing and packaging the 35 spade bit as illustrated in blocks 72, 74, 7 6 and 78, respectively.

Alternatively, the spade bit 10 of NZ 300765 can be f°™ed by a forging method as illustrated in Figure 18. While principally described below as a cold forging method, the workpiece can be 5 heated prior to the forging step such that the forging method is a warm or hot forging method. The temperature ranges in which each of the various materials from which the workpiece can be formed must be heated in order to be cold, warm or hot forged 10 depend, among other things, upon the strength and internal properties of the respective material, and are known to those skilled in the art. For example, workpieces comprised of steel alloys typically have a temperature of between room temperature and 300*F 15 during cold forging operations, a temperature of between 200*F and 1400'F during warm forging operations, and a temperature of between 1200*F and 2200*F during hot forging operations. In addition, the forging method of the present invention which includes 20 a step of hot forging a workpiece is particularly effective to forge workpieces comprised of a material having a relatively low melting point, such as aluminum, brass, zinc and copper.

In addition, while described in conjunction 25 with the fabrication of a plurality of spade bits of nz 300765, the cold forging method illustrated in Figure 18 can produce a wide variety of parts including, without limitation, screwdriver bits and router bits, and is suitable for manufacturing 30 other metal parts, such as armature shafts.

As illustrated in Figure 18, a. plurality of parts, such as the spade bit, are forged according to the method of the present invention from a continuous length of metal stock 80, such as continuous wire 35 stock. Typically, the metal stock is comprised of a steel alloy, however, the metal stock can be comprised of any forgeable material known to those skilled in the art. For example, the metal stock can be comprised of copper, aluminum, titanium, zinc, brass or alloys thereof.

Regardless of the material, the continuous 5 metal stock is initially straightened, such as by passing the metal stock through a series of aligned rollers, as shown in block 82. The straightened metal stock is then incrementally advanced, such as by an indexer, as shown in block 84. The indexer 10 incrementally advances the continuous metal stock longitudinally a predetermined linear distance in a downstream direction. As illustrated in block 86, a leading portion of the continuous metal stock is clamped, typically by a clamp such as a pair of opposed 15 clamping dies, following each incremental advance of the metal stock, such that the leading portion of the metal stock is held at a fixed location.

Each time the metal stock 80 is clamped and held at a fixed location, a portion of the continuous 20 metal stock, upstream of the leading portion which is clamped, is forged. As shown schematically in block 88 and discussed in more detail belo$ in conjunction with Figures 19-21, the meansj£on forging is typically a forge including a plurality of dies 90 which are 25 radially closed about trie continuous metal stock. The plurality of closed die§ define a cavity of a predetermined shape which, in ^urn, defines the resulting shdpe of the forged portion of the metal stock. In addition, the' plurality of closed dies 30 define entry and exit ports through which the continuous metal stock extends during the forging step.

As shown in block 85, the metal stock 80 can be warmed prior to the forging step to increase the malleability of the metal stock. For example, an 35 induction coil can be disposed about the continuous metal stock upstream of the plurality of dies 90. Alternatively, the dies can include heating elements to 331GS5 warm the metal stock within the dies, such as by induction heating, during the forging step. However, as described above, the method of the present invention also includes cold forging in which the metal stock is 5 generally unheated or, for a steel alloy stock, has a temperature of between room temperature and 3 00*F, for example.

During the forging step 88, the continuous metal stock 80 grows longitudinally. This longitudinal 10 growth is compensated by a compensator which permits upstream longitudinal movement of that portion of continuous metal stock which is upstream of the fixed location. In one embodiment, the plurality of forging dies 90 are mounted on a carriage 92 which is adapted 15 to move longitudinally. Thus, the longitudinal growth of the continuous metal stock between the forged portion about which the plurality of dies are radially closed and the leading portion which is clamped causes the carriage to move in the upstream longitudinal 20 direction. Thus, the plurality of dies remain closed about the same portion of the metal stock during each forging step while permitting upstream longitudinal movement of the continuous metal stock, and, in some embodiments, corresponding rotation of the spool upon 25 which the supply of metal stock is mounted, to compensate -for longitudinal growth of the metal stock. As illustrated in Figure 18, the carriage can be longitudinally biased, such as by a spring or other biasing means 94, to prevent excessive movement in the 30 upstream direction and to return the carriage to its initial position after each forging step.

