| 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 | 无人水下航行器的远距离输送 | CN201580010769.4 | 2015-01-15 | CN106068438A | 2016-11-02 | 凯勒·斯托尔斯 |
| 一种射弹(100)包括引导飞行中的射弹的引导组件(102、103)。射弹进一步包括壳体和中空的鼻锥体(106)。壳体与引导组件配合并且鼻锥体与壳体耦合。鼻锥体包括被配置为容纳UUV(202)的内表面。射弹进一步包括控制器(108)，其识别用于部署飞行中的UUV的条件并且响应于确定条件满足使鼻锥体从壳体脱离。 | ||||||
| 2 | STAND-OFF DELIVERY OF UNMANNED UNDERWATER VEHICLES | EP15703353.1 | 2015-01-15 | EP3123102A1 | 2017-02-01 | STOWERS, Kyle |
| Embodiments described herein provide apparatus and method for stand-off deployment of UUVs utilizing self-directed projectiles that include guidance kits. One embodiment is a projectile that includes a guidance kit that directs the projectile in flight. The projectile further includes a shell and a hollow nose cone. The shell mates with the guidance kit and the nose cone couples with the shell. The nose cone includes an interior surface configured to house a UUV. The projectile further includes a controller that identifies a condition for deploying the UUV in flight, and detaches the nose cone from the shell in response to determining that the condition is satisfied. | ||||||
| 3 | JPS6228399B2 - | JP1666386 | 1986-01-28 | JPS6228399B2 | 1987-06-19 | AREN SHII HEEGERUBAAGU; KURAAKU II ARAATO; UORUTAA EI ROBITSUTSU; ROBAATO OO SOONBAAGU; JOOJI EFU JINMAAMAN; GEIRII ERU RETSUTAAMAN; JON UIRIAMU HERUBOON |
| 4 | Antisubmarine weapon | JP1666386 | 1986-01-28 | JPS61205800A | 1986-09-11 | AREN SHII HEEGERUBAAGU; KURAAKU II ARAATO; UORUTAA EI ROBITSUTSU; ROBAATO OO SOONBAAGU; JIYOOJI EFU JINMAAMAN; GEIRII ERU RETSUTAAMAN; JIYON UIRIAMU HERUBOON |
| 5 | Anti-submarine weapon | JP2365881 | 1981-02-19 | JPS56138700A | 1981-10-29 | AREN SHII HEEGERUBAAGU; KURAAKU II ARAATO; UORUTAA EI ROBITSUTSU; ROBAATO OO SOONBAAGU; JIYOOJI EFU JINMAAMAN; GEIRII ERU RETSUTAAMAN; JIYON UIRIAMU HERUBOON |
| 6 | Storage cover separation device of flying object | JP26163797 | 1997-09-26 | JPH1194500A | 1999-04-09 | MATSUI TOSHIHIKO |
| PROBLEM TO BE SOLVED: To positively achieve separation without any risk of touching a mounted object by providing at least one steering wing that normally performing a flight control operation and at the same time is separated and operated according to a command signal at each storage cover. SOLUTION: Steering wings 3a and 3b are provided at the left and right of the front part of each storage cover 1 being divided into two portions vertically, a command signal is sent to a thruster 2a for separation and the steering wings 3a and 3b from an auto-pilot device 8 when a specific target location is reached, the connection of the storage cover 1 is untied, and at the same time the steering wings 3a and 3b are operated by the same command signal, thus achieving a steering angle so that an air force is generated and performing travel and separation in a direction away from an underwater cruising body 5. Therefore, since the size of the air force and the scattering in an operation direction are small, the separation operation of the storage cover 1 is made positive and the estimation accuracy of the trace of the storage cover 1 after separation increases, thus preventing collision against a mounted object. | ||||||
| 7 | JPS6137559B2 - | JP2365881 | 1981-02-19 | JPS6137559B2 | 1986-08-25 | AREN SHII HEEGERUBAAGU; KURAAKU II ARAATO; UORUTAA EI ROBITSUTSU; ROBAATO OO SOONBAAGU; JOOJI EFU JINMAAMAN; GEIRII ERU RETSUTAAMAN; JON UIRIAMU HERUBOON |
| 8 | Interception by submarine and intercepting underwater missile | JP16035678 | 1978-12-25 | JPS5587694A | 1980-07-02 | ENDOU YUKITOSHI; KAMANARI YOSHIO |
