| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 141 | Flare pellet and process for making same | EP95300617.8 | 1995-01-31 | EP0665415A3 | 1996-05-01 | Dillehay, David R.; Turner, David W. |
A process for forming decoy flare pellets which satisfy predetermined burn requirements without milling additional grooves into the pellet flare material after that material is consolidated, involves providing sufficient surface area to the flare material during consolidation to eliminate the need for milling. Consolidated flare pellets are then coated with an ignition composition and installed in a decoy flare housing. |
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| 142 | PROCEDE, COMPOSITION PYROTECHNIQUE ET DISPOSITIF POUR PRODUIRE DES FLAMMES COLOREES | EP93911795.0 | 1993-04-28 | EP0638161A1 | 1995-02-15 | BERNARDY, Claude |
| The invention provides for the production of a flame which has variable sizes, colors and shapes. The invention discloses also a torch which forms a self-contained and easy-to-handle lighting lamp. The handling of said lamp or torch is easy and provides satisfactory security conditions to the user. The compositions enable the vaporization of liquids in small amounts and are usable to colour the flames of lighters. | ||||||
| 143 | Infrared illuminant | EP91304243.8 | 1991-05-10 | EP0457518B1 | 1994-12-07 | Nielson, Daniel B.; Jones, Leon L. |
| 144 | Infrared illuminant | EP90312213.3 | 1990-11-08 | EP0430464B1 | 1994-09-28 | Nielson, Daniel B.; Jones, Leon L. |
| 145 | Infrared illuminant | EP91304243.8 | 1991-05-10 | EP0457518A3 | 1992-04-15 | Nielson, Daniel B.; Jones, Leon L. |
An infrared illuminant composition and flares produced therefrom having increased burn rate and increased infrared intensity while maintaining low visible light intensity. The composition comprises potassium nitrate, cesium nitrate, hexamine, boron, silicon, ferric oxide and a binder. A process to produce infrared illuminant flares prevents or substantially eliminates chunking out of burning pieces of the illuminant at pressing increments in the flares. A multi-stepped pressing foot (10) is used for pressing the composition in the case. |
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| 146 | SMOKE GRENADE | EP86902527.0 | 1986-04-14 | EP0220228B1 | 1989-06-28 | VARMO, Kjell, Ole |
| A smoke grenade comprising a launching device (1), an instantaneous smoke device (2) and an IR-smoke generator (3) is provided with a casing (4) which can be deformed to guiding/supporting fins (4'). | ||||||
| 147 | Infrared signature enhancement decoy | EP88307857.8 | 1988-08-24 | EP0309097A1 | 1989-03-29 | Dunne, Anthony L.; Huber, Joseph C., Jr. |
This invention generally relates to aircraft counter-measures and more particularly to an infrared decoy flare (40,60,70,80,90,100,110) which operates in a substantially aerodynamic configuration and effectively shields aerodynamic cooling associated with its operation when ejected into the adjacent windstream of a tactical aircraft. The decoy provides an enhanced infrared signature to IR and heat-seeking threats to effectively decoy them away from the protected aircraft. |
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| 148 | Projectile for emitting IR radiation | EP86105294 | 1986-04-16 | EP0204115A3 | 1988-09-21 | |
| 149 | A flare charge insulation, a method of its manufacture and a flare charge manufactured according thereto | EP87850163.4 | 1987-05-15 | EP0247013A2 | 1987-11-25 | Gellerstedt, Nils; Johansson, Siv |
The present invention relates to a novel type of flare charge insulation for retally burning flare charges. The flare charge insulation (4) according to the present invention is produced by compaction of a particulate material or granulate of a mean particle size wich does not exceed 1 mm. The major component parts of the granulate are an organic metal salt, and minor amounts of a combustible binder. Moreover, particulate melamine may be included in an amount of up to 2O weight per cent. The present invention also includes a novel method of producing flare charges (1) in which both the flare charge and flare charge insulation are terminally compacted together to form a continuous unit. Consequently, the present invention also relates to the finished flare charge manufactured according thereto. |
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| 150 | Eclairant pyrotechnique de grande puissance | EP82400716.5 | 1982-04-21 | EP0064444B1 | 1985-06-26 | Billard, Alain |
| 151 | Eclairant pyrotechnique de grande puissance | EP82400716.5 | 1982-04-21 | EP0064444A1 | 1982-11-10 | Billard, Alain |
Une structure-support creuse (1) reçoit intérieurement et axialement une première composition pyrotechnique à retard (2), tandis qu'elle reçoit dans des orifices (101 à 151), placés radialement, et de longueur décroissante, une seconde composition pyrotechnique (4) plus lente que la première. Un initiateur (3) déclenche la première composition (2) du côté où les orifices traversants radiaux sont les plus longs. A l'extérieur est placée une composition éclairante (5), qui peut alors être allumée pratiquement en même temps sur toute la longueur du produit. Application notamment comme contre-mesure optique ou infrarouge. |
