This invention relates to a method and apparatus for illuminating and propelling a projectile. The preferred embodiment disclosed herein has particular application to toy guns wherein a projectile simulating a tracer round is fired by the user. However, the invention does have application to other arrangements wherein it is desired to fire projectiles which emit a light, an example being a signal gun.
Many toys exist which simulate in some manner the operation of fire arms. It is well known, for example, to propel darts, balls and other projectiles from gun-like devices. The propulsion systems utilized in such devices vary widely and can include springs, pressurized gas systems and so forth. Quite a number of prior art designs for simulated weapons incorporate electrical or pyrotechnic means for providing lighting or sound effects. These audio and visual displays are sometimes employed in conjunction with toy weapons which propel a projectile of some type. In other cases, the lighting and sound effects are incorporated in simulated weapons which do not in fact propel a projectile of any type.
The preferred form of apparatus disclosed herein relates to a toy gun, cannon, rocket launcher or other projectile launching means which utilizes one or more illuminated projectiles to simulate tracer rounds. Typically, tracer ammunition utilized in actual weaponry contains a small pyrotechnic charge positioned in a hollow portion of a projectile. When the propelling charge is burned, the tracer charge is ignited and burns brightly as the projectile proceeds toward the intended target. Due to the photochemical persistence of the human eye, this traveling light source is perceived as an arc of light. When tracer ammunition is used at night, the trajectory of the projectile is easily monitored by this display.
The following United States patents disclose devices believed to be representative of the current state of the prior art in this field: U.S. Pat. No. 7,108,576, U.S. Pat. No. 6,648,726, U.S. Pat. No. 5,415,151, U.S. Pat. No. 5,032,098, U.S. Pat. No. 5,102,131, U.S. Pat. No. 5,388,825, U.S. Pat. No. 5,490,047, U.S. Pat. No. 5,186,458, U.S. Pat. No. 5,564,964, U.S. Pat. No. 5,779,575 and U.S. Pat. No. 6,464,602.
With the present invention simulation of tracer bullets or other projectiles is accomplished without the use of a burning projectile component. The structural elements and method steps utilized to accomplish the intended result are relatively simple, inexpensive and address the concerns of safety. The invention utilizes lighted projectiles powered by rechargeable power sources which are rapidly charged by a launcher to provide a toy that is not only inherently safe but highly interesting. The brilliant glow of the projectiles remains visible for a considerable length of time, making it a relatively easy matter to locate the projectiles in the dark after they have been projected. Light produced by the projectiles may be of any color desired. The projectile may even be made to emit infrared or ultraviolet light, viewable only by special equipment as may be desired for covert operation.
Projectile propulsion apparatus of the present invention is employed to charge and propel a projectile, said projectile including light emitting structure and a rechargeable power source.
Prior to or during launch the rechargeable power source of the projectile is charged by the projectile propulsion apparatus whereby the projectile will emit light at least after being launched from the apparatus.
The light emitting means includes at least one LED, incandescent lamp, electroluminescent device or other electric means for illuminating the projectile. The apparatus additionally comprises an electrical energy source for charging the rechargeable power source of the projectile.
Other features, advantages and objects of the present invention will become apparent with reference to the following description and accompanying drawings.
a is an exploded view of the projectile embodiment shown in
b is an exploded view of a second embodiment of projectile of the instant invention showing illumination structure, a rechargeable power source, charging electrodes and a control circuit;
Referring now to
Situated within the launch tube is projectile 30. Referring now to
Light emitting structure 15 may comprise an incandescent lamp, an LED, an electroluminescent device or any other suitable electrically powered light emitting means but is preferably an LED. An LED provides a compact, efficient, high intensity source of light which is well suited to the operation of the present invention.
Rechargeable power source 16 may comprise a battery such as a nickel-cadnium battery, a lithium battery, a capacitor, or any other suitable electric energy storage means. Rechargeable power source 16 is preferably a supercapacitor. A supercapacitor or ultracapacitor is an electrochemical capacitor that has an unusually high energy density when compared to common capacitors. Such capacitors are well suited to the instant invention in that they are very small with respect to the energy that they can store, are relatively light in weight and can be charged extremely rapidly without damage to the device. It has been found that a supercapacitor with a value of 0.6 Farad and a voltage rating of 3 Volts can, after charging, power an LED brilliantly for many minutes. Additionally, supercapacitors of this type have recently become common components in cell phones and other portable electronic devices so they are readily available and very inexpensive. One manufacturer of suitable supercapacitors is Kyocera Corporation, Kyoto, Japan.
