Light gas gun projectile
10119780 ยท 2018-11-06
Inventors
Cpc classification
F41B11/64
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F41B11/646
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F42B6/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F41B11/723
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F41B11/68
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F41A21/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F41A13/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F42B12/74
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F41A21/28
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F42B30/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F41B11/73
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F42B6/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F41B11/723
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F41B11/68
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F41A1/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F41A21/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F41B11/73
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F41A21/28
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
An improved light gas gun launches a projectile in a light gas atmosphere as it travels through a frictionless barrel to achieve high muzzle velocities, decreased acoustic signatures, and increased ranges. The light gas atmosphere is introduced by a purge valve prior to firing or by a muzzle valve that holds a positive light gas pressure on the barrel and breech. The muzzle valve also routes the majority of propellant gases through a suppression canister, reducing the light gas gun's acoustic signature. The frictionless barrel uses light gas propellant routed through gas bearings to keep the projectile centered in the barrel and preclude the projectile from contacting the barrel walls, eliminating barrel wear. The system includes a projectile assembly that stores light gas from the firing and injects it into the boundary layer, reducing drag, increasing range and lethality, and decreasing acoustic signature of the projectile down range.
Claims
1. A projectile assembly comprising: a projectile body generally ogive in shape at the forward end with a rounded nose and a boat tail shape toward the rear of the projectile; said projectile body is manufactured in two parts, the forward projectile body and the aft projectile body; said forward projectile body having a bore with a predetermined diameter extending a predetermined depth from a flat aft face, the bore being internally threaded; said aft projectile body having a through-bore with a second predetermined diameter, the through-bore having a taper at the rear of said aft projectile body and the aft projectile body is threaded externally to allow said forward projectile body and aft projectile body to be screwed together; said aft projectile body contains a spring loaded valve that seats in the taper at the aft end of said aft projectile body; said spring loaded valve opens the projectile body to accept and store high pressure light gas internally when light gas pressure externally is greater than the gas pressure internal to said projectile body; said spring loaded valve closes when external pressure drops below the pressure internal to said projectile assembly; said projectile body comprised of sintered metal with appropriately coarse grains to allow light gas to flow through the walls of said projectile body, injecting light gas into a boundary layer surrounding said projectile assembly during flight, thereby reducing aerodynamic drag and ballistic disturbances as said projectile assembly travels downrange, which increases range and accuracy while decreasing acoustic signature of said projectile assembly as it travels through the atmosphere; said projectile body having a forward center of gravity and rearward center of pressure to increase ballistic stability in flight through all flight regimes ranging from supersonic, transonic, to subsonic velocities.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1)
(2)
(3)
(4)
(5)
(6)
DEFINITIONS
(7) Aft Projectile Body. The rearward piece of the projectile assembly that contains the spring loaded valve and the projectile spring. The aft projectile body is hollow and threaded into the forward projectile body. Assembled, they make up the projectile assembly.
(8) Barrel Assembly. A two piece barrel made up of an inner tube and an outer tube. The inner tube is press fit into the outer tube and has channels cut into the outer diameter and holes drilled in the channels that allow light gas to flow down the barrel and into the interior of the inner tube, acting as gas bearings to keep the round centered in the barrel.
(9) Breech. The cylindrical cavity where the projectile or projectile assembly rests prior to firing the light gas gun.
(10) Breech Assembly. Made up of the breech body, the receiver locking bolt, the trigger valve, and the receiver safety. The breech assembly is mechanically connected to the barrel assembly on the front or muzzle end and to the light gas source.
(11) Breech Assembly Body. The part to which the receiver locking bolt, trigger valve, receiver safety, and barrel assembly are connected. The breech is bored into the breech assembly body and aligned with the barrel assembly.
(12) Channel. Rectangular grooves milled into the outside wall of the inner tube to allow light gas to flow the length of the barrel, supplying gas to the gas bearing ports drilled into the bottom of the channels. Channels are milled at angles in embodiment one and three in order to create a vortex to spin stabilize the round, but normal to the outside wall for embodiments two and four where spin stabilization is not required.
(13) CO.sub.2 Piston. The driving piston in the dual piston assembly shown in embodiment four, and part of the best mode. Larger in diameter than the light gas piston so as to multiply the force on the light gas piston. In addition to using high pressure CO.sub.2, it is assisted by a pressure boosting spring.
(14) Dual Piston Assembly. The mechanism that provides the light gas propellant to the breech assembly in embodiment four. It consists of a CO.sub.2 piston, a light gas piston, mechanisms for actuating the assembly, and the necessary gas connections and vents to prepare the assembly for firing.
