CPC F42B 6/06 (2013.01) | 11 Claims |
1. Stabilizing vane for arrows, comprising:
a base shaped to be connected at a tail of a shaft of an arrow, said base extending along a first direction between a first and a second end, the first direction coinciding with the flight direction of the vane when the arrow is in flight;
a body connected to the base and extending away from the base substantially along a second direction, orthogonal to the first direction, starting from a first point positioned at a marginal position of a first side positioned at the first end and from a second point positioned at a marginal position of a second side positioned at the second end of said base; said body further extending between a third side and a fourth side of the base; said first point and said second point facing the fourth side, said body having an airfoil having a convex upper surface and a concave lower surface, said body further having a variable thickness
wherein said airfoil is described by an NACA airfoil wherein M is between 1.5% and 4.5%, P is between 35.0% and 55.0% and T is between 1.5% and 4.5%.
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8. Covering for arrows comprising:
a sheath extending along a main extension direction and configured to fit on a shaft of an arrow extending along a longitudinal direction coinciding with said main extension direction when the sheath fits on the shaft;
one or more stabilizing vanes placed at an end portion of the sheath, each stabilizing vane comprising:
a base extending along a first direction between a first and a second end, the first direction coinciding with the main extension direction of the sheath;
a body connected to the base and extending away from the base substantially along a second direction orthogonal to the first direction, said body having an airfoil having a convex upper surface and a concave lower surface, said airfoil being described by an NACA airfoil.
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10. Arrow comprising:
a shaft extending along a shaft direction between a tip and a tail,
one or more stabilizing vanes arranged at the tail, said tail having one or more seats to each accommodate a respective stabilizing vane, each stabilizing vane comprising:
a base shaped to be connected at a tail of a shaft of an arrow, said base extending along a first direction between a first and a second end, the first direction coinciding with the flight direction of the stabilizing vane when the arrow is in flight;
a body connected to the base and extending away from the base substantially along a second direction orthogonal to the first direction, said body having an airfoil having a convex upper surface and a concave lower surface, said airfoil being described by an NACA airfoil.
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