1. Field of the Invention
In general, the present invention relates to toy bow systems that project toy arrows into flight. More particularly, the present invention relates to the structure of toy projectile launchers and the mechanisms for loading and releasing projectiles.
2. Prior Art Description
Bow and arrow sets that are designed for children's play have existed throughout recorded history. In the modern era, toy bow and arrow sets typically have a plastic molded bow, a string, and safety-tipped arrows. To ensure safety, the functional design of the bow is also commonly altered. In a real bow, the string has a fixed length. The spring force used to launch an arrow comes from the flexing of the arms of the bow. The problem with this design is its failure mode. If a bow is drawn beyond its limit, then the arms or the string of the bow may break. Depending upon where the breakage occurs, the broken string and/or bow may fly toward the person holding the bow as the stored energy is accidentally released.
To reduce the likelihood of this hazard from occurring, many toy bows are manufactured as static structures. An elastic string is used to create the arrow launching force. If such a bow is overdrawn, there is no significant chance of the bow breaking. Rather, the elastic string can break and will most likely move in a direction away from the person drawing the bow. The failure mode of a string breaking is far less dangerous than the failure mode of the bow breaking. However, the failure mode of broken string does present some danger depending upon where the elastic string breaks and how much energy is stored in the elastic string at the time it breaks.
Toy bows that use a static bow and an elastic string are exemplified by U.S. Pat. No. 5,247,920 to Harbin, entitled Toy Bow; and U.S. Pat. No. 7,748,369 to Chee, entitled Launching Apparatus and Assembly. Such elastic string toy bows are also shown in the applicant's earlier patent application Ser. Nos. 12/878,985 and 13/411,951.
Although toy bows with elastic strings are safer than flexible bows with non-elastic strings, a danger still is present. If an elastic string is stretched into a fully drawn state and the elastic string breaks near its mounting point with the bow, then the broken elastic string may whip toward the person pulling on the elastic string. The broken elastic string therefore has the potential to cause physical danger to the child pulling on the string, especially to the eyes of the child.
Many toy bows that have elastic strings use elastic strings that are made from a synthetic polymer, such as silicon, TPR, or some other synthetic rubber. On the toy, such elastic strings are constantly under tension. As such, if the material of the string creeps or degrades, the elastic string will break. In addition to the danger presented, this stops the toy bow from being functional.
Most all plastic degrades in some fashion over time. However, it has been found that one of the fastest ways to degrade the preferred polymers used for the bowstring is to expose the bowstring to UV light. A bowstring that can last for years inside a home may only last for a few days if taken outside and left in sunlight. Damage caused by exposure to sunlight has therefore caused customers to return products and/or consumer's to be dissatisfied.
A need therefore exists for a toy bow and arrow design that inhibits degradation in the elastic string caused by exposure to light. A need also exists for a toy bow and arrow design that eliminates the dangers to a child who may overdraw the bow to a point of string failure. These needs are met by the present invention as described and claimed below.
The present invention is a toy projectile launching system that launches a toy projectile. A launcher is provided with a first spring loaded spool and a second spring loaded spool. The first spring loaded spool and the second spring loaded spool are disposed on opposite sides of a common open area.
At least one first elastic element is at least partially wound around the first spring loaded spool. Likewise, at least one second elastic element is at least partially wound around the second spring loaded spool.
A first termination is coupled to each first elastic element. The first termination extends into the common open area. Likewise, a second termination is coupled to each second elastic element. The second termination extends into the common open area. The first termination and the second termination selectively interconnect with the toy projectile. As the toy projectile is drawn through the common central open area, it engages the first and second terminations. The projectile applies tension to the various elastic elements. The tension causes the elastic elements to unwind from the spring loaded spools and stretch. The spring energy stored on the spools and the elastic energy stored in the elastic elements is then used to launch the toy projectile into flight.
For a better understanding of the present invention, reference is made to the following description of exemplary embodiments thereof, considered in conjunction with the accompanying drawings, in which:
Although the present invention projectile launching system can be embodied in many ways, only two embodiments of the present invention system are illustrated. These embodiments are selected in order to set forth two of the best modes contemplated for the invention. The illustrated embodiments, however, are merely exemplary and should not be considered limitations when interpreting the scope of the appended claims.
