子分类：
| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 121 | Projectile head for a training cartridge | US10919478 | 2004-08-17 | US20050183614A1 | 2005-08-25 | Uwe Naderhoff; Jurgen Kolodzev; Martin Berg |
| A projectile head is provided for a training cartridge having a propulsion unit, with an integrated projectile tail section, which can be used equally for training cartridges as well as combat cartridges of the same caliber size, wherein the projectile tail section is connectable to the projectile head with the aid of an extension on the projectile tail section, the extension is insertable into a receptacle in the projectile head, and the extension contains a recessed area, open on the front, for receiving a warhead detonator. The projectile head has a receptacle in the projectile head for receiving the extension of the projectile tail section, and an end stop which extends into the receptacle. The end stop is for contacting a warhead detonator present on the projectile tail section during assembly of the propulsion unit and the projectile head to prevent the extension from reaching a fully assembled position in the receptacle. | ||||||
| 122 | Hollow training round | US327770 | 1994-10-24 | US5501155A | 1996-03-26 | Michael S. L. Hollis; Fred J. Brandon; Edward W. Kennedy; Edward M. Schmidt |
| A fin stabilized kinetic energy tank training device comprising a project having a nose and having nose and end sections, and constructed of a low density material such as aluminum, and having a hollowed-out section to further reduce weight thereof, so as to minimizing penetration of an armor system on impact thereon. | ||||||
| 123 | Training projectile | US273032 | 1994-07-07 | US5498160A | 1996-03-12 | Anthony Farina; Mark Young |
| The disclosure is of a projectile having a main body, a nose and a tail iuding a flared tail member, the projectile having its center of gravity close to the nose thereof. | ||||||
| 124 | Training device for simulating an unexploded submunition | US5695 | 1993-01-19 | US5326268A | 1994-07-05 | Carl Campagnuolo |
| An acoustic training device for simulating the effects of an unexploded sunition in a tactical engagement simulation system generates an audible signal of a predetermined frequency and duration when handled or otherwise disturbed. A timing circuit allows the referee to place the armed device in the playing field without activating the audible signal. Exemplary submunitions include the M118 Rockeye with an integral horn, the blue series of spherical bomblets, and the M42/46 grenade submunition. | ||||||
| 125 | Parachute recovery system for projectiles | US871158 | 1992-04-20 | USH1150H | 1993-03-02 | Paul L. Fritch |
| An improved parachute recovery system for a gun fired projectile is discld. The projectile has a nose, a payload and a base section. The base section has a hollow cylindrical parachute cannister which is separated from the base section by rearward motion of an internal piston which is actuated by expulsion gas pressure initiated by a time fuze. The parachute cannister is thereby exposed and jettisoned to cause inflation of a parachute attached to the base section so that the parachute floats down in a nose-deployed projectile position for a soft landing and recovery. Also disclosed are alternative embodiments of a projectile base-deployed parachute recovery system. | ||||||
| 126 | Hollow charge shell constructed as drill ammunition | US904031 | 1986-09-05 | US4798144A | 1989-01-17 | Horst Apholt |
| A wing-stabilized hollow charge shell constructed as dummy ammunition and having a tail unit (13) of the same caliber comprises a front explosive chamber (1) and a rear explosive chamber (2) and at the end face of the shell case is provided with a detonator rod (4). The entire shell case, including the detonator rod (4), is formed by parts (3, 5, 7) consisting of the same or similar material which are undetachably connected together. | ||||||
| 127 | Training projectile | US657796 | 1984-10-04 | US4596191A | 1986-06-24 | Gerhard Glotz; Hansjorg Becker; Jurgen Boecker |
| A supersonic nonspinning training projectile has a projectile body extending along an axis and having axially spaced front and rear ends and an aerodynamic rod projecting axially forwardly from the front end of the body. Thus when the projectile is fired axially forward the rod creates turbulence effective laterally on the projectile body at a wind-attack point which moves axially forward from a rear point to a front point as projectile speed drops. It is possible according to the invention to vary the mass distribution of the projectile and thereby displace the center of mass of the projectile axially between the front and rear points. Thus when the wind-attack point moves axially forward of the center of mass the flight of the projectile destabilizes. Such an arrangement works well even at supersonic speeds, so that the projectile can be set to only fly accurately through a relatively short range, as the principal factor determining range after elevation is projectile speed and shape. | ||||||
