US20050181898A1 - Unitary broadhead blade unit - Google Patents

Unitary broadhead blade unit Download PDF

Info

Publication number
US20050181898A1
US20050181898A1 US11/102,939 US10293905A US2005181898A1 US 20050181898 A1 US20050181898 A1 US 20050181898A1 US 10293905 A US10293905 A US 10293905A US 2005181898 A1 US2005181898 A1 US 2005181898A1
Authority
US
United States
Prior art keywords
blade unit
ferrule
energy beam
blade
broadhead
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US11/102,939
Inventor
Philip Muller
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from US09/922,550 external-priority patent/US6726581B2/en
Priority claimed from US10/094,125 external-priority patent/US6605012B2/en
Application filed by Individual filed Critical Individual
Priority to US11/102,939 priority Critical patent/US20050181898A1/en
Publication of US20050181898A1 publication Critical patent/US20050181898A1/en
Priority to US11/234,353 priority patent/US20060030439A1/en
Priority to US11/758,710 priority patent/US20070228022A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B6/00Projectiles or missiles specially adapted for projection without use of explosive or combustible propellant charge, e.g. for blow guns, bows or crossbows, hand-held spring or air guns
    • F42B6/02Arrows; Crossbow bolts; Harpoons for hand-held spring or air guns
    • F42B6/08Arrow heads; Harpoon heads