Light emitting structure 15 may be positioned in any portion of projectile body 12 as may be desired. Additionally, light emitting structure 15 may be oriented in any manner as may be desired. Further, light emitting structure 15 may comprise multiple light emitters such as a plurality of LEDs or other light emitting means as may be desired in any combination of colors as may be desired. Further, the light emitting structure may be caused to flash or pulse in any sequence or combination as may be desired.
The exact means of propulsion of the projectile is not important, though typically, springs or gas pressure may be employed for this purpose. The embodiment shown in
A convenient means of coupling electric energy to rechargeable power source 16 from the launcher is by means of charging projectile launching apparatus electrodes 14 as illustrated in
b shows an embodiment of projectile 30A with light emitting structure which is incorporated with a control circuit 18. Said circuit may be constructed on a circuit board 17 and may employ a means such as a microchip to control the operation of light emitting structure 15. Additionally, acceleration sensor 19 may be employed to trigger an action of light emitting structure 15, for example, a bright flash upon impact of the projectile or other desired visual or sound effect which is related to a change in acceleration of projectile 30A. Acceleration sensor 19 may comprise any of the well-known acceleration sensors or switches such as, but not limited to, piezoelectric sensors, magnetic sensors, “gravity switches” or any other suitable sensor or switch. Said sensor or switch may interact directly with light emitting structure 15 or provide a signal to control circuit 18 to achieve the desired effect.
Among other functions, control circuit 18 may cause light emitting structure 15 to flash, fade, change color or provide any other desired optical effect. Additionally, the light emitting structure may be controlled in such a manner that a signal or other telemetry may be transmitted from the projectile which may be received by a remote receiver, which receiver may be for example, coupled with the projectile launcher. Such telemetry could relay the status of the projectile, or be used to transmit data collected by the projectile. Further, an audio transducer such as a speaker or buzzer may be employed as part of the system integral to the projectile so that a sound effect can be generated by the projectile. Said transducer could derive any electrical power from the aforementioned rechargeable power source. It is anticipated by the instant invention that the control circuit previously described might be of a programmable nature whereby the circuit receives program instructions from the launcher prior to, during or after charging of the rechargeable power source. Said program instructions could be transferred via the same charging electrodes as are used to charge the rechargeable power source. Additional electrodes or any form of wireless technology could also be employed to provide these instructions.
Mating projectile launching apparatus electrodes on the launcher are designed so that their mechanical contact, while sufficient to transfer electrical energy reliably, does not significantly reduce the launch velocity of the projectile. The mating electrodes on the launcher may be designed to automatically retract from the projectile immediately before the projectile is propelled from the launcher so that they do not drag on the projectile or may be otherwise configured so as to provide minimal drag on the projectile.
Another method of transferring electrical energy to the rechargeable power source is by means of electromagnetic induction. Since a conductor moving through a magnetic field generates a voltage potential, such a system may be employed to advantage.
This application is based on and claims the benefit of U.S. Provisional Patent Application Ser. No. 60/900,260, filed Feb. 7, 2007.
Number | Name | Date | Kind |
---|---|---|---|
5032098 | Balogh et al. | Jul 1991 | A |
5102131 | Remington | Apr 1992 | A |
5134552 | Call et al. | Jul 1992 | A |
5186458 | Redondo | Feb 1993 | A |
5388825 | Myers et al. | Feb 1995 | A |
5415151 | Fusi et al. | May 1995 | A |
5490047 | O'Rourke et al. | Feb 1996 | A |
5564964 | Chin-Chien | Oct 1996 | A |
5762058 | Cheng et al. | Jun 1998 | A |
5779575 | Hsieh | Jul 1998 | A |
6048280 | Palmer et al. | Apr 2000 | A |
6123631 | Ginder | Sep 2000 | A |
6390642 | Simonton | May 2002 | B1 |
6464602 | Rottger | Oct 2002 | B1 |
6648726 | Hornsby et al. | Nov 2003 | B2 |
6736742 | Price et al. | May 2004 | B2 |
7108576 | LaPointe | Sep 2006 | B2 |
Number | Date | Country | |
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60900260 | Feb 2007 | US |