After forging a portion of the metal stock 80, the plurality of dies 90 are radially opened and the leading portion of the metal stock is released by 35 the clamping dies at 86 such that the continuous metal stock can be incrementally advanced by the indexer 84. Thereafter, the clamping and forging steps are f preferably repeated to forge another part from the continuous metal stock. As illustrated in block 86, the clamping dies also preferably stamp an identification mark on a previously forged part. In 5 addition, a previously forged part can be trimmed to the predetermined shape of the part by removing the flash or excess material generated during forging of the part as shown in block 87 while the metal stock is clamped and another part is being forged. 10 As shown in block 96, the part is only cut, such as by cutting means, from the portion of the continuous metal stock 80 which extends beyond the clamped leading portion of the metal stock after the forging and stamping steps. Once separated, the 15 discrete parts can be heat-treated, finished and packaged as shown in blocks 98, 100 and 102, respectively.

By processing the plurality of parts while still joined by the continuous metal stock, the amount 20 of handling of discrete parts is significantly reduced. In addition, the alignment of the dies 90 of the forging means relative to the metal stock can be more accurately maintained to produce high quality parts having sharply defined features, such as, for example, 25 the above-described radial, angular and longitudinal separation of the spur cutting edge 32 from the forward cutting edge 34 of the respective side segments 20 of the blade portion 18 of the spade bit 10 of the present invention. In addition, by altering the amount of the 30 longitudinal advance provided by the indexer, parts of varying lengths can be produced from the same continuous metal stock, such as spade bits having an elongate shank of varying lengths.

As illustrated in Figures 19-21, a part of a 35 predetermined shape can be forged from a workpiece 120 according to the forging method and apparatus of NZ 3341 60. According to InlltLLtliiUr.L i'lVjrcn'Y »Jri il'„ OF fj.z. - 5 MAR 1999 69$ NZ 334160, a plurality of parts, such as spade bits, can be forged from a continuous metal stock as described above or, alternatively, one or more discrete parts can be forged. In addition, the forging method and apparatus of NZ 334160 can also produce a wide variety of other parts, such as screwdriver bits and router bits, and is believed to be suitable for manufacturing other metal parts, such as armature shafts and the chamfered corner portions of the side segments, as best shown in Figures 3, 8 and 15. portion 18 which includes laterally opposed side segments 20 having respective chamfered corner portions 35, the side segments of the spade bit of NZ 30 0765 are typically ground, such as by a conventional grinding process, following the forging process to form the respective chamfered corner portions. Accordingly, chamfered corner portions which define a predetermined chamfer angle 37 with respect to a line parallel to the central longitudinal axis 14 can be precisely ground into the respective side segments. 110' includes opposed forging dies 112, typically a pair of opposed forging dies, which define a cavity 114 therebetween. The cavity, in turn, defines the resulting shape of the part formed by the forging method and apparatus. More specifically, at least one, and preferably each, forging die can include a contact surface 116 of somewhat Z-shaped configuration and which defines a portion of the cavity. According to one embodiment, the opposed forging dies includes two opposed sets of forging dies, each set of which includes at least one forging die having a contact surface of somewhat Z-shaped configuration.

NZ 300765 In addition, while the spade bit 10 of could be forged so as to have a blade As shown in Figure 19, the forging apparatus l."'jThLLh(j; <JAl I -.tj: OF NZ I I v'l [ i -5 MAR 1999 RECEIVED j? °' 6$5 As described above in conjunction with the spade bit of nz 300765, the Z-shaped cavity includes a central portion 134 defining a central plane 136 and opposed side portions 138 extending from opposite sides of the central portion. The opposed side portions define respective lateral planes 140 which are oblique to the central plane. The respective contact surfaces contact and shape the workpiece 120 into the predetermined shape of the resulting part.

Each respective contact surface 116 also preferably includes at least a portion which is relatively flat and defines a contact plane 118, and which is parallel to the relatively flat portion of the other die.