(15) Forward Projectile Body. The forward piece of the projectile assembly, threaded to accept the aft projectile body, and bored down the centerline to provide a path for light gas to the meplat of the round.
(16) Gas Bearings. Holes in the inner tube, aligned the length of the barrel, equally spaced around the circumference of the inner tube, and connected by channels running from the breech end of the inner tube to just shy of the muzzle end of the inner tube. The gas bearings direct high pressure light gas axially inward, toward the round, keeping it centered in the inner tube.
(17) Gas Bearing Port. One of the holes drilled in the inner tube that directs light gas toward the projectile.
(18) Gas Directing Tube. The hole bored into the forward projectile body to direct light gas to the meplat of the round, ensuring sufficient light gas flow into the boundary layer at the front of the round.
(19) Inner Tube. The interior cylinder of the barrel assembly, press fit into the outer tube, with channels milled the length of the tube and gas bearing ports drilled at specified distances, centered in the channels.
(20) Leaf Bore. A hole bored in the muzzle valve leaf that allows the round to exit the light gas gun when aligned with the barrel assembly bore and the other muzzle valve leaves.
(21) Light Gas. Elemental helium or molecular hydrogen.
(22) Light Gas Piston. The piston that compresses the light gas used as the propellant in embodiment four. Driven by the CO.sub.2 piston. It is also used to reset the CO.sub.2 piston after firing by venting the gas in the CO.sub.2 piston and driving both pistons and compressing the pressure boosting spring back to their firing position with light gas from the supply source.
(23) Muzzle Valve. The valve that opens to allow the round to exit the light gas gun and closes to retain unused light gas. The muzzle valve and opposing multi-leaf valve are used interchangeably in embodiment four. The opposing multi-leaf valve is a specific type of muzzle valve.
(24) Muzzle Valve Assembly. Consists of a muzzle valve body, a muzzle valve, a plurality of muzzle vent valves, hydraulic actuators to drive the muzzle valve, and a suppression canister. The assembly seals the light gas gun in order to hold a positive pressure in the breech and barrel. Opens the muzzle valve to allow the round to exit and to vent propellant gases to the atmosphere through the suppression canister. The muzzle valve assembly is mechanically connected to the barrel assembly on the muzzle end.
(25) Muzzle Valve Body. The structure to which all other muzzle valve components are attached.
(26) Muzzle Valve Chamber. The space between the end of the barrel assembly and the muzzle valve where propellant light gas is directed to the muzzle vent valves.
(27) Muzzle Valve Leaf. A component of the specific opposing multi-leaf valve used in embodiments three and four. A plurality of the leaves are used to allow the round to leave the light gas gun when they are hydraulically driven together to align the holes bored in the individual leaves with the bore of the barrel. When hydraulic pressure is released, the leaves are then reset by springs that drive them back into their pre-fire positions, sealing the muzzle.
(28) Muzzle Vent Valve. A small pressure relief valve that opens whenever pressure in the muzzle chamber rises above a predetermined level. The muzzle vent valve vents to the atmosphere through the suppression chamber.
(29) Opposing Multi-Leaf Valve. The specific type of muzzle valve used in the third and fourth embodiments, designed to minimize the impulse imparted to the light gas gun while opening and closing. May be used interchangeably with muzzle valve.
(30) Outer Tube. The exterior cylinder of the barrel assembly. Attached to the breech assembly and, in embodiments three and four, the muzzle valve assembly. The inner tube is press fit into the outer tube.
(31) Projectile. A standard caliber bullet or artillery round
(32) Projectile Assembly. A specialized bullet that stores high pressure light gas that it injects into the boundary layer as the bullet travels downrange.
(33) Projectile Spring. The spring in the projectile assembly that keeps the spring loaded valve seated. The spring is compressed when external pressure exceeds the projectile assembly internal pressure plus the compression strength of the spring, opening the spring loaded valve. When the pressures are equalized the spring loaded valve closes.
(34) Purge Valve. A valve that is triggered in the firing sequence to put medium pressure light gas into the front of the breech. The light gas flows long enough to ensure the barrel is clear of air and filled with light gas. The valve closes as the trigger valve opens.
(35) Receiver Locking Bolt. The mechanism that allows a round to be loaded into the breech. It unlocks, moves toward the rear sufficiently far to allow loading of the round, then moves forward after the round is loaded, locks, and seals the breech in preparation for firing.