Definitions

  • the present invention generally relates to archery equipment. More particularly, the present invention relates to a unitary broadhead blade unit for hunting arrows, along with a method for manufacturing a unitary blade unit for a modular broadhead.
  • archery broadheads are made from multiple pieces that are fitted together.
  • the pieces may include individual blades, a tip, and/or other connecting parts.
  • Traditional broadheads also include a means for connecting the broadhead to an arrow, such as a receptacle designed to fit over the shaft of an arrow, with threads or glue to secure the broadhead to an arrow.
  • a receptacle designed to fit over the shaft of an arrow, with threads or glue to secure the broadhead to an arrow.
  • Such broadheads can be expensive to manufacture, and they can become loose, and may even separate, through use or transport.
  • FIG. 1 hereto discloses a monolilthic broadhead, including a ferrule 8 and a plurality of blades 5 .
  • FIGS. 8A, 8B , and 9 of Grace, Jr. which along with the accompanying text at col. 2, line 49 through col. 4, line 29 are incorporated herein by reference, discloses a method of manufacturing the broadhead using a process known as metal injection molding.
  • the broadhead produced by the method described in Grace, Jr. provides several disadvantages.
  • the entire unit must be replaced in order to replace the blades, even if the remainder of the unit (i.e., the ferrule) is suitable for re-use.
  • the entire unit must be replaced.
  • a method of manufacturing a unitary blade unit for a modular broadhead includes providing (i.e., using) a mold having one or more cavities that define a multiple-bladed blade unit.
  • a mixture of metal and binder is inserted into the mold, and the mixture is compacted in the mold to form an intermediate blade unit.
  • the intermediate blade unit is processed to remove at least a portion of the binder and sintered to form a sintered blade unit.
  • the blades of the sintered blade unite are sharpened to form a cutting edge on each blade to yield a final blade unit.
  • the final blade unit requires a separate ferrule in order to attach to an arrow.
  • the mixture is in powdered form, and the sintering step may include sintering at an elevated temperature and pressure.
  • a method of manufacturing a blade unit for a modular broadhead includes using metal injection molding to form a blade unit from a mixture that includes metal and a binder.
  • the blade unit has at least two blades and requires a separate ferrule in order to attach to an arrow.
  • the method may also include manufacturing a separate adapter for securing the blade unit to the ferrule.
  • the method may include forming the blade unit to include a first integral adapter for securing the blade unit to the ferrule, as well as manufacturing a second separate adapter for further securing the blade unit to the ferrule.
  • a method of manufacturing a blade unit for a modular broadhead includes arranging multiple components in the form of a blade unit for a modular broadhead.
  • An energy beam is directed toward contact segments (i.e., locations where at least two components are in contact) to weld the components into a blade unit.
  • the components may include blades, a cap structure for receiving a separable ferrule, and/or a collar for receiving a separable ferrule.
  • the energy beam may be a laser
  • the method may include focusing the energy beam toward a contact segment using one or more devices such as a focus cell, a lens, and/or a mirror. A focal point of the energy beam may be moved along a contact segment in a direction from a tip of the blade unit to a base of the blade unit.
  • FIG. 1 illustrates a prior art monolithic broadhead.
  • FIG. 2 illustrates an exploded view of a preferred embodiment of the present inventive unitary blade unit, with a separate ferrule.
  • FIG. 3 is a non-exploded view of the blade unit of FIG. 2 , also illustrating a separate ferrule before the ferrule engages with the blade unit.
  • FIG. 4 illustrates an alternate embodiment of a unitary blade unit before a ferrule engages with the blade unit.
  • FIGS. 5A, 5B , and 5 C show isolated views of the base collar originally shown in FIGS. 2 and 3 with preferred dimensions.
  • FIGS. 6A, 6B , and 6 C show isolated views of the cap originally shown in FIGS. 2 and 3 with preferred dimensions.
  • FIGS. 7A and 7B illustrate variations of a unitary blade unit where a separate cap is not required.
  • FIG. 8 illustrates preferred steps of manufacturing a unitary blade unit using metal injection molding.
  • FIG. 9 illustrates exemplary blades that may be produced when manufacturing a blade unit using metal injection molding.
  • FIG. 10 illustrates a preferred laser welding process
  • FIG. 11 provides a close-up view of an exemplary tip structure for a blade unit as produced by the laser welding process of FIG. 10 .
  • FIGS. 2 and 3 illustrate a first preferred embodiment of the invention.
  • FIG. 2 defines the preferred elements of an embodiment in an expanded view of a blade unit as it receives a ferrule
  • FIG. 3 illustrates an as-built view of the embodiment while receiving a ferrule.
  • blade unit 10 includes three blades 16 . More than three blades may be used, although three is the preferred number of blades.
  • Each blade 16 has a razor edge 12 and a base 14 .
  • each blade extends radially from a common frontal point 18 to its base 14 .
  • frontal point 18 is formed by the intersection of the at least two of the razor edges 12 to provide the ability to cut a target with the razor edges 12 on contact.
  • a tip is sometimes referred to as a “chisel-type” or “cut on contact” tip.
  • the frontal point 18 may comprise another tip, such as a conical, cylindrical, pyramid-shaped, screwdriver-tip-shaped, or any other type of point that provides a shield or initial contact point over or adjacent to a frontal area of the blades for a “punch cut” before the razor edges meet the target.
  • An example of a conical tip 6 for a punch cut is shown in FIG. 1 .
  • the blades 16 are interconnected to provide a single, solid blade unit 10 . This may be done by welding or brazing the three blades 16 together. Alternately, the blade unit 10 may be singly formed with casting or metal injection molding. The blade unit may also be made by any other means now known or later developed so long as the process produces a unitary blade unit with a tip of some type that is integral with the blade unit.
  • each blade 16 is connected to a base collar 20 that has a central aperture 22 in alignment with a cap 24 .
  • the cap 24 is connected to an interior portion of each blade 16 at a location that is between the collar 20 and the frontal point 18 .
  • the cap 24 has a first means for receiving a ferrule 30 after a ferrule 30 is passed through the central aperture 22 of the base collar 20 .
  • the means for receiving the ferrule is preferably a series of threads 26 , which optionally may be tapered to mate with a tapered series of threads 32 on the ferrule 30 .
  • FIGS. 2 and 3 illustrate an exemplary ferrule 30 having a body 34 , threads 32 for connecting the ferrule to the blade unit, and threads 36 for connecting the ferrule to an arrow shaft.
  • FIGS. 2 and 3 illustrate an exemplary ferrule 30 having a body 34 , threads 32 for connecting the ferrule to the blade unit, and threads 36 for connecting the ferrule to an arrow shaft.
  • other means such as tabs, holes and pins, or other mechanisms are possible.
  • the base collar 20 such as that illustrated in FIGS. 2 and 3 is preferably integral with the blade unit.
  • the integral base collar may be omitted.
  • a locking collar 25 may be provided, with a means of mating with the ferrule 31 , such as threads 27 as illustrated in FIG. 3 , although other mating means may be used.