The forging apparatus 110 of NZ 334160 also includes means for radially closing the opposed forging dies. As described below with respect to Figures 20 and 21, the means for radially closing the forging dies includes a die housing 130. In particular, the forging dies 112 move radially inward in a predetermined direction, as shown by the arrows in Figure 19, upon relative movement between the die housing and the pair of opposed forging dies as shown in Figure 20, and as described below in detail.

A contact plane 118 of a forging die 112 can be defined by various portions of the respective contact surface 116. For example, as shown in Figure 19, the centfer portions 117 of the respective contact surfaces are oblique to the predetermined direction in which the forging dies close and define respective contact planes. Thus, the contact planes impart both axial and radial forces 142 and 144, respectively, to the workpiece which, in turn, result in compressive, tensile and shear stresses within the workpiece during the deformation process. The resulting compressive and shear force components therefore deform the workpiece liVTELlt'UiJAL. I-Kur'ch FY Uri ,'Cv OF N.Z. - 5 MAR 1999 «v ""7 r\ c-.:. 50 : 0 -J :j 120 outwardly into the predetermined shape defined by the forging dies.

More particularly, an angle 122 is defined between the respective contact planes 118 and a 5 reference plane 12 4 perpendicular to the predetermined direction in which the forging dies 112 move as shown in Figure 19. In a preferred embodiment, the angle is between about 5° and about 15° and, in one specific example, is about 10°. As used herein, the term 10 "compressive force" includes those forces in the predetermined direction in which the forging dies move, and the term "shear force" includes those lateral forces which tend to deform the workpiece 120 radially outward. Thus, for a given amount of input power, the 15 amount of shear force and compressive force imparted to the workpiece increases and decreases, respectively, as the angle defined between a respective contact plane and the reference plane increases. Likewise, for a given amount of input power, the amount of shear force 20 and compressive force imparted to the workpiece decreases and increases, respectively, as the angle defined between a respective contact plane and the reference plane decreases.

At least parts of the workpiece 120 which are 25 subjected to shear force, and hence shear stress, are more readily deformed since the shear strength of most common workpieces, i.e., most metallic materials, is less than the compressive strength of the same material. Typically, the shear strength of metallic 30 materials is approximately 60% of the compressive strength of the same material. For example, during the formation of a spade bit according to this method, both side segments are preferably subjected to relatively high shear stresses for producing the maximum 35 lateral displacement form a workpiece, or wire, of the smallest initial diameter.

INTELLECTUAL PROPERTY OFFICE OF N.Z. 1 2 FEB 1999 RECEIVED 3s Thus, significantly less input power is required to deform a workpiece 120 with shear forces than with compressive forces. In addition, the application of shear forces which more readily deform a workpiece radially outward allows the ratio of the thickness of a part to the width or diameter of a part to be decreased such that thin parts having a relatively large diameter, such as a spade bit, can be readily forged according to the method of NZ 334160.

However, the application of shear force to deform the workpiece 120 significantly increases the forces which the forging dies and die housing must withstand during the forging process and, accordingly, 15 has been avoided in conventional forging processes in which the forging dies are closed in a rectilinear manner to impart compressive forces on the workpiece. In order to withstand the increased forces, the opposed forging dies 112 are comprised, in one preferred 20 embodiment, of a high speed steel and, more preferably, are comprised of CPM® REX"* M4 high speed steel, or an equivalent, marketed by Colt Industries Crucible Specialty Metals Division of Syracuse, New York and described in more detail in a publication entitled 25 Crucible Data Sheet by Colt Industries Crucible Specialty Metals Division bearing document number D88 308-5M-776.

