An apparatus is disclosed for launching a toy projectile(s). The apparatus may be configured to store one or more returnable projectiles, and may function to impart a spin in the projectiles during launch so that the projectile may be induced to travel away from and then back towards the launch point.
The boomerang is an ancient weapon of war and hunting that may be best known for its ability to change direction in flight and return to the thrower. Over time, this direction changing feature of the boomerang has aided its evolution from use as a weapon into a children's plaything.
Boomerangs are produced in a variety of shapes and sizes. One traditional form of boomerang is essentially a rotating wing shaped from a single flat curved blade. Other boomerang designs include the “fast catch” variety, which usually have three or more symmetrical wings (in the platform view), and “long distance” boomerangs, which are shaped similar to a question mark.
Boomerang throwing techniques can differ from person to person, and depending on the desired result. However, known prior art boomerangs are all thrown by hand. According, it would be advantageous to have an apparatus that may store and successively launch multiple boomerangs or similar projectiles.
A toy apparatus may include a projectile and a housing or launcher. The projectile may include one or more wing or blade portions that each may have end, a leading edge and a trailing edge. The housing or launcher of the apparatus may include a grip, a trigger, and a projectile support platform. A projectile launch key may be positioned on the projectile support platform. This projectile launch key may be dimensioned to removably receive the end of the wing of the projectile and also engage the trailing edge of the wing. Moreover, the projectile launch key may be coupled to the trigger so that the pulling or retraction of the trigger may result in the rotation of the projectile launch key through an arc of between 90 and 80 degrees upon retraction of the trigger.
The projectile launch key may take a variety of forms. For example, the projectile launch key may include a rotatable base having a wall that extends at least partially around the parameter of the base and is dimensioned to engage the end and trailing edge of a wing or blade of a projectile. As shown herein, the projectile launch key may include a rotatable base having a retainer wall dimensioned to engage the end of a wing or blade of a projectile, and a pin dimensioned to engage the trailing edge of a wing or blade. To that end, the trailing edge of the wing of the projectile may include a notched portion that may be engaged by the pin of the projectile launch key and aid in the stable launch of the projectile.
The housing may also include a magazine that is dimensioned to retain a plurality of projectiles and may be configured to cooperate with the trigger to dispense or load projectiles onto the projectile launch key. The magazine, for example, may include a top face, a bottom face that may be spaced from the projectile support platform, and an aperture that extends through the magazine between the top and bottom faces.
To assist in dispensing or loading of projectiles, the magazine may also include a first floor plate and a second floor plate. The plates may be positioned proximate the bottom face of the magazine, with the second floor plate being positioned between the first floor plate and the projectile support platform. The first floor plate may be coupled to the trigger and configured to rotate upon retraction of the trigger to aid in ejecting a projectile from the magazine.
Reference will be made below to a number of figures in which like referenced numerals refer to like parts throughout and wherein:
Additional figures and photographs are attached hereto as Appendix A1-A23 which is incorporated into this application in its entirety by reference.
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Referring now to FIGS. 4 and 8-11, the projectiles 12 may be supported within the aperture 32 of the magazine 22 by the first 28 and a second 30 floor plates. More specifically, each plate 28, 30 may include an aperture 36, 38 dimensioned to conform to the shape of the projectile 12. The plates 28, 30 may also be positioned on or proximate an end 40 of the aperture 32 opposite the open end 34 bottom and function as a (full or partial) support floor for the projectile 12. More specifically, the plates 28, 30 may be positioned relative to each other so that their apertures 36, 38 are in axial alignment, and relative to the aperture 32 of the body 26 so that a portion of each plate (e.g., an edge portion of each aperture 36, 38) extends at least partially across the end 40 of the aperture 32 of the body 26.