  • the bases 15 of each blade would include a projection 29 such as a tab to further secure the base 15 to the slot 33 .
  • the locking collar 25 secures the blade unit 11 to the ferrule 31 .
  • a cap between the locking collar 25 and the frontal point 19 is not required.
  • FIGS. 5A, 5B , and 5 C show isolated views of a preferred embodiment of the base collar 20 with preferred dimensions. However, other dimensions are possible, depending on the size of the ferrule and desired blade unit. Similarly FIGS. 6A, 6B , and 6 C show isolated views of a cap 24 with preferred dimensions. Other dimensions are possible, depending on the size of the ferrule and desired blade unit. As a further alternative, FIGS. 7A and 7B illustrate embodiments where a separate cap is not required. Instead, in these embodiments, a means for receiving the edge or tip of a ferrule is formed by the undersides of the blades 40 themselves.
  • the “cap” may comprise the blades themselves, which are preferably formed with grooves 42 to receive threads of a ferrule, tabs 43 to lock with one or more recesses of a ferrule, or holes, pins, raised edges, or other means to secure a ferrule in place, preferably and optionally after a ferrule is placed through an integral collar 44 .
  • the collar 44 may include threads to further secure the ferrule to the blade unit.
  • the embodiment using a base collar 20 may also include an optional means for connection to a ferrule 30 .
  • a means may include, for example, a taper, preferably about two degrees to about ten degrees, more preferably about five degrees, to mate with the ferrule and prevent it from moving through a force fit.
  • the taper may be on the body 34 of the ferrule, as shown in FIGS. 2 and 3 , or it may be elsewhere.
  • the blade unit 10 may receive the ferrule 30 when a person or device inserts the front portion of the ferrule 30 through the base collar 20 until the front portion (such as threaded area 32 ) is received by the cap 24 .
  • the ferrule 30 is then rotated such that the threaded area 32 screws into the cap 24 .
  • the central portion 34 of the ferrule is drawn into, mates inside of, and tightens in the central aperture 22 of the base collar 20 .
  • a secure connection is made.
  • other means of connection such as pins or locking tabs, may be used. Examples of blade units that may connect by tabs and/or grooves are shown in FIGS. 4, 7A and 7 B.
  • the frontal point 18 of the blade unit is the first part that will contact a target. Since it is just a point, and since it will receive a tremendous force upon impact, it is preferred that the blade unit be constructed in such a way that it has additional strength. This can be accomplished by tapered grinding, moving over a sharpening stone, or other sharpening of the razor edges 12 . With such a procedure, each razor edge 12 may be sharpened at an angle that is greater than the angle that the razor edge 12 is adjacent to the base 14 of the blade 16 . Near the frontal point 18 , the angle is preferably less sharp, this providing a wider cutting edge near the frontal point 18 than near the base 14 .
  • the unitary blade unit is preferably made of any metal. More preferably, the unitary blade unit is made using carbon steel, stainless steel, spring steel, tool steel, or titanium, or a composition including any of the above.
  • the unitary blade unit may be formed by blending a metal powder and binder (such as plastic or wax).
  • the blending may be done in a single step 80 , or in two or more graduated steps 82 .
  • the mixture is pelletized and/or powdered 84 (optionally in combination with the blending step), and it is injected 86 into a blade unit mold having one or more cavities that provide a desired blade unit design.
  • the method may use a mold that provides a blade unit having two, three, four, or more blades, although the preferred number is three blades.
  • the mixture is compacted in the mold with pressure to yield an intermediate piece.
  • the piece is processed (such as by immersion in a solvent 88 , optionally followed by heating 90 ) to remove at least a portion of the binder.
  • the piece is then sintered 92 at an elevated temperature and/or pressure to reduce the size and increase the density of the blade unit.
  • the blade unit edges may be sharpened 94 using either a conventional or a specially-designed sharpening tool.
  • Other embodiments of molding may also be used to manufacture the blade unit.
  • This preferred method embodiment of the present invention is intended to include the use of metal injection molding to manufacture any unitary blade-unit that is separate from a ferrule, including but not limited to the blade units illustrated in FIGS. 2, 3 , and 4 and variants thereof.
  • each blade is tapered so that it is thicker at its base than it is at the frontal tip.
  • FIG. 9 illustrates rear views of exemplary blades 50 and 54 , each of which has a base 51 and 55 and having a thickness that begins to taper at some point between the base and the tip or outer edge 52 and 56 .
  • the blade unit may be made by assembling the blades into a unitary structure.
  • the blades will be fastened together using any commonly known welding procedure such as laser welding, electron beam welding, TIG welding, plasma welding, resistance welding, electron beam welding, fusion welding, pressure welding, friction welding, ultrasonic welding, or other welding methods.
  • the weld of each seam is begun at or near the frontal point and proceeds toward the base.
  • fastening methods other than welding may be used. Exemplary laser welding equipment and procedures are illustrated in FIG. 10 . Referring to FIG. 10 , a laser unit 60 directs a beam of energy toward an intersection of two blades of an exemplary blade unit 66 .
  • FIG. 11 A closer view of the tip structure of blade unit 66 is provided in FIG. 11 , which also shows the points of intersection 67 .
  • the beam of energy is preferably directed toward the intersection 67 using a focus cell 61 , mirror, or other device that focuses the beam toward the point of intersection.
  • the energy beam fuses the blades at the point of intersection 67 .
  • This process is performed for each point of intersection, preferably simultaneously with multiple lasers and focus cells such as is shown in FIG. 10 , but optionally with a single laser that welds on a joint-by-joint basis.
  • the weld is performed into the tip structure to provide a “cut on contact” blade unit.
  • alternate tip structures are possible.
  • the unitary blade unit provides several advantages over the prior art. For example, by providing a separate blade unit and ferrule, a user can replace only one part (i.e., either the blade or the ferrule) without replacing the other, thus reducing replacement costs.
  • the separation of blade and ferrule allows the manufacturer to provide a weight-adaptable broadhead by manufacturing a standard blade unit and varying ferrules having different weights.
  • the blade unit and the ferrule may be made of different materials.
  • the weight of the overall broadhead i.e., the combination of the blade and ferrule
  • optionally may be varied by changing the ferrule without replacing the blades, or vice versa.
  • the blade-unit can be sharpened by grinding, polishing, sanding, or any standard sharpening method
  • the user may decide to simply dispose of the unitary blade unit and attach a new blade unit to an existing ferrule, resulting in ease of use for the user and the potential for increased sales for the manufacturer.
  • metal injection molding When made by metal injection molding, the blade unit designer receives a tremendous amount of freedom in the shaping and designing of the unit. Exact radii, tapering, and other intricacies can be achieved with minimal cost difference. Metal injection molding also allows metal parts to have a complex geometry with great strength.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)

