Broadhead arrowhead

[0002] 1. Field of the Invention

[0003] This invention relates to arrows and arrowheads. More particularly, the invention relates to arrowheads of the type commonly referred to as “broadhead” arrowheads typically, but not exclusively, used by hunters.

[0004] FIG. 1 shows a side perspective view of the broadhead arrowhead of this invention;

[0005] FIG. 2 shows an end view of the broadhead arrowhead looking rearwardly from the forward end of the arrowhead.

[0006] FIG. 3 shows a side detail view of the arrowhead.

[0007] FIG. 4 shows a detailed view of one of the blade assemblies of the arrowhead.

[0008] FIG. 4A shows the curvature of the blade assembly at three sections taken along section lines “A—A”, “B—B”, “C—C”, respectively, in FIG. 4.

[0009] FIG. 5 shows the broadhead arrowhead mounted to an arrow shaft.

[0010] Referring to the drawings, the broadhead arrowhead of this invention comprises a body or ferrule 102. At one end, called, for convenience, the proximal end, ferrule 102 incorporates a first, or head, end portion 104. End portion 104 typically tapers to a point 105. Ferrule 102 also has second, or distal, end portion 106. End portion 106 may be slightly flared outwardly. It is not necessary that end portion 106 be flared outwardly. In some embodiments, end portion 106 may continue substantially straight to the rear end of body 102. Ferrule 102 is typically symmetrical about a longitudinal axis 118 between first end portion 104 and second end portion 106.

[0011] A mounting stub 108 extends rearwardly from distal end portion 106 of arrowhead body 102. Typically, stub 108 is symmetrical about and coaxial with longitudinal axis 118. Mounting stub 108 is intended to fit into a mating recess typically located at one end of a standard arrow shaft. Stub 108 may be threaded to mate with matching threads in the arrow shaft recess or it may be seated in the recess in a press fit arrangement. Alternatively, mounting stub 108 may be glued or otherwise sealed into the mating recess of the arrow shaft.

[0012] In other variations of mounting means, instead of a stub 108, distal end 106 of ferrule 102 may be hollowed out to fit over an arrow shaft. In such an arrangement, the inside of hollow distal end 106 may be threaded to mate with threads on the outer suface of the arrow shaft; or distal end 106 may be press fit over the arrow shaft. Alternatively, distal end 106 may be fitted over the end of the arrow shaft and glued or otherwise sealed to the arrow shaft.

[0013] One or more blade assemblies 110 extend laterally outwardly from ferrule 102. Preferably the arrowhead is constructed with two, three or four blade assemblies. Typically, if two blade assemblies are used, they are disposed substantially diametrically opposite each other about longitudinal axis 118 of ferrule 102. Three blade assemblies are typically disposed at angles of approximately 120° around longitudinal axis 118. Correspondingly, four blade assemblies 110 are typically mounted at 90° angles relative to each other about horizontal axis 118.

[0014] Blade assembly 110 is shown in detail in FIGS. 1 and 4. Each blade assembly 110 comprises a first substantially planar blade assembly portion 112 and a second blade assembly portion 114. A leading edge 113 of first portion 112 is typically sharpened to better allow the arrowhead to penetrate a target. First blade assembly portion 112 may comprise a solid substantially flat planar portion or optionally may have a cutout section 116. Second blade assembly portion 114 extends rearwardly from first blade assembly portion 112. Second blade assembly portion 114 is preferably curved, with a radius of curvature optimally between about 0.2″ and 0.5″, giving the blade the characteristics of an airfoil. The radius of curvature may vary over the surface of the blade. A trailing edge 119 of the blade is at an angle to arrowhead body 102. This angle may be as great as 45 degrees or more, but optimally it increases from approximately 5 degrees to approximately 35 degrees at the blade tip. The blades, acting together, form an axial-flow turbine.

