Expanding broadhead

Information

  • Patent Grant
  • 6669586
  • Patent Number
    6,669,586
  • Date Filed
    Wednesday, January 15, 2003
    21 years ago
  • Date Issued
    Tuesday, December 30, 2003
    20 years ago
Abstract
A broadhead being attachable to an arrow shaft, includes a blade support having an internal passage defined in a blade receiving body, the blade receiving body having a plurality of slots defined therein extending from the internal passage to a blade receiving body external margin and having a camming surface. A translatable ring is disposed in the internal passage, and a plurality of extendable blades, each blade being shiftably coupled to the ring proximate a blade first end and being at least partially disposed in a respective slot when in a blade retracted disposition, a blade second end being cammable outward to a blade extended disposition by interaction with the body camming surface. A method of operating an expandable broadhead is further included.
Description




TECHNICAL FIELD




The present invention relates to an arrowhead and more particularly to a broadhead with extendable/retractable blades.




BACKGROUND OF THE INVENTION




In the past, various blade extending broadhead arrow tips have been provided and various mechanical arrangements to achieve the radial shifting of the blades affords the change from a compressed, in-flight, blade position to the expanded, wound enlarging position and are found in the prior art. The broadhead of U.S. Pat. No. 6,270,435 (owned by the present assignee) typifies such art.




In the past, various blade extending broadhead arrow tips have been provided and various mechanical arrangements to achieve the radial shifting of the blades affords the change from a compressed, in-flight, blade position to the expanded, wound enlarging position and are found in the prior art. Applicants, however, are not aware of any such broadhead which does not include mechanical shifting elements to arrive at the blade position change.




SUMMARY OF THE INVENTION




The present invention is a new expanding broadhead having ring mounted blades with a selected number of blades commonly mounted on a single or multiple ring which ring moves longitudinally internally of the body of the broadhead and the blades move from an in-flight, compressed position to a hide or flesh cutting, outwardly extending position upon striking a target to enlarge the entrance opening into an animal.




The blades of the broadhead are rotatably mounted to a longitudinally moving ring member which is arranged within a longitudinally extending cavity within the body of the broadhead and, further, may be arranged within longitudinally extending slots in the body to allow for a compressed, in-flight position which blades are cammed outwardly from such slots upon the broadhead striking an object. A portion of the blade carrying body or other member affixed to the body at the rear of the slots provides the camming action to the blades.




With the arrangement provided herein, the rearward and resulting radial shifting of the blades results from the entry of the broadhead into the object upon contact. The common ring mounting of the blades insures simultaneous movement of the blades.




The present invention is a broadhead being attachable to an arrow shaft, including a blade support having an internal passage defined in a blade receiving body, the blade receiving body having a plurality of slots defined therein extending from the internal passage to a blade receiving body external margin and having a camming surface. A translatable ring is disposed in the internal passage, and a plurality of extendable blades, each blade being shiftably coupled to the ring proximate a blade first end and being at least partially disposed in a respective slot when in a blade retracted disposition, a blade second end being cammable outward to a blade extended disposition by interaction with the body camming surface. A method of operating an expandable broadhead is further included.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is a side elevation of the expanding broadhead embodying the concepts of the applicants' invention in its compressed, in-flight position;





FIG. 2

is a front view thereof;





FIG. 3

is a longitudinal section taken substantially along Line


3





3


of

FIG. 2

in which the tip of the broadhead is separated from the body of the broadhead for illustrative purposes; and





FIG. 4

is a longitudinal section similar to that of

FIG. 3

but illustrating the broadhead in a partially, blade expanded position.











DETAILED DESCRIPTION OF THE DRAWINGS




In accordance with the accompanying drawings, applicants' broadhead


10


includes a penetrating tip


11


and a blade support


12


. The broadhead


10


, including blade support


12


and tip


11


is secured to an arrow shaft S by threaded


12




a


and shouldered


12




b


longitudinal, rearwardly directed extensions.




Tip


11


provides a longitudinally extending body having internal threads on the rearmost end thereof, not shown, with the opposite end of the same being faceted to provide a penetrating end consisting of a plurality of cutting surfaces and edges


11




a


,


11




b


. Although the applicants have elected to illustrate four (4) such surfaces


11




a


and edges


11




b


and though the broadhead body


11


illustrated includes three (3) expanding blades and therefore does not reflect this concept, the number of such surfaces


11




a


and edges


11




b


will normally correspond to the number of blades provided on the broadhead blade support


12


. The number of blades is selectively chosen and may include up to, for example, eight (8). Applicants' design will work equally well with various selections.




Blade support


12


includes a longitudinally extending generally cylindrical blade receiving body


13


having a front, threaded tip receiving section


13




a


connectable with tip


11


and a rear blade camming section


13




b


having a camming surface


13




c


. A longitudinally extending, generally cylindrical internal passage


14


is provided within said blade support


12


and terminates in spaced relation from the threaded front


13




a


and extensions


12




a


,


12




b.