Abstract

A unitary blade unit for an archery broadhead includes a tip structure and blades inseparably connected into a single blade unit. The blade unit is made by molding such as metal injection molding or laser welding.

Description

    RELATED APPLICATIONS AND CLAIMS OF PRIORITY
  • This application claims priority to, is a continuation of, and incorporates by reference U.S. Patent Application. No. 10/185,089, filed Jun. 28, 2002, which in turn claims priority to: (1) U.S. Provisional Patent Application No. 60/354,214, filed Feb. 4, 2002; (2) U.S. Provisional Patent Application No. 60/365,249, filed Mar. 18, 2002; (3) U.S. Pat. No. 6,726,581, filed Aug. 4, 2001 (continuation-in-part), which claimed priority to U.S. Provisional Patent Application No. 60/265,114, filed Jan. 31, 2001, and U.S. Provisional Patent Application No. 60/293,307, filed May 24, 2001; and (4) U.S. Pat. No. 6,605,012, filed Mar. 8, 2002 (continuation-in-part), which claimed priority to U.S. Provisional Patent Application No. 60/273,819, filed Mar. 8, 2001, and U.S. Provisional Patent Application No. 60/286,030, filed Apr. 24, 2001.
  • FIELD OF THE INVENTION
  • The present invention generally relates to archery equipment. More particularly, the present invention relates to a unitary broadhead blade unit for hunting arrows, along with a method for manufacturing a unitary blade unit for a modular broadhead.
  • BACKGROUND OF THE INVENTION
  • Traditionally, archery broadheads are made from multiple pieces that are fitted together. The pieces may include individual blades, a tip, and/or other connecting parts. Traditional broadheads also include a means for connecting the broadhead to an arrow, such as a receptacle designed to fit over the shaft of an arrow, with threads or glue to secure the broadhead to an arrow. However, such broadheads can be expensive to manufacture, and they can become loose, and may even separate, through use or transport.
  • One attempt to overcome this problem is described in U.S. Pat. No. 6,290,903, to Grace, Jr. As described in FIG. 1 hereto, Grace, Jr. discloses a monolilthic broadhead, including a ferrule 8 and a plurality of blades 5. FIGS. 8A, 8B, and 9 of Grace, Jr., which along with the accompanying text at col. 2, line 49 through col. 4, line 29 are incorporated herein by reference, discloses a method of manufacturing the broadhead using a process known as metal injection molding. However, the broadhead produced by the method described in Grace, Jr. provides several disadvantages. For example, by combining both the ferrule and blade in a single unit, the entire unit must be replaced in order to replace the blades, even if the remainder of the unit (i.e., the ferrule) is suitable for re-use. Alternatively, if the threads or other parts of the ferrule become damaged, the entire unit must be replaced.
  • Accordingly, it is desirable to provide an improved unitary blade unit for a modular broadhead.
  • SUMMARY OF THE INVENTION
  • In accordance with one embodiment of the invention, a method of manufacturing a unitary blade unit for a modular broadhead includes providing (i.e., using) a mold having one or more cavities that define a multiple-bladed blade unit. A mixture of metal and binder is inserted into the mold, and the mixture is compacted in the mold to form an intermediate blade unit. The intermediate blade unit is processed to remove at least a portion of the binder and sintered to form a sintered blade unit. The blades of the sintered blade unite are sharpened to form a cutting edge on each blade to yield a final blade unit. The final blade unit requires a separate ferrule in order to attach to an arrow. In certain embodiments, the mixture is in powdered form, and the sintering step may include sintering at an elevated temperature and pressure.
  • In accordance with another embodiment, a method of manufacturing a blade unit for a modular broadhead includes using metal injection molding to form a blade unit from a mixture that includes metal and a binder. The blade unit has at least two blades and requires a separate ferrule in order to attach to an arrow. In embodiments, the method may also include manufacturing a separate adapter for securing the blade unit to the ferrule. Further, the method may include forming the blade unit to include a first integral adapter for securing the blade unit to the ferrule, as well as manufacturing a second separate adapter for further securing the blade unit to the ferrule.
  • In accordance with an alternate embodiment, a method of manufacturing a blade unit for a modular broadhead includes arranging multiple components in the form of a blade unit for a modular broadhead. An energy beam is directed toward contact segments (i.e., locations where at least two components are in contact) to weld the components into a blade unit. The components may include blades, a cap structure for receiving a separable ferrule, and/or a collar for receiving a separable ferrule. In embodiments, the energy beam may be a laser, and the method may include focusing the energy beam toward a contact segment using one or more devices such as a focus cell, a lens, and/or a mirror. A focal point of the energy beam may be moved along a contact segment in a direction from a tip of the blade unit to a base of the blade unit.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1 illustrates a prior art monolithic broadhead.
  • FIG. 2 illustrates an exploded view of a preferred embodiment of the present inventive unitary blade unit, with a separate ferrule.
  • FIG. 3 is a non-exploded view of the blade unit of FIG. 2, also illustrating a separate ferrule before the ferrule engages with the blade unit.
  • FIG. 4 illustrates an alternate embodiment of a unitary blade unit before a ferrule engages with the blade unit.
  • FIGS. 5A, 5B, and 5C show isolated views of the base collar originally shown in FIGS. 2 and 3 with preferred dimensions.
  • FIGS. 6A, 6B, and 6C show isolated views of the cap originally shown in FIGS. 2 and 3 with preferred dimensions.
  • FIGS. 7A and 7B illustrate variations of a unitary blade unit where a separate cap is not required.
  • FIG. 8 illustrates preferred steps of manufacturing a unitary blade unit using metal injection molding.
  • FIG. 9 illustrates exemplary blades that may be produced when manufacturing a blade unit using metal injection molding.
  • FIG. 10 illustrates a preferred laser welding process.
  • FIG. 11 provides a close-up view of an exemplary tip structure for a blade unit as produced by the laser welding process of FIG. 10.
  • DETAILED DESCRIPTION
  • FIGS. 2 and 3 illustrate a first preferred embodiment of the invention. FIG. 2 defines the preferred elements of an embodiment in an expanded view of a blade unit as it receives a ferrule, while FIG. 3 illustrates an as-built view of the embodiment while receiving a ferrule. Referring to FIGS. 2 and 3, blade unit 10 includes three blades 16. More than three blades may be used, although three is the preferred number of blades. Each blade 16 has a razor edge 12 and a base 14.
  • In the embodiment illustrated in FIGS. 2 and 3, each blade extends radially from a common frontal point 18 to its base 14. Preferably, and as illustrated, frontal point 18 is formed by the intersection of the at least two of the razor edges 12 to provide the ability to cut a target with the razor edges 12 on contact. Such a tip is sometimes referred to as a “chisel-type” or “cut on contact” tip. However, optionally and alternatively the frontal point 18 may comprise another tip, such as a conical, cylindrical, pyramid-shaped, screwdriver-tip-shaped, or any other type of point that provides a shield or initial contact point over or adjacent to a frontal area of the blades for a “punch cut” before the razor edges meet the target. An example of a conical tip 6 for a punch cut is shown in FIG. 1.
  • Returning to FIGS. 2 and 3, the blades 16 are interconnected to provide a single, solid blade unit 10. This may be done by welding or brazing the three blades 16 together. Alternately, the blade unit 10 may be singly formed with casting or metal injection molding. The blade unit may also be made by any other means now known or later developed so long as the process produces a unitary blade unit with a tip of some type that is integral with the blade unit.
  • In the preferred embodiment shown in FIGS. 2 and 3, the base 14 of each blade 16 is connected to a base collar 20 that has a central aperture 22 in alignment with a cap 24. The cap 24 is connected to an interior portion of each blade 16 at a location that is between the collar 20 and the frontal point 18. The cap 24 has a first means for receiving a ferrule 30 after a ferrule 30 is passed through the central aperture 22 of the base collar 20. As illustrated in FIGS. 2 and 3, the means for receiving the ferrule is preferably a series of threads 26, which optionally may be tapered to mate with a tapered series of threads 32 on the ferrule 30. However, other means, such as tabs, holes and pins, or other mechanisms are possible. As used herein, the term “ferrule” means a central shaft or any other separable device that connects the blade unit to the shaft of an arrow. FIGS. 2 and 3 illustrate an exemplary ferrule 30 having a body 34, threads 32 for connecting the ferrule to the blade unit, and threads 36 for connecting the ferrule to an arrow shaft. Again, other means, such as tabs, holes and pins, or other mechanisms are possible.
