Cut-on-Contact Broadhead

Abstract

A cut-on-contact broadhead having a ferrule and a plurality of deployable blades pivotally coupled to the ferrule. The ferrule includes a plurality of recesses, and at least one protrusion extending away from a surface of one or more of the plurality of recesses. Each of the plurality of blades includes a tip, an impact region, a first cutting edge, and a second cutting edge. During flight, the blades are in a fully retracted configuration forming a chisel tip having cutting edges defined at least in part by the first cutting edge of each blade. Upon impact, the plurality of blades are deployed into a swept-back configuration whereby the second cutting edges expand the bore initiated by the chisel tip.

Description

STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT

Not applicable.

TECHNICAL FIELD

The instant disclosure relates to archery. More particularly, the instant disclosure pertains to broadheads.

BACKGROUND

A wide range of arrowhead designs suitable for archery are commercially available. One category of arrowheads is the broadhead—a bladed arrowhead featuring multiple sharp cutting blades that are designed to greatly increase the effective cutting area of the arrowhead when it impacts a target. Broadheads are popular in the bowhunting industry, as the increased cutting radius of a broadhead results in larger entrance and exit wounds in a game animal struck by the broadhead, causing increased blood loss which kills the animal quickly and humanely, and provides a better blood trail for tracking and retrieval of the carcass.

While broadheads provide an improved cutting capability when compared to non-bladed field point or nib point arrowheads, some broadhead designs suffer from inferior aerodynamic properties in comparison with their non-bladed counterparts. The blades of the broadhead, if deployed during the flight of an arrow, can result in undesirable effects and cause the arrow to veer off course from the flight path.

Prior art broadhead designs have attempted to resolve the aerodynamic issues by retaining, at least in part, the deployable cutting blades of the broadhead within the ferrule body of the broadhead during flight. Upon impacting the target, the blades are deployed, moving outwardly from the ferrule body and exposing the sharp cutting edges of the blades once fully deployed. Such designs are known by those skilled in the art as an “expandable broadhead.”

SUMMARY

A non-limiting exemplary embodiment of a broadhead includes a ferrule having a distal end, a plurality of recesses extending proximally from proximate the distal end, and at least one protrusion extending away from a surface of at least one of the plurality of recesses, wherein an outer edge of the at least one protrusion is configured as a cutting edge.

Another non-limiting exemplary embodiment of a broadhead includes a ferrule and a plurality of deployable blades. The ferrule includes a distal end, a plurality of recesses extending proximally from proximate the distal end, at least one protrusion extending away from a surface of at least one of the plurality of recesses, and a plurality of channels extending proximally from proximate the distal end, wherein each channel is disposed between adjacent recesses. At least a portion of each blade is disposed within and is pivotally coupled to one of the plurality of channels. Each blade includes a tip, an impact region, a first cutting edge extending from the tip to proximate the impact region, and a second cutting edge extending from the tip to proximate the channel to which the blade is pivotally coupled.

Yet another non-limiting exemplary embodiment of a broadhead includes a ferrule and a plurality of deployable blades. The ferrule includes a distal end, a plurality of recesses extending proximally from proximate the distal end, at least one protrusion extending away from a surface of one or more of the plurality of recesses, and a plurality of channels extending proximally from proximate the distal end, wherein each channel is disposed between adjacent recesses. At least a portion of each blade of the plurality of blades is disposed within and is pivotally coupled to one of the plurality of channels. Each blade includes a tip, an impact region, a first cutting edge extending from the tip to proximate the impact region, and a second cutting edge extending from the tip to proximate the channel to which the blade is pivotally coupled. During flight, the tips of each blade converge to form a chisel tip having cutting edges defined at least in part by the first cutting edge of each blade.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a perspective view of a non-limiting exemplary embodiment of a broadhead illustrated with a plurality of blades in a fully deployed configuration;

FIG. 2 is another perspective view of the broadhead of FIG. 1;

FIG. 3 is another perspective view of the broadhead of FIG. 1;

FIG. 4 is another perspective view of the broadhead of FIG. 1;

FIG. 5 is an elevation view of the broadhead of FIG. 1 as viewed from a proximal (rear) location;

FIG. 6 is an elevation view of the broadhead of FIG. 1 as viewed from a distal (front) location;

FIG. 7 is a plan view of the broadhead of FIG. 1;

FIG. 8 is another plan view of the broadhead of FIG. 1;

FIG. 9 is another plan view of the broadhead of FIG. 1;

FIG. 10 is another plan view of the broadhead of FIG. 1;