Referring to
The elastic elements 20, 22 are connected to launching hooks 24, 26. The toy projectile 14 has hook receptacles 28 that engage the launching hooks 24, 26. As a person engages the toy projectile 14 with the launching hooks 24, 26 and pulls on the toy projectile 14, the elastic elements 20, 22, unwind from the spring loaded spool assemblies 16, 18 and stretch in tension. Since there are multiple elastic elements 20, 22, each of the elastic elements 20, 22 need only provide part the force needed to propel the toy projectile 14 into flight. The elastic elements 20, 22 are therefore difficult to overstretch in the proper operation of the projectile launching system 10. Furthermore, since the toy projectile 14 engages multiple separate and distinct elastic elements 20, 22, the chance of all the elastic elements 20, 22, breaking simultaneously is highly improbable. Accordingly, if one elastic element were to break, the toy projectile 14 would still be engaged with other elastic elements and the person pulling the toy projectile 14 will not pull the toy projectile 14 into himself/herself at the time of the breakage.
The launcher 12 includes a rigid plastic framework 30. The framework 30 has a handle 32 and two supports 34, 36 that extend from opposite ends of the handle 32. The two supports 34, 36 are generally coplanar. However, the handle 32 is offset from the plane shared by the supports 34, 36. The offset of the handle 32 creates a central open area 38 that is generally C-shaped, being defined on one side by the handle 32 and on the top and bottom by the two supports 34, 36.
The supports 34, 36 of the framework 30 are shaped as the arms of a bow. However, in the present invention, the supports 34, 36 serve as aesthetic elements and are not required for the function of the toy. Rather, the mechanism used to launch the toy projectile 14 is contained within the spring-loaded spool assemblies 16, 18 and the resiliency of the elastic elements 20, 22 that are wound within the spring loaded spool assemblies 16, 18.
The spring-loaded spool assemblies 16, 18 are carried by the framework 30. Two cylindrical compartments 40, 42 are formed in the framework 30. The cylindrical compartments 40, 42 are parallel and are oriented to be perpendicular to the primary vertical progression of the handle 32. The first cylindrical compartment 40 is located near the forward most part of the first support 34. Similarly, the second cylindrical compartment 42 is also located near the forward most part of the second support 36. The two cylindrical compartments 40, 42 are positioned above and below the central open area 38 created by the offset handle 32.
Slots 44, 46 are formed in the cylindrical compartments 40, 42. The slots 44, 46 face toward each other across the central open area 38. Two guides 48, 50 are provided. The guides 48, 50 are positioned above and below the central open area 38 created by the offset handle 32. The guides 48, 50 are positioned directly between the cylindrical compartments 40, 42 and the central open area 38. Each of the guides 48, 50 contains two narrow passages 51, 52. Each of the narrow passages 51, 52 is sized to enable a length of one of the elastic elements 20, 22 to extend therethrough. The narrow passages 51, 52 are aligned with the slots 44, 46 in the cylindrical compartments 40, 42.
The spring-loaded spool assemblies 16, 18 are set into the cylindrical compartments 40, 42. The spring loaded spool assemblies 16, 18 have central posts 54, 56 that are concentrically positioned within the cylindrical compartments 40, 42. Torsion springs 58, 60 are set around the central posts 54, 56. Spools 61, 62 are placed around the central posts 54, 56. The torsion springs 58, 60 have ends that engage the spools 61, 62 and opposite ends that engage the central posts 54, 56. In this manner, when the spools 61, 62 are rotated on the central posts 54, 56, they cause the torsion springs 58, 60 to rotate and store spring energy.
Each of the spools 61, 62 contains two end flanges 63, 65. The end flanges 63, 65 guide the elastic elements 20, 22 on and off the spools 61, 62 and the spools 61, 62 rotate.
The projectile launching 12 includes the use of two separate and distinct elastic elements 20, 22, wherein one of the elastic elements is dedicated to each of the spring-loaded spool assemblies 16, 18. The first elastic elements 20 attaches to the first spring loaded spool assembly 16. The first elastic element 20 has one end that is anchored to the first spool 61. The second elastic element 22 is anchored to the second spool 62. The opposite ends of both the first and second elastic elements 20, 22 attach to the first and second launching hook 24, 26, respectively.
Both lengths of the elastic elements 20, 22 pass through short lengths of reinforcement tubing 70 just prior to attaching to the first launching hook 24 or the second launching hook 26. The elastic elements 20, 22 are prevented from tangling and/or over retracting into the spring loaded spool assemblies 16, 18 by the guides 48, 50. The elastic elements 20, 22 pass through the passages 51, 52 in the two guides 48, 50. The guides 48, 50 are sized to enable the elastic elements 20, 22 to pass. However, the reinforcement tubing 70 is too large to pass through the passages 51, 52. Consequently, the sections of the elastic elements 20, 22 that pass through the reinforcement tubing 70 remain dangling below the guides 48, 50 in the central open area 38. Likewise, the launching hooks 24, 26 supported by the elastic elements 20, 22 remain dangling in the central open area 38.