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| 152 | COMPOSITIONS USABLE AS FLARE COMPOSITIONS | US16208840 | 2018-12-04 | US20190100473A1 | 2019-04-04 | Daniel B. Nielson; Curtis W. Fielding |
| A composition that includes a fuel and a perfluoropolyether (PFPE) is disclosed. The composition may be used as a flare composition in a countermeasure device. Countermeasure devices including the flare composition are also disclosed, as are methods of forming grains of the countermeasure device. | ||||||
| 153 | System and method of coordinated infrared suppression and flare launch | US15252850 | 2016-08-31 | US09915506B1 | 2018-03-13 | David Anthony Vaitekunas |
| Systems and methods are provided that employ an IR suppression system to alter the signature of a vessel during a missile engagement with the objective of confusing a seeker of an incoming missile so as to increase the probability that the seeker is seduced by a flare. The flare is launched and IR suppression is enabled or set to an increased level, with coordinated timing, such that the IR signature of the target vessel is changed at about the same time that the flare is launched. | ||||||
| 154 | FLOATING OIL SPILL IGNITION DEVICE | US15611389 | 2017-06-01 | US20170350084A1 | 2017-12-07 | Chris Seyfarth |
| An igniter device (10) operable to remediate a floating oil spill in a body of water is provided. The device (10) comprises a pyrotechnic device (28) that is actuated through an actuator assembly (20) comprising time delay circuitry (24). Upon actuation, the time delay circuitry (24) begins a countdown permitting the device (10) to be safely deployed from an aerial vehicle. The pyrotechnic device (28) ignites a fuel source (38), which in turn ignites the floating oil spill. | ||||||
| 155 | Countermeasure Flares | US15646022 | 2017-07-10 | US20170314896A1 | 2017-11-02 | Jahangir S. Rastegar; Richard T. Murray; Gretel Raibeck; Jay Poret; Brandon Andreola; Andrew Zimmer |
| A flare including: a casing; and a grain assembly, at least a portion of the grain assembly being slidably disposed in the casing, the grain assembly including: a shell structure; and a grain component at least partially disposed in the shell structure, the grain component including at least one combustible material and at least one reactive material positioned relative to the combustible material and configured to ignite combustion of the at least one combustible material; wherein the shell structure includes one or more nozzles at an aft end of the shell structure for generating a thrust resulting from ignition of the at least one combustible material. | ||||||
| 156 | Low foreign object damage (FOD) weighted nose decoy flare | US13946547 | 2013-07-19 | US09494393B1 | 2016-11-15 | David W. Herbage; Alan Phillips; Everard Leifson; Keven Thomas |
| 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. | ||||||
| 157 | Countermeasure Flares | US13971831 | 2013-08-20 | US20160216086A1 | 2016-07-28 | Jahangir S. Rastegar; Richard T. Murray; Gretel Raibeck; Jay Poret; Brandon Andreola; Andrew Zimmer |
| Methods and devices for ejecting a grain assembly from a casing of a flare. Where a combustible material in the casing is ignited to eject the grain assembly and one or more of the following features are provided to the device: imparting a spin on the grain assembly after it is ejected from the casing, stabilizing a flight of the grain assembly or generating a thrust from an aft end of the grain assembly. | ||||||
| 158 | Torch for cutting or perforation | US14012373 | 2013-08-28 | US09259795B1 | 2016-02-16 | Aaron M. Taylor; John J. Granier; Dennis E. Wilson; Darrel R. Barnette |
| One example of a system includes a reactive material, a nozzle, a liner, and an igniter in a breaching tool suitable for hand-held operation. The nozzle includes at least one exit aperture and is configured to direct a discharge produced by combustion of the reactive material. The liner is disposed around the reactive material and connected to the nozzle. The liner is configured to confine the discharge to the at least one exit aperture. The igniter is disposed within the liner and in contact with the reactive material. | ||||||
| 159 | Spooling Pyrotechnic Device | US14703452 | 2015-05-04 | US20150233686A1 | 2015-08-20 | Darren Naud |
| A pyrotechnic device including a combustion chamber including a wall, the combustion chamber containing combustible powder; an ignition source adapted to ignite said combustible powder within said combustion chamber; wherein the wall of the combustion chamber is adapted to burst at a predetermined pressure caused by combustion of the combustible powder; wherein the combustion chamber is disposed within a launch structure beneath a projectile and wherein a preselected amount of free space volume is disposed between said combustion chamber and said projectile. | ||||||
| 160 | Encapsulated effect body for an infrared decoy | US13627451 | 2012-09-