Claims
- 1. A paintball marker powered by an engine that generates combustion-gas-pressure pulses transmitted directly to paintballs.
- 2. The marker of claim 1 in which the engine includes a combustion chamber adapted for receiving a charge of fuel and air and a combustion accelerating system for increasing a burn rate of the charge of fuel and air.
- 3. The marker of claim 2 in which the combustion accelerating system includes a displacer that redistributes space between a mixing chamber and the combustion chamber.
- 4. The marker of claim 3 including an ignition timing system that adjusts the timing between movement of the displacer and ignition of the charge in the combustion chamber.
- 5. The marker of claim 3 including an actuating system that relatively moves the displacer in a first direction for expanding the mixing chamber and contracting the combustion chamber and in a second direction for contracting the mixing chamber and expanding the combustion chamber.
- 6. The marker of claim 5 in which the actuating system includes a biasing mechanism that relatively moves the displacer in the first direction for admitting air into the mixing chamber and expelling exhaust gases from the combustion chamber.
- 7. The marker of claim 5 in which the actuating system includes a rechargeable source of potential energy that can be used to move the displacer in the second direction for transferring a charge of fuel and air from the mixing chamber into the combustion chamber.
- 8. The marker of claim 7 in which the actuating system includes a resettable actuator that recharges the rechargeable source.
- 9. The marker of claim 8 in which the rechargeable source includes a main spring and the resettable actuator restores the main spring to an initial latched position.
- 10. The marker of claim 9 in which the resettable actuator is a manual actuator.
- 11. The marker of claim 10 in which the manual actuator can be released from a latched position for allowing the main spring to move the displacer in the second direction.
- 12. The marker of claim 9 in which the resettable actuator includes a plunger that is exposed to combustion pressures within the combustion chamber for restoring the main spring to the initial latched position.
- 13. The marker of claim 8 in which the resettable actuator includes a valve member that regulates discharges of the combustion-gas-pressure pulses from the combustion chamber.
- 14. The marker of claim 13 in which the displacer includes an aperture for discharging the combustion-gas-pressure pulses from the combustion chamber, and the valve member regulates an opening and closing of the aperture.
- 15. The marker of claim 14 in which the valve member is shaped in relation to the aperture for varying an opening size of the aperture as a function of the position of the valve member.
- 16. The marker of claim 14 in which the valve member is biased by the rechargeable source into a closed position against the aperture and includes an area that is exposed to combustion pressures of the combustion chamber.
- 17. The marker of claim 16 in which the valve member closes the aperture until a threshold combustion pressure is reached that overcomes the bias of the rechargeable source.
- 18. The marker of claim 13 in which at least one aperture is formed in the combustion chamber independently of the displacer for directing the combustion-gas-pressure pulses from the combustion chamber and the valve member regulates an opening and closing of the aperture.
- 19. The marker of claim 18 in which the at least one aperture is formed in a peripheral surface of the combustion chamber and the valve member includes a mating peripheral surface for opening and closing the aperture.
- 20. A paintball marker having an onboard gas-powered engine that discharges combustion gases through a barrel.
- 21. The marker of claim 20 in which the combustion gases are directed in the form of gas pressure pulses from a combustion chamber into the barrel for propelling individual paintballs.
- 22. The marker of claim 21 in which the combustion gases are allowed to rise in pressure within a confined volume of space before being released through a valve into the barrel for applying an enhanced pressure pulse to the paintball.
- 23. The marker of claim 21 in which a discharge conduit conveys the gas pressure pulses from the combustion chamber to the barrel.
- 24. The marker of claim 23 in which the valve is located between the combustion chamber and the discharge conduit for regulating the release of pressure pulses from the combustion chamber.
- 25. The marker of claim 21 including an automatic loading system incorporates a bolt for alternately admitting and blocking the entrance of paintballs into the barrel from a magazine holding a plurality of paint balls.
- 26. The marker of claim 25 in which the bolt moves together with a displacer that redistributes space between a mixing chamber and the combustion chamber.
- 27. The marker of claim 26 in which the bolt is moveable together with the displacer in a first direction that expands the mixing chamber, contracts the combustion chamber, and opens a breech for admitting a paintball from the magazine.
- 28. The marker of claim 27 in which the bolt is moveable together with the displacer in a second direction that contracts the mixing chamber, expands the combustion chamber, and closes the breech for blocking the entrance of paintballs from the magazine.
- 29. The marker of claim 28 in with the movement of the bolt in the second direction also advances the paintball into a launch position within the barrel.
- 30. The marker of claim 26 in which the bolt has the form of a discharge conduit that conveys the gas pressure pulses from the combustion chamber to the barrel.
- 31. A paintball marker having a pump displacer driven by combustion gases of a gas-powered engine for pumping ambient air through a barrel, wherein the ambient air is compressed within a confined volume of space before being released through a valve into the barrel for shaping pressure pulses transmitted to the paintball.
- 32. The marker of claim 31 in which the pump displacer is a part of a displacement pump driven by the combustion gases for compressing the ambient air.