A plurality of longitudinal grooves


15


are formed in said blade receiving body


13


and may extend the entire longitudinal dimension of internal passage


14


. The grooves


15


extend from the internal passage


14


to the external margin of the blade receiving body


13


.




The illustrated blade mounting ring


16


(see

FIGS. 3 and 4

) is designed for ease of placement on and removal of blades


17


and is provided to slide freely within said passage


14


. The ring


16


has a hinge point


16




a


corresponding to each of the blades


17


. The hinge points


16




a


are preferably equiangular displaced around the ring


16


.




A plurality of blades, each designated


17


, is mounted onto ring


16


for free rotation thereon with a mounting passage


17




a


being hingeably coupled to a respective hinge point


16




a


. Each of the blades


17


includes a longitudinally extending body having an inner edge


17




b


, a sharpened outer edge


17




c


, a forward end


17




d


, and a rearward end


17




e


and is of a thickness to be received into and allow movement of the blades within slots


15


of blade receiving body


13


.




The width of the blades


17


provides that the blades


17


will extend radially outwardly of the blade support


12


during what is termed an in-flight or retracted position as best shown in

FIGS. 1 and 2

. In this position, the sharpened outer edge


17




c


is exposed and is generally parallel to the longitudinal axis


18


. The width of the blades


17


also provides that the forward ends


17




d


thereof are exposed in the retracted disposition will impact with an object struck by the broadhead


10


to drive the ring-blade assembly


16


,


17


rearward to react against the end of slots


15


and camming area


13




b


, the blades


17


being driven outwardly to an extended, entrance aperture enlarging position, as depicted in FIG.


4


. During the in-flight or retracted position, the inner edges


17




b


of the blades


17


may be within slots


15


. The rearward end


17




e


of blades


17


may be, as shown, angularly arranged with respect to the inner


17




b


, and outer


17




c


edges of the blades


17


such that camming motion for blade expansion is easily initiated upon rearward movement of the ring-blade


16


,


17


assembly.




Such camming motion is initiated by the blade leading edge


17




d


striking an object at high speed. Resistance of the object to penetration by the broadhead


10


drives the ring


16


and all the blades


17


rearward (leftward in FIGS.


3


and


4


). This motion drives the blade rearward end


17




e


against the camming surface


13




c


and shifts the blades


17


from the retracted disposition (FIG.


3


) to the extended disposition (FIG.


4


). The blades


17


extend radially outward by the camming action of the interaction of the blade rearward end


17




e


and the camming surface


13




c


. Impact of a single blade


17


with an object will result in extension of all the blades


17


since all the blades


17


are joined to the common ring


16


.




When in the extended disposition, the camming surface


13




c


supports the blade inner edge


17




b


. The blades


17


are caused to stay in the extended disposition during passage of the broadhead


10


through an object as result of the force F1 (see

FIG. 4

) generated on the leading edge


17




d


and the transverse component of the force F2 generated on the portion of the blade


17


forward of the point of contact with the camming surface


13




c


being greater than the transverse component of the force F3 generated on the portion of the blade


17


rearward of the point of contact with the camming surface


13




c.






As depicted in

FIG. 3

, a retaining member


20


, either cutable or rearwardly displaceable may be provided about the blades


17


to, at least during a portion of the retracted in-flight position, maintain said blades


17


in such position. Such a member


20


would be cut by outward expansion of the blades or simply moved by target contact. Such a member


20


could be, for example, an O-ring or a rubber band.




To assemble the broadhead


10


, the blades


17


are first coupled to the ring


16


at the respective hinge points


16




a


to form a ring/blade assembly


16


,


17


. The ring/blade assembly


16


,


17


is arranged within passage


14


with the blades


17


arranged in slots


15


. The tip


11


is then threadedly attached to the blade support


12


. With the ring/blade assembly


16


,


17


in its forwardmost, in-flight, retracted position, the arrow S is ready for shooting. During flight, with or without the mentioned retainer


20


, the blades


17


will remain in slots


15


or in close proximity to the blade support


12


, and upon striking and penetrating an object, a rearward force (forces F1, F2, and F3) is directed to the blades


17


, causing the ring-blade


16


-


17


assembly to move rearwardly, camming the blades


17


into extended position.




To reverse this process, the blades


17


will either be radially, inwardly moved to cause forward motion or forwardly moved allowing radial shifting to return to the in-flight, retracted position for a subsequent shooting. In either manner, it is not essential to disassemble the tip


11


from the blade support


12


. It should be noted, however, that the ring/blade assembly


16


,


17


structure allows for removal and replacement of such assembly


16


,


17


should one or several of the blades


17


become dull or broken. This is a definite advantage to a hunter as the hunter is not required to remove the broadhead


10


from the arrow shaft S for such repair.