FIG. 11 is a perspective view of the broadhead of FIG. 1 illustrated with the plurality of blades in a fully retracted state;

FIG. 12 is another perspective view of the broadhead of FIG. 11;

FIG. 13 is another perspective view of the broadhead of FIG. 11;

FIG. 14 is another perspective view of the broadhead of FIG. 11;

FIG. 15 is an elevation view of the broadhead of FIG. 11 as viewed from the proximal (rear) location;

FIG. 16 is an elevation view of the broadhead of FIG. 11 as viewed from the distal (front) location;

FIG. 17 is a plan view of the broadhead of FIG. 11;

FIG. 18 is another plan view of the broadhead of FIG. 11;

FIG. 19 is another plan view of the broadhead of FIG. 11;

FIG. 20 is another plan view of the broadhead of FIG. 11;

FIG. 21 is a plan view of the broadhead of FIG. 11 illustrated having a non-limiting exemplary embodiment of a collar for retaining the blades in the fully retracted configuration;

FIG. 22 is a perspective view of a non-limiting exemplary embodiment of a ferrule for the broadhead of FIG. 1;

FIG. 23 is another perspective view of the ferrule of FIG. 22;

FIG. 24 is another perspective view of the ferrule of FIG. 22;

FIG. 25 is another perspective view of the ferrule of FIG. 22;

FIG. 26 is an elevation view of the ferrule of FIG. 22 as viewed from the proximal (rear) location;

FIG. 27 is an elevation view of the ferrule of FIG. 22 as viewed from the distal (front) location;

FIG. 28 is a plan view of the ferrule of FIG. 22;

FIG. 29 is another plan view of the ferrule of FIG. 22;

FIG. 30 is a perspective view of another non-limiting exemplary embodiment of a broadhead illustrated with a plurality of blades in a fully deployed configuration;

FIG. 31 is another perspective view of the broadhead of FIG. 30;

FIG. 32 is another perspective view of the broadhead of FIG. 30;

FIG. 33 is another perspective view of the broadhead of FIG. 30;

FIG. 34 is an elevation view of the broadhead of FIG. 30 as viewed from a proximal (rear) location;

FIG. 35 is an elevation view of the broadhead of FIG. 30 as viewed from a distal (front) location;

FIG. 36 is a plan view of the broadhead of FIG. 30;

FIG. 37 is another plan view of the broadhead of FIG. 30;

FIG. 38 is another plan view of the broadhead of FIG. 30;

FIG. 39 is another plan view of the broadhead of FIG. 30;

FIG. 40 is a perspective view of the broadhead of FIG. 30 illustrated with the plurality of blades in a fully retracted state;

FIG. 41 is another perspective view of the broadhead of FIG. 40;

FIG. 42 is another perspective view of the broadhead of FIG. 40;

FIG. 43 is another perspective view of the broadhead of FIG. 40;

FIG. 44 is an elevation view of the broadhead of FIG. 40 as viewed from the proximal (rear) location;

FIG. 45 is an elevation view of the broadhead of FIG. 40 as viewed from the distal (front) location;

FIG. 46 is a plan view of the broadhead of FIG. 40;

FIG. 47 is another plan view of the broadhead of FIG. 40;

FIG. 48 is another plan view of the broadhead of FIG. 40;

FIG. 49 is another plan view of the broadhead of FIG. 40;

FIG. 50 is a plan view of the broadhead of FIG. 40 illustrated having a non-limiting exemplary embodiment of a collar for retaining the blades in the fully retracted configuration;

FIG. 51 is a perspective view of a non-limiting exemplary embodiment of a ferrule for the broadhead of FIG. 30;

FIG. 52 is another perspective view of the ferrule of FIG. 51;

FIG. 53 is another perspective view of the ferrule of FIG. 51;

FIG. 54 is another perspective view of the ferrule of FIG. 51;

FIG. 55 is an elevation view of the ferrule of FIG. 51 as viewed from the proximal (rear) location;

FIG. 56 is an elevation view of the ferrule of FIG. 51 as viewed from the distal (front) location;

FIG. 57 is a plan view of the ferrule of FIG. 51;

FIG. 58 is another plan view of the ferrule of FIG. 51;

FIG. 59 is a perspective view of a non-limiting exemplary embodiment of a blade for the broadhead of FIGS. 1 and 30; and

FIG. 60 is a plan view of the blade of FIG. 59.