- 33. The marker of claim 32 in which the barrel has an axis along which the paintball is launched and the pump displacer is moveable along the barrel axis for compressing the ambient air.
- 34. The marker of claim 32 in which the displacement pump is located between a combustion chamber and the valve for converting combustion gases into an ambient air pressure pulse released by the valve into the barrel for launching the paintball.
- 35. A projectile launcher comprising:
a combustion accelerating system for increasing a burn rate of a charge of fuel and air including:
a mixing chamber; a combustion chamber; and a displacer that redistributes space between the mixing chamber and the combustion chamber; a barrel adapted for launching projectiles; and the combustion chamber being connected to the barrel so that combustion gases generated within the combustion chamber are directed in the form of gas pressure pulses from the combustion chamber into the barrel for propelling the projectiles.
- 36. The launcher of claim 35 further comprising a discharge conduit that conveys the gas pressure pulses from the combustion chamber to the barrel.
- 37. The launcher of claim 36 in which the discharge conduit is connected to the combustion chamber through an aperture formed through the displacer.
- 38. The launcher of claim 36 further comprising a valve located between the combustion chamber and the discharge conduit that provides for allowing combustion gas pressure to rise within a confined volume of the combustion chamber before releasing the combustion gases into the discharge conduit for generating enhanced pressure pulses for launching the projectiles from the barrel.
- 39. The launcher of claim 38 in which the valve includes a valve member that is moveable between a closed and open position by exposure to the combustion gases.
- 40. The launcher of claim 35 further comprising an ignition timing system that adjusts the timing between movement of the displacer and ignition of the charge in the combustion chamber.
- 41. The launcher of claim 35 in which the barrel has an axis along which the projectiles are launched and the displacer is moveable along the axis of the barrel.
- 42. The launcher of claim 35 further comprising an automatic loading system incorporating a bolt for alternately admitting and blocking the entrance of projectiles into the barrel from a magazine holding a plurality of projectiles, and the bolt being moveable together with the displacer that redistributes space between the mixing chamber and the combustion chamber.
- 43. The launcher of claim 42 further comprising a discharge conduit that conveys the gas pressure pulses from the combustion chamber to the barrel, and in which the discharge conduit is formed through the bolt.
- 44. The launcher of claim 35 including an actuating system that relatively moves the displacer in a first direction for expanding the mixing chamber and contracting the combustion chamber and in a second direction for contracting the mixing chamber and expanding the combustion chamber.
- 45. The launcher of claim 44 in which the actuating system includes a biasing mechanism that relatively moves the displacer in the first direction for admitting air into the mixing chamber and expelling exhaust gases from the combustion chamber.
- 46. The launcher of claim 44 in which the actuating system includes a rechargeable source of potential energy that can be used to move the displacer in the second direction for transferring a charge of fuel and air from the mixing chamber into the combustion chamber.
- 47. The launcher of claim 46 in which the actuating system includes a resettable actuator that recharges the rechargeable source.
- 48. The launcher of claim 47 in which the resettable actuator is a manual actuator for recharging the rechargeable source.
- 49. The launcher of claim 47 in which the resettable actuator is an automatic actuator that is exposed to combustion pressures within the combustion chamber for recharging the rechargeable source.
- 50. A projectile launcher comprising:
a barrel adapted for launching projectiles along an axis; a gas-powered engine that generates combustion gases by igniting a charge of fuel and air; a displacement pump driven by the combustion gases for pumping a non-combustion gas through the barrel for launching the projectile; and the engine and the displacement pump being aligned along the axis of the barrel.
- 51. The launcher of claim 50 in which the displacement pump includes a pump displacer that is moveable along the axis of the barrel for converting a combustion-gas-pressure pulse into a non-combustion-gas-pressure pulse for launching the projectiles.
- 52. The launcher of claim 51 further comprising a valve located between a pumping chamber of the displacement pump and the barrel for compressing the non-combustion gas within a confined volume of the pumping chamber before releasing the non-combustion gas into the barrel for generating an enhanced gas pressure pulse for launching the projectiles.
- 53. The launcher of claim 50 further comprising a combustion accelerating system that redistributes space between a mixing chamber and a combustion chamber.
- 54. The launcher of claim 53 in which the combustion accelerating system includes a mixing piston that is moveable along the axis of the barrel for redistributing space between the mixing chamber and the combustion chamber.
- 55. The launcher of claim 54 in which an aperture through the mixing piston allows the combustion gases to exit the combustion chamber through the mixing piston along a pathway to the barrel.
- 56. An automatic loading system for a projectile launcher including a bolt coupled to a displacer of a combustion-gas-powered engine for alternately admitting and blocking the entrance of projectiles into a barrel from a magazine holding a plurality of projectiles.
- 57. The loading system of claim 56 in which the displacer is a mixing piston that redistributes space between a mixing chamber and a combustion chamber.
- 58. The loading system of claim 57 in which the bolt is formed by an air discharge conduit that directs combustion gases from the combustion chamber to the barrel through an aperture in the mixing piston.