The applicants have provided a new and unique, expanding broadhead that relies only upon successful hunting use to activate its intended use. That is to say that the shooting of the broadhead into an object results in the expanding of the blades to effect the desired, entrance opening enlargement for generation of an expanded channel in the object.




It will be obvious to those skilled in the art that other embodiments in addition to the ones described herein are indicated to be within the scope and breadth of the present application. Accordingly, the applicant intends to be limited only by the claims appended hereto.



Claims
  • 1. A broadhead being attachable to an arrow shaft, comprising;a blade support having an internal passage defined in a blade receiving body, the blade receiving body having a plurality of slots defined therein extending from the internal passage to a blade receiving body external margin and having a camming surface; a translatable ring disposed in the internal passage; and a plurality of extendable blades, each blade being shiftably coupled to the ring proximate a blade first end and being at least partially disposed in a respective slot when in a blade retracted disposition, a blade second end being cammable outward to a blade extended disposition by interaction with the body camming surface.
  • 2. The broadhead of claim 1, each blade having a blade leading edge disposed proximate the blade first end, the blade leading edge being exposed when the blade is in the retracted disposition.
  • 3. The broadhead of claim 2, the blade leading edge being strikeable with an object, the impact of such striking acting to force the blade second end into interaction with the body camming surface for camming the blade outward into the extended disposition.
  • 4. The broadhead of claim 2 wherein a force imposed on the leading edge of a blade acts to force the blade second end of all blades into interaction with the body camming surface for camming all the blades outward into the extended disposition.
  • 5. The broadhead of claim 1, a blade inner edge being supported by the camming surface when the blade is in the extended disposition.
  • 6. The broadhead of claim 1 wherein an assembly comprising the plurality of blades coupled to the ring is retained in the internal passage by a tip, the tip being in threaded engagement with the blade support.
  • 7. The broadhead of claim 1 wherein the blades are retained in the retracted disposition by a circumferential retaining member.
  • 8. The broadhead of claim 1 wherein the blades are retained in the retracted disposition by a circumferential retaining member that is severable by the blades during shifting of the blades from the retracted disposition to the extended disposition.
  • 9. The broadhead of claim 1 wherein the blades are retained in the extended disposition by a force exerted on the blades by passage of the blades through an object.
  • 10. The broadhead of claim 9 wherein the blades are retained in the extended disposition by a force exerted on the blades during passage through an object, a first portion of the force exerted on a blade leading edge and on a first portion of a blade cutting edge being greater than a second portion of the force exerted on a second portion of a blade cutting edge.
  • 11. A method of operating an expandable broadhead, comprising:defining an internal passage in a blade receiving body of a blade support, defining in the blade receiving body a plurality of slots extending from the internal passage to a blade receiving body external margin and forming a body camming surface; translatably disposing a ring in the internal passage; and shiftably coupling each blade of a plurality of extendable blades to the ring proximate a blade first end and at least partially disposing each blade in a respective slot when in a blade retracted disposition and camming outward a blade second end to a blade extended disposition by blade second end interaction with the body camming surface.
  • 12. The method of claim 11, forming a blade leading edge on each blade proximate the blade first end, exposing the blade leading edge when the blade is in the retracted disposition.
  • 13. The method of claim 12, striking the blade leading edge with an object, forcing the blade second end into interaction with the body camming surface by the impact of such striking, and camming the blade outward into the extended disposition.
  • 14. The method of claim 12, imposing a force on the leading edge of a blade acts to force the blade second end of all blades into interaction with the body camming surface and camming all the blades outward into the extended disposition.
  • 15. The method of claim 11, supporting a blade inner edge by the camming surface when the blade is in the extended disposition.
  • 16. The method of claim 11 retaining an assembly comprising the plurality of blades coupled to the ring in the internal passage by a tip and threadedly engaging the tip with the blade support.
  • 17. The method of claim 11, including retaining the blades in the retracted disposition by a circumferential retaining member.
  • 18. The method of claim 11 including retaining the blades in the retracted disposition by a circumferential retaining member and severing the circumferential retaining member by the blades during shifting of the blades from the retracted disposition to the extended disposition.
  • 19. The method of claim 11 including retaining the blades in the extended disposition by a force exerted on the blades as a result of passage of the blades through an object.
  • 20. The method of claim 19 including exerting a portion of the force on a blade leading edge and on a first portion of a blade cutting edge that is greater than a portion of the force exerted on a second portion of a blade cutting edge.
RELATED APPLICATIONS

The present application claims the benefit of U.S. Provisional Patent Application No. 60/348,538, filed Jan. 16, 2002 and incorporated herein by reference.

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Provisional Applications (1)
Number Date Country
60/348538 Jan 2002 US