| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 181 | Magazine loaded recoilless gun | US61471945 | 1945-09-06 | US2503578A | 1950-04-11 | DENNISTOUN BURNEY CHARLES |
| 182 | Recoilless gun with breech closing mechanism | US61471745 | 1945-09-06 | US2489954A | 1949-11-29 | DENNISTOUN BURNEY CHARLES |
| 183 | Controlled pressure gun | US61471445 | 1945-09-06 | US2489748A | 1949-11-29 | DENNISTOUN BURNEY CHARLES |
| 184 | Reduced recoil type gun | US55234744 | 1944-09-01 | US2489747A | 1949-11-29 | DENNISTOUN BURNEY CHARLES |
| 185 | Venturi vise | US69817946 | 1946-09-20 | US2475384A | 1949-07-05 | FOWLER KENNETH R |
| 186 | Recoilless firearm and ammunition therefor | US2318548 | 1948-04-26 | US2466714A | 1949-04-12 | KROEGER WILLIAM J; WALTON MUSSER CLARENCE |
| 187 | Recoilless firearm | US62864745 | 1945-11-14 | US2444949A | 1948-07-13 | WALTON MUSSER CLARENCE |
| 188 | Recoil absorber for guns | US57522445 | 1945-01-30 | US2420492A | 1947-05-13 | MARSEILLES WILLIAM M |
| 189 | Rocket gun | US71921024 | 1924-06-10 | US1661091A | 1928-02-28 | DMITRI RIABOUCHINSKI |
| 190 | giles | US1394490D | US1394490A | 1921-10-18 | ||
| 191 | Non-recoil gun for aeroplanes | US19177217 | 1917-09-17 | US1373381A | 1921-03-29 | JOHN COOKE CHARLES |
| 192 | Non-recoil ordnance. | US18317517 | 1917-07-27 | US1280579A | 1918-10-01 | SHUKER WILLIAM |
| 193 | Apparatus for firing projectiles from air-craft. | US1913777763 | 1913-07-07 | US1108716A | 1914-08-25 | DAVIS CLELAND |
| 194 | Autonomous automatic electromagnetic launch system with adjustable launch velocity, low recoil force, low acoustic report, and low visible and infra-red signature | US15453592 | 2017-03-08 | US10054387B2 | 2018-08-21 | Thomas Gregory Engel |
| Apparatus for electromagnetic launching system for the linear acceleration of macro particles. The apparatus disclosed is autonomously-powered, compact, and lightweight. The apparatus disclosed has low recoil force, low acoustic report, and low visible and infra-red signature. The apparatus disclosed is capable of automatic operation and the maximum particle velocity can be adjusted. The apparatus disclosed includes a trigger, controller, component power source, particle container, particle loader, propellant container, propellant loader, igniter, combustion chamber, sound suppressor, linear electrical generator, linear electrical motor, and thermal barrier. | ||||||
| 195 | AUTONOMOUS AUTOMATIC ELECTROMAGNETIC LAUNCH SYSTEM WITH ADJUSTABLE LAUNCH VELOCITY, LOW RECOIL FORCE, LOW ACOUSTIC REPORT, AND LOW VISIBLE AND INFRA-RED SIGNATURE | US15453592 | 2017-03-08 | US20170314887A1 | 2017-11-02 | Thomas Gregory Engel |
| Apparatus for electromagnetic launching system for the linear acceleration of macro particles. The apparatus disclosed is autonomously-powered, compact, and lightweight. The apparatus disclosed has low recoil force, low acoustic report, and low visible and infra-red signature. The apparatus disclosed is capable of automatic operation and the maximum particle velocity can be adjusted. The apparatus disclosed includes a trigger, controller, component power source, particle container, particle loader, propellant container, propellant loader, igniter, combustion chamber, sound suppressor, linear electrical generator, linear electrical motor, and thermal barrier. | ||||||
| 196 | RECOIL MITIGATING APPARATUS AND METHODS | US14298804 | 2014-06-06 | US20150226507A1 | 2015-08-13 | GREGORY Wilson PALMER |
| Apparatus and methods for reduction of recoil in for example a ballistic system. In one embodiment, the ballistic system comprises a firearm such as a rifle or handgun, and the apparatus includes a momentum or energy capture device. The capture device utilizes the recoil of e.g., the bolt of the firearm to drive a compensating mechanism such as a flywheel, which compensates for at least some of the recoil. | ||||||
| 197 | Method and apparatus for launch recoil abatement | US13739854 | 2013-01-11 | US08960067B2 | 2015-02-24 | Wayne K. Schroeder |
| Recoil forces of a launched missile and the moment force imposed on the launch platform can be reduced by use of a recoil abatement element in communication with a launch tube. The recoil abatement element includes at least one nozzle configured to receive therethrough exhaust gasses from a missile when launched. The nozzle can be canted or otherwise configured to direct the exhaust gasses in a desired direction to thereby offset moment force imposed on the platform by the exhaust gasses. | ||||||
| 198 | TRAINING WEAPON SYSTEM FOR RECOILLESS ANTITANK RIFLE WEAPONS | US13697444 | 2010-05-11 | US20130280677A1 | 2013-10-24 | Johnny Liljeholm |
| The invention relates to a training weapon system (1) intended for a recoilless antitank rifle (2), the training weapon system (1) comprising a sub-calibre barrel (3) for firing sub-calibre practice projectiles (4) provided with base plates (5), the sub-calibre barrel (3) being arranged in a shell-like body (6) in the barrel (7) of the recoilless antitank rifle (2), the front part of the sub-calibre barrel (3) being fitted in a guide part (8) for centring the barrel (3), and a rear part of the barrel (3) being fitted in a breech (9), comprising a firing channel (10) and a nozzle screw thread (11) for fitting a nozzle screw (12), which is arranged in the rear part of the shell-like body (6). The invention is characterized in that the training weapon system (1) comprises at least one locking part (13, 14), the function of which is to prevent the nozzle screw (12) or the base plate (5) of the projectile (4) or part of the base plate (5) being expelled backwards through the nozzle funnel (21) of the antitank rifle (2) as loose flying projectiles. | ||||||
| 199 | Firearm with enhanced recoil and control characteristics | US12007482 | 2008-01-10 | US20100064566A1 | 2010-03-18 | Renaud Kerbrat; Timothy Lindsay |
| The invention comprises improved designs in a recoil control device comprising a bolt and slider for use in a variety of firearms. In one embodiment, the bolt and slider are articulated so that the displacement of the bolt results in a force component accompanying the slider as it moves along a slider path that traverses a line formed by a linear firing axis of the barrel of the firearm. The slider can have additional structural and functional features, including stabilizing features, vibrational damping elements, elements of the fire control mechanism, and devices to manage the peak impulse of the slider movement as it contacts a base or terminus point. | ||||||
| 200 | SUBMARINE | US10883944 | 2004-07-02 | US20070215030A1 | 2007-09-20 | Wolfgang Scharf; Joachim Reuter; Rolf Korver |
| A submarine is equipped with an extending apparatus on whose free end a container (4) resistant to underwater pressure is arranged, in which an essentially recoil-free gun (5) lies. The container (4) in the submerged condition of the submarine may be brought to the water surface (15) by way of the extending apparatus, and pivoted out so that one may also shoot in the submerged condition. | ||||||
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