| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 1 | 液体炸弹 | CN201610569026.7 | 2016-07-12 | CN106066136A | 2016-11-02 | 李志 |
| 一种液体炸弹，它是选取可以承受一定压力的材质的薄板，根据需要的威力大小制成一定体积的圆形或椭圆形的容器，将一定量的低温液体(如液体空气)充入该容器中，并留有一定的气相空间，然后将该容器密封，低温液体会在常温下迅速挥发成为气体，该容器中的气体压力便会迅速增大，当气体压力增大至超过圆形或椭圆形的容器所能承受的压力时，圆形或椭圆形的容器就会发生突然的破裂而发生爆炸，这种突然的爆炸所产生的冲击波要远远大于炸药爆炸所产生的冲击波，因而更具有杀伤力。 | ||||||
| 2 | Missile launcher | JP51006489 | 1989-06-19 | JPH0646159B2 | 1994-06-15 | FUROTSUKU TOOMASU JII; REISHINGAA SUKOTSUTO DEI |
| 3 | JPH03501878A - | JP51006489 | 1989-06-19 | JPH03501878A | 1991-04-25 | |
| 4 | MISSILE LAUNCHER | EP89910756.0 | 1989-06-19 | EP0380657A1 | 1990-08-08 | FLOCK, Thomas, G.; BAYSINGER, Scott, D. |
| Un sac élastique (13) allongé étanche aux gaz comporte une extrémité ouverte fixée à un gonfleur/propulseur (16) pouvant être actionné pour remplir rapidement le sac de gaz. Le sac et le gonfleur/propulseur sont situés à l'intérieur d'un tube (11) lance-missiles, le sac gonflant lorsqu'il se remplit de gaz de manière à lancer le missile (10). | ||||||
| 5 | Cartridge containing a projectile and a ramming device | EP86304187.7 | 1986-06-02 | EP0204539B1 | 1989-05-10 | Barton, Arthur Edward Mackenzie; Meston, Spencer Davidson |
| 6 | REDUCED FIRING SIGNATURE WEAPON CARTRIDGE | US11880384 | 2007-07-20 | US20110083575A1 | 2011-04-14 | Frank J. Dindl; Kenneth R. Jones |
| A reduced signature weapon cartridge is provided which, when fired, produces little or no muzzle blast or noise signature. In particular, a reduced signature weapon cartridge of the present invention comprises a movable piston disposed within the cartridge, disposed in between the high pressure chamber and the projectile. When fired, propellant gases rapidly force the piston forward within the cartridge case, thereby launching the projectile at a subsonic velocity, thereby eliminating the conventional noise signature associated with supersonic velocities. Thereafter, the propellant gases are slowly released from the cartridge case via perforations formed within the piston, grooves formed in the periphery of the piston, or via a gap between the piston and cartridge wall, thereby reducing or eliminating the conventional muzzle blast. | ||||||
| 7 | Afterburning reduction | US801023 | 1985-11-22 | US4630683A | 1986-12-23 | Barry D. Allan |
| A method of reducing the visible flash caused from afterburning of a rocketotor by injecting a fire extinguishing suppressant material into the exhaust gases from the rocket motor and injecting the fire extinguishing suppressant material near the exhaust end of the rocket motor nozzle and about an internal periphery of the exhaust nozzle. An effective fire extinguisher suppressant includes fluoro halogenated carbon compounds and specifically CBrF.sub.3. | ||||||
| 8 | Projectile-firing weapons | US193598 | 1980-10-03 | US4406209A | 1983-09-27 | Francois Arene; Bernard Castagner; Jean-Serge Peyroux |
| A projectile-firing weapon wherein the firing of the projectile is brought about, at least partly, by the unfolding of a flexible bag under the effect of a pressure within the bag. | ||||||
| 9 | Launching device for projectiles | US3800656D | 1971-11-04 | US3800656A | 1974-04-02 | SCHNABELE W |
| A launching device for a projectile comprises a barrel having an interior projectile chamber directly adjacent a muzzle opening at one end. The projectile is positioned behind the muzzle opening and is sealed from a propellant chamber directly behind the projectile chamber by means of a sealing member which permits expansion of the propellant chamber during the discharge of the projectile through the muzzle opening. The sealing member moves outwardly along the interior of the barrel, but is maintained in sealing engagement with the barrel to close off the propulsion chmaber even after firing of the missile. In one embodiment, the sealing member comprises a piston which moves along the interior of the barrel and is retained at the outer end thereof by retaining elements formed inwardly at the muzzle opening. In another arrangement, the sealing means comprises a membrane having its outer edges sealed around the periphery of the end of the barrel at the muzzle opening but extending backwardly to envelop the missile and to seal off the remaining portion of the interior of the barrel from the missile at the propulsion chamber. The propulsion chamber may be sealed at opposite sides by a piston arranged on each side of a propulsion charge or means for generating and introducing high pressure gases between the piston at each end. Instead of a piston, the device may comprise a membrane which is engageable with the barrel or even a flexible member in the form of a bellows which is secured to the interior of the barrel and expands outwardly in one or both directions.