In addition, the time required to deform a workpiece 120 with shear forces is generally greater 30 than the corresponding time required to deform a similar workpiece with compressive forces. Thus, for parts which have a relatively small diameter, such as spade bits having a diameter of about 3/8 inch or less, in which deformation of the workpiece with shear forces 35 will not conserve a significant amount of input power, the angle 122 defined between the respective contact planes 118 and the reference plane 124~as d.ecrea.sed-r--or "'.ILLLLII i L'.!. IV...Pi y,: ' 0r i-j Z. ~5 MAR 1999 Q '» > c s C1 o o _t t> o O eliminated, such that increasing amounts of compressive force are imparted to the workpiece and the deformation process proceeds more quickly. In these embodiments, however, shear forces can still be imparted, albeit in 5 lesser amounts, by the contact surfaces which include oblique lateral portions such as illustrated by the z- shaped cavity of Figure 19. For parts with a * relatively large diameter, such as spade bits having a diameter of about 7/16 inch or greater, in which 10 deformation of the workpiece with shear force will conserve a significant amount of input power, the respective contact planes are preferably disposed at an angle, such as 10°, for example, with respect to the reference plane.

The means for closing the opposed forging dies preferably includes means for maintaining a predetermined alignment of the opposed forging dies 112 during the forging process. As illustrated in Figures 19 and 21, the means for maintaining alignment of the 20 opposed forging dies preferably includes a pair of opposed side dies 126. The opposed side dies are positioned adjacent to the opposed side surfaces 128 defined by the opposed forging dies. As shown schematically in Figure 21, the opposed forging dies 25 and the pair of side dies define a die assembly which has a generally conical shape.

As also shown schematically in Figures 2 0 and 21, the means for closing the opposed forging dies preferably includes a die housing 130, including end 30 plates 146, defining a conical cavity therein. The internal conical cavity defined by the die housing is adapted for receiving the complementarily-shaped conical die assembly such that the die housing circumferentially encompasses the die assembly. Thus, 35 by axially inserting the die assembly into the die housing, such as with a die press or conical ram (not illustrated), the opposed forging dies and the pair of ' 6 g side dies are radially closed about the workpiece. The strength of the die assembly and its resulting ability to withstand forces generated during the deformation of the workpiece with axial and compressive forces 142 and 5 144 which, in turn, generate compressive, tensile and shear stresses is further enhanced by radial direction in which the die assembly is closed and the surrounding relationship of the die housing to the die assembly.

The die housing 130 is also preferably 10 comprised of a relatively strong material, such as by high speed steel and, more preferably, CPM® REX* M4 high speed steel. Further, while the pressure or force required to insert the die assembly into the die housing will vary depending upon the processing 15 conditions, including the type of material from which the workpiece is formed and the size and shape of the resulting part, a hydraulic press, such as a 500 ton press, has produced spade bits of NZ 300765 from 1050 carbon steel. 2 0 In addition, one embodiment of the die assembly of this aspect of the present invention can also define entry and exit ports 132 as shown in Figure 20 through which a continuous metal stock can extend such that a plurality of parts can be formed as 25 described above. However, the forging method and apparatus of NZ 334160 can also be employed to form discrete parts without departing from the scope of the invention.

In the drawings and the specification, there 3 0 has been set forth preferred embodiments of the invention and, although specific terms are employed, the terms are used in a generic and descriptive sense only and not for purpose of limitation, the scope of the invention being set forth in the following claims. liJTfcLLiXflnt Ori n-'.

OF N.Z. - 5 MAR 1999 RECEIVED O <"» > p ?■ o o j. b b O

Claims (2)