  • The base collar 20 such as that illustrated in FIGS. 2 and 3 is preferably integral with the blade unit. However, in an alternate embodiment, as illustrated in FIG. 4, if a ferrule 31 is equipped with slots 33 or other means to receive the bases 15 of each blade 17, the integral base collar may be omitted. In such an embodiment, a locking collar 25 may be provided, with a means of mating with the ferrule 31, such as threads 27 as illustrated in FIG. 3, although other mating means may be used. Returning to FIG. 4, optionally and preferably, the bases 15 of each blade would include a projection 29 such as a tab to further secure the base 15 to the slot 33. However, whether or not this option is used, the locking collar 25 secures the blade unit 11 to the ferrule 31. In such an embodiment, a cap between the locking collar 25 and the frontal point 19 is not required.
  • FIGS. 5A, 5B, and 5C show isolated views of a preferred embodiment of the base collar 20 with preferred dimensions. However, other dimensions are possible, depending on the size of the ferrule and desired blade unit. Similarly FIGS. 6A, 6B, and 6C show isolated views of a cap 24 with preferred dimensions. Other dimensions are possible, depending on the size of the ferrule and desired blade unit. As a further alternative, FIGS. 7A and 7B illustrate embodiments where a separate cap is not required. Instead, in these embodiments, a means for receiving the edge or tip of a ferrule is formed by the undersides of the blades 40 themselves. Here, the “cap” may comprise the blades themselves, which are preferably formed with grooves 42 to receive threads of a ferrule, tabs 43 to lock with one or more recesses of a ferrule, or holes, pins, raised edges, or other means to secure a ferrule in place, preferably and optionally after a ferrule is placed through an integral collar 44. Optionally, the collar 44 may include threads to further secure the ferrule to the blade unit.
  • Returning to FIGS. 2 and 3, the embodiment using a base collar 20 may also include an optional means for connection to a ferrule 30. Such a means may include, for example, a taper, preferably about two degrees to about ten degrees, more preferably about five degrees, to mate with the ferrule and prevent it from moving through a force fit. The taper may be on the body 34 of the ferrule, as shown in FIGS. 2 and 3, or it may be elsewhere.
  • In the preferred embodiment of FIGS. 2 and 3, the blade unit 10 may receive the ferrule 30 when a person or device inserts the front portion of the ferrule 30 through the base collar 20 until the front portion (such as threaded area 32) is received by the cap 24. The ferrule 30 is then rotated such that the threaded area 32 screws into the cap 24. As the front portion 32 is drawn into and connects with the cap 24, the central portion 34 of the ferrule is drawn into, mates inside of, and tightens in the central aperture 22 of the base collar 20. By screwing the ferrule 30 tightly into the blade unit 10, a secure connection is made. Of course, as mentioned above, other means of connection, such as pins or locking tabs, may be used. Examples of blade units that may connect by tabs and/or grooves are shown in FIGS. 4, 7A and 7B.
  • The frontal point 18 of the blade unit is the first part that will contact a target. Since it is just a point, and since it will receive a tremendous force upon impact, it is preferred that the blade unit be constructed in such a way that it has additional strength. This can be accomplished by tapered grinding, moving over a sharpening stone, or other sharpening of the razor edges 12. With such a procedure, each razor edge 12 may be sharpened at an angle that is greater than the angle that the razor edge 12 is adjacent to the base 14 of the blade 16. Near the frontal point 18, the angle is preferably less sharp, this providing a wider cutting edge near the frontal point 18 than near the base 14.
  • The unitary blade unit is preferably made of any metal. More preferably, the unitary blade unit is made using carbon steel, stainless steel, spring steel, tool steel, or titanium, or a composition including any of the above.
  • In a preferred method of manufacturing the unit using metal injection molding, the steps shown in FIG. 8 may be followed. Referring to FIG. 8, the unitary blade unit may be formed by blending a metal powder and binder (such as plastic or wax). The blending may be done in a single step 80, or in two or more graduated steps 82. The mixture is pelletized and/or powdered 84 (optionally in combination with the blending step), and it is injected 86 into a blade unit mold having one or more cavities that provide a desired blade unit design. The method may use a mold that provides a blade unit having two, three, four, or more blades, although the preferred number is three blades. Preferably, the mixture is compacted in the mold with pressure to yield an intermediate piece. The piece is processed (such as by immersion in a solvent 88, optionally followed by heating 90) to remove at least a portion of the binder. The piece is then sintered 92 at an elevated temperature and/or pressure to reduce the size and increase the density of the blade unit. After sintering, optionally and preferably the blade unit edges may be sharpened 94 using either a conventional or a specially-designed sharpening tool. Other embodiments of molding may also be used to manufacture the blade unit. This preferred method embodiment of the present invention is intended to include the use of metal injection molding to manufacture any unitary blade-unit that is separate from a ferrule, including but not limited to the blade units illustrated in FIGS. 2, 3, and 4 and variants thereof. Preferably, although not a necessary element, when manufacturing a blade unit using metal injection molding, each blade is tapered so that it is thicker at its base than it is at the frontal tip. Examples of such tapered blades are shown in FIG. 9, which illustrates rear views of exemplary blades 50 and 54, each of which has a base 51 and 55 and having a thickness that begins to taper at some point between the base and the tip or outer edge 52 and 56.
  • Alternatively, the blade unit may be made by assembling the blades into a unitary structure. Preferably, with this method the blades will be fastened together using any commonly known welding procedure such as laser welding, electron beam welding, TIG welding, plasma welding, resistance welding, electron beam welding, fusion welding, pressure welding, friction welding, ultrasonic welding, or other welding methods. Preferably, when manufacturing the unit by welding, the weld of each seam is begun at or near the frontal point and proceeds toward the base. Alternatively, fastening methods other than welding may be used. Exemplary laser welding equipment and procedures are illustrated in FIG. 10. Referring to FIG. 10, a laser unit 60 directs a beam of energy toward an intersection of two blades of an exemplary blade unit 66. A closer view of the tip structure of blade unit 66 is provided in FIG. 11, which also shows the points of intersection 67. The beam of energy is preferably directed toward the intersection 67 using a focus cell 61, mirror, or other device that focuses the beam toward the point of intersection. The energy beam fuses the blades at the point of intersection 67. This process is performed for each point of intersection, preferably simultaneously with multiple lasers and focus cells such as is shown in FIG. 10, but optionally with a single laser that welds on a joint-by-joint basis. Preferably, the weld is performed into the tip structure to provide a “cut on contact” blade unit. However, alternate tip structures are possible.
  • The unitary blade unit provides several advantages over the prior art. For example, by providing a separate blade unit and ferrule, a user can replace only one part (i.e., either the blade or the ferrule) without replacing the other, thus reducing replacement costs. In addition, the separation of blade and ferrule allows the manufacturer to provide a weight-adaptable broadhead by manufacturing a standard blade unit and varying ferrules having different weights. In addition, the blade unit and the ferrule may be made of different materials. Thus, the weight of the overall broadhead (i.e., the combination of the blade and ferrule) optionally may be varied by changing the ferrule without replacing the blades, or vice versa. Further, although the blade-unit can be sharpened by grinding, polishing, sanding, or any standard sharpening method, the user may decide to simply dispose of the unitary blade unit and attach a new blade unit to an existing ferrule, resulting in ease of use for the user and the potential for increased sales for the manufacturer.
  • When made by metal injection molding, the blade unit designer receives a tremendous amount of freedom in the shaping and designing of the unit. Exact radii, tapering, and other intricacies can be achieved with minimal cost difference. Metal injection molding also allows metal parts to have a complex geometry with great strength.
  • The many features and advantages of the invention are apparent from the detailed specification. Thus, the invention is intended to include all such features and advantages of the invention which fall within the true spirits and scope of the invention. Further, since numerous modifications and variations will readily occur to those skilled in the art, it is not desired to limit the invention to the exact construction and operation illustrated and described in the specification, claims, and drawings herein. Accordingly, all appropriate modifications and equivalents may be included within the scope of the invention.