DETAILED DESCRIPTION

One or more non-limiting embodiments are described herein with reference to the accompanying drawings, wherein like numerals designate like elements. It should be clearly understood that there is no intent, implied or otherwise, to limit the disclosure in any way, shape or form to the embodiments illustrated and described herein. While multiple exemplary embodiments are provided, variations thereof will become apparent or obvious to a person of ordinary skills. Accordingly, any and all variants for providing functionalities similar to those described herein are considered as being within the metes and bounds of the instant disclosure.

FIGS. 1-10 are various views of a non-limiting exemplary embodiment of a broadhead 10 of the instant disclosure illustrated with a plurality of blades 12 in a fully deployed configuration. FIGS. 1-4 are perspective views of the broadhead 10 as viewed from different vantage points. FIGS. 1 and 2 are front perspective views of the broadhead 10 as viewed from above and below; and FIGS. 3 and 4 are rear perspective views of the broadhead 10 as viewed from above and below. FIGS. 5 and 6, respectively, are elevational views of the broadhead 10 as viewed from the rear, i.e., in the distal direction, and the front, i.e., in the proximal direction. FIGS. 7-10 are plan views of the broadhead 10 in different orientations about a longitudinal axis thereof. FIGS. 7-9 illustrate the broadhead 10 in different orientations about the longitudinal axis such that only two of the plurality of blades 12 are viewable or visible with the other blade being “underneath” (or “hidden under”) the broadhead 10; and FIG. 10 illustrates the broadhead 10 oriented about the longitudinal axis such that all of the plurality of blades 12 are visible or viewable when looking down along a plane of the blade 12 extending out of the paper.

FIGS. 11-20 are various views of the broadhead 10 illustrated with the plurality of blades 12 in a fully retracted configuration such as for example during flight. FIGS. 11-14 are perspective views of the broadhead 10 as viewed from different vantage points. FIGS. 15 and 16, respectively, are the elevational views of the broadhead 10 as viewed from the rear, i.e., in the distal direction, and the front, i.e., in the proximal direction. FIGS. 17-20 are plan views of the broadhead 10 in different orientations about the longitudinal axis thereof.

FIG. 21 illustrates the broadhead 10 of FIGS. 11-20 having a non-limiting exemplary embodiment of a collar 14 encircling at least a portion of each of the plurality of blades 12. In some embodiments, as will be described in detail infra, the collar 14 is configured for retaining the plurality of blades 12 in the retracted configuration such as for example during flight.

FIGS. 22-29 illustrate various views of a non-limiting exemplary embodiment of a ferrule 16 for the broadhead 10. FIGS. 22-25 are perspective views of the ferrule 16 as viewed from different vantage points. FIGS. 26 and 27, respectively, are the elevational views of the ferrule 16 as viewed from the rear and the front. FIGS. 28 and 29 are plan views of the ferrule 16 in different orientations about a longitudinal axis thereof

In a non-limiting exemplary embodiment, the broadhead 10 includes the plurality of blades 12 and the ferrule 16. The ferrule 16 includes a distal end 18 and a proximal end 20. In a non-limiting exemplary embodiment, the ferrule 16 includes a plurality of recesses 22 extending proximally from proximate the distal end 18. In some embodiments, the plurality of recesses 22 extend along a portion of the longitudinal extent of the ferrule 16. In certain embodiments, the plurality of recesses 22 extend along an entire longitudinal extent of the ferrule 16. In some embodiments, some of the plurality of recesses 22 extend along a portion of the longitudinal extent of the ferrule 16 in combination with some of the plurality of recesses 22 extending along the entire longitudinal extent of the ferrule 16. In certain embodiments, one or more of the plurality of recesses 22 includes a channel 24.

In a non-limiting exemplary embodiment, the ferrule 16 includes a plurality of channels 26 extending proximally from proximate the distal end 18. In some embodiments, the plurality of channels 26 extend along a portion of the longitudinal extent of the ferrule 16. In certain embodiments, the plurality of channels 26 extend along an entire longitudinal extent of the ferrule 16. In some embodiments, some of the plurality of channels 26 extend along a portion of the longitudinal extent of the ferrule 16 in combination with some of the plurality of channels 26 extending along the entire longitudinal extent of the ferrule 16. In certain embodiments, each channel of the plurality of channels 26 is disposed between adjacent recesses of the plurality of recesses 22.

In a non-limiting exemplary embodiment, one or more of the plurality of recesses 22 is configured for relieving fluid pressure generated at the distal end 18 of the ferrule 16 as the broadhead 10 penetrates a target. In a non-limiting exemplary embodiment, the channel 24 in one or more of the plurality of recesses 22 is configured for relieving fluid pressure generated at the distal end 18 of the ferrule 16 as the broadhead 10 penetrates a target. In a non-limiting exemplary embodiment, one or more of the plurality of channels 26 is configured for relieving fluid pressure generated at the distal end 18 of the ferrule 16 as the broadhead 10 penetrates a target. In certain embodiments, one or more of the plurality of recesses 22 and one or more of the plurality of channels 26 are configured for relieving fluid pressure generated at the distal end 18 of the ferrule 16 as the broadhead 10 penetrates a target.