(36) Receiver Safety. A spring-loaded mechanism that holds the round in place in the breech. It includes a mechanical lock that prevents the round from moving until the firing safety is turned to the fire position. This prevents accidental firing of the round.
(37) Round. Used interchangeably to denote either the projectile or the projectile assembly
(38) Suppression Canister. A hollow cylinder connected to the muzzle valve assembly that surrounds the barrel assembly and is connected to the breech assembly. The cylinder contains baffles and flame retardant foam that allows the light gas entering from the muzzle valve assembly to exit to the atmosphere through vent holes in the side of the cylinder, directing the light gas away from the operator. The baffles and the foam reduce the acoustic signature of the light gas gun and help to prevent contaminants from reaching light gas gun mechanisms.
(39) Suppression Vent. The holes drilled into the side of the suppression canister that direct light gases away from the operator.
(40) Trigger Valve. The valve that controls the light gas flow to the rear of the breech. The trigger valve is actuated with the pull of the trigger to allow high pressure light gas to flow for sufficient time to propel the round out of the barrel.
DETAILED DESCRIPTION OF THE INVENTION
(41) This system description describes four different embodiments of the invention. Each embodiment is representative of different potential applications and will have different means of providing the necessary light gas to be used as the propellant.
(42) The light gas gun of this invention
(43) The first embodiment
(44) The second embodiment,
(45) The second embodiment would also typically use a simple reservoir to provide the light gas propellant. By adding a heater to the reservoir, the light gas could be heated prior to use to increase the speed of sound in the light gas. The hotter light gas would mostly impact the projectile assembly 20 performance by injecting the hotter gas into the boundary layer.
(46) The second embodiment contains the other elements from the first embodiment, the breech assembly
(47) The third embodiment introduces the muzzle valve assembly
(48) The fourth embodiment is the best mode, and includes the projectile assembly 20, the frictionless barrel assembly
(49) There are numerous applications for the different embodiments described herein, including handguns, rifles, ground artillery, naval guns, industrial processes, research, and even orbital launch systems. These different applications might use substantially different methodologies for providing the necessary light gas propellant at the pressures, temperatures, and quantities required, but they all contain the respective elements of the four embodiments. A relatively simple reservoir of light gas large enough to ensure a constant pressure at the firing valve after it is opened might be sufficient for some applications. Others would likely need a two stage piston that could be powered by other pressurized gas, steam, hydraulics or combustive propellants.
First Embodiment
(50) The projectile 10 is loaded into the breech assembly
Second Embodiment
(51) The second embodiment is identical to the first with two exceptions. The projectile assembly 20 is substituted for the known projectile 10. The channels 12 and gas bearing ports 13 are cut and drilled normal to outside wall of the inner tube 15, as it is no longer necessary to impart spin on the projectile assembly 20.
(52) The projectile assembly 20 is loaded in the same fashion as in the first embodiment. When the light gas gun is fired, the pressure behind the projectile assembly 20 increases rapidly. The spring loaded valve 40 in the aft projectile body 41 of the projectile assembly 20 opens as the pressure external to the projectile assembly 20 is greater than the internal pressure plus the compression strength of the projectile spring 43. The spring loaded valve 40 closes as the internal and external pressures equalize. The forward and aft projectile bodies 42/41, as well as the spring loaded valve 40, are constructed of sintered metal. With high pressure light gas stored in the projectile assembly 20, the light gas starts to flow through the walls of the projectile into the boundary layer as the projectile assembly 20 travels down range. A gas directing tube 44, bored along the centerline of the forward projectile body 42 of the projectile assembly 20, ensures there is sufficient gas flow to the meplat of the projectile assembly. The flow rate through the sintered metal of the projectile assembly will ensure that there will be light gas flowing into the boundary layer for the entire flight of the projectile assembly 20.
(53) The projectile assembly shape, center of gravity, and center of pressure provide for stable flight through all regimes of the projectile assembly 20 flight, from supersonic, through transonic, to subsonic. Using a center of gravity significantly forward of the center of pressure eliminates spin drift. Because the projectile assembly 20 has no striations from lands and grooves, the body of the round remains smooth and is subject to fewer air flow disturbances, which also improves accuracy.
(54) The light gas gun's other mechanisms, the frictionless barrel
Third Embodiment
(55) In the third embodiment, the necessity to purge the barrel assembly
(56) The muzzle valve 23 as shown in
(57) As the pressure wave in the barrel assembly
(58) In the third embodiment, the light gas is provided by a piston assembly (not shown) powered by steam, hydraulics, or electrical power. The piston chamber is filled with sufficient light gas that when compressed will produce the desired muzzle velocity. When the trigger signal is received, the motive force moves the piston in the piston chamber, compressing the light gas to the necessary pressure and temperature. When this pressure is reached, the trigger valve 14 opens, providing high pressure light gas to the aft end of the breech 38.