| PURPOSE:To enable to intercept an aerial target from underwater by a method wherein an underwater missile is launched from a submarine by a target sensing signal issued from a radar floating on the sea level so as to allow an aerial missile to launch from the said underwater missile by guiding it close to the launching point at the surface. CONSTITUTION:When a target such as an enemy airplane approaches overhead, a radar unit C is floated from a submarine A on the sea level D, and a friendly submarine A simultaneously takes evading movement. The floating radar unit C starts searching operation to pick up the target, the information of which is transmitted to the submarine A through a sonic wave or a cable. On accepting the information, the submarine A launches an underwater missile B from a launcher. During running, a missile B according to the information available from the radar unit C through the cable 10 joining the submarine A and the underwater missile B. When the underwater missile B is guided to reach under the sea level close to the target E, the aerial missile 7 is launched towards the target E from the missile B enabling the missile to hit by homing against the target E. | ||||||
| 9 | VORRICHTUNG UND VERFAHREN ZUM STARTEN EINES UNTERWASSERLAUFKÖRPERS | EP10715813.1 | 2010-04-22 | EP2425200B1 | 2016-05-11 | BRENNER, Axel; BARTHOLOMÄUS, Ralf; BÜNSCH, Wolfgang; HUCKFELDT, Sönke; FUHRMANN, Dirk |
| 10 | Dispositif d'éjection pour munition amphibie et propulseur indépendant en faisant partie | EP90401862.9 | 1990-06-28 | EP0406114A1 | 1991-01-02 | Knur, Lionel; Siegwald, Roland |
Dispositif d'éjection pour munition amphibie (2), comportant un tube lance-torpilles (3) au sein duquel est disposé un propulseur à poudre (5) indépendant de la munition et placé en appui sur l'arrière de cette munition. |
||||||
| 11 | Procédé et véhicule de lancement par un sous-marin en plongée d'un missile aérien | EP86401832.0 | 1986-08-19 | EP0257163B1 | 1990-08-08 | Stauff, Emile; Guillot, Jean; Pinel, André |
| 12 | Supercavitating Projectile and Operation Thereof | US12327550 | 2008-12-03 | US20090173248A1 | 2009-07-09 | Jyun-Horng Fu |
| A method for operating a supercavitating projectile is disclosed. | ||||||
| 13 | Extended range artillery projectile | US130944 | 1993-10-04 | US5353711A | 1994-10-11 | Richard D. Botticelli; Frank A. Brody; Francis Ottaviano |
| The disclosure is of an artillery projectile including a projectile body taining, among other things, a rocket motor at the front of the projectile and coupled to nozzles in the body of the projectile through which burning propellant gases flow. | ||||||
| 14 | Transient surface contact vehicle | US505815 | 1983-06-20 | US4505442A | 1985-03-19 | Jerome Kirsch; M. Alan Kopsco; Edward Markow; Michael Sturm |
| A transient surface contact vehicle for transporting a load from a surface starting point to a surface end point has a structure for carrying the load from the starting point to the end point. A vehicle support extends from the structure. A buoyancy control device mounted in the structure is coupled to the vehicle support for selectively making the support buoyant and non-buoyant whereby when the support is buoyant it abuts the surface of a body of water thereby supporting the vehicle at a predetermined distance above the surface of the body of water. An acquisition sensor mounted on the structure initiates water surface operations. A sensor is mounted on the structure and cooperates with the acquisition sensor to energize upon tracking of the target and to move the vehicle along the water surface to impact with the target at the end point. A position control mounted on the vehicle produces a negative pitching moment to maintain the structure in surface-following contact with the body of water. | ||||||
| 15 | Self-consuming ramjet vehicle | US3504631D | 1963-09-16 | US3504631A | 1970-04-07 | LINDLEY CHARLES ALEXANDER |
| 16 | Autopilot | US26697852 | 1952-01-17 | US3011738A | 1961-12-05 | SKRAMSTAD HAROLD K; HART JOHN A |
| 17 | Ahead-thrown weapon for submarine warfare | US18362550 | 1950-09-07 | US2758542A | 1956-08-14 | SOLOMON BURG |
| 18 | Aerial torpedo | US44850542 | 1942-06-25 | US2419866A | 1947-04-29 | GORDON WILSON WALTER |
| 19 | Self-propelled bomb | US42820142 | 1942-01-26 | US2327621A | 1943-08-24 | CONRAD SAMUEL L |
| 20 | Gyroscopic apparatus for directing flight | US25386039 | 1939-01-31 | US2183314A | 1939-12-12 | GODDARD ROBERT H |
QQ群二维码
意见反馈
意见反馈