While the broadhead 10 of the instant disclosure is illustrated having three cutting blades 12 in a balanced or even distribution, e.g., 120 degrees apart from one another, around the ferrule 16, this should not be construed a requirement or a limitation. In some non-limiting exemplary embodiments, the broadhead 10 includes two cutting blades 12 disposed 180 degrees apart from each other on the ferrule 16. In certain non-limiting exemplary embodiments, the broadhead 10 includes more than three cutting blades 12 in a balanced distribution around the ferrule 16. For instance, an exemplary broadhead includes four cutting blades 12 disposed 90 degrees apart from one another around the ferrule 16. Accordingly, broadheads with two or more cutting blades 12 are considered as being within the metes and bounds of the instant disclosure.

In a non-limiting exemplary embodiment, each blade 12 of the plurality of blades includes a tip 28, an impact region 30 having an impact shoulder 54, a first sharp cutting edge 32, a second sharp cutting edge 34, and an opening 36. In some embodiments, the first cutting edge 32 extends between the tip 28 and the impact region 30. In certain embodiments, the first cutting edge 32 extends between the tip 28 and the impact shoulder 54. However, this extent or size or length of the first cutting edge 32 should not be construed as a limitation or a requirement. In some embodiments, the first cutting edge 32 extends along a portion of the distance between the tip 28 and the impact shoulder 54. In certain embodiments, the second cutting edge 34 extends from the tip 28 to proximate the opening 36. However, this extent or size or length of the second cutting edge 34 should not be construed as a limitation or a requirement. In some embodiments, the second cutting edge 34 extends along a portion of the distance between the tip 28 and the opening 36.

In a non-limiting exemplary embodiment, each channel of the plurality of channels 26 is configured for receiving or housing or accommodating and pivotally coupling at least a portion of one of the plurality of blades 12. In some embodiments, each channel of the plurality of channels 26 includes openings 38 in opposing walls or sides 40. In certain embodiments, the section 42 of each blade 12 having the opening 36 is placed within one of the plurality of channels 26 between opposing walls 40. The openings 36 and 38 are aligned, and the blade 12 is pivotally coupled to the channel 26 with a fastener or a dowel extending through the openings 36 and 38. The fastener or dowel can be a pivot pin or any other mechanism known in the art for pivotally coupling the blade 12 and the channel 26 such that the blade 12 is not hindered from rotation. In some embodiments, the second cutting edge 34 of the blade 12 extends from the tip 28 to a location proximate the channel 26 to which the blade 12 is coupled.

In a non-limiting exemplary embodiment, the collar 14 is configured for retaining the plurality of blades 12 in the fully retracted position or state or configuration. Accordingly, in some embodiments, each channel of the plurality of channels 26 is configured for receiving or accommodating or housing at least a portion of the second cutting edge 34 while the blade 12 is in the fully retracted, i.e., un-deployed, state. In certain embodiments, for minimizing dulling of the sharp cutting edge 34, each blade 12 and/or each channel 26 are/is configured or designed to ensure minimal contact between the second cutting edge 34 and the bottom of the corresponding channel 26. In some embodiments, the tips 28 of each of the plurality of blades 12 converge or almost converge to form a distal tip or end 44 of the broadhead 10. In certain embodiments, the distal tip 44 of the broadhead 10 is a chisel tip having cutting edges defined at least in part by the first cutting edge 32 of each blade 12. In some embodiments, the plurality of blades 12 are configured such that the distal (or chisel) tip 44 of the broadhead 10 is formed distally or in front of or beyond the distal end 18 of the ferrule 16. In certain embodiments, the plurality of blades 12 are configured such that the distal (or chisel) tip 44 of the broadhead 10 is formed at or is proximate to the distal end 18 of the ferrule 16. In some embodiments, the plurality of blades 12 are configured such that the distal (or chisel) tip 44 of the broadhead 10 is formed at a location proximal of the distal end 18 of the ferrule 16. Other configurations for forming the distal tip 44 as a chisel tip with sharp cutting edges that may become apparent to one skilled in the art are considered as being within the metes and bounds of the instant disclosure.

