US2010313742A1PendingUtilityA1
Projectile Launcher
Est. expiryJun 11, 2029(~2.8 yrs left)· nominal 20-yr term from priority
Inventors:Everson Fortes Silva
F41A 1/04
26
PatentIndex Score
0
Cited by
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References
0
Claims
Abstract
An apparatus to launch projectiles such as paintballs, BBs, grenades, rocket foam and others. The apparatus uses a cordless nailer fuel cell to provide combustible material to a fan-assisted combustion chamber; the combustible is ignited generating energy to propel the projectile out of the apparatus.
Claims
exact text as granted — not AI-modified1 . An apparatus for launching a projectile using a cordless nailer fuel cell and the metering valve provided with, comprising: A main body including a combustion area, a launching area, a fuel cell housing, a fan-assisted combustion chamber, main valve means controlling the air flow into said chamber and the exhausting of gases of combustion from said combustion chamber, means to provide fuel to said fan-assisted combustion chamber igniting means to ignite the fuel to launching a projectile, trigger control means, and a fuel cell release lever.
2 . The apparatus of claim 1 , in which the fuel cell housing is located close to said combustion chamber.
3 . The apparatus of claim 1 , in which said fan-assisted combustion chamber includes at least one fan or at least one rigid or flexible vane and means to operate same, to create of gas transport, turbulence or change of pressure inside of said chamber.
4 . The apparatus of claim 1 , in which the main valve means includes a main valve body with inlet ports and a main valve seal that closes off said combustion chamber during combustion and open said ports to permit scavenging of said combustion chamber.
5 . The apparatus of claim 1 in which the main valve means includes at least one switch to inform its status.
6 . The apparatus of claim 1 , in which the means for providing fuel into said combustion chamber includes the cordless nailer fuel cell and said metering valve to introduce a predetermined quantity of fuel into said combustion chamber.
7 . The apparatus of claim 1 , in which the means to providing fuel into said combustion chamber includes said fuel cell installed in said housing, said metering valve connected to said fuel cell, and said fuel cell release lever surrounding at least part of fuel cell and constructed and arranged to move same, said release lever defining a depending portion adapted to be contacted by mechanic means to move said fuel cell and operate said valve to introduce a metered amount of fuel into the combustion chamber.
8 . The apparatus of claim 1 , in which the trigger control means operates said main valve to control air flow inside of said combustion chamber.
9 . The apparatus of claim 1 , in which said trigger control mean includes at least one electronic switch to control a high voltage coil to provide a high voltage to said spark plug to ignite the fuel in said combustion chamber.
10 . An apparatus for launching foam rockets and projectiles previously loaded in muzzle loading grenade shells using a cordless nailer fuel cell and the metering valve provided with, comprising: A main body including a combustion area, a launching area, a fuel cell housing, main valve means controlling the flow of air into said chamber and the exhausting of the gases of combustion from said combustion chamber, a fan-assisted combustion chamber formed within said main body having said main valve as one wall, and said grenade shell or said rocket as another wall, means to provide fuel to said combustion chamber and ignite same for launching the projectile, trigger control means, a fuel cell release lever, trigger with fuel cell injector lever, and a connection means for grenade shells.
11 . The apparatus of claim 10 , in which the fuel cell housing is attached to said main body, close to said combustion chamber.
12 . The apparatus of claim 10 , in which said fan-assisted combustion chamber includes at least one fan or at least one rigid or flexible vane and controls therefor to operate same, to create of gas transport, turbulence or change of pressure inside of said chamber.
13 . The apparatus of claim 10 , in which the main valve means includes a main valve body with inlet ports and a main valve seal that closes off said combustion chamber during combustion and open said ports to permit scavenging of said combustion chamber.
14 . The apparatus of claim 10 , in which the main valve means includes at least one switch to inform its status.
15 . The apparatus of claim 10 , in which the means for providing fuel into said combustion chamber includes the cordless nailer fuel cell and said metering valve to introduce a predetermined quantity of fuel into said combustion chamber.
16 . The apparatus of claim 10 , in which the means to providing fuel into said combustion chamber includes said fuel cell installed in said housing, said metering valve connected to said fuel cell, and said fuel cell release lever surrounding at least part of fuel cell constructed and arranged to move same, said release lever defining a depending portion adapted to be contacted by the fuel injector lever to move said fuel cell and operate said valve to introduce a metered amount of fuel into the combustion chamber.
17 . The apparatus of claim 10 , in which the trigger control means operates said main valve to control air flow inside of said combustion chamber.
18 . The apparatus of claim 10 , in which said trigger control mean includes at least one electronic switch to control a high voltage coil to provide a high voltage to said spark plug to ignite the fuel in said combustion chamber.
19 . The apparatus of claim 10 , in which The connecting means to connect and lock said grenade shell on muzzle of said main body and a security means to eject the grenade shell when it is not properly locked into said main body.
20 . A method for launching a projectile from a projectile launcher using a cordless nailer fuel cell and the metering valve supplied with, to supply combustible material inside of a fan-assisted combustion chamber, the method comprising the steps of:
(a) Loading a projectile on the launching area; (b) Closing off and sealing the chamber; (c) Starting at least one fan inside of the chamber to cause some turbulence; (d) Operating the fuel cell metering valve to inject the metered amount of fuel inside of said combustion chamber which has to have the appropriate volume to work with the amount of fuel that the fuel cell in use provides; (e) Waiting a predetermined time while the combustible and air are mixed by the fan means; (f) Generating a spark on a spark plug inside of the chamber, which ignites the mixture and propels the projectile out of the launcher; (g) Opening the chamber; (h) Keeping the fan working for predetermined time; (i) Waiting until the gases resultants of combustion are expelled; (j) Waiting until the chamber and launching area cool down; (k) Drawing fresh air within the chamber; (l) Turning the fan off.Join the waitlist — get patent alerts
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