The current application is directed towards a fixed-blade arrowhead that includes an aerodynamic control surface which assists imparting rotation of the arrow during flight, which improves efficiency, flight characteristics, and accuracy while other features ensure proper weight, speed and balance throughout the flightpath.
1. An arrowhead, comprising:
a central body having a longitudinal axis, an outer surface, a front end and a rear end, the central body configured for attachment to a shaft of an arrow; and
a plurality of wing blades positioned about the outer surface of the central body, wherein each wing blade comprises:
a blade element comprising an upper surface, a lower surface, a leading edge, a trailing edge, and a root edge defined where the blade element meets the central body; and
a steering portion comprising an aerodynamic control surface defined by a leading edge, a trailing edge, an inner edge, and an outer edge; the leading edge of the steering portion is colinear with the leading edge of the blade element and merges at a point with the root edge of the blade element, the aerodynamic control surface diverging from the blade element upper surface extending aftward from the leading edge.
2. The arrowhead of claim 1 , wherein each wing blade extends radially at an angle from the front end of the central body, the wing blades spaced equidistantly about a circumference of the central body.
3. The arrowhead of claim 2 , wherein the leading edge is at a predetermined angle with respect to the longitudinal axis of the central body and the trailing edge is parallel to the leading edge defining a constant width therebetween.
4. The arrowhead of claim 3 , wherein the trailing edge of the aerodynamic control surface is positioned aftward of the trailing edge of the upper surface.
5. The arrowhead according to claim 1 , wherein each the wing blade is removably attached to the central body.
6. The arrowhead of claim 5 , wherein each wing blade further comprises a shoulder portion having a forward extension and a rear extension; wherein the central body further comprises a conical tip and a plurality of longitudinally extending slots configured to receive and seat the respective shoulder portion of each wing blade, each of the plurality of longitudinally extending slots extending from the rear end of the central body and through the conical tip.
7. The arrowhead according to claim 1 , wherein the aerodynamic control surface is flat.
8. The arrowhead according to claim 1 , wherein the aerodynamic control surface is curved.
9. An arrowhead, comprising:
a central body having a longitudinal axis, an outer surface, a front end and a rear end configured for attachment to a shaft of an arrow; and
a plurality of wing blades attached to the central body, each wing blade extending radially at an angle from the front end of the central body, the wing blades spaced equidistantly about a circumference of the central body, wherein each wing blade comprises:
a blade element comprising an upper surface, a lower surface, a leading edge, a trailing edge, and a root edge defined where the wing blade meets the central body, wherein the leading edge is at a predetermined angle with respect to the longitudinal axis of the central body and the trailing edge is parallel to the leading edge defining a constant width therebetween; and
a steering portion comprising an aerodynamic control surface defined by a leading edge, a trailing edge, an inner edge, and an outer edge; the leading edge of the steering portion is colinear with the leading edge of the blade element and merges at a point with the root edge of the blade element, the aerodynamic control surface diverging from the blade element upper surface from the leading edge, the trailing edge of the aerodynamic control surface is positioned aftward of the trailing edge of the upper surface.
10. The arrowhead according to claim 9 , wherein the aerodynamic control surface is flat.
11. The arrowhead according to claim 9 , wherein the aerodynamic control surface is curved.
12. The arrowhead according to claim 9 , wherein each the wing blade is removably attached to said central body.
13. The arrowhead of claim 12 , wherein each wing blade further comprises a shoulder portion having a forward extension and a rear extension; wherein the central body further comprises a conical tip and a plurality of longitudinally extending slots configured to receive and seat the respective shoulder portion of each wing blade, each of the plurality of longitudinally extending slots extending from the rear end of the central body and through the conical tip.
14. An arrowhead, comprising:
a central body having a longitudinal axis, an outer surface, a front end terminating at a conical tip, and a rear end configured for attachment to a shaft of an arrow, wherein the central body comprises a plurality of longitudinally extending slots exposed within the outer surface extending from the rear end and longitudinally through the conical tip; and
a plurality of wing blades attached to the central body, each wing blade extending radially at an angle from the front end of the central body, the wing blades spaced equidistantly about a circumference of the central body, wherein each wing blade comprises:
a shoulder portion having a forward extension and a rear extension, the shoulder portion operably configured to seat within a respective longitudinal slot of the central body, wherein the forward extension couples with and through the conical tip;
a blade element comprising an upper surface, a lower surface, a leading edge, a trailing edge, and a root edge defined where the wing blade meets the central body, wherein the leading edge is at a predetermined angle with respect to the longitudinal axis of the central body and the trailing edge is parallel to the leading edge defining a constant width therebetween; and
a steering portion comprising an aerodynamic control surface defined by a leading edge, a trailing edge, an inner edge, and an outer edge; the leading edge of the steering portion is colinear with the leading edge of the blade element and merges at a point with the root edge of the blade element, the aerodynamic control surface diverging from the blade element upper surface from the leading edge, the trailing edge of the aerodynamic control surface is positioned aftward of the trailing edge of the upper surface.
15. The arrowhead according to claim 14 , wherein the aerodynamic control surface is flat.
16. The arrowhead according to claim 14 , wherein the aerodynamic control surface is curved.
17. The arrowhead according to claim 14 , wherein the central body further comprises a base support which expands in diameter from a first diameter to a greater diameter forming a conical frustum.