Claims (18)

1. A method of manufacturing a unitary blade unit for a modular broadhead, comprising:
providing a mold having one or more cavities that define a multiple-bladed blade unit;
inserting a mixture of metal and binder into the mold;
compacting the mixture in the mold to form an intermediate blade unit;
processing the intermediate blade unit to remove at least a portion of the binder;
sintering the intermediate blade unit to form a sintered blade unit; and
sharpening the blades to form a cutting edge on each blade to yield a final blade unit, wherein the final blade unit requires a separate ferrule in order to attach to an arrow.
2. The method of claim 1 wherein the mixture is in powdered form.
3. The method of claim 1 wherein the sintering step comprises sintering at an elevated temperature and pressure.
4. A method of manufacturing a blade unit for a modular broadhead, comprising using metal injection molding to form a blade unit from a mixture that includes metal and a binder, wherein the blade unit has at least two blades and requires a separate ferrule in order to attach to an arrow.
5. The method of claim 4 further comprising manufacturing a separate adapter for securing the blade unit to the ferrule.
6. The method of claim 4 wherein the method includes forming the blade unit to include a first integral adapter for securing the blade unit to the ferrule.
7. The method of claim 4 wherein the method further includes manufacturing a second separate adapter for further securing the blade unit to the ferrule.
8. A method of manufacturing a blade unit for a modular broadhead, the method comprising:
arranging a plurality of components in the form of a blade unit for a modular broadhead; and
directing an energy beam toward a plurality of contact segments to weld the plurality of components into a blade unit, wherein each contact segment comprises a location where at least two of the plurality of components are in contact.
9. The method of claim 8 wherein the plurality of components comprises a plurality of blades.
10. The method of claim 9 wherein the plurality of components further comprises a cap structure for receiving a separable ferrule.
11. The method of claim 9 wherein the plurality of components further comprises a collar structure for receiving a separable ferrule.
12. The method of claim 9 wherein the plurality of components further comprises a tip structure.
13. The method of claim 8 wherein the energy beam is a laser.
14. The method of claim 8 wherein directing an energy beam comprises performing laser welding.
15. The method of claim 8 wherein directing an energy beam comprises focusing the energy beam toward a contact segment using a device.
16. The method of claim 8 wherein the device comprises one or more of a focus cell, a lens, and a mirror.
17. The method of claim 8 wherein directing an energy beam comprises moving a focal point of the energy beam along a contact segment in a direction from a tip of the blade unit to a base of the blade unit.
18. The method of claim 8 wherein a plurality of energy beams are directed toward a plurality of contact segments simultaneously, wherein each energy beam is directed toward a particular contact segment.
US11/102,939 2001-01-31 2005-04-11 Unitary broadhead blade unit Abandoned US20050181898A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
US11/102,939 US20050181898A1 (en) 2001-01-31 2005-04-11 Unitary broadhead blade unit
US11/234,353 US20060030439A1 (en) 2001-01-31 2005-09-23 Laser welded broadhead
US11/758,710 US20070228022A1 (en) 2001-01-31 2007-06-06 Laser welded broadhead

Applications Claiming Priority (10)

Application Number Priority Date Filing Date Title
US26511401P 2001-01-31 2001-01-31
US27381901P 2001-03-08 2001-03-08
US28603001P 2001-04-24 2001-04-24
US29330701P 2001-05-24 2001-05-24
US09/922,550 US6726581B2 (en) 2001-01-31 2001-08-04 Unitary broadhead blade unit and ferrule for same
US35421402P 2002-02-04 2002-02-04
US10/094,125 US6605012B2 (en) 2001-03-08 2002-03-08 Modular broadhead
US36524902P 2002-03-18 2002-03-18
US10/185,089 US6939258B2 (en) 2001-01-31 2002-06-28 Unitary broadhead blade unit
US11/102,939 US20050181898A1 (en) 2001-01-31 2005-04-11 Unitary broadhead blade unit

Related Parent Applications (2)

Application Number Title Priority Date Filing Date
US09/922,550 Continuation-In-Part US6726581B2 (en) 2001-01-31 2001-08-04 Unitary broadhead blade unit and ferrule for same
US10/185,089 Continuation US6939258B2 (en) 2001-01-31 2002-06-28 Unitary broadhead blade unit

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US11/234,353 Continuation-In-Part US20060030439A1 (en) 2001-01-31 2005-09-23 Laser welded broadhead

Publications (1)

Publication Number Publication Date
US20050181898A1 true US20050181898A1 (en) 2005-08-18

Family

ID=34842141

Family Applications (2)

Application Number Title Priority Date Filing Date
US10/185,089 Expired - Fee Related US6939258B2 (en) 2001-01-31 2002-06-28 Unitary broadhead blade unit
US11/102,939 Abandoned US20050181898A1 (en) 2001-01-31 2005-04-11 Unitary broadhead blade unit

Family Applications Before (1)

Application Number Title Priority Date Filing Date
US10/185,089 Expired - Fee Related US6939258B2 (en) 2001-01-31 2002-06-28 Unitary broadhead blade unit

Country Status (1)

Country Link
US (2) US6939258B2 (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060183578A1 (en) * 2005-02-11 2006-08-17 Michael Sohm A Broadhead Blade Assembly Comprising an Improved Blade Design
US20060276276A1 (en) * 2005-06-07 2006-12-07 Polando Scott A Broadhead Adapter and Arrow
US20070123378A1 (en) * 2005-11-29 2007-05-31 Polando Scott A Adjustable Weight Broadhead Adapter Bolt and Arrow
US20080146388A1 (en) * 2006-12-19 2008-06-19 Easton Technical Products, Inc. Arrow point alignment system
US7905795B1 (en) 2007-01-05 2011-03-15 Acropolis Engineering Unitary broadhead with laser welded ferrule
US8460134B2 (en) 2006-12-19 2013-06-11 Easton Technical Products, Inc. Arrow point alignment system
US11460278B2 (en) * 2020-12-09 2022-10-04 Bear Archery, Inc. Modular weight broadhead
USD1023213S1 (en) * 2021-11-23 2024-04-16 Xiaohong Weng Arrowhead
USD1030936S1 (en) * 2021-11-23 2024-06-11 Xiaohong Weng Arrowhead