It will be apparent to one skilled in the art that the collar 14 functions or operates to at least form the distal chisel tip 44 with cutting edges defined at least in part by the first cutting edge 32 of each of the plurality of blades 12. The collar 14 functions as such during flight, i.e., before the broadhead 10 impacts a target, and perhaps also momentarily after the broadhead 10 impacts the target. As is well known to those skilled in the art, the arrow or bolt, and the broadhead or tip at the distal end thereof, rotates or spins about its longitudinal axis at a relatively high angular velocity after being discharged from a bow and while in flight towards the target. In a non-limiting exemplary embodiment, when the distal chisel tip 44 touches the target, the spinning or rotating cutting edges of the distal chisel tip 44, i.e., the first cutting edges 32 of the blades 12, create a bore and the distal chisel tip 44 of the broadhead 10 bores into the target. As the broadhead 10, with the fully retracted blades 12 spinning, penetrates the target, a force is exerted by the target onto the impact region 30, and in particular on the impact shoulder 54, in the proximal direction. The force causes the blades 12 to rotate outward away from the ferrule 16. In some embodiments, the outward rotation of the blades 12 causes the collar 14 to disintegrate (i.e., shatter or break). As the blades 12 continue to rotate outwards, the second cutting edge 34 of each blade 12 is exposed out of the corresponding channel 26 in the direction away from the ferrule 16. The first cutting edges 32 continue to widen and lengthen the bore as the broadhead 10 continues to penetrate the target and the blades 12, and more particularly the second cutting edges 34, continue rotating outwards away from the ferrule 16. In a non-limiting exemplary embodiment, the blades 12 are configured such that when the second cutting edges 34 are sufficiently exposed, the target starts exerting the force onto the exposed second cutting edges 34 in the proximal direction until the blades 12 are fully extended or deployed into a swept-back configuration exposing the entirety of the second cutting edges 34. The second cutting edges 34 of the blades 12 act to cut into the target and widen and lengthen the bore as the broadhead 10 continues to bore or penetrate into the target.

In a non-limiting exemplary embodiment, the collar 14 is an O-ring or an elastic band. In some embodiments, the outward rotation of the blades 12 upon impact causes the collar 14 to “slide” in the proximal direction along the contours of the blades 12 until it “slips off” the blades 12 without disintegrating. Thereafter, the broadhead 10 and blades 12 operate or function as described supra. Other forms and/or configurations of collars for retaining the blades 12 in the retracted state during flight as are well-known in the art are considered as being within the metes and bounds of the instant disclosure.

In a non-limiting exemplary embodiment, the distal end 18 of the ferrule 16 is configured as a chisel tip or a multi-faceted tip or a trocar tip having a plurality of facets and sharp cutting edges disposed between adjacent facets such as those disclosed at least in applicant's co-owned U.S. Pat. Nos. 9,410,778, 9,404,722, 8,986,141, 7,771,298, 7,182,706, 7,011,589, 6,942,588, 6,669,586, 6,626,776, 6,554,727, 6,517,454, among others, and in International Publication No. WO 2018/075356, among others, all of which are herein incorporated by reference in their entirety. As disclosed in one or more of these patents and/or publications, the distal end 18, in some embodiments, is formed as an integral part of the ferrule 16. Also as disclosed in one or more of these patents and/or publications, the distal end 18, in some embodiments, is a discrete component attached to the ferrule 16.

In a non-limiting exemplary embodiment, one or more of the plurality of recesses 22 includes at least one protrusion 46 extending outwardly or away from a surface 48 of each of the plurality of recesses 22. In some embodiments, the protrusion 46 extends radially from the surface 48. In certain embodiments, the protrusion 46 extends substantially orthogonally relative to the longitudinal axis of the ferrule 16. In some embodiments, the protrusion 46 has a small curvature or is slightly curved as it extends away from the surface 48.

In a non-limiting exemplary embodiment, the channel 24 in the plurality of recesses 22 extends through the base or bottom of one or more of the protrusion 46. In a non-limiting exemplary embodiment, one or more of the protrusion 46 includes a channel (not shown) extending therethrough either in addition to the channel 24 or as an alternative to the channel 24. In some embodiments, the channel 24 and/or the channel extending through the protrusion 46 is configured for relieving fluid pressure generated at the distal end 18 of the ferrule 16 as the broadhead 10 penetrates a target.

In a non-limiting exemplary embodiment, at least a portion of an outermost edge 52 of the protrusion 46 is configured as a cutting edge. While the figures illustrate an embodiment wherein at least a portion of the outermost edge 52 of the protrusion 46 extends substantially parallel to the longitudinal axis of the ferrule 16, this should not be construed as limiting or a requirement. In a non-limiting exemplary embodiment, the outermost edge 52 of the protrusion 46 extends away from and/or extends towards the longitudinal axis of the ferrule 16.

