| 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 | Fuse safety device | JP15049081 | 1981-09-22 | JPS5787600A | 1982-06-01 | URUFU YANDERU |
| 2 | Automatic release safety device for gas generator mechanical ignition device | JP2596093 | 1993-01-22 | JPH06219233A | 1994-08-09 | NISHIZAWA MUNEO; HAMAGAMI TETSUYA; HIRUTA MITSUHIKO; HIRAMATSU KOJI |
| PURPOSE: To automatically release a safety device for a gas generator mechanical ignition device when it is installed to a vehicle. CONSTITUTION: A mechanical ignition device 5, which is arranged so as to ignite a detonator installed in a gas generator according to acceleration, is provided with a safety device 6, which is provided with a weight 51 as a movable element, a latch lever 52, and a firing pin 53 while consists of a safety pin 61 immobilizing the latch lever 52 and a controlling means 62 connected to the safety pin 61 so as to release the immovable condition of the latch lever 52 by the safely pin 61. The controlling means 62 is provided with a plate spring 62A, which is displaced by being brought in contact with an inner panel when the mechanical ignition device 5 is installed to a vehicle body via a cylinder block 30 and a retractor base 10 and transmits the displacement to the safety pin 61. COPYRIGHT: (C)1994,JPO&Japio | ||||||
| 3 | Dispositif de sécurité et d'armement notamment pour mine | EP97400962.3 | 1997-04-29 | EP0809085B1 | 2001-08-22 | Philipot, Maurice; Blin, André |
| 4 | SUBMARINE FLARE. | EP87905920 | 1987-08-21 | EP0318515A4 | 1990-06-27 | RAMSAY PETER; WHIFFEN BRIAN WILLIAM; BUSHNELL GERALD MONTAGUE; NANUT VICTOR; CZIGLEDY ROBERT CHARLES; SWINTON ROBERT JAMES; COXHEAD MAXWELL JOHN; CLARKE TIMOTHY ROBERT |
| A flare (1) for submarine use. The flare (1) is caused to be deployed from a submarine location where it will rise to the surface of the water because of its buoyant casing. A hydrostatic valve means (147) is provided within the casing and it opens when the flare is at or near the surface of the water to render said flare ready to project a flare composition (5) into the air. The hydrostatic valve means (147) is held inoperative by a latch mechanism (51) which is tripped as the flare is deployed from a firing tube at the submarine location. The flare composition (5) cannot be projected into the air until the flare (1) is within a range of vertical attitude determined by inclination means (13). The flare composition (5) cannot be projected into the air until the nose is above water. The flare (1) thus has a sensor (23) at its forward nose to determine that the nose is above the water. A time delay means (87) is provided which is initiated by a pyrotechnic medium (85) used to project the flare composition (5) into the air, to delay ignition of the flare composition (5) until it has at leastcleared the surface of the water. | ||||||
| 5 | SUBMARINE FLARE | EP87905920.0 | 1987-08-21 | EP0318515A1 | 1989-06-07 | RAMSAY, Peter; WHIFFEN, Brian, William; BUSHNELL, Gerald, Montague; NANUT, Victor; CZIGLEDY, Robert, Charles; SWINTON, Robert, James; COXHEAD, Maxwell, John; CLARKE, Timothy, Robert |
| Une fusée de signalisation éclairante (1) pour sous-marins est lancée à partir de l'endroit d'un sous-marin d'où elle atteint la surface de l'eau grâce à son enveloppe flottante. Une soupape hydrostatique (147) est disposée dans l'enveloppe et s'ouvre lorsque la fusée de signalisation se trouve à la surface ou à proximité de la surface de l'eau, rendant ainsi la fusée de signalisation prête à projeter dans les airs une composition éclairante (5). La soupape hydrostatique (147) est maintenue en position de non-fonctionnement par un mécanisme de verrouillage (51) qui est déclenché au moment où la fusée de signalisation est lancée depuis un tube de mise à feu se trouvant à l'endroit du sous-marin. La composition éclairante (5) ne peut être projetée dans les airs que si la fusée de signalisation (1) se trouve dans une position sensiblement verticale déterminée par un organe d'inclinaison (13). La composition éclairante (5) ne peut être projetée dans les airs que si le nez se trouve au-dessus de l'eau. La fusée de signalisation (1) comporte par conséquent à la pointe de son nez un détecteur (23) destiné à déterminer si le nez se trouve au-dessus de l'eau. Un organe de retardement (87), mis en route par la substance pyrotechnique (85) utilisée pour projeter dans les airs la composition éclairante (5), permet de retarder l'ignition de la composition éclairante (5) jusqu'à ce qu'elle ait au moins dépassé la surface de l'eau. | ||||||
| 6 | 점화기 안전 장치 및 아암, 그를 구비한 점화기 조립체 및 플레어, 및 점화기 조립체용 안전 장치 제공 방법 | KR1020097009640 | 2007-11-13 | KR1020090088369A | 2009-08-19 | 리차드스케빈더블유.; 다이켄달; 요네스로버트지. |
| A parachute flare igniter assembly includes a novel safety for arresting the motion of a slider when subjected to external forces, but allows slider motion when subjected to intended cable actuation forces. The igniter safety includes a housing, a slider, a cable and a sleeve. The slider, connected to the cable, is slidably received within the housing. The cable moves the slider by applying a cable force conventionally obtained by actuation of a parachute associated with the flare and connected to an end of the cable opposite an end connected to the slider. The sleeve is connected to the cable and is disposed between the housing and the slider, so that the sleeve will arrest the slider with respect to the housing when the cable force is not present. A flare and a method of providing a safety in an igniter assembly is also provided. ® KIPO & WIPO 2009 | ||||||
| 7 | 자체 파괴형 충격 퓨즈 | KR1020017009720 | 1999-04-23 | KR100521410B1 | 2005-10-12 | 아우쳉호크; 이구안순; 탄치안치오우 |
| 본 발명은 다수의 구체들(50) 및 챔버가 회전할 때 상기 구체들(50)의 노출부들에 대한 표면상에 다수의 방사상의 개구부들(49)을 보유하기 위한 속이 빈 원심 챔버(48)를 구비하는 원통형의 점화 핀이다. 상기 챔버(48)의 일측 단에는 상기 챔버(48)의 길이축을 따라서 압축력을 가하기 위한 스프링(54)이 있으며 다른측 단에는 상기 뇌관(26)을 치기위한 자체 파괴형(SD: Self Destructing) 점화 핀(52)이 있다. 상기 길이 축으로부터 피벗(pivot)오프셋(offset)을 가지는 원심성 록(lock)(40)은 상기 원심 챔버(48)의 표면상의 홈(groove)(46)과 정합시킴으로써 제자리에 상기 챔버(48)를 보유한다. 상기 원통형의 점화 핀은 프레임(30)내에 동심으로 놓이고 상기 뇌관(26)을 특징짓는 탈착장치 어셈블리(escapement assembly)위에 배치된다. 상기 뇌관(26)은 상기 퓨즈를 통합한 상기 발사체가 최소 전술 거리(minimum tactical distance)를 이동한 후에 상기 자체 파괴형 점화 핀(52)과 일직선이 되도록 회전된다. 상기 프레임(30)은 상기 뇌관(26)을 치기위한 점 폭발(PD: Point Detonation) 점화 핀(36)을 특징짓는 기부(base)(34)와 더 결합된다. | ||||||
| 8 | VERROU POUR LEVIER DE BOUCHON ALLUMEUR | EP01921488.1 | 2001-04-05 | EP1269107B1 | 2006-11-02 | TEILHOL, Frédéric; VALEMBOIS, Guy; RIFFET, Régis; BARICOS, Jean |
| The invention concerns an igniter plug for a pyrotechnic device, in particular a hand-launch or mechanical launch grenade, comprising a body (104) provided with a control mechanism including a fly-off lever (101) and a percussion mechanism (128) co-operating with a primary pyrotechnic module (105) for initiating the charge (119) of the associated device. The invention is characterised in that it further comprises a lock (150) engaged with the lever (101), in storage position, to prevent the fly-off lever (101) from moving towards its release position, the lock (150) being configured to impose, when the igniter plug is activated, an initial movement of the lever (101) countering its displacement required for releasing the percussion mechanism (128), so as to disengage the lock (150) and the fly-off lever (101). | ||||||
| 9 | Fusée de munition comprenant au moins une sécurité liée à un environnement extérieur | EP03104580.0 | 2003-12-08 | EP1431702A1 | 2004-06-23 | CLEMENT, Benoît; FOURCOT, Didier; COHE, Patrick |
L'invention a pour objet une fusée (F) de munition comprenant au moins une sécurité (17, 33) empêchant d'armer la fusée, un volet (25) présentant une prise au vent, agencé pour être mis en mouvement sous l'effet de la force aérodynamique exercée lorsque la fusée se déplace, le volet étant lié mécaniquement à la sécurité pour la désactiver lorsque le volet est mis en mouvement. L'invention s'applique aux fusées présentant une chaîne pyrotechnique désalignée, destinées à l'amorçage des munitions tirées dans les matériels à âme lisse. |
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| 10 | SELF DESTRUCTING IMPACT FUSE | EP99931740.7 | 1999-04-23 | EP1155279B1 | 2003-07-30 | AW, Cheng, Hok; EE, Guan, Soon; TAN, Chian, Chiow |
| A self destructing impact fuse including a cylindrical firing pin having a hollow centrifugal chamber for holding a number of spheres and a number of radial openings on its surface for exposing portions of the spheres when the chamber is spun. At one end of the chamber is a spring for exerting compression force along the longitudinal axis of the chamber and at the other end is a self-destructing (SD) firing pin for striking the detonator. A centrifugal lock having a pivot offset from the longitudinal axis holds the chamber in place by mating with a groove on the surface of the centrifugal chamber. The cylindrical firing pin is seated concentrically within a frame and disposed over an escapement assembly featuring the detonator. The detonator is rotated into alignment with the SD firing pin after the projectile, incorporating the fuse, travels the minimum tactical distance. The frame is further coupled with a base, which features a point detonation (PD) firing pin for striking the detonator. | ||||||
| 11 | VERROU POUR LEVIER DE BOUCHON ALLUMEUR | EP01921488.1 | 2001-04-05 | EP1269107A1 | 2003-01-02 | TEILHOL, Frédéric; VALEMBOIS, Guy; RIFFET, Régis; BARICOS, Jean |
| The invention concerns an igniter plug for a pyrotechnic device, in particular a hand-launch or mechanical launch grenade, comprising a body (104) provided with a control mechanism including a fly-off lever (101) and a percussion mechanism (128) co-operating with a primary pyrotechnic module (105) for initiating the charge (119) of the associated device. The invention is characterised in that it further comprises a lock (150) engaged with the lever (101), in storage position, to prevent the fly-off lever (101) from moving towards its release position, the lock (150) being configured to impose, when the igniter plug is activated, an initial movement of the lever (101) countering its displacement required for releasing the percussion mechanism (128), so as to disengage the lock (150) and the fly-off lever (101). | ||||||
| 12 | Dispositif de sécurité et d'armement notamment pour mine | EP97400962.3 | 1997-04-29 | EP0809085A1 | 1997-11-26 | Philipot, Maurice; Blin, André |
Le secteur technique de l'invention est celui des dispositifs de sécurité et d'armement pour munitions, notamment pour mines. Le dispositif selon l'invention comporte un système de temporisation horlogère (33) qui est armé par le déplacement d'un moyen de commande (39) et qui provoque le passage d'un système porte amorce (3) d'une position de sécurité à une position armée, il est caractérisé en ce que le moyen de commande est constitué par une tige (39) montée de façon coulissante dans un corps (2) du dispositif et en ce que le dispositif comporte des moyens de verrouillage (41,58) en translation de la tige de commande (39), moyens qui sont activés consécutivement à la traction de cette dernière. |
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| 13 | Mechanism for a munition device | EP90202944.6 | 1990-11-07 | EP0437871A3 | 1991-09-04 | Karlstedt, Gustav |
Mechanism for a muniton device. The mechanism includes a housing (1) containing an arming element (3) and a spindle (9) capable of giving the arming element an axial movement. The spindle (9) is operatively connected to the arming element (3) via a conveyor means (10) which has a thread profile (12), the conveyor means being pivotally journalled in the arming element such that it is able to be turned between a first position (Figures 1 and 2), wherein the thread profile (12) is in engagement with the spindle (9), to a second position (Figures 4 and 7) wherein the thread profile (12) of the conveyor means is disengaged from the spindle. Spring means (4, 13), are arranged, in the armed position of the conveyor means, to return the arming element to said engagement with the movable member. |
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| 14 | Sicherheitsvorrichtung für einen Aufschlagzünder an einem Geschoss | EP84110184.3 | 1984-08-27 | EP0139173A1 | 1985-05-02 | Apothéloz, Robert, Dipl. Masch. Tech. |
Der Aufschlagzünder besitzt einen Querschieber (10) mit einer Zündpille 11, die aus einer Sicherheitsstellung in eine Scharfstellung verschiebbar ist, wobei der Schieber (10) einerseits durch eine auf die Abschussbeschleunigung ansprechende Sperrvorrichtung (17) und andererseits durch einen manuell entriegelbaren Zündstift (4) in seiner Sicherheitsstellung gehalten ist. Eine zusätzliche Verriegelung (32,33) verhindert, dass der Querschieber (10) durch den Zündstift (4) freigegeben werden kann, falls die Sperrvorrichtung (17) den Querschieber (10) bereits freigegeben hat. |
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| 15 | VORRICHTUNG UND VERFAHREN ZUR BESEITIGUNG EINES NICHT EXPLODIERTEN KAMPFMITTELS UNTER WASSER | EP19158392.1 | 2019-02-20 | EP3527928A1 | 2019-08-21 | Michael, Freudenthal |
Die vorliegende Erfindung betrifft eine Vorrichtung und ein Verfahren zur Beseitigung eines nicht explodierten Kampfmittels, das unter Wasser auf Grund liegt. Die Vorrichtung ist als Kampfmittelräumungsgerät (1) mit einem Rahmen (5) für einen Transport und eine Positionierung durch einen Tauch-Roboter (ROV) ausgebildet und umfasst neben einer Sprengladung (4) mit einem Zünder (34) eine von dem Kampfmittelräumungsgerät (1) lösbare und sodann an die Wasseroberfläche (WO) aufsteigende Boje (2). Um eine bekannte Vorrichtung weiterzubilden, um damit auch ein entsprechendes Verfahren unter Erschließung weiterer Kosten- und Effizienz-Potentiale bei erhöhter Sicherheit und vereinfachter Handhabung noch effizienter zu gestalten, wird vorgeschlagen, dass das Kampfmittelräumungsgerät (1) eine Einrichtung (14) aufweist, durch die die Boje (2) durch das ROV von dem Kampfmittelräumungsgerät (1) lösbar ist, wobei diese Einrichtung (14) im Bereich des Rahmens (5) ein federelastisch gesichertes Sperrelement insbesondere in Form eines Federsteckers (20) umfasst, das durch den Tauch-Roboter (ROV) abziehbar ist.
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| 16 | WIEDERSICHERUNG FÜR EINEN KIPPHEBELZÜNDER | EP11721437.9 | 2011-05-14 | EP2577219B1 | 2014-07-23 | MÜLLER, Christian Johann; BASSE, Klaus; BOSSE, llka; SCHÜTZENDÜBEL, Wolfgang; WETZEL, Gabriele |
| 17 | WIEDERSICHERUNG FÜR EINEN KIPPHEBELZÜNDER | EP11721437.9 | 2011-05-14 | EP2577219A1 | 2013-04-10 | MÜLLER, Christian Johann; BASSE, Klaus; BOSSE, llka; SCHÜTZENDÜBEL, Wolfgang; WETZEL, Gabriele |
| The invention relates to a re-securing element for a rocker-arm detonator (1) of an explosive body, such as a hand grenade or stun grenade, formed by a securing mechanism (3), which allows the rocker-arm detonator to be re-secured after the explosive body has been activated, comprising at least one profiled part (4, 4'), which is rotatably supported and which can engage with the explosive body, in particular with the detonating head (5, 5') and with the rocker arm (2), by means of an element (9). | ||||||
| 18 | SELF DESTRUCTING IMPACT FUSE | EP99931740.7 | 1999-04-23 | EP1155279A1 | 2001-11-21 | AW, Cheng, Hok; EE, Guan, Soon; TAN, Chian, Chiow |
| A self destructing impact fuse including a cylindrical firing pin having a hollow centrifugal chamber for holding a number of spheres and a number of radial openings on its surface for exposing portions of the spheres when the chamber is spun. At one end of the chamber is a spring for exerting compression force along the longitudinal axis of the chamber and at the other end is a self-destructing (SD) firing pin for striking the detonator. A centrifugal lock having a pivot offset from the longitudinal axis holds the chamber in place by mating with a groove on the surface of the centrifugal chamber. The cylindrical firing pin is seated concentrically within a frame and disposed over an escapement assembly featuring the detonator. The detonator is rotated into alignment with the SD firing pin after the projectile, incorporating the fuse, travels the minimum tactical distance. The frame is further coupled with a base, which features a point detonation (PD) firing pin for striking the detonator. | ||||||
| 19 | Mechanism for a munition device | EP90202944.6 | 1990-11-07 | EP0437871B1 | 1994-07-20 | Karlstedt, Gustav |
| 20 | SUBMARINE FLARE | EP87905920.2 | 1987-08-21 | EP0318515B1 | 1992-08-05 | RAMSAY, Peter; WHIFFEN, Brian, William; BUSHNELL, Gerald, Montague; NANUT, Victor; CZIGLEDY, Robert, Charles; SWINTON, Robert, James; COXHEAD, Maxwell, John; CLARKE, Timothy, Robert |
| A flare (1) for submarine use. The flare (1) is caused to be deployed from a submarine location where it will rise to the surface of the water because of its buoyant casing. A hydrostatic valve means (147) is provided within the casing and it opens when the flare is at or near the surface of the water to render said flare ready to project a flare composition (5) into the air. The hydrostatic valve means (147) is held inoperative by a latch mechanism (51) which is tripped as the flare is deployed from a firing tube at the submarine location. The flare composition (5) cannot be projected into the air until the flare (1) is within a range of vertical attitude determined by inclination means (13). The flare composition (5) cannot be projected into the air until the nose is above water. The flare (1) thus has a sensor (23) at its forward nose to determine that the nose is above the water. A time delay means (87) is provided which is initiated by a pyrotechnic medium (85) used to project the flare composition (5) into the air, to delay ignition of the flare composition (5) until it has at leastcleared the surface of the water. | ||||||
