| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 41 | Bomb carrier and control for the bombs | US37716441 | 1941-02-03 | US2342523A | 1944-02-22 | GEORGE BAXTER |
| 42 | Bomb | US18028137 | 1937-12-17 | US2151916A | 1939-03-28 | PIERRE HULSWIT JAN |
| 43 | Torpedo for launching from alpha flying machine | US54710931 | 1931-06-26 | US1923612A | 1933-08-22 | ANDREAS BULL JOHAN |
| 44 | Wireless-controlled aerial torpedo | US20778617 | 1917-12-18 | US1792937A | 1931-02-17 | SPERRY ELMER A |
| 45 | Torpedo | US63038823 | 1923-04-08 | US1571487A | 1926-02-02 | MCVAY JR CHARLES R |
| 46 | AN APPARATUS FOR ALTERING THE COURSE OF TRAVELLING OF A MOVING ARTICLE AND A METHOD THEREOF | EP05810615.4 | 2005-12-02 | EP1834154B1 | 2011-10-05 | LUI, Pao, Chuen; FONG, Saik, Hay; TAN, Hong, Soon; TOH, Tee, Peng |
| The present invention relates to an apparatus for altering the course of a moving article and a method thereof comprising of a launching aircraft or surface craft to deploy said apparatus towards a moving article. The apparatus comprises of a driving mechanism (10), wherein said driving mechanism (10) further comprises of a plurality of sections such as a nose section (12), a propulsion section (14), a drag chute section (16) and a cutting section (18), and wherein said sections are integrally connected with one another in a tight and secure manner. The driving mechanism (10) is capable to be launched from an aircraft or a surface craft towards a target and wherein upon launch said driving mechanism (10) is capable of steering itself on its own towards its target and thereafter attaching itself to the target and wherein by using the drag chute section (16). The driving mechanism (10) is designed and configured to alter the initial trajectory or direction of the target to another direction by dragging it and wherein permanently changing the course of the said target. | ||||||
| 47 | AN APPARATUS FOR ALTERING THE COURSE OF TRAVELLING OF A MOVING ARTICLE AND A METHOD THEREOF | EP05810615 | 2005-12-02 | EP1834154A4 | 2010-05-19 | LUI PAO CHUEN; FONG SAIK HAY; TAN HONG SOON; TOH TEE PENG |
| 48 | METHOD AND DEVICE FOR DISCOVERING AND DESTRUCTING SUBMARINE VESSELS FROM AN AIRCRAFT | EP89908547.6 | 1989-07-11 | EP0426726B1 | 1993-12-22 | GUSTAVSSON, Mats; OLSSON, Jan; OLSSON, Thord |
| The invention relates to a method for locating and destructing submarine vehicles from airborne vehicles disposed above the water surface, wherein a device (10) suspended from said airborne vehicle comprises sensing means (14) scanning generally in the horizontal plane to discover submarine vehicles in the water is submerged in the water from the airborne vehicle, said sensing means scanning the surrounding water to detect presence of and direction to submarine vehicles in the water. The device submerged in the water comprises a propulsion mechanism (12) and an explosive charge (11) and is released from the airborne vehicle and during continuous scanning of the water and detection of the presence of and direction to submarine vehicles is propelled independently through the water and steered for the submarine vehicle from the point of release. | ||||||
| 49 | Underwater vehicle guided by a Lidar imaging system | EP92118653.2 | 1992-10-31 | EP0534496A3 | 1993-06-16 | Keeler, Norris R.; Kaman, Charles H.; Ulich, Bobby Lee; Cardero, Silvio A.; Manthy, Robert S. |
An underwater manoeuvrable vehicle (10) is presented which carries an explosive charge and can be used for immediate removal or destruction of various menaces to navigation and other underwater hazards (58). The battery powered vehicle (10) is preferably air dropped from an airborne platform (12) which carries an imaging lidar system (36) to obtain an image of the vehicle (10) and the selected navigational hazard (58). An optical lidar downlink (132) is used to control the submerged underwater manoeuvrable vehicle (10) from the airbrone platform (12). The downlink (132) is pulse space modulated. Command signals (132) are decoded aboard the vehicle (10). Control in speed, heading and depth, as well as command detonation are available using this technique. |