In a non-limiting exemplary embodiment, the proximal end 20 of the ferrule 16 is configured for attaching the broadhead 10 to a shaft of an arrow or a bolt. While the figures of the instant disclosure might imply that the proximal end 20 is threaded, this should not be construed as limiting. In some embodiments, the proximal end 20 is an un-threaded shaft or cylinder. Other forms and/or configurations for attaching or coupling a broadhead to the shaft of an arrow or bolt, as are well known in the art, are considered as being within the metes and bounds of the instant disclosure.

It will be readily apparent that as the blades 12 rotate from the fully retracted in-flight configuration to the fully extended (or deployed) swept-back configuration, the blades 12 traverse a plane substantially orthogonal to the longitudinal axis of the broadhead 12 (or the ferrule 16). Consequently, the tip 28 of each blade 12 traverses an arc having a center at the location whereat the blade 12 is coupled to the corresponding channel 26.

FIGS. 30-58 illustrate a non-limiting exemplary embodiment of another broadhead 100 of the instant disclosure, wherein elements same as those of the broadhead 10 are identified by like numerals.

FIGS. 30-39 are various views of the broadhead 100 illustrated with the plurality of blades 12 in a fully deployed configuration. FIGS. 30-33 are perspective views of the broadhead 100 as viewed from different vantage points. FIGS. 30 and 31 are front perspective views of the broadhead 100 as viewed from above and below; and FIGS. 32 and 33 are rear perspective views of the broadhead 100 as viewed from above and below. FIGS. 34 and 35, respectively, are elevational views of the broadhead 100 as viewed from the rear, i.e., in the distal direction, and the front, i.e., in the proximal direction. FIGS. 36-39 are plan views of the broadhead 100 in different orientations about a longitudinal axis thereof. FIGS. 36-38 illustrate the broadhead 100 in different orientations about the longitudinal axis such that only two of the plurality of blades 12 are viewable or visible with the other blade being “underneath” (or “hidden under”) the broadhead 100; and FIG. 39 illustrates the broadhead 100 oriented about the longitudinal axis such that all of the plurality of blades 12 are visible or viewable when looking down along a plane of the blade 12 extending out of the paper.

FIGS. 40-49 are various views of the broadhead 100 illustrated with the plurality of blades 12 in a fully retracted configuration such as for example during flight. FIGS. 40-43 are perspective views of the broadhead 100 as viewed from different vantage points. FIGS. 44 and 45, respectively, are the elevational views of the broadhead 100 as viewed from the rear, i.e., in the distal direction, and the front, i.e., in the proximal direction. FIGS. 46-49 are plan views of the broadhead 100 in different orientations about the longitudinal axis thereof.

FIG. 50 illustrates the broadhead 100 of FIGS. 40-49 having the collar 14 encircling at least a portion of each of the plurality of blades 12. In some embodiments, as described in detail supra, the collar 14 is configured for retaining the plurality of blades 12 in the retracted configuration such as for example during flight.

In contrast to the ferrule 16 of the broadhead 10, a non-limiting exemplary embodiment of the broadhead 100 includes a ferrule 116. FIGS. 51-58 illustrate various views of a non-limiting exemplary embodiment of the ferrule 116. FIGS. 51-54 are perspective views of the ferrule 116 as viewed from different vantage points. FIGS. 55 and 56, respectively, are the elevational views of the ferrule 116 as viewed from the rear, i.e., in the distal direction, and the front, i.e., in the proximal direction. FIGS. 57 and 58 are plan views of the ferrule 116 in different orientations about a longitudinal axis thereof.