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| 10 | Firing equipment | US3500715D | 1968-09-30 | US3500715A | 1970-03-17 | BATOU BORIS |
| 11 | Projectile | US58780966 | 1966-10-19 | US3417697A | 1968-12-24 | LUCY CARL F; WOODS HAROLD J |
| 12 | Zip cartridge | US44394365 | 1965-03-30 | US3249010A | 1966-05-03 | BLAIN JIM W; LEAMAN AUDLEY B; NELSON ROBERT A; ZAPF DONALD C |
| 13 | Projectile | US20832662 | 1962-07-09 | US3134330A | 1964-05-26 | BORIS BATOU |
| 14 | Propulsion unit fireable from an enclosure | US709908 | 1991-05-30 | US5099764A | 1992-03-31 | Malcolm K. Dale; Thomas O'Brien; David Wilson; Christopher Rinaldi |
| A recoilless propulsion unit fireable from an enclosure utilizes a releasy sealed multi-holed nozzle member to expel a fluid therefrom by a closed-breech type piston that is activated by a propellant charge. The propulsion unit after firing has minimum impact of overpressure, noise on both the launch crew and has no flash or smoke signature emitted therefrom. | ||||||
| 15 | Device for flash suppression of a rocket motor | US747742 | 1985-06-24 | US4630539A | 1986-12-23 | Lawrence B. Thorn; Robert E. Betts |
| A device in which a solid suppressant is ablated and dispensed into the gs of a main burning rocket motor in which a fast burning smokeless type solid propellant is burning to allow the suppressant to control afterburning of the gases from the burning solid propellant and the suppressant being dispensed by a sustained action igniter pyrotechnic that is also used to ignite the main motor solid propellant. | ||||||
| 16 | Mechanical noise suppressor for small rocket motors | US183604 | 1980-09-02 | US4319660A | 1982-03-16 | Charles R. Bishop |
| A noise suppressor for small rocket motors including a plurality of perfoed metal cylinders disposed in concentric relation and secured to a support plate. A noise suppression material is disposed in the chamber of each adjacent cylinder. Noise suppression material is also disposed in the center cylinder and is expelled by the rocket motor thrust. A collar on the support plate secures the motor to the suppressor. | ||||||
| 17 | Percussion ignition system for a smokeless, flashless, low noise cartridge | US533438 | 1974-12-17 | US3967552A | 1976-07-06 | Charles P. Settles; Edward R. Evans |
| A sealed combustion cartridge mechanism is used to propel a projectile ando ignite an impact percussion type primer which in turn activates a delay train located in the projectile. The forward end of a cup seal telescoping propelling member is axially dimpled so that it will hold the primer in close proximity to the delay train. The convex portion of the dimple protrudes toward a movable propellant cup slidably contained within the closed combustion telescoping member. The propellant cup upon ignition of the propellant is forcibly thrown, by the rapidly expanding gases, against the protruding dimple and the rear of the projectile. The kinetic energy of impact of the propellant cup against the dimpled surface of the telescoping member is utilized not only to help the expanding telescoped cup seal member drive the projectile from the cartridge, but also to ignite the primer and start the delay train of the propelled round. | ||||||
| 18 | Silent launch gun for projectiles | US29187872 | 1972-09-25 | US3837107A | 1974-09-24 | SWAIM F; WIDMAYER R |
| A silent launching system for projectiles having a launch tube with a breech to receive a special cartridge and a constricted muzzle and containing a sabot. The projectile, such as an arrow, is loaded tail-first into the muzzle to contact the sabot. When the cartridge is fired, the sabot and projectile accelerate toward the muzzle, where the sabot is arrested in the constriction and the projectile continues out the muzzle to the target. The arrested sabot traps the expanding gases within the launch tube, providing a flashless, smokeless, and noiseless launch.
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| 19 | Grenade round with means giving forward momentum to the fired case | US3738271D | 1970-12-18 | US3738271A | 1973-06-12 | LA COSTA N |
| A grenade round containing a case with a telescopic tubular actuator, which is extended responsive to propellant discharge therein against the forwardly disposed grenade, is provided with a propellant wad which is unrolled and then is freed for forward impact against the extended actuator by residual discharge gas pressure to give forward momentum to the case after the grenade is propelled therefrom.
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| 20 | Injector assembly for eliminating the smoke trail of a solid propellant rocket motor | US3491539D | 1967-07-13 | US3491539A | 1970-01-27 | MANGUM GRAFTON F |
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