1. WHAT WE CLAIM IS: 1. A method of forging a plurality of parts from a continuous metal stock, the method comprising the steps of: incrementally advancing the continuous metal stock a predetermined linear distance such that the metal stock advances longitudinally in a downstream direction; forging a portion of the continuous metal stock upstream of the leading portion each time the metal stock is-clamped and held at the fixed location; and compensating for longitudinal growth of the continuous metal stock created during each forging step by permitting upstream longitudinal movement of that portion of the continuous metal stock which is upstream gf the fixed location. 2. A forging method according to Claim 1, further comprising the step of clamping a leading portion of the continuous metal stock following each incremental advance of the metal stock so as to hold the leading portion at a fixed location.
2. 2. A forging method according to Claim 1 wherein each forging step includes a step of radially closing a plurality of dies about the continuous metal stock wherein the plurality of closed dies define a cavity of a predetermined shape which defines the resulting shape of the forged portion of the metal stock and wherein the plurality of closed dies define entry and exit ports through which the continuous metal stock extends during each forging step. -40- 33ACS5 4 . A forging method according to Claim -3 wherein the plurality of dies are mounted on a carriage which is adapted to move longitudinally, and wherein said compensating step further comprises the step of mounting the carriage such that the longitudinal growth of the continuous metal stock between the forged portion about which the plurality of dies are radially closed and the leading portion which is clamped causes the carriage to move in the upstream longitudinal direction such that the plurality of dies remain closed about the same portion of the metal stock during said forging step. 5. A forging method according to Claim 4 further comprising the step of longitudinally biasing the carriage on which the plurality of dies are mounted to prevent excessive movement of the carriage in an upstream direction and to return the carriage to an initial position after each forging step. 6. A forging method according to Claim 1 further comprising the steps of: radially opening-the plurality of dies after forging a portion of the metal stock; releasing the leading portion of the metal stock such that the continuous metal stock can be incrementally advanced; and repeating the steps of the method to forge another part. 7. A forging method according to Claim 1 further comprising the step of cutting a previously forged part from a portion of the continuous metal stock which extends beyond the clamped leading portion of the metal stock to thereby separate the forged metal stock into a plurality of discrete parts. -41- -v f- \ : \ ,i n H ■ -- - ^. j 8. A forging method according to Claim 1 wherein said clamping step comprises the step of stamping an identification mark on a previously forged part. 9. A forging method according to claim 1, wherein said part is a spade-type boring bit. 10. An apparatus for forging a plurality of parts from a continuous metal stock according to the method of Claim 1, the apparatus comprising: indexing means for incrementally advancing the continuous metal stock a predetermined linear distance such that the metal stock advances longitudinally in a downstream direction through the forging apparatus; forging means for forging a portion of the continuous metal stock following each incremental advance of the continuous metal stock; and means for compensating for longitudinal growth of the continuous metal stock created during each cold forging by permitting upstream longitudinal movement of that portion of the continuous metal stock which is upstream of the portion of the metal stock which is being forged. A forging apparatus according to Claim 10 wherein said forging means comprises: a plurality of dies radially disposed about the continuous metal stock; and means for radially closing said plurality of dies about the continuous metal stock, wherein said plurality of dies define a cavity of a predetermined shape which defines the resulting shape of the forged portion of the metal stock and wherein said plurality of dies define entry and exit ports through which the continuous metal stock extends. INTELLECTUAL PROPERTY OFFIC OF N1. 12 FEB 1999 RECEIVED 9 '» » 6 o a ^ o 22.■ A forging apparatus according to Claim 11 further comprising means for clamping a leading portion of the continuous metal stock, upstream of the portion of metal stock being forged, following each incremental advance of the metal stock so as to hold the leading portion at a fixed location. 13. A forging apparatus according to Claim 12 wherein said compensating means comprises a carriage on which said plurality of dies are mounted, and wherein said carriage is mounted so that the longitudinal growth of the continuous metal stock between the forged portion about which the plurality of dies are radially closed and the leading portion which is clamped causes said carriage to move in the upstream longitudinal direction. 14. A forging apparatus according to Claim 13 wherein said compensating means further comprises biasing means for urging said carriage in. a downstream direction to prevent excessive movement of said carriage in an upstream direction and "tc return said carriage to an initial position after each forging operation. .15, A forging apparatus according to Claim 11 further comprising cutting means for separating a previously forged part from a portion of the continuous metal stock which extends beyond the clamped leading portion of the metal stock to thereby separate the forged metal stock into a plurality of discrete parts . 