Aerodynamic air gun projectile

• US 7,222,573 B2
• Filed: 03/29/2006
• Issued: 05/29/2007
• Est. Priority Date: 04/01/2005
• Status: Expired due to Fees

• Current Assignee: James M. Pontieri
• Original Assignee: James M. Pontieri
• Inventors: Pontieri, James M.
• Primary Examiner(s): Clement; Michelle
• Assistant Examiner(s): Lee; Benjamin P.
• Application Number:
  US11/391,865
• Publication Number:
  US 20070074637A1
• Time in Patent Office: 426 Days
• Field of Search: 102/501, 102/502, 102/524, D22/115, D22/116
• US Class Current: 102/501
• CPC Class Codes: F42B 10/24 with inclined grooves
• CPC Class Codes: F42B 10/26 using spin F42B10/04, F42B10/12, F42B10/14, F42B10/24, F42B14/02 take precedence
• CPC Class Codes: F42B 6/10 Air gun pellets ; Ammunition for air guns, e.g. propellant-gas containers

Abstract

A projectile for an air arm is integrally formed from a single piece of dense malleable material formed as a body of revolution about a longitudinal axis having a head portion dimensioned for free sliding in the bore of an air arm and a skirt-like portion of frusto-conical form. The rearward end of the skirt portion is dimensioned to be in slight interference fit with the bore and the forward end is joined with the head portion to define a reduced diameter waist. The frustum is shell-walled, having a central recess opening to the rear and extending forwardly into the head portion. The head portion has a parabolically shaped outer surface which transitions smoothly into a hyperbolically shaped outer skirt surface for aerodynamic efficiency. Vanes are formed on the head portion to enhance in-flight spiraling rotation.

Claims

1. In a projectile for an air arm molded as a body of revolution about a longitudinal axis comprising a head portion dimensioned for free sliding in the bore of an air arm and a skirt portion of frusto-conical form of which the rearward end is dimensioned to be in interference fit with said bore and the forward end is joined with the head portion in a reduced diameter waist, the frustum being shell-walled and having a central recess opening to the rear and extending forwardly into the head portion, an improvement wherein said projectile has an external surface form characterized by a parabolic head which smoothly transitions axially into a hyperbolic skirt,

said projectile further comprising one or more vanes formed substantially symmetrically on the outer surface of said head portion, each vane extending axially in a helix configuration with a characteristic pitch which varies along the axial extent thereof.

2. The air arm projectile of claim 1, wherein said vanes are operative to induce continued rotation of said projectile about its axis as it traverses a line of trajectory after being discharged from said air arm.

3. The air arm projectile of claim 1, wherein said vanes extend substantially the entire axial extent of said head portion.

4. The air arm projectile of claim 1, wherein at least some of said vanes are incused beneath said head portion surface.

5. The air arm projectile of claim 1, wherein at least some of said vanes are raised above said head portion surface.

6. The air arm projectile of claim 1, wherein said vanes are circumferentially symmetrical in cross-section.

7. The air arm projectile of claim 1, wherein said vanes are circumferentially asymmetrical in cross-section.

8. The air arm projectile of claim 1, wherein said vanes are substantially notch shaped, comprising substantially planar sidewalls.

9. The air arm projectile of claim 1, wherein said vanes define curvilinear sidewalls.

10. The air arm projectile of claim 1, wherein said vanes are integrally formed with a homogeneous material composition making up said projectile.

11. The air arm projectile of claim 1, wherein said projectile has a characteristic center of gravity axially positioned intermediate leading and trailing ends of said vanes.

12. The air arm projectile of claim 1, wherein the forward end of said skirt portion is conjoined with said head portion to form a radially outwardly facing forward guide surface, said forward guide surface having a nominal diameter equal to or exceeding the maximum nominal diameter of the head portion.

13. The air arm projectile of claim 12, wherein the rearward end of said skirt portion forms a radially outwardly facing rear guide surface, said rear guide surface having a nominal diameter substantially equaling the nominal diameter of said forward guide surface and disposed in axial alignment therewith, the rearward end of said skirt portion further forming a radially outwardly directed abutment collar operative, prior to discharge of the air arm, to limit axial displacement of the projectile in at least one axial direction within the breech of the air arm.

