| 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 | FUZING SYSTEM FOR A SUBMARINE SIGNAL FLARE | EP11853651.5 | 2011-12-27 | EP2659220A1 | 2013-11-06 | HAGEL, Johan; HAGEL, Erik; PETTERSSON, Lars-Erik; BORGSTRÖM, Ulf; FLODQVIST, Urban |
| The present invention relates to a fuzing system for a signal flare for use on a submarine vessel, said system comprising an ignition system that is operationally connected to a signalling substance in such a way that said signalling substance can be ignited by activating said ignition system, wherein a hydrostatic device is arranged to activate said ignition system at a predetermined pressure | ||||||
| 122 | Dispositif d'allumage | EP12187334.3 | 2012-10-05 | EP2578077A1 | 2013-04-10 | Villanou, Jean-Pierre |
La présente invention concerne un dispositif (1) d'allumage (1), constitué d'une enveloppe fermée à une extrémité et comprenant une ouverture à l'extrémité opposée, caractérisé par le fait que ladite enveloppe est divisée en au moins deux compartiments, un premier compartiment situé du coté de ladite ouverture étant rempli au moins en partie d'un matériau déflagrant (11), et un second compartiment étant rempli au moins en partie d'un matériau inflammable (18), ledit dispositif (1) comprenant encore des moyens d'ignition (10) au moins dudit matériau déflagrant (11).
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| 123 | AKTIVIERUNGSEINHEIT FÜR MUNITIONSFREIE SCHEINZIELE | EP09776700.8 | 2009-06-08 | EP2300772B1 | 2012-10-17 | GUTH, Sven; EGLAUER, Heribert; OLIVER, Frank; HUBER, Florian; PRELIC, Nenad |
| 124 | AKTIVIERUNGSEINHEIT FÜR MUNITIONSFREIE SCHEINZIELE | EP10754888.5 | 2010-09-15 | EP2483624A1 | 2012-08-08 | PRELIC, Nenad; EGLAUER, Heribert |
| The invention relates to an arc-based active body activation unit (10). To this end, ignition of the active mass or flare is effected by means of arcing (19, 20). The arc (19, 20) can be used immediately and is low-maintenance. For that purpose, electrode pairs (11, 12, 21, 22) are disposed around the ejector tube, at least one of which pairs serves the ignition of the arc(s) (19, 20). For that purpose, the electrode pairs (11, 12, 21, 22) are electrically connected by means of connecting lines (15-18) to at least one control unit (13, 14). | ||||||
| 125 | VERBRENNBARER WIRKMASSENCONTAINER | EP10723950.1 | 2010-06-15 | EP2446218A1 | 2012-05-02 | PRELIC, Nenad; KADAVANICH, Vikorn Martin; EGLAUER, Heribert; GAISBAUER, Rainer; HUBER, Florian |
| Proposed is an active body (2) comprising, as active mass, multiple flares (3, 4) arranged behind each other or stacked, in particular for the generation of decoys. The active body (2) is enclosed in a plastics-like container (1) such as a plastic film (5) or a shrink tube (7). Plastics disks or films (8) are placed on the end face of the container and are connected to the plastics film (5) or the tube (7) by adhesion or heat sealing (6) such that the container (1) is hermetically sealed. | ||||||
| 126 | AKTIVIERUNGSEINHEIT FÜR WIRKMASSEN BZW. WIRKKÖRPER | EP10713857.0 | 2010-04-16 | EP2427720A1 | 2012-03-14 | PRELIC, Nenand; FRANK, Oliver; EGLAUER, Heribert; HUBER, Florian |
| The invention relates to an activation unit (1) for explosive masses or explosive bodies (3), characterized by an ejector tube (2) and high-performance heating elements (4) mounted around the ejector tube (2), each made of at least one heating wire (6) supplied with electrical power by a control unit. Each heating wire (6) is enclosed in a jacket (7) and at least embedded in a material minimizing heat loss. When the explosive body (3) is passed through the activation unit (1), the jacket surface of the explosive body (3) contacts the individual elements (4) of the activation unit (1) in a direct or non-contact manner. The thermal energy is transferred to the explosive body (3) by means of the heating wires (6), and said body ignites at the contact points. A further activation unit (1', 1") comprises heating elements (10, 10') in the ejector tube (2', 2") at least partially fed longitudinally through the ejector tube (2', 2") made of heating wire (14) clad with CrNi steel (11) and contact tabs (13) soldered thereto. | ||||||
| 127 | DATA BUS FOR LOW POWER TAG | EP10701396.3 | 2010-01-12 | EP2425347A1 | 2012-03-07 | BIRKBECK, John |
| A power supply and communication system comprising a single-wire data bus, itself having comprising a source end and a termination end, the termination end being connected to ground through a resistance of less than 10Ω. A circuit is connected at the termination end, between the single-wire data bus and ground, and the circuit comprises means for deriving its supply voltage and receiving input data from a time-variant signal applied to the single-wire data bus. | ||||||
| 128 | LOW FOREIGN OBJECT DAMAGE (FOD) WEIGHTED NOSE DECOY FLARE | EP10767679.3 | 2010-04-21 | EP2422162A1 | 2012-02-29 | HERBAGE, David W.; PHILLIPS, Alan; LEIFSON, Everard; THOMAS, Keven |
| The present invention discloses a low foreign object damage nose weight for affixing to a either a standard or kinematic decoy flare comprising a thin walled nose cup having a closed end, an open end, an internal cavity, and at least one sidewall attached to said closed end and surrounding said internal cavity; and a metal powder disposed within the internal cavity for weighing down the forward end of the decoy flare, said nose cup capable of being affixed to a forward end of a decoy flare such that said powder is jettisoned from said nose cup upon burn out of a flare pellet subassembly of said decoy flare thereby reducing the weight of the nose cup and the possibility of foreign object damage to aircraft, ground troops, ground equipment and buildings resulting from the falling nose weight. | ||||||
| 129 | WIRKKÖRPER | EP05768690.9 | 2005-07-28 | EP1794537B1 | 2012-02-29 | GAISBAUER, Rainer; BANNACH, Heinz; KADAVANICH, Vikron; FEGG, Martin; WAGNER, Christian |
| The invention relates to an explosive body comprising at least one explosive material block (1) made of monobasic or polybasic high-energy materials, such as a nitrocellulose mixture consisting of approximately 60 % nitroglycerin and 40 % diethylene glycol dinitrate, provided with structures on the surface (2) as well as in the interior (3). The inner structures (3) are, in addition, preferably filled up with an explosive material substance (4). The ignition ensues by means of a pyrotechnical primer composition (7) that initiates the explosive body preferably from the inside. | ||||||
| 130 | Flugkörper mit einem pyrotechnischen Satz | EP10009315.2 | 2010-09-08 | EP2295927A2 | 2011-03-16 | Hahma, Arno |
Die Erfindung betrifft einen Flugkörper mit einem pyrotechnischen Satz (2), wobei der Flugkörper so ausgestaltet ist, dass der pyrotechnische Satz (2) bei bestimmungsgemäßer Verwendung des Flugkörpers deflagrativ zum Abbrand gebracht wird, wobei der pyrotechnische Satz (2) ein Gemisch umfasst, welches mindestens ein Metall oder eine Metalllegierung als Brennstoff und mindestens ein Metalloxid als Oxidationsmittel enthält, wobei der Brennstoff und das Oxidationsmittel so gewählt sind, dass sie durch Abbrand miteinander reagieren können, wobei das Gemisch auf eine Dichte von mindestens 85 % der theoretischen Dichte des Gemischs verdichtet ist, wobei der Brennstoff, das Oxidationsmittel und das Mengenverhältnis zwischen dem Brennstoff und dem Oxidationsmittel so gewählt sind, dass die Dichte des Gemischs mindestens 6 g/cm3 beträgt.
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| 131 | FLARE MIT FLAREANZÜNDUNG SOWIE AUSSTOSSSYSTEM DAFÜR | EP09776699.2 | 2009-06-08 | EP2288866A1 | 2011-03-02 | GUTH, Sven |
| A flare ignition for an ejectable flare (10) for protecting moving and/or stationary objects from heat-seeking threats is disclosed, characterised by a heat transfer within a type of tube or tube nozzle (1) with heating elements. Said flare ignition is integrated in an ejector system (2) which additionally comprises an accelerator unit (3) surrounding the tube nozzle (1) and a heat insulation (4) bound between the two. | ||||||
| 132 | Munition oder Geschoss zur Gefechtsfeldbeleuchtung | EP08017765.2 | 2008-10-10 | EP2063215A2 | 2009-05-27 | Aumund-Kopp, Ralf; Dau, Ole; Münzner, Sebastian; Naderhoff, Uwe; Schwenzer, Michael; Thape, Manfred; Rybol, Martin |
Vorgeschlagen wird ein Geschoss (1) mit mehreren Leuchtkörpern (7), die in einer Geschosshülle (2) exzentrisch eingebracht sind und über wenigstens ein Verzögerungselement (11, 12) je Leuchtkörper (7) gezündet werden. Die Übertragung der Ausstoßgase von einer Geschossogive (9) zu den Verzögerungselementen (11, 12) erfolgt durch Füllelemente (8), die mittig im Geschoss (1) einen Kanal (10) für die Ausstoßgase bilden.
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| 133 | A thermic lance | EP07251551.3 | 2007-04-11 | EP1845231A3 | 2007-11-14 | Downie, Neil Alexander |
The present invention relates to use of a thermic lance (102) as a firework. Frictional (558) or electrical ignition (126) of a thermic lance is more convenient and safer than conventional methods. In addition, when used as a firework, the lance is safer and provides less pollution than conventional fireworks.
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| 134 | A thermic lance | EP07251551.3 | 2007-04-11 | EP1845231A2 | 2007-10-17 | Downie, Neil Alexander |
The present invention relates to use of a thermic lance (102) as a firework. Frictional (558) or electrical ignition (126) of a thermic lance is more convenient and safer than conventional methods. In addition, when used as a firework, the lance is safer and provides less pollution than conventional fireworks.
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| 135 | INFRA-RED EMITTING DECOY FLARE | EP00993925.7 | 2000-12-13 | EP1342047B1 | 2006-02-22 | CALLAWAY, James Dominic, DSTL; SUTLIEF, Timothy Douglas, DSTL Fort Halstead |
| An infra-red emitting decoy flare capable of diverting an incoming missile equipped with a counter-countermeasures system away from an intended target consisting of a primer flare (2), a spectral flare (4) and a means for igniting the primer flare (22, 30), all contained within a flare casing (6). The primer flare (2) is formed from a fast burning pyrotechnic composition and is adapted to produce an intense infra-red source of short duration on ignition. The spectral flare (4) is ignited by the burning of the primer flare (2) and is adapted to produce a slower burning composition having a fixed ratio in the intensity of infra-red radiation emitted, when burning, in at least two fixed bands. | ||||||
| 136 | SCHLEPPKÖRPER ZUR FLUGZIELDARSTELLUNG | EP01995580.6 | 2001-12-06 | EP1348102A1 | 2003-10-01 | KAPP, Rolf; WEIMER, Peter |
| The invention relates to a towed body for representing an airborne target. The towed body comprises infrared flares (3) situated at the rear thereof, whereby the infrared flares can be ejected from the towed body and are towed during the burning duration of the infrared flare by the towed body by means of a towing cable that can unreel. According to the invention, the infrared flares (3) have an annular wing (1) situated at the rear. | ||||||
| 137 | Nozzles for pyrophoric IR decoy flares | EP98306250.6 | 1998-08-05 | EP0905472B1 | 2002-10-30 | Brière, Paul; St-Onge, Michel; Roy, André |
| 138 | HIGH-INTENSITY INFRARED DECOY FLARE | EP96913021 | 1996-04-23 | EP0870164A4 | 2000-10-18 | TAPPAN RALPH S II; ANDERSON RICHARD C; ENDICOTT DAVID W JR |
| An infrared decoy flare (10) having enhanced infrared intensity is disclosed. The flare includes a case (12) in which an infrared illuminant composition (14) is disposed. The bore diameter and length of the case are advantageously selected to be compatible with preexisting chaff dispensers and their cartridges located on aircraft. The illuminant composition, the nozzle throat area, the geometry of the illuminant composition, and the volume of the combustion chamber are selected such that combustion of the illuminant composition results in an unstable combustion condition during the first second of combustion, thereby increasing the peak intensity of the radiation emitted by the propellant. Preferably, the flare is configured such that the unstable combustion occurs during the first 0.2 to 0.5 seconds of combustion of the illuminant composition. | ||||||
| 139 | HIGH-INTENSITY INFRARED DECOY FLARE | EP96913021.0 | 1996-04-23 | EP0870164A1 | 1998-10-14 | TAPPAN, Ralph, S., II; ANDERSON, Richard, C.; ENDICOTT, David, W., Jr. |
| An infrared decoy flare (10) having enhanced infrared intensity is disclosed. The flare includes a case (12) in which an infrared illuminant composition (14) is disposed. The bore diameter and length of the case are advantageously selected to be compatible with preexisting chaff dispensers and their cartridges located on aircraft. The illuminant composition, the nozzle throat area, the geometry of the illuminant composition, and the volume of the combustion chamber are selected such that combustion of the illuminant composition results in an unstable combustion condition during the first second of combustion, thereby increasing the peak intensity of the radiation emitted by the propellant. Preferably, the flare is configured such that the unstable combustion occurs during the first 0.2 to 0.5 seconds of combustion of the illuminant composition. | ||||||
| 140 | Leurre stabilisé et propulsé émettant dans l'infra-rouge | EP93401683.3 | 1993-06-30 | EP0583176B1 | 1997-05-14 | Meili, Gérard; Pinchot, Jean-Luc |
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