As with ferrule 16, a non-limiting exemplary embodiment of the ferrule 116 also includes distal and proximal ends 18 and 20, plurality of recesses 22, and plurality of channels 26. While both ferrules 16 and 116 include at least one protrusion 46 and 146, respectively, extending outwardly or away from the surface 48 of each of the plurality of recesses 22, one difference between the ferrules 16 and 116 is in the location of the distal point or end 50 and 150, respectively, of the protrusions 46 and 146. As perhaps best seen in FIGS. 22, 23, 28 and 29, the distal point or end 50 of the protrusion 46 is proximate to or coincident with the distal end 18 of the ferrule 16. In contrast, as perhaps best seen in FIGS. 51, 52, 57 and 58, the distal point or end 150 of the protrusion 146 is at a location proximal of the distal end 18 of the ferrule 116. In other words, the protrusion 46 starts at or from a location proximate to or coincident with the distal end 18 of the ferrule 16, whereas the protrusion 146 starts at or from a location that is not proximate to or coincident with the distal end 18 of the ferrule 116. In all other aspects, the protrusions 46 and 146 are substantially similar to each other. For instance, in some non-limiting exemplary embodiments, the channel 24 in the plurality of recesses 22 extends through the base or bottom of the protrusion 46 and/or the protrusion 146. In other non-limiting exemplary embodiments, the protrusion 46 and/or the protrusion 146 includes a channel (not shown) extending therethrough either in addition to the channel 24 or as an alternative to the channel 24. In some embodiments, the channel 24 and/or the channel extending through the protrusions is configured for relieving fluid pressure generated at the distal ends 18. In some non-limiting exemplary embodiments, at least a portion of respective outer edges 52 of the protrusions 46 and 146 are configured as cutting edges. While the figures illustrate an embodiment wherein at least a portion of the outermost edge 52 of the protrusions 46 and 146 extends substantially parallel to the longitudinal axis of respective ferrules 16 and 116, this should not be construed as limiting or a requirement. In some non-limiting exemplary embodiments, the outermost edge 52 of the protrusion 46 and/or the protrusion 146 extends away from and/or extends towards the longitudinal axis of respective ferrules 16 and 116.

FIGS. 59 and 60, respectively, are a perspective view and a plan view of a non-limiting exemplary embodiment of one of the plurality of blades 12 for the broadhead 10.

In view thereof, modified and/or alternate configurations of the embodiments described herein may become apparent or obvious to one of ordinary skill. All such variations are considered as being within the metes and bounds of the instant disclosure. For instance, while reference may have been made to particular feature(s) and/or function(s), the disclosure is considered to also encompass any and all equivalents providing functionalities similar to those disclosed herein with reference to the accompanying drawings. Accordingly, the spirit, scope and intent of the instant disclosure is to embrace all such variations. Consequently, the metes and bounds of the instant disclosure are defined by the appended claims and any and all equivalents thereof.

Claims

1. A broadhead, comprising a ferrule comprising: a distal end;a plurality of recesses extending proximally from proximate the distal end; andat least one protrusion extending away from a surface of at least one of the plurality of recesses;wherein, an outer edge of the at least one protrusion is configured as a cutting edge.

2. The broadhead of claim 1, comprising a channel extending through the at least one protrusion.

3. The broadhead of claim 2, wherein the channel extending through the protrusion is configured for relieving pressure as the broadhead penetrates the target.

4. The broadhead of claim 1, wherein a distal end of the at least one protrusion is proximate the distal end of the ferrule.

5. The broadhead of claim 1, wherein a distal end of the at least one protrusion is proximal of the distal end of the ferrule.

6. The broadhead of claim 1, wherein the cutting edge of the at least one protrusion creates a bore in a target.

7. The broadhead of claim 1, wherein at least one of the plurality of recesses is configured for relieving pressure as the broadhead penetrates a target.

8. The broadhead of claim 1, comprising: a plurality of channels extending proximally from proximate the distal end of the ferrule, wherein each channel is disposed between adjacent recesses; anda plurality of deployable blades, wherein at least a portion of each blade is disposed within and is pivotally coupled to one of the plurality of channels, each blade comprising: a tip;an impact region;a first cutting edge extending from the tip to proximate the impact region; anda second cutting edge extending from the tip to proximate the channel to which the blade is pivotally coupled;wherein, during flight the tips of each blade converge to form a chisel tip comprising cutting edges defined at least in part by the first cutting edge of each blade.

9. The broadhead of claim 8, wherein the first cutting edge of each of the plurality of blades creates a bore in a target.

10. The broadhead of claim 8, wherein the second cutting edge of each of the plurality of blades widens a bore in a target.

11. The broadhead of claim 8, wherein a tip of the chisel tip is distal of the distal end of the ferrule.

12. The broadhead of claim 8, wherein a tip of the chisel tip is proximate the distal end of the ferrule.

13. The broadhead of claim 8, wherein a tip of the chisel tip is proximal of the distal end of the ferrule.

14. The broadhead of claim 8, wherein at least one of the plurality of channels is configured for relieving pressure as the broadhead penetrates a target.