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6910979B2 (en) 2000-03-13 2005-06-28 Bruce Barrie Expandable broadhead
USRE40273E1 (en) * 2000-04-10 2008-04-29 G5 Outdoors, L.L.C. Method of manufacturing an archery broadhead with sintered components
US6595881B1 (en) 2000-04-10 2003-07-22 Louis Grace, Jr. Expanding-blade archery broadhead
US20060030439A1 (en) * 2001-01-31 2006-02-09 Philip Muller Laser welded broadhead
US7713151B2 (en) * 2006-01-06 2010-05-11 Brett Fulton Mechanical broadhead with expandable blades
US7771298B2 (en) 2006-08-18 2010-08-10 Field Logic, Inc. Expandable broadhead with rear deploying blades
US8062155B2 (en) * 2007-03-23 2011-11-22 Eastman Outdoors Inc. Arrowhead having both fixed and mechanically expandable blades
US8210971B1 (en) 2008-02-20 2012-07-03 Brett Fulton Pivoting-blade deep-penetration arrowhead
USD730471S1 (en) 2013-12-18 2015-05-26 Out Rage, Llc Broadhead
USD776782S1 (en) 2015-05-22 2017-01-17 Feradyne Outdoors, Llc Broadhead arrowhead having both expandable and fixed cutting blades

Citations (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2930620A (en) * 1957-07-31 1960-03-29 Wendell R Brooks Arrow head
US2940758A (en) * 1958-01-02 1960-06-14 John A Richter Arrowhead
US4036499A (en) * 1975-11-26 1977-07-19 Sherwin Donald D Arrow broadhead
US4175749A (en) * 1975-10-06 1979-11-27 New Archery Products Corp. Arrowhead body
US4210330A (en) * 1978-02-13 1980-07-01 Dynamic Sports concepts, Inc. Modular broadhead arrowhead
US4505482A (en) * 1983-11-07 1985-03-19 Martin Sr Ricky T Archery broadhead
US4536928A (en) * 1983-11-17 1985-08-27 Honeywell Inc. Manufacture of projectiles
US4570941A (en) * 1982-05-06 1986-02-18 Saunders Archery Company Broadhead assembly for arrow
US4643435A (en) * 1985-12-11 1987-02-17 John Musacchia Hunting arrow
US4928969A (en) * 1989-08-07 1990-05-29 Nagatori Wesley S Arrowhead
US4944520A (en) * 1987-09-29 1990-07-31 Afc, Inc. Arrow shaft end adaptor apparatus and balance pin apparatus and method
US5018747A (en) * 1990-03-06 1991-05-28 Brown Jim W Bladed dart projectile
US5137282A (en) * 1991-01-07 1992-08-11 Folsom Sports, Inc. Plastic molded arrowhead and method
US5192081A (en) * 1990-01-09 1993-03-09 Cooper Gary L Multi-blade arrowhead
USD338942S (en) * 1991-04-08 1993-08-31 Giannetti Nickolas J Broadhead connector for carbon-shaft bow arrows
USRE34397E (en) * 1991-04-10 1993-10-05 Delmonte Nicholas J Arrow ringed broadhead
US5494297A (en) * 1994-08-02 1996-02-27 Macneil; Ronald J. Lacrosse stick head
US5494298A (en) * 1991-01-04 1996-02-27 Maleski; Richard Broadhead for an arrow and method of securement
US5496043A (en) * 1992-08-07 1996-03-05 Ester; Lee Over the arrow shaft broad head
US5616261A (en) * 1995-06-07 1997-04-01 Chrysler Corporation Laser welding system
US5636846A (en) * 1992-11-02 1997-06-10 Tinsley; Greg E. Arrowhead
US5896642A (en) * 1996-07-17 1999-04-27 Amorphous Technologies International Die-formed amorphous metallic articles and their fabrication
US5931751A (en) * 1997-05-06 1999-08-03 Cooper; Gary L. Arrowhead
US5950704A (en) * 1996-07-18 1999-09-14 Amorphous Technologies International Replication of surface features from a master model to an amorphous metallic article
US6290902B1 (en) * 1999-05-03 2001-09-18 Sandvik Ab Method for producing Ti (C,N)—(Ti,Ta,W) (C,N)—Co alloys for cutting tool applications
US6403916B1 (en) * 2000-05-12 2002-06-11 Isostar International, Inc. System and automated method for producing welded end closures in thin-walled metal tubes
US6818857B1 (en) * 2000-11-28 2004-11-16 Heung Ki Cho Method and apparatus for welding

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4504063A (en) * 1984-06-22 1985-03-12 Lebus Charles F Hunting broadhead arrow
US5165697A (en) * 1988-08-30 1992-11-24 Lauriski Stanley E Broadhead archery hunting point
US5288344A (en) 1993-04-07 1994-02-22 California Institute Of Technology Berylllium bearing amorphous metallic alloys formed by low cooling rates
US5368659A (en) 1993-04-07 1994-11-29 California Institute Of Technology Method of forming berryllium bearing metallic glass
US5482580A (en) 1994-06-13 1996-01-09 Amorphous Alloys Corp. Joining of metals using a bulk amorphous intermediate layer
US5567532A (en) 1994-08-01 1996-10-22 Amorphous Alloys Corp. Amorphous metal/diamond composite material
US5567251A (en) 1994-08-01 1996-10-22 Amorphous Alloys Corp. Amorphous metal/reinforcement composite material
US5618359A (en) 1995-02-08 1997-04-08 California Institute Of Technology Metallic glass alloys of Zr, Ti, Cu and Ni
US5711363A (en) 1996-02-16 1998-01-27 Amorphous Technologies International Die casting of bulk-solidifying amorphous alloys
US5772803A (en) 1996-08-26 1998-06-30 Amorphous Technologies International Torsionally reacting spring made of a bulk-solidifying amorphous metallic alloy
US5797443A (en) 1996-09-30 1998-08-25 Amorphous Technologies International Method of casting articles of a bulk-solidifying amorphous alloy
US6290903B1 (en) 2000-04-10 2001-09-18 Louis Grace, Jr. Broadhead and method of manufacture