[0015] As shown in FIG. 3, second blade assembly portion 114 is joined to first blade assembly portion 112 by a continuously curved region 120. The radius of curvature of region 120 is in the range of between about 0.2″ and 0.5″. An angle θ generally defines the angle between first planar portion 112 and second planar portion 114. This angle θ is in the range of between about 5° and 25°. This configuration gives the blade assembly an airfoil-type shape. The length of first substantially planar portion 112 is between about 50% and 80% of the total length of blade assembly 110. Correspondingly, second substantially planar portion 114 comprises between about 20% and 50% of the total length of blades assembly 110. It will be understood by those skilled in the art that where the arrowhead has more than one blade assembly 110, each blade assembly portion 114 is preferably angled relative to each corresponding blade assembly portion 112 in the same direction and at substantially the same angle for each blade assembly 110.

[0016] Alternatively, first planar portion 112 and second angled planar portion 114 may be joined at a more sharply defined angle θ with a radius of curvature close to or at “0”. However, this alternative configuration does not produce the same high quality of aerodynamic effects as does the airfoil shape shown in FIG. 3.

[0017] FIG. 4A shows the curvature of the blade assembly 110 at three sections taken along section lines “A—A”, “B—B”, “C—C”, respectively, in FIG. 4.

[0018] Arrowhead body 102 and blade assemblies 110 may be made of any suitable material, such as, but not limited to, steel, aluminum, plastic, etc. As shown in FIG. 4, planar portion 112 of blade assembly 110 has a short extension 117 that fits into a slotted opening in ferrule 102. Extension 117 extends from the inner edge of planar portion 112 substantially up to but just short of curved region 120. Extension 117 may be glued, welded or soldered to the slot in body 102. Alternatively, blade assembly 110 and body 102 may be integrally formed as by molding. Other techniques for securing blade assembly 110 to body 102 would be apparent to those skilled in the relevant arts.

[0019] In summary, each blade assembly 110 comprises a substantially flat planar portion 112 extending laterally outwardly of body 102 and substantially parallel to longitudinal axis 118. A second blade assembly portion 114 is angled at an angle of between about 5° and 25° out of the plane of section 112 away from alignment with axis 118 and at an angle of between about 5° and about 45° to the ferrule body 102. FIG. 2 shows end portions 114 of each blade angled slightly clockwise relative to the major plane of section 112. Alternatively, end portions 114 can be angled slightly counterclockwise relative to the major plane of section 112.

[0020] In the embodiment shown, each blade assembly 110 has the general shape of a substantially triangular or delta wing configuration. In other embodiments, blade assembly 110 can have the general shape of a swept wing or straight wing.

[0021] Much like the control surfaces of an aircraft wing, the ratio of angled portion length to overall blade assembly length can be relatively small. For example, in one embodiment, the ratio of the length of angled portion 114 to the overall length of blade assembly 110 is in the range of between 10% and 50%, and preferably between about 20% and 50%.

[0022] Each blade of the broadhead arrowhead incorporates a substantially similar airfoil that produces a rotational torque about longitudinal axis 118. In flight, these forces induce a rapid rotation of the arrow about longitudinal axis 118 while minimizing aerodynamic drag. The plane of each blade assembly 110 remains parallel to the shaft of the arrow along its cutting edge 113.

[0023] One of the features of the arrowhead of this invention is its ability to produce stabilized arrow flight without the use of fletching or tail fins (or feathers). FIG. 5 shows the broadhead arrowhead of this invention mounted to an arrow shaft 122 without fletching. Tests have shown that an arrow using the broadhead of this invention without fletching tracks true in flight and does not deviate significantly from the planned flight course. This is due to the rotation induced in the arrow by the aerodynamically designed broadhead blades, which is sufficient to stabilize the arrow in flight. Eliminating the fletching in fact improves flight characteristics because the rotational drag normally induced by the fletching is avoided. It should be noted, however, that the arrowhead of the invention can be used with fletched arrow shafts, as well.

[0024] While various embodiments of the present invention have been described above, it should be understood that they have been presented by way of example only, and not limitation. Thus, the breadth and scope of the present invention should not be limited by any of the above-described exemplary embodiments, but should be defined only in accordance with the following claims and their equivalents.