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| 50 | Underwater vehicle guided by a Lidar imaging system | EP92118653.2 | 1992-10-31 | EP0534496A2 | 1993-03-31 | Keeler, Norris R.; Kaman, Charles H.; Ulich, Bobby Lee; Cardero, Silvio A.; Manthy, Robert S. |
An underwater manoeuvrable vehicle (10) is presented which carries an explosive charge and can be used for immediate removal or destruction of various menaces to navigation and other underwater hazards (58). The battery powered vehicle (10) is preferably air dropped from an airborne platform (12) which carries an imaging lidar system (36) to obtain an image of the vehicle (10) and the selected navigational hazard (58). An optical lidar downlink (132) is used to control the submerged underwater manoeuvrable vehicle (10) from the airbrone platform (12). The downlink (132) is pulse space modulated. Command signals (132) are decoded aboard the vehicle (10). Control in speed, heading and depth, as well as command detonation are available using this technique. |
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| 51 | METHOD AND DEVICE FOR DISCOVERING AND DESTRUCTING SUBMARINE VESSELS FROM AN AIRCRAFT | EP89908547.0 | 1989-07-11 | EP0426726A1 | 1991-05-15 | GUSTAVSSON, Mats; OLSSON, Jan; OLSSON, Thord |
| Selon un procédé de localisation et de destruction de véhicules sous-marins depuis des véhicules aériens situés au-dessus de la surface de l'eau, un dispositif (10) suspendu du véhicule aérien comprend un capteur (14) de balayage généralement sur un plan horizontal utilisé pour repérer des véhicules sous-marins dans l'eau et submergé dans l'eau depuis le véhicule aérien. Le capteur balaie les eaux environnantes afin de détecter la présence et le sens de déplacement de véhicules sous-marins dans l'eau. Le dispositif submergé dans l'eau comprend un mécanisme propulseur (12) et une charge explosive (11). Il est largué par le véhicule aérien, propulsé indépendamment à travers l'eau pendant le balayage en continu de l'eau et la détection de la présence et du sens de déplacement des véhicules sous-marins, et dirigé vers le véhicule sous-marin depuis le point de largage. | ||||||
| 52 | STAND-OFF DELIVERY OF UNMANNED UNDERWATER VEHICLES | EP15703353.1 | 2015-01-15 | EP3123102B1 | 2018-07-04 | 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. | ||||||
| 53 | SCHWERGEWICHTSTORPEDO, TRANSPORTSCHLITTEN UND FLUGZEUG | EP16703906.4 | 2016-01-13 | EP3247973A1 | 2017-11-29 | LÄMMLE, Knud |
| The invention relates to a heavyweight torpedo for dropping into a body of water outside of a visibility range of a target, comprising a parachute, a parachute/torpedo connection, and a parachute-releasing element, wherein the parachute-releasing element has a two-stage design and the first stage is initiated by activation of the parachute and the forces of the parachute on the heavyweight torpedo and the second stage is put into an activation mode by the initiation of the first stage and the second stage comprises detachment of the parachute. | ||||||
| 54 | AN APPARATUS FOR ALTERING THE COURSE OF TRAVELLING OF A MOVING ARTICLE AND A METHOD THEREOF | EP05810615.4 | 2005-12-02 | EP1834154A1 | 2007-09-19 | LUI, Pao, Chuen; FONG, Saik, Hay; TAN, Hong, Soon; TOH, Tee, Peng |
| The present invention relates to an apparatus for altering the course of a moving article and a method thereof comprising of a launching aircraft or surface craft to deploy said apparatus towards a moving article. The apparatus comprises of a driving mechanism (10), wherein said driving mechanism (10) further comprises of a plurality of sections such as a nose section (12), a propulsion section (14), a drag chute section (16) and a cutting section (18), and wherein said sections are integrally connected with one another in a tight and secure manner. The driving mechanism (10) is capable to be launched from an aircraft or a surface craft towards a target and wherein upon launch said driving mechanism (10) is capable of steering itself on its own towards its target and thereafter attaching itself to the target and wherein by using the drag chute section (16). The driving mechanism (10) is designed and configured to alter the initial trajectory or direction of the target to another direction by dragging it and wherein permanently changing the course of the said target. | ||||||