Patent Citations (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2930620A (en) * 1957-07-31 1960-03-29 Wendell R Brooks Arrow head
US2940758A (en) * 1958-01-02 1960-06-14 John A Richter Arrowhead
US4175749A (en) * 1975-10-06 1979-11-27 New Archery Products Corp. Arrowhead body
US4036499A (en) * 1975-11-26 1977-07-19 Sherwin Donald D Arrow broadhead
US4210330A (en) * 1978-02-13 1980-07-01 Dynamic Sports concepts, Inc. Modular broadhead arrowhead
US4570941A (en) * 1982-05-06 1986-02-18 Saunders Archery Company Broadhead assembly for arrow
US4505482A (en) * 1983-11-07 1985-03-19 Martin Sr Ricky T Archery broadhead
US4536928A (en) * 1983-11-17 1985-08-27 Honeywell Inc. Manufacture of projectiles
US4643435A (en) * 1985-12-11 1987-02-17 John Musacchia Hunting arrow
US4944520A (en) * 1987-09-29 1990-07-31 Afc, Inc. Arrow shaft end adaptor apparatus and balance pin apparatus and method
US4928969A (en) * 1989-08-07 1990-05-29 Nagatori Wesley S Arrowhead
US5192081A (en) * 1990-01-09 1993-03-09 Cooper Gary L Multi-blade arrowhead
US5018747A (en) * 1990-03-06 1991-05-28 Brown Jim W Bladed dart projectile
US5494298A (en) * 1991-01-04 1996-02-27 Maleski; Richard Broadhead for an arrow and method of securement
US5137282A (en) * 1991-01-07 1992-08-11 Folsom Sports, Inc. Plastic molded arrowhead and method
USD338942S (en) * 1991-04-08 1993-08-31 Giannetti Nickolas J Broadhead connector for carbon-shaft bow arrows
USRE34397E (en) * 1991-04-10 1993-10-05 Delmonte Nicholas J Arrow ringed broadhead
US5496043A (en) * 1992-08-07 1996-03-05 Ester; Lee Over the arrow shaft broad head
US5636846A (en) * 1992-11-02 1997-06-10 Tinsley; Greg E. Arrowhead
US6045468A (en) * 1992-11-02 2000-04-04 Tinsley; Greg E. Arrowhead
US5494297A (en) * 1994-08-02 1996-02-27 Macneil; Ronald J. Lacrosse stick head
US5616261A (en) * 1995-06-07 1997-04-01 Chrysler Corporation Laser welding system
US5896642A (en) * 1996-07-17 1999-04-27 Amorphous Technologies International Die-formed amorphous metallic articles and their fabrication
US5950704A (en) * 1996-07-18 1999-09-14 Amorphous Technologies International Replication of surface features from a master model to an amorphous metallic article
US5931751A (en) * 1997-05-06 1999-08-03 Cooper; Gary L. Arrowhead
US6290902B1 (en) * 1999-05-03 2001-09-18 Sandvik Ab Method for producing Ti (C,N)—(Ti,Ta,W) (C,N)—Co alloys for cutting tool applications
US6403916B1 (en) * 2000-05-12 2002-06-11 Isostar International, Inc. System and automated method for producing welded end closures in thin-walled metal tubes
US6818857B1 (en) * 2000-11-28 2004-11-16 Heung Ki Cho Method and apparatus for welding

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7160217B2 (en) 2005-02-11 2007-01-09 Michael Sohm Broadhead blade assembly comprising an improved blade design
US20070111831A1 (en) * 2005-02-11 2007-05-17 Magnus, Inc. A Broadhead Blade Assembly Comprising an Improved Blade Design
US20060183578A1 (en) * 2005-02-11 2006-08-17 Michael Sohm A Broadhead Blade Assembly Comprising an Improved Blade Design
US7597637B2 (en) * 2005-02-11 2009-10-06 Magnus, Inc. Broadhead blade assembly comprising an improved blade design
US7374505B2 (en) 2005-06-07 2008-05-20 Polando Scott A Broadhead adapter and arrow
US20060276276A1 (en) * 2005-06-07 2006-12-07 Polando Scott A Broadhead Adapter and Arrow
US20070123378A1 (en) * 2005-11-29 2007-05-31 Polando Scott A Adjustable Weight Broadhead Adapter Bolt and Arrow
US7318783B2 (en) 2005-11-29 2008-01-15 Polando Scott A Adjustable weight broadhead adapter bolt and arrow
US20080146388A1 (en) * 2006-12-19 2008-06-19 Easton Technical Products, Inc. Arrow point alignment system
US7811186B2 (en) 2006-12-19 2010-10-12 Easton Technical Products, Inc. Arrow point alignment system
US8262518B2 (en) 2006-12-19 2012-09-11 Easton Technical Products, Inc. Arrow point alignment system
US8460134B2 (en) 2006-12-19 2013-06-11 Easton Technical Products, Inc. Arrow point alignment system
US7905795B1 (en) 2007-01-05 2011-03-15 Acropolis Engineering Unitary broadhead with laser welded ferrule
US11460278B2 (en) * 2020-12-09 2022-10-04 Bear Archery, Inc. Modular weight broadhead
USD1023213S1 (en) * 2021-11-23 2024-04-16 Xiaohong Weng Arrowhead
USD1030936S1 (en) * 2021-11-23 2024-06-11 Xiaohong Weng Arrowhead

Also Published As

Publication number Publication date
US20030022741A1 (en) 2003-01-30
US6939258B2 (en) 2005-09-06

Similar Documents

Publication Publication Date Title
US20050181898A1 (en) Unitary broadhead blade unit
US20060030439A1 (en) Laser welded broadhead
EP2167263B1 (en) A tool for chip removing machining as well as a basic body therefor
US5112165A (en) Tool for cutting solid material
US6739327B2 (en) Cutting tool with hardened tip having a tapered base
KR101570139B1 (en) Rotor Shaft of a Turbomachine and Method for the Production of a Rotor of a Turbomachine
CN100427251C (en) A cutting tool, a part thereof, as well as a method for the manufacture of such a cutting tool
KR102349807B1 (en) Interchangeable face-milling head with integrally formed threaded shank-connector
US6290903B1 (en) Broadhead and method of manufacture
US6726581B2 (en) Unitary broadhead blade unit and ferrule for same
US5048375A (en) Method for constructing a rotating cutting tool
EP0934788B1 (en) Endmill and cutting method
US6605012B2 (en) Modular broadhead
CN102438782B (en) Rotary cutting tool
KR100373816B1 (en) Supporting pads for drill
CN102458735A (en) A tool for chip removing machining as well as a solid indexable cutting insert and a solid basic body therefor
JP7444793B2 (en) How to manufacture modular cutting tool bodies
EP1590120B1 (en) Milling cutter with convexly curved cutting edge
EP0183902A2 (en) Method of attaching segments to cutting tool
CN110392622B (en) Blank for shaft milling cutter
CN101890521A (en) Drill bit
EP2749366A1 (en) Holder and cutting tool
KR20200125700A (en) Rotary cutting head with rigid mounting protrusion and rotary cutting tool
US20210145460A1 (en) Monobloc acetabular reamer
JP2002257149A (en) Coupling method and cam shaft

Legal Events

Date Code Title Description
STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION