Claims
- 1. A method for selectively controlling the flight trajectory of an aerial projectile comprising the steps of:
- forming a skeletal shell for the aerial projectile, the skeletal shell generally defining a three-dimensional configuration of the aerial projectile;
- confining within said shell a body of resilient, highly flexible plastic foam which serves as baffling material to increase wind resistance to the flight of said projectile and to cushion the impact of said projectile;
- providing a plurality of openings in the skeletal shell so as to permit portions of said baffling material to protrude through said openings substantially beyond the periphery of said shell, thereby increasing the wind resistance to said projectile during flight providing an impact absorbent periphery; and
- altering the flight pattern of the aerial projectile by adjusting the amount of baffling material which protrudes from said openings so as to selectively alter the degree of wind resistance imparted to the aerial projectile by the protruded and exposed baffling material.
- 2. An aerial projectile comprising in combination:
- a resilient, highly flexible plastic foam which serves as baffling material to effectively increase wind resistance to said projectile's flight; and
- a shell formed from resilient material which resists deformation after impact, said shell encircling said baffling material and having a plurality of openings formed therein through which portions of said baffling material protrude substantially beyond the periphery of said shell to increase wind resistance to said projectile's flight.
- 3. An aerial projectile as defined in claim 2 wherein said shell is essentially spherical in configuration and said openings are essentially symmetrically oriented about the periphery of said shell.
- 4. An aerial projectile as defined in claim 2 wherein said openings are sufficiently large in relation to the overall periphery of said shell that said protruding baffling material substantially obscures said shell by forming a second periphery about said shell.
- 5. An aerial projectile as defined in claim 2 wherein said shell forms a hollow that essentially encloses said baffling material except for said openings.
- 6. An aerial projectile as defined in claim 2 wherein said shell comprises a first portion which completely encloses said baffling material and a second portion having openings formed therein from which said baffling material protrudes substantially beyond the periphery of said shell.
- 7. An aerial projectile as defined in claim 6 wherein said baffling material extends radially through said openings in long, finger-like projections so as to function as flight vanes, in the manner of a shuttlecock.
- 8. An aerial projectile as defined in claim 7 wherein said first portion of said shell is separable from said second portion of said shell.
- 9. An aerial projectile as defined in claim 2 wherein said shell comprises a plurality of individual bands forming a framework for said baffling material.
- 10. An aerial projectile as defined in claim 9 wherein said baffling material is interwoven with said bands of said framework.
- 11. An aerial projectile as defined in claim 10 wherein said framework is configurated in an elongated, generally football-like shape and wherein said bands are connected together at a plurality of joints.
- 12. An aerial projectile as defined in claim 11 wherein said baffling material is supported by said bands of said framework so as to form a hollow space which extends longitudinally through said framework and the baffling material supported thereon.
- 13. An aerial projectile comprising in combination:
- a resilient, highly flexible plastic foam which serves as baffling material to effectively increase wind resistance to said projectile's flight; and
- a shell formed from resilient material which resists deformation after impact, said shell having an essentially spherical configuration and encircling said baffling material, said shell further having a plurality of openings through which portions of said baffling material protrude substantially beyond the periphery of said shell to increase wind resistance to said projectile's flight, said openings being essentially symmetrically oriented about the periphery of said shell and said openings further being of sufficient size in relation to the overall periphery of said shell that said baffling material protrudes sufficiently beyond the periphery of said shell to substantially form a second impact absorbent periphery about said shell.
Parent Case Info
This is a continuation-in-part application of my copending application Ser. No. 666,468 filed Mar. 12, 1976, now abandoned.
US Referenced Citations (5)
Foreign Referenced Citations (1)
Number |
Date |
Country |
16231 OF |
Jan 1910 |
GBX |
Continuation in Parts (1)
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Number |
Date |
Country |
Parent |
666468 |
Mar 1976 |
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