Each of the elastic elements 20, 22 is made from a highly elastic elastomeric material that enables each of the elastic elements 20, 22, to resiliently stretch at least threefold without breaking. In the shown embodiments, the elastic elements 20, 22 are shaped as belts with generally rectangular cross-sectional profiles. It will be understood that the elastic elements 20, 22 can have many shapes and can be configured as cords or braided elements.
Referring to both
To load the toy projectile 14, the toy projectile 14 is drawn through the central open area 38 so that the launching hooks 24, 26 engage the hook receptacles 28. Once engaged with the launching hooks 24, 26, the toy projectile 14 is pulled in the manner of a traditional bow and arrow. As the toy projectile 14 is drawn away through the central open area 38, the elastic elements 20, 22 are pulled in tension. This causes the elastic elements 20, 22 to unwind from the spring loaded spool assemblies 16, 18. This causes the spools 61, 62 to rotate and the torsion springs 58, 60 to turn and store spring energy. Furthermore, when the elastic elements 20, 22 are fully unwound from the spools 61, 62, the elastic elements 20, 22 stretch and store elastic energy.
When the toy projectile 14 is released, the elastic elements 20, 22 contract and release the stored elastic energy. Likewise, the torsion springs 58, 60 recoil the spools 61, 62 and release the stored spring energy. As a result, the toy projectile 14 is accelerated through the central open area 38. The momentum of the toy projectile 14 causes the toy projectile 14 to continue its forward movement past the central open area 38. This launches the toy projectile 14 into flight as the launching hooks 24, 26 disengage the hook receptacle 28.
The strength of the torsion springs 58, 60 are preferably coordinated with the strength of the elastic elements 20, 22. In this manner, the spools 61, 62 unwind just as the elastic elements 20, 22 reach their optimal degree of elongation.
The launcher 12 is normally in the condition shown in
Referring to
In
It will be understood that the embodiments of the present invention that are illustrated and described are merely exemplary and that a person skilled in the art can make many variations to those embodiments. For instance, the bow structure can have many different ornamental shapes. Likewise, the toy projectiles can be configured as airplanes, rocket ships or any other flying projectile. All such embodiments are intended to be included within the scope of the present invention as defined by the claims.
Number | Name | Date | Kind |
---|---|---|---|
1153415 | Beaty | Sep 1915 | A |
2995129 | Malott | Aug 1961 | A |
3974820 | Ott | Aug 1976 | A |
4169453 | Hunsicker | Oct 1979 | A |
4411248 | Kivenson | Oct 1983 | A |
4458658 | Blair | Jul 1984 | A |
4651707 | Bozek | Mar 1987 | A |
4662344 | Mitchell | May 1987 | A |
4703744 | Taylor | Nov 1987 | A |
4903677 | Colley | Feb 1990 | A |
5054463 | Colley | Oct 1991 | A |
5072715 | Barr | Dec 1991 | A |
5125388 | Nicely | Jun 1992 | A |
5243955 | Farless | Sep 1993 | A |
5247920 | Harbin | Sep 1993 | A |
5282453 | Chia | Feb 1994 | A |
5345922 | Ott | Sep 1994 | A |
5531209 | Liedtke | Jul 1996 | A |
5678528 | Hadley | Oct 1997 | A |
5720268 | Koltze | Feb 1998 | A |
5762056 | Kysilka | Jun 1998 | A |
5830029 | Siegel | Nov 1998 | A |
6500042 | LaPointe | Dec 2002 | B1 |
7448371 | Sapir | Nov 2008 | B2 |
7748369 | Chee | Jul 2010 | B2 |
8485168 | Walterscheid | Jul 2013 | B2 |
20090032002 | Howard et al. | Feb 2009 | A1 |
20100263649 | Fields | Oct 2010 | A1 |
20130167819 | Walterscheid | Jul 2013 | A1 |
20140251294 | Novikov | Sep 2014 | A1 |
20140338647 | Cummings | Nov 2014 | A1 |
Number | Date | Country | |
---|---|---|---|
20150176940 A1 | Jun 2015 | US |