Fourth Embodiment and Best Mode
(59) The fourth embodiment, also offered as the best mode, includes the projectile assembly 20, the frictionless barrel assembly
(60) The projectile assembly 20 is loaded into the breech assembly
(61) When the light gas gun is fired, the pressure behind the projectile assembly 20 increases rapidly. The spring loaded valve 40 in the aft projectile body 41 of the projectile assembly 20, opens as the pressure external to the projectile assembly 20 is greater than the internal pressure plus the compression strength of the projectile spring 43. The valve 40 closes as the internal and external pressures equalize. With high pressure light gas stored in the projectile assembly 20, and because the forward and aft projectile bodies 42/41 and the spring loaded valve 40 are constructed from sintered metal, the light gas starts to flow through the walls of the projectile assembly 20 into the boundary layer as the projectile assembly 20 travels down range. A gas directing tube 44, bored along the centerline of the forward projectile body 42, in the projectile assembly 20 ensures there is sufficient light gas flow to the meplat of the projectile assembly 20. The flow rate through the sintered metal of the projectile assembly 20, will ensure that there will be light gas flowing into the boundary layer for the entire flight of the projectile assembly 20.
(62) The projectile assembly's shape, center of gravity, and center of pressure provide for stable flight through all regimes of the projectile assembly 20 flight, from supersonic, through transonic, to subsonic. Using a center of gravity significantly forward of the center of pressure eliminates spin drift resulting from a spin stabilized round. Because the projectile assembly has no striations from lands and grooves, the body of the projectile assembly 20 remains smooth and is subject to fewer air flow disturbances, which also improves accuracy.
(63) The muzzle valve assembly
(64) The muzzle valve 23 is an opposing multi-leaf valve 28, as shown in
(65) In the fourth embodiment, the light gas is provided by a dual piston assembly
(66) Enablement of the Invention
(67) The barrel assembly
(68) Channels 12 that allow high pressure gas to travel down the barrel are milled on the outside of the inner tube 16. These channels 12 are small compared to the caliber. The interior tube 16 is press fit into the outer tube 15.
(69) There are two different type valves in the muzzle valve assembly
(70) The suppression canister 25 is a cylindrical canister partially filled with porous, non-flammable, acoustic deadening foam. The canister 25 releases the high pressure light gas into the atmosphere through suppression canister vents 26, while minimizing the acoustic signature caused by the escaping gas. The gas must travel through a series of foam baffles to exit the canister 25. The foam also inhibits dust, dirt, and other particulates from entering the rifle barrel and fouling the valves in the muzzle valve assembly
(71) The muzzle valve assembly
(72) The breech assembly
(73) The operator loads the projectile assembly 20 into the breech 38, using compressed CO.sub.2 gas to open the receiver locking bolt 17 and push the round into a loading ramp, then closes and locks the receiver locking bolt 17. The round is held in place by the receiver safety 53, which is a mechanical lock in the breech 38, to keep the round in the correct position in the chamber. This is necessary because the round has a non-cylindrical shape and smaller diameter than the barrel bore. It also provides spacing to let gas escape should there be a leak in trigger valve 14.
(74) High pressure light gas is compressed to the working pressure by the pressure boosting spring 45 and CO.sub.2-driven piston 46. CO.sub.2 is used as the actuating gas because it can be stored at room temperature as a liquid. When the dual piston assembly
(75) The breech assembly
(76) The breech assembly
(77) The projectile assembly 20 is manufactured using standard machining processes. The forward projectile body 42 and aft projectile body 41 are compression molded using sintered metal. Boring and threading are accomplished by standard CNC lathes, as is lapping of the spring loaded valve 40 and seat in the aft projectile body 41. The forward projectile body is bored to a predetermined depth, and then threaded. A second boring operation drills a gas delivery tube 44 to the front of the forward projectile body, just shy of the meplat. This tube helps to distribute light gas to the forward end of the projectile assembly. Assembly starts by installing the valve spring 43 onto the spring loaded valve seat 40 and inserting the spring loaded valve seat 40 into the aft projectile body 41. This assembly is then screwed into the forward projectile body 42. The milling and boring processes tend to close surface pores, but the small hydrogen molecule and elemental helium will still have acceptable flow. Electric discharge machining can be used if the flow is insufficient, instead of using standard milling operations.