Still referring to FIGS. 4 and 8-11, the upper plate 28 may be rotatably mounted to the body 26 and coupled to the trigger 16. For example, the plate 28 and trigger 16 may be mechanically connected by a simple arrangement of gears. It will, however, be appreciated that any mechanical or non-mechanical assembly, including gears, springs, tension means, etc., and other coupling systems known in the art may be used to couple movement of the trigger 16 with a corresponding rotation of the plate 28. Thus, in operation, pulling of the trigger 16 may cause the plate 28 to rotate and retract that portion of the plate 28 that extends across the bottom end 40 of the aperture 32 of the body 26. Stated differently, the plate 28 may rotate so that the aperture 36 of the plate 28 moves into axial alignment with the aperture 32 of the body 26. This movement of the plate 28 allows a projectile 12 in the aperture 32 of the body 26 to descend onto the lower plate 30. The release of the trigger 16 returns the plate 28 to its initial state during which the plate 28 may engage the projectile 12 (which now rests on the lower plate 30) to urge the projectile off and through the aperture of the lower plate 30 so that the projectile 12 may descend into the key 20 of the launch platform 18.
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As shown, the key 20 may be positioned at a central point of the launch platform 18. It will however be appreciated that the key should be located a distance from a backside 42 of the platform 18 sufficient to allow a projectile 12 to rotate completely around the platform 18 during launch as will be described further below. The launch key 20 may include a base 41, and a retainer wall 42 and a pin 44 that extend from the base 41. The wall 42 may be dimensioned to engage and removably retain an end or apex of an wing of a projectile 12. The vertically extending pin may be positioned on the key 20 so that it may engage a trailing edge of the wing of the projectile 12 that is engaged by the retainer wall 42. A notch 46 may be included in the trailing edge of the wing of the projectile that may be engaged by the pin 44 to assist in the engagement of the projectile 12 by the key 20.
In operation, a user loads a projectile into the aperture 32 so that it rests upon the upper plate 28, which functions as the floor of the magazine 22. A user may then pull the trigger, causing the plate 32 to retract out of position and allow the projectile 12 to descend so that it rests on the lower plate 30 of the magazine 22. Then, upon release of the trigger 16, the upper plate 28 (in returning to its unretracted original state) urges the projectile 12 off the lower plate 30 and into the key 20 of the launch platform 18. Pulling the trigger 16 again may result in the rapid rotation of the launch key 20 through an arc of about 450 degrees (although any greater (e.g., 810 degrees) or lesser (e.g., 90 degrees) predetermined angle of rotation may be used depending on the needs of the user). The projectile 12 is likewise urged through this rotation by operation/rotation of the key 20. For example, in the disclosed embodiment, the retainer wall 42 and pin 44 may engage the projectile, allowing it to be propelled and then launched by rotation of the key 20. More specifically, the rotation of the key 20 has the effect of inducing speed, forward momentum and rotation on the projectile 12 causing it to travel outward from the housing/launcher. The shape of the projectile 12, and/or the orientation at which the apparatus 10 is held during launch (e.g., an angle of attack between 0 and positive 60 degrees relative to the horizon) may also aid in the return of the projectile to at or near the point of launch.
Having thus described an embodiment of the apparatus, various other embodiments will become apparent to those of skill in the art that do not depart from the skill of the claims.
This application claims priority of U.S. Provisional Patent Application Ser. No. 61/289,748 filed Dec. 23, 2009, the disclosure of which is incorporated herein by reference in its entirety.
Number | Name | Date | Kind |
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849166 | Smith et al. | Apr 1907 | A |
3717136 | Gay et al. | Feb 1973 | A |
4248202 | Jaworski et al. | Feb 1981 | A |
4372281 | Fiorani | Feb 1983 | A |
5050575 | Killion | Sep 1991 | A |
5996564 | Kotowski | Dec 1999 | A |
6733356 | Lee | May 2004 | B2 |
Number | Date | Country | |
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20110151741 A1 | Jun 2011 | US |
Number | Date | Country | |
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61289748 | Dec 2009 | US |