- 59. The loading system of claim 57 in which the bolt is moveable together with the mixing piston in a first direction that expands the mixing chamber, contracts the combustion chamber, and opens a breech for admitting a projectile from the magazine.
- 60. The loading system of claim 59 in which the bolt is moveable together with the displacer in a second direction that contracts the mixing chamber, expands the combustion chamber, and closes the breech for blocking the entrance of projectiles from the magazine.
- 61. The loading system of claim 60 in with the movement of the bolt in the second direction also advances the projectile into a launch position within the barrel.
- 62. A pulse-shaping system for a projectile launcher comprising:
a combustion chamber of a combustion-gas-powered engine connected to a barrel of the launcher for communicating a pressure pulse generated within the combustion chamber to the barrel for launching a projectile; and a valve interrupting the connection between the combustion chamber and the barrel for shaping a pressure profile of the pressure pulse before launching the projectile.
- 63. The pulse-shaping system of claim 62 in which the combustion chamber includes an exit port and the valve regulates flows of combustion gas through the exit port.
- 64. The pulse-shaping system of claim 63 in which the valve is closed at a start of combustion within the combustion chamber and is opened by combustion pressure within the combustion chamber.
- 65. The pulse-shaping system of claim 62 in which the valve includes two relatively moveable members that provide for varying flow rates through the valve as the valve is opened between fully closed and fully opened positions.
- 66. A combustion accelerating system for a projectile launcher comprising:
a combustion chamber; a mixing chamber; a displacer that redistributes space between the mixing chamber and the combustion chamber; a discharge conduit that conveys combustion pressure pulses from the combustion chamber for powering the launch of projectiles; and an actuating system that relatively moves the displacer in a first direction for expanding the mixing chamber and contracting the combustion chamber and in a second direction for contracting the mixing chamber and expanding the combustion chamber.
- 67. The accelerating system of claim 66 in which the actuating system includes a biasing mechanism that relatively moves the displacer in the first direction for admitting air into the mixing chamber and expelling exhaust gases from the combustion chamber.
- 68. The accelerating system of claim 66 in which the actuating system includes a rechargeable source of potential energy that can be used to move the displacer in the second direction for transferring a charge of fuel and air from the mixing chamber into the combustion chamber.
- 69. The accelerating system of claim 68 in which the actuating system includes a resettable actuator that recharges the rechargeable source.
- 70. The accelerating system of claim 69 in which the resettable actuator is a manual actuator for recharging the rechargeable source.
- 71. The accelerating system of claim 69 in which the resettable actuator is an automatic actuator that is exposed to combustion pressures within the combustion chamber for recharging the rechargeable source.
- 72. The accelerating system of claim 66 in which the displacer includes a mixing piston that is moveable along an axis of a barrel from which the projectiles are launched.
- 73. The accelerating system of claim 72 in which an aperture through the mixing piston allows combustion gases to exit the combustion chamber through the mixing piston along the discharge conduit to the barrel.
- 74. The accelerating system of claim 66 in which the discharge conduit that conveys combustion pressure pulses from the combustion chamber into a barrel for launching the projectiles.
- 75. The accelerating system of claim 66 further comprising an ignition timing system that adjusts the timing between movement of the displacer and ignition of a charge of fuel and air in the combustion chamber.
- 76. A method of launching paintballs from a paintball marker including the steps of:
loading a paintball into a paintball marker; and utilizing pressures generated by combusting a fuel and air mixture to launch the paintball from the marker.
- 77. The method of claim 76 including a further step of drawing the fuel from a supply of fuel mounted on the marker.
- 78. The method of claim 76 including a further step of turbulating the fuel and air mixture in advance of its combustion.
- 79. The method of claim 78 in which the step of loading the paintball is linked to the step of turbulating the fuel and air mixture by a physical connection between apparatus for turbulating the mixture and apparatus for loading the paintball.
- 80. The method of claim 76 including a further step of regulating a pressure profile of pressure pulses generated by the combustion of the fuel and air mix.
- 81. A method of launching projectiles from a projectile launcher comprising the steps of:
loading a projectile into a projectile launcher having an on-board combustion-gas-powered engine; igniting a charge of fuel and air within the engine for generating a combustion-gas-pressure pulse; directing the combustion-gas-pressure pulse through a pulse-shaping system for optimizing a profile of the pressure pulse; and applying the optimized pressure pulse for launching the projectile.
- 82. The method of claim 81 in which the step of directing includes directing the combustion-gas-pressure pulse through a valve for shaping the pressure pulse.
- 83. The method of claim 82 in which the step of directing includes using the valve to confine the combustion gases within a combustion chamber until a threshold pressure is reached within the combustion chamber.
CROSS-REFERENCE TO RELATED APPLICATIONS
[0001] Priority is claimed to Provisional Application No. 60/443,520, filed 29 Jan. 2003, the disclosure of which is hereby incorporated by reference.
Provisional Applications (1)
|
Number |
Date |
Country |
|
60443520 |
Jan 2003 |
US |