| 55 | Method and apparatus for removing navigational hazards in water | EP92104957.3 | 1992-03-23 | EP0494092B1 | 1996-09-11 | Manthy, Robert S.; Daniels, Kirk; Wells, Anthony R.; Keeler, Norris R.; Renehan, Patrick L. |
| 56 | Method and apparatus for removing navigational hazards in water | EP92104957.3 | 1992-03-23 | EP0494092A3 | 1993-06-16 | Manthy, Robert S.; Daniels, Kirk; Wells, Anthony R.; Keeler, Norris R.; Renehan, Patrick L. |
An underwater maneuverable vehicle (10) is presented which carries an explosive charge and can be used for immediate removal or destruction of various menaces to navigation and other underwater hazards (58). The battery powered vehicle (10) is air dropped from a platform (12) which carries an imaging lidar system (36) for detection and is operated and navigationally controlled in conjunction with an imaging lidar system. |
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| 57 | 유도활공 기뢰 어셈블리의 설치방법 | KR1020140125110 | 2014-09-19 | KR101575132B1 | 2015-12-07 | 박영근; 여주엽; 이대열; 이인원; 황영은 |
| 본발명은설치목표위치와원거리에서공중에서투하되어활공한후 목표지점에서입수하여수중에설치되는유도활공기뢰어셈블리및 이의설치방법에관한것이다. 본발명에따른유도활공기뢰어셈블리는, 내부에폭발물이채워지고수중에설치되는기뢰부(10)와, 상기기뢰부(10)와일체가되도록상기기뢰부(10)에고정되고, 상기기뢰부(10)를활공시키며, 항공기(F)에분리가능하게설치되는활공체부(20)를포함하고, 이의설치방법은, 항공기(F)로부터기뢰어셈블리(1)가분리되어상기기뢰어셈블리(1)가투하되는투하단계(S110)와, 상기기뢰어셈블리(1)의항공기(F)에설치된날개가전개되는날개전개단계(S120)와, 상기기뢰어셈블리(1)의날개가전개된이후, 상기기뢰어셈블리(1)가최종설치목표위치(T3)에인접한자율활공종료위치(T1)까지상기기뢰어셈블리(1)의위치를제어하면서활공하는자율활공단계(S130)와, 상기자율활공종료위치(T1)로부터상기기뢰어셈블리(1)의입수각도및 속도를조절하기위해상기기뢰어셈블리(1)가실속속도가되는활공종료위치(T2)로상승시키는입수조건조절단계(S140)와, 상기기뢰어셈블리(1)를설치목표위치(T3)의상방으로부터수면을통하여수중으로입수시키는입수단계(S150)를포함한다. | ||||||
| 58 | 쉘 조립체, 이를 구비하는 유도탄 및 유도탄의 충격완화방법 | KR1020100120064 | 2010-11-29 | KR1020120058335A | 2012-06-07 | 김인학 |
| PURPOSE: A shell assembly, a guided missile therewith, and a shock reducing method of the guided missile are provided to securely protect the front body of the guided missile when the shell assembly is launched. CONSTITUTION: A shell assembly(130) comprises a shell(134), a first support(131), and a second support(132). One end of the shell has a mounting surface, and the other end is formed in a hollow cylindrical shape. The first support is attached on the inner surface of the shell and supports an axial load. The second support is coupled to the first support and is separated from the first support by lateral expansion pressure. And the second support transfers the lateral expansion pressure to the shell. | ||||||
| 59 | 유도무기 제어판 영점 조정 방법 및 장치 | KR1020100094770 | 2010-09-29 | KR1020120033155A | 2012-04-06 | 조현진; 최철호 |
| PURPOSE: Zero-point adjustment method and device for a control board of guided munitions are provided to measure the actual mechanical errors of a control board and simply adjust the zero point of the control board in real time. CONSTITUTION: Zero-point adjustment method and device for a control board of guided munitions are as follows. A rudder angle is input to the driving controller(10) of guided munitions at a test signal input/output unit(100). A rudder angle(30) of the control board actually driven by a driving unit receiving a rudder angle from a driving controller is compared with that of a driving unit measured at a location sensor(40). The rudder angle of the control board actually driven and the rudder angle of the driving unit measured at the location sensor are matched by controlling the reference value of the location sensor. | ||||||
| 60 | 어뢰 탑재용 밴드 어셈블리 | KR1020020002051 | 2002-01-14 | KR100515027B1 | 2005-09-15 | 김인학; 독고욱; 전완수 |
| 본 발명은 초계기와 어뢰가 탑재된 밴드 어셈블리가 분리될 때 작동 케이블이 투하되는 어뢰에 영향을 미치지 않도록 하여 어뢰의 초기 투하자세를 안전하게 유지할 수 있고, 밴드 어셈블리와 어뢰가 분리될 때 밴드 어셈블리가 어뢰로부터 일정 거리만큼 이탈되기 때문에 어뢰에서 전개되는 낙하산과 밴드 어셈블리 사이의 간섭을 피할 수 있어 안정성 및 작동 신뢰성을 향상시킬 수 있는 어뢰 탑재용 밴드 어셈블리를 제공하기 위한 것으로, 어뢰에 감싸지는 한 쌍의 밴드와, 상기 밴드의 일측이 회전 가능하게 연결되고 초계기에 고정되는 파이론에 탑재되는 탑재부와, 상기 밴드의 타측에 탑재되고 어뢰에 감싸진 밴드를 잠금 및 잠금해제 작용을 하는 개폐부와, 상기 개폐부의 일측에 설치되어 개폐부의 록킹이 해제될 때 록킹 해제작용을 일정 시간� ��안 지연시키는 시간 지연장치와, 상기 밴드의 일측에 연결되어 상기 밴드에서 어뢰가 분리될 때 탄성력을 부여하는 탄성수단과, 상기 파이론의 지지대에 연결되고, 상기 시간 지연장치에 끼워지는 장전핀이 연결되어 상기 어뢰가 초계기로부터 분리될 때 시간 지연장치에서 장전핀을 이탈시켜 시간 지연장치를 작동시키는 케이블을 포함하여 구성된다. | ||||||
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