16. A forging apparatus according to Claim 15 further comprising: means, upstream of said forging means, for straightening the continuous metal stock; trimming means, downstream of the said forging means., for trimming flash produced by said forging means from the forged part; -43- * 7/ ^ /T\\ f , '-'•w 5-6 1 6l; :i means, downstream of said cutting means, for heat treating the forged parts; means, downstream of said heat treating means, for finishing the surface of the forged parts; and means, downstream of said finishing means, for packaging the finished parts. 17. A forging apparatus according to Claim 12 wherein said clamping means comprises means for stamping an identification mark on a previously forged part. 18. A forging apparatus which carries out the steps of the method claimed in claim 1, comprising: opposed forging dies defining a cavity therebetween of the predetermined shape of the resulting part, at least one forging die including a contact surface which defines a portion of the cavity for contacting and shaping the workpiece into the predetermined shape of the resulting part, each respective contact surface including at least one relatively flat portion defining a contact plane and which opposes and is parallel to a relatively flat portion of the other die; and a die housing defining an internal cavity for receiving and circumferentially encompassing the opposed forging dies wherein said opposed forging dies are radially closed upon their insertion into said die housing such that said forging dies move radially inward in a predetermined direction, the predetermined direction being oblique to the respective contact planes defined by the opposed contact surfaces such that the respective contact surfaces impart both axial and radial forces to at least portions of the workpiece to generate compressive and shear forces within the workpiece and to form the part of predetermined shape within the cavity defined between the opposed forcrina I INTELLECTUAL PROPERTY OFF OF N.Z. 1 2 FEB 1999 RECEIVED -44- O 'i » i<■ o •- <•' *-> b h* O dies, and wherein said circumferentially encompassing die housing reinforces said opposed forging dies against forces imparted upon insertion of said opposed dies in said die housing. 19. A method according to Claim 18 wherein said forging apparatus further comprises means for maintaining a predetermined alignment of said opposed forging dies while said forging dies are radially closed. 20. A method according to Claim 19 wherein said opposed forging dies define opposed side surfaces, and wherein said means for maintaining the predetermined alignment of the forging dies includes a pair of side dies, one of which is positioned adjacent each side surface defined by opposed forging dies. 21. A method according to Claim 20 wherein said opposed forging dies and said pair of side dies define a conical die assembly, and the internal aperture defined by said die housing is conical for receiving the complimentarily-shaped conical die assembly such that by inserting the die assembly into said die housing, said opposed forging dies and said pair of side dies are radially closed. 22. A method according to Claim 18 wherein the contact plane of each respective forging die and a reference plane perpendicular to the predetermined direction of movement of said opposed forging dies define an angle of between about 5° and about 15° therebetween. 23. A method according to Claim 18 wherein said opposed forging dies define entry and exit ports through which a continuous metal stock extends such that a plurality of parts of the predetermined shape can be forged. 24. A method according to Claim 18 wherein said opposed forging dies are comprised of M4 high speed steel. 25. A method according to Claim 18 wherein said die housing is comprised of M4 high speed steel. ^ ^ 1 £ 0 i \J U 'J L- ,j t. 26. A method according to Claim 18 for forging a part having a diameter of at least 7/16 inch wherein an angle of about 10° is defined between each respective contact plane and a plane perpendicular to the predetermined direction in which the opposed forging dies move radially inward. 27. A method according to Claim 18 for forging a part having a diameter of less than 7/1 6 inch wherein each respective contact plane is parallel to a plane perpendicular to the predetermined direction in which the opposed forging dies move radially inward. 28. A method of forging a plurality of parts from a continuous metal stock according to claim 1, substantially as herein described. 29. A method according to any one of claims 1-9, substantially as herein described. 30. An apparatus for forging a plurality of parts from a continuous metal stock, substantially as herein described with reference to any one of the accompanying drawings thereof. 31. An apparatus according to any one of claims 10-17, substantially as herein described. 32. A method according to claim 18, substantially as herein described with reference to any one of the accompanying drawings thereof. 33. A method according to any one of claims 1 8-27, substantially as herein described. INTELLECTUAL PROPERTY OFFI OF N.Z. 1 2 FEB 1999 RECEIVED -46- 34. A spade-type boring bit, when forged according to a method of any one of claims 1-9, substantially as herein described. 35. A spade-type boring bit according to claim 34, comprising a chamfered corner portion. 36. A spade-type boring bit, when produced by an apparatus according to any one of claims 10 to 17. END OF CLAIMS INTELLECTUAL PROPERTY OFFICI OF NZ 1 2 FEB 1999 RECEIVED