14. The air arm projectile of claim 1, wherein said projectile has a characteristic substantially continuously recurved profile comprising a generally convex segment defined by said head portion and a generally concave segment defined by said skirt portion.

15. The air arm projectile of claim 1, wherein said body of revolution is molded from relatively dense metallic material or alloy.

16. The air arm projectile of claim 1, wherein said body of revolution is molded from a composition consisting of a major weight proportion of a dense material of a particulate form loading a matrix of a minor weight portion of a resinous binder.

17. The air arm projectile of claim 1, wherein the projectile has a characteristic head diameter of about 4.2 mm and a trailing edge diameter of about 4.65 mm.

18. The air arm projectile of claim 1, wherein the axial length of said skirt portion equals or exceeds the axial length of said head portion.

19. A projectile for an air arm molded as a body of revolution about a longitudinal axis, said projectile comprising:

a head portion dimensioned for free sliding in the bore of an air arm;

a skirt portion of frusto-conical shape integrally formed with said head portion from common homogeneous material, said skirt portion including a rearward end dimensioned to be in interference fit with said bore and a forward end joined with said head portion in a reduced diameter waist, the frustum being shell-walled and having a central recess opening to the rear and extending forwardly into the head portion,

wherein said head portion has a parabolic outer surface and said skirt portion has a hyperbolic outer surface, said head portion outer surface and said skirt portion outer surface having a common nominal diameter dimension at a point of transition there between to effect a smooth transition in a direction along said longitudinal axis; and

means for inducing rotation of said projectile about its longitudinal axis as it traverses a line of trajectory after being discharged from said air arm, said means for inducing rotation comprising one or more vanes formed substantially symmetrically on the outer surfaces of said head portion and the reduced diameter waist portion of said skirt portion, each vane extending axially in a helix configuration which varies in pitch along its axial extent, and at least some of said vanes incused within said head portion,

wherein said projectile has a characteristic center of gravity located within the head portion along the longitudinal axis at a point intermediate the forwardmost and rearward most ends of said vanes formed on the outer surface of said head portion, and

wherein the axial length of said skirt portion equals or exceeds the axial length of said head portion.

20. In a projectile for an air arm molded as a body of revolution about a longitudinal axis comprising a head portion dimensioned for free sliding in the bore of an air arm and a skirt portion of frusto-conical form of which the rearward end is dimensioned to be in interference fit with said bore and the forward end is joined with the head portion in a reduced diameter waist, the frustum being shell-walled and having a central recess opening to the rear and extending forwardly into the head portion, an improvement wherein said projectile has an external surface form characterized by a parabolic head which smoothly transitions axially into a hyperbolic skirt,

said projectile further comprising means operative to induce continued rotation of said projectile about its axis as it traverses a line of trajectory after being discharged from said air arm,

wherein said means operative to induce continued rotation comprises one or more vanes formed substantially symmetrically on the outer surface of said head portion, each vane extending axially in a helix configuration, and

wherein one or more of said vanes extend axially along at least a portion of the outer surface of said skirt portion.

21. In a projectile for an air arm molded as a body of revolution about a longitudinal axis comprising a head portion dimensioned for free sliding in the bore of an air arm and a skirt portion of frusto-conical form of which the rearward end is dimensioned to be in interference fit with said bore and the forward end is joined with the head portion in a reduced diameter waist, the frustum being shell-walled and having a central recess opening to the rear and extending forwardly into the head portion, an improvement wherein said projectile has an external surface form characterized by a parabolic head which smoothly transitions axially into a hyperbolic skirt,

said projectile further comprising means operative to induce continued rotation of said projectile about its axis as it traverses a line of trajectory after being discharged from said air arm,

wherein said means operative to induce continued rotation comprises one or more vanes formed substantially symmetrically on the outer surface of said head portion, each vane extending axially in a helix configuration, and

wherein said vanes have a characteristic pitch which varies along the axial extent thereof.