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US4421320A Expired / Lapsed US ⏱️ 0.0 years remaining

Boomerang

Assignee: Individual
•
Filing: 1982-04-13
•
Granted: 1983-12-20
•
Expires: 2002-04-13
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Abstract

Abstract The disclosure is directed to a multi-arm boomerang with a structural configuration with permits simple modification of operational flight characteristics. The boomerang comprises a plurality of airfoil-shaped arms spaced about a central axis with an airfoil-shaped control device, preferably in the form of a ring, interconnecting the arms. By altering the cross sectional shape of the control device means, the flight characteristics of the boomerang may be modified. Furthermore, by constructing the disclosed boomerang of a resilient material there is created an entertainment device with safety features far in advance of those heretofore known.

Inventors

  • 👤 David P. Robson

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-07 18:34
CPC Classifications
A; A63; A63B; A63B65/00; A63B65/08

Claims Analysis

Total Claims: 7
Claim 1
Independent Claim 82 words
In a boomerang with a plurality of airfoil-shaped arms spaced about a central axis and extending outwardly thereabout the improvement wherein: the boomerang has a top surface and an opposing bottom surface and an airfoil-shaped lift producing control means interconnecting said plurality of arms, said control means being generally open-centered and symmetrical about said central axis, said airfoil-shaped arms providing a net lift toward said top surface, said control means providing a net lift toward said bottom surface for controlling lay down.
Claim 2
Dependent Claim 82 words
In a boomerang with a plurality of airfoil-shaped arms spaced about a central axis and extending outwardly thereabout the improvement wherein: the boomerang has a top surface and an opposing bottom surface and an airfoil-shaped lift producing control means interconnecting said plurality of arms, said control means being generally open-centered and symmetrical about said central axis, said airfoil-shaped arms providing a net lift toward said top surface, said control means providing a net lift toward said bottom surface for controlling lay down.
Claim 3
Dependent Claim 18 words
The boomerang of claim 1 wherein: said control means and said arms are statically balanced about said axis.
Claim 4
Dependent Claim 12 words
The boomerang of claim 2 wherein: said control means comprises a ring.
Claim 5
Dependent Claim 14 words
The boomerang of claim 3 wherein: said arms are spaced symmetrically about said axis.
Claim 6
Dependent Claim 22 words
The boomerang of claim 4 wherein: said arms do not extend inwardly toward said axis beyond the inner periphery of sai ring.
Claim 7
Dependent Claim 18 words
The boomerang of claim 5 wherein: said arms and ring are generally planar and comprise a resilient material.

References Cited (Backward Citations)

US692608A Cited
US2324022A Cited
GB746643A Cited
US3036832A Cited
US3082572A Cited
US3565434A Cited
US3742643A Cited
US3955817A Cited
US4045029A Cited
US4203249A Cited
US4222573A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1986-12-19 1987-06-20 1987-12-20 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1990-12-19 1991-06-20 1991-12-20 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1994-12-19 1995-06-20 1995-12-20 $7700.00 Window Closed / Lapsed

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