15. A broadhead, comprising: a ferrule comprising: a distal end;a plurality of recesses extending proximally from proximate the distal end;at least one protrusion extending away from a surface of at least one of the plurality of recesses; anda plurality of channels extending proximally from proximate the distal end, wherein each channel is disposed between adjacent recesses; anda plurality of deployable blades, wherein at least a portion of each blade is disposed within and is pivotally coupled to one of the plurality of channels, each blade comprising: a tip;an impact region;a first cutting edge extending from the tip to proximate the impact region; anda second cutting edge extending from the tip to proximate the channel to which the blade is pivotally coupled.

16. The broadhead of claim 15, comprising a channel extending through the at least one protrusion.

17. The broadhead of claim 16, wherein the channel extending through the protrusion is configured for relieving pressure as the broadhead penetrates the target.

18. The broadhead of claim 15, wherein a distal end of the at least one protrusion is proximate the distal end of the ferrule.

19. The broadhead of claim 15, wherein a distal end of the at least one protrusion is proximal of the distal end of the ferrule.

20. The broadhead of claim 15, wherein the cutting edge of the at least one protrusion creates a bore in a target.

21. The broadhead of claim 15, wherein at least one of the plurality of recesses is configured for relieving pressure as the broadhead penetrates a target.

22. The broadhead of claim 15, wherein the first cutting edge of each of the plurality of blades creates a bore in a target.

23. The broadhead of claim 15, wherein the second cutting edge of each of the plurality of blades widens a bore in a target.

24. The broadhead of claim 15, wherein during flight the tips of each blade converge to form a chisel tip comprising cutting edges defined at least in part by the first cutting edge of each blade.

25. The broadhead of claim 24, wherein a tip of the chisel tip is distal of the distal end of the ferrule.

26. The broadhead of claim 24, wherein a tip of the chisel tip is proximate the distal end of the ferrule.

27. The broadhead of claim 24, wherein a tip of the chisel tip is proximal of the distal end of the ferrule.

28. The broadhead of claim 15, wherein at least one of the plurality of channels is configured for relieving pressure as the broadhead penetrates a target.

29. A broadhead, comprising: a ferrule comprising: a distal end;a plurality of recesses extending proximally from proximate the distal end;at least one protrusion extending away from a surface of at least one of the plurality of recesses; anda plurality of channels extending proximally from proximate the distal end, wherein each channel is disposed between adjacent recesses; anda plurality of deployable blades, wherein at least a portion of each blade is disposed within and is pivotally coupled to one of the plurality of channels, each blade comprising: a tip;an impact region;a first cutting edge extending from the tip to proximate the impact region; anda second cutting edge extending from the tip to proximate the channel to which the blade is pivotally coupled;wherein, during flight the tips of each blade converge to form a chisel tip comprising cutting edges defined at least in part by the first cutting edge of each blade.

30. The broadhead of claim 29, wherein the chisel tip creates a bore in a target.

31. The broadhead of claim 29, wherein the first cutting edge of each of the plurality of blades creates a bore in a target.

32. The broadhead of claim 29, wherein the plurality of blades deploy into a swept-back configuration exposing their respective second cutting edges.

33. The broadhead of claim 32, wherein each of the plurality of blades traverses a plane substantially orthogonal to a longitudinal axis of the broadhead.

34. The broadhead of claim 32, wherein the tip of each of the plurality of blades traverses an arc having a center at a location where the blade is pivotally coupled to the channel.

35. The broadhead of claim 32, wherein the second cutting edge of each of the plurality of blades widens a bore in a target.

36. The broadhead of claim 29, wherein a tip of the chisel tip is distal of the distal end of the ferrule.

37. The broadhead of claim 29, wherein a tip of the chisel tip is proximate the distal end of the ferrule.

38. The broadhead of claim 29, wherein a tip of the chisel tip is proximal of the distal end of the ferrule.

39. The broadhead of claim 29, wherein at least one of the plurality of recesses is configured for relieving pressure as the broadhead penetrates a target.

40. The broadhead of claim 29, comprising a channel extending through the at least one protrusion extending away from the surface of the recess.

41. The broadhead of claim 40, wherein the channel extending through the protrusion is configured for relieving pressure as the broadhead penetrates the target.

42. The broadhead of claim 29, wherein at least one of the plurality of channels is configured for relieving pressure as the broadhead penetrates a target.

43. The broadhead of claim 29, wherein a distal end of the at least one protrusion is proximate the distal end of the ferrule.

44. The broadhead of claim 29, wherein a distal end of the at least one protrusion is proximal of the distal end of the ferrule.

45. The broadhead of claim 29, wherein an outer edge of the at least one protrusion is configured as a cutting edge.

46. The broadhead of claim 45, wherein the cutting edge of the at least one protrusion creates a bore in a target.