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US3982489A Expired / Lapsed US ⏱️ 0.0 years remaining

Kinetic energy ring projectile

Assignee: Individual
•
Filing: 1972-11-29
•
Granted: 1976-09-28
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Expires: 1992-11-29
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Abstract

Abstract A rotatable airfoil non-lethal sting projectile comprising a hollow closed circular ring wing surrounding a central open area. The projectile consists of an aerodynamic lifting body of a thick ring wing geometry which uses spin imparted to it from a launching means for its gyroscopic stability. The combination of aerodynamic stability characteristics and high spin rate (i.e. above 2,000 rpm) results in a flat trajectory and extended range capability. The projectile is intended as a riot control weapon. Impact is non-lethal, but may be painful. The subsonic launch velocity, the non-metallic light weight structure, the soft resilience, and relatively large size of the projectile avoids serious bodily harm due to impact with a person even at point-blank range.

Inventors

  • 👤 Abraham Flatau
  • 👤 Donald N. Olson
  • 👤 Miles C. Miller

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-31 18:46
CPC Classifications
F; F42; F42B; F42B10/00; F42B10/32; F42B10/34; F42B10/36; F42B12/00; F42B12/72; F42B12/74; F42B12/745

Claims Analysis

Total Claims: 8
Claim 1
Independent Claim 76 words
A non-lethal, non-fragmenting, kinetic energy type rotatable projectile comprising: an annular ring shaped, closed structure of a tear drop airfoil cross-section; said structure being composed of resilient material and defined externally by major annular inner and outer surfaces defining the diametric extent of said structure, and being terminated by leading and trailing edges defining the longitudinal extent of said structure; said structure defining an internal annular hollow portion which is occupied by a second unified material.
Claim 2
Dependent Claim 76 words
A non-lethal, non-fragmenting, kinetic energy type rotatable projectile comprising: an annular ring shaped, closed structure of a tear drop airfoil cross-section; said structure being composed of resilient material and defined externally by major annular inner and outer surfaces defining the diametric extent of said structure, and being terminated by leading and trailing edges defining the longitudinal extent of said structure; said structure defining an internal annular hollow portion which is occupied by a second unified material.
Claim 3
Dependent Claim 13 words
The projectile of claim 1 wherein said second material is a foam material.
Claim 4
Dependent Claim 12 words
The projectile of claim 2 wherein said material serves as a ballast.
Claim 5
Dependent Claim 12 words
The invention of claim 1 wherein said resilient material is molded foam.
Claim 6
Dependent Claim 16 words
The invention of claim 4 wherein said hollow portion is occupied by a second foam material.
Claim 7
Dependent Claim 44 words
The invention of claim 5 wherein the density and location of said second foam material and the density of the structure are variable to produce the desired peak impact energy and total impact energy in order to have maximum impact effectiveness without being lethal.
Claim 8
Dependent Claim 23 words
The invention of claim 1 wherein the diametric extent exceeds 2 inches so that permanent injury to the human target will be minimized.

References Cited (Backward Citations)

US1204282A Cited
GB1054077A Cited
US3264776A Cited
US3732826A Cited
US3732821A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1979-09-28 1980-03-29 1980-09-28 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1983-09-28 1984-03-29 1984-09-28 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1987-09-28 1988-03-29 1988-09-28 $7700.00 Window Closed / Lapsed

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