| 128 | Finless gun-fired practice round | US408316 | 1982-08-16 | US4428294A | 1984-01-31 | Edmund W. Falkowski; Michael J. Kolasa |
| A finless non-spinning round is able to maintain range accuracy and reducedun tube wear by the use of a single base cool burning propellant, an improved shape wear liner, and a warhead projectile configured to position the center of gravity of the warhead so that it is equal to or greater than 0.5 calibers forward of the warhead's aerodynamic center of pressure. | ||||||
| 129 | Training projectile | US749424 | 1976-12-10 | US4133265A | 1979-01-09 | Walter Diesinger; Axel Homburg |
| A training projectile having an auxiliary drive mechanism for counteracting the aerodynamic resistance to which the projectile is exposed during the training flight phase of projectile travel. The auxiliary drive mechanism preferably is in the form of a rocket or jet drive. The training projectile is also provided with a mass so that the ratio of the resultant axial force to the mass of the training projectile is at least approximately equal to the ratio of the resistance force to the mass of a corresponding live projectile during the training flight phase. | ||||||
| 130 | Blank ammunition | JP2005082220 | 2005-03-22 | JP3977846B2 | 2007-09-19 | 清司 大内; 郁雄 小山; 周平 川口; 圭介 足立; 行雄 青田 |
| 131 | Blank ammunition | JP2000051036 | 2000-02-28 | JP3681317B2 | 2005-08-10 | 清司 大内; 郁雄 小山; 周平 川口; 圭介 足立; 行雄 青田 |
| 132 | Blank ammunition | JP2005082220 | 2005-03-22 | JP2005180919A | 2005-07-07 | KAWAGUCHI SHUHEI; ADACHI KEISUKE; KOYAMA IKUO; AOTA YUKIO; OUCHI SEIJI |
| PROBLEM TO BE SOLVED: To provide a blank ammunition, the shell of which is divided and crushed in shooting as smaller broken pieces with a narrowed flying range of the broken pieces, and which can be continuously shot and is easily biodegradable. SOLUTION: This blank ammunition comprises a cap, a cartridge containing a firing agent and a shooting agent, and a point part. The point part has a shell molded of a biodegradable resin, and a filler having a specific gravity of 1-10 and a maximum grain size of 3 mm or less is arranged in the inner part thereof. COPYRIGHT: (C)2005,JPO&NCIPI | ||||||
| 133 | Ammunition for blank cartridge | JP2000051036 | 2000-02-28 | JP2001241899A | 2001-09-07 | KAWAGUCHI SHUHEI; ADACHI KEISUKE; KOYAMA IKUO; AOTA YUKIO; OUCHI SEIJI |
| PROBLEM TO BE SOLVED: To provide an ammunition for a blank cartridge whose projectile unit is split and crushed upon firing and the fragment thereof is crushed into small pieces, while the flying range of the small pieces is narrow and continuous firing can be effected, further, the ammunition is readily biodegradable. SOLUTION: In the ammunition for the blank cartridge consisting of a cartridge unit equipped therein with a detonator, an igniting charge, a propellant and the projectile unit, the projectile unit is constituted of a biodegradable resin and fillers, whose specific gravity is 1-10 and the maximum grain size thereof is smaller than 3 mm. COPYRIGHT: (C)2001,JPO | ||||||
| 134 | Training ammunition | JP14135689 | 1989-06-02 | JPH0814476B2 | 1996-02-14 | 実 光野; 孝昇 松浦; 祐康 片貝 |
| 135 | Tank shells for training | JP22036986 | 1986-09-18 | JPH0752079B2 | 1995-06-05 | 了 小路; 憲一 山本; 修 明石; 促通 有薗; 武 金子 |
| 136 | Training ammunition | JP15675488 | 1988-11-30 | JPH0717999Y2 | 1995-04-26 | 勝 宇治; 秀樹 有馬; 孝昇 松浦; 邦良 檜山; 春雄 清水; 祐康 片貝 |
| 137 | Training ammunition | JP15675588 | 1988-11-30 | JPH0711355Y2 | 1995-03-15 | 秀樹 有馬; 孝昇 松浦; 邦良 桧山; 英孝 河西; 春雄 清水; 清澄 菊地原 |
| 138 | Tank shells for training | JP22037286 | 1986-09-18 | JPH0694999B2 | 1994-11-24 | 了 小路; 憲一 山本; 修 明石; 促通 有薗; 武 金子 |
| 139 | Tank shells for training | JP22037186 | 1986-09-18 | JPH0694998B2 | 1994-11-24 | 了 小路; 憲一 山本; 修 明石; 促通 有薗; 武 金子 |
| 140 | Artillery shell for training | JP8097390 | 1990-03-30 | JPH03282199A | 1991-12-12 | ARAKAWA HARUHIKO |
| PURPOSE: To fly with a flying characteristic same as an actual projectile along a trajectory same as the actual projectile until the projectile arrives at a target and the flying speed is decelerated suddenly after passing through the target to curve downward, shorten the range thereof and drop in a training area by providing the tail of a fuselage with an annular wing. CONSTITUTION: The distribution of sectional areas of flow passages produced by an annular wing 2 and a fuselage 1 is set properly whereby the flow passages swallow shock wave and the resistance of the projectile is decreased at some speed or mach 3.0 or more, for example, while the shock wave is discharged on the contrary by the flow passages at some speed or a mach number of less than 3.0 whereby the resistance of the projectile can be increased. According to such an aerodynamic characteristic, the projectile can be flown with a flying characteristic same as the actual projectile along a trajectory same as the actual projectile until the projectile arrives at a target while the speed can be decelerated suddenly after arriving at the target and the projectile can be dropped in a training area. COPYRIGHT: (C)1991,JPO&Japio | ||||||
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