U.S. provisional patent application No. 62/677,096 filed May 28, 2018 is incorporated by reference in its entirety for all purposes.
The disclosed methods and apparatus generally relate to toy and model projectile launchers using an aerosol spray device containing a flammable liquid.
For many years toy launching devices have been popular among children of all ages. One method of launching projectiles has relied on the use of solid-fuel rocket engines. However, many dangers exist when solid-fuel engines are used. For example, in a solid-fuel rocket, once the fuel is ignited it generally will not stop until the entire fuel supply is spent.
Other projectile launchers employ a pressure tank in which pressurized air or water is stored and later expelled through a nozzle as a means to propel the projectile. However, once these types of launchers are fully pressurized they generally cannot be removed from the launcher without firing the projectile, and a pressurized container can burst and be dangerous.
In the methods and apparatus disclosed herein, a projectile launcher is described that can be used to safely and repeatably launch projectiles very fast and very high into the air.
The apparatus uses an aerosol spray device containing a flammable liquid. The apparatus comprises a chamber and a tube, wherein the tube is fixedly attached to an opening in the chamber. Inside the chamber is a spark gap connected by an electrical cable to a spark power source. The cable has sufficient length to permit the spark power source to be located a safe distance away from the chamber and projectile.
A projectile can be slid over the tube. Flammable liquid from the aerosol device is then sprayed into the chamber. When the spark power source is activated by a user, the mixture of air and flammable liquid ignites.
The ignition of the mixture of air and flammable liquid thereby propels the projectile rapidly away from the projectile launcher apparatus.
Safety mechanisms prevent over-pressurization of the chamber and prevent improper fuel sources from being used. The launcher apparatus also allows for a launch to be safely aborted without having to launch the projectile.
Disclosed is a projectile launcher apparatus as shown in an embodiment in
The apparatus includes a chamber (3) and a tube (1). The tube (1) has an open bottom end and an open top end. The open bottom end of the tube (1) is fixedly attached to an opening in the chamber (3). It will be appreciated that the tube (1) has a generally constant cross section. The open top end of the tube (1) has a screen (2) there-across to prevent undesired foreign objects and fuels from entering the tube (1).
The chamber (3) has a volume of at least one liter and in an embodiment it may have a conically-shaped top end (4) and a conically-shaped bottom end (9). The chamber (3) is located above the launcher apparatus base (8). The chamber (3) has an input port (5) configured to connect to an aerosol spray device (13) allowing the chamber (3) to be filled with flammable liquid, thereby yielding a mixture of air and atomized flammable liquid (14) in the chamber (3). The chamber (3) is also configured to include a pressure relief valve (12), designed to prevent over-pressurization of the chamber (3). In an embodiment an air pump (11) is connected to the chamber (3) to pump air into the chamber (3). This can flush out old or burnt propellant.
The shape of the lower chamber (9) acts as an upside-down rocket nose and it amplifies the pressure causing increased efficiency and the rocket or projectile to go higher. The shape of the upper chamber (4) causes the pressure to be consolidated by focusing the pressure into an upside-down funnel. This also magnifies, focuses and amplifies pressure which causes the rocket to go higher.
Inside the chamber (3) is a spark gap (10). The spark gap (10) is connected by an electrical cable (16) containing at least two electrical wires to a power source (7). The cable (16) has sufficient length to permit the spark power source (7) to be a safe distance away, for example at least three feet away, from the chamber (3) and the projectile (15). The spark power source (7) may be activated to trigger the spark gap (10), for example by using a switch or a button.
The projectile (15) has a closed top end and an open bottom end, and is shaped to fit in a slidable way over the tube (1).
In an embodiment an activating device (6), such as a lever, is included in the apparatus to manipulate the aerosol spray device (13) containing a flammable liquid in a controlled manner such that the chamber (3) is filled with some of the flammable liquid.
In an embodiment the input port (5) configured to connect to the aerosol spray device (13) has a specially keyed nozzle. In this embodiment the specially keyed nozzle will only connect to a specific aerosol spray device (13).
In an embodiment the flammable liquid is comprised of hydrotreated light distillates (petroleum), butane, hydrofluorocarbon 152a, propane, fragrance, isobutane, and amyl cinnamal.
In an embodiment the projectile launcher apparatus of
The air pump (11) may then be used to pump air into the chamber (3) (Step 102), thereby expelling some residual propellant, for example residual propellant from a previous launch or a failed launch or an aborted launch.
The projectile (15) may then be placed back on the tube (1) (step 103).
Some flammable liquid from the aerosol spray device (13) may then be sprayed into the chamber (3), for example by using an aerosol spray device activator (6), thereby yielding a mixture of air and atomized flammable liquid (14) in the chamber (3) (Step 104).
The projectile apparatus and projectile (15) may then be pointed in a desired direction that is not downwards (Step 105).
Multiple chambers can be stacked and fueled separately. This can greatly increase pressure and volume of reaction, to launch much bigger projectiles with heavier payloads.
The spark power source (7) may then be activated, for example by using a switch (Step 106), thereby giving rise to a spark across the spark gap (10). This ignites the mixture of air and atomized flammable liquid (14), thereby causing a rapid expansion of exhaust gas in the chamber (3). Some of the exhaust gas then passes rapidly out the tube (1), thereby propelling the projectile (15) rapidly away from the projectile launcher apparatus.
In an embodiment the projectile launcher apparatus of
The air pump (11) may then be used to pump air into the chamber (3) (Step 202), thereby expelling some residual or burnt propellant, for example residual propellant from a previous launch or a failed launch or an aborted launch.
The projectile (15) may then be placed back on the tube (1) (step 203).
Some flammable liquid from the aerosol spray device (13) may then be sprayed into the chamber (3), for example by using an aerosol spray device activator (6), thereby yielding a mixture of air and atomized flammable liquid (14) in the chamber (3) (Step 204).
To abort the launch attempt the projectile (15) may then be removed from the tube (1) (Step 205).
The air pump (11) may then be used to pump air into the chamber (3) (Step 206), thereby expelling some of the mixture of air and atomized flammable liquid (14) out of the chamber (3).
The above-described apparatus and methods for using the apparatus allow for safe, repeatable, and fun projectile launches.
Those skilled in the art will have no difficulty devising obvious variants and improvements of the disclosure described above, all of which are intended to be encompassed within the scope of the patent application.
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Number | Date | Country | |
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20200038769 A1 | Feb 2020 | US |
Number | Date | Country | |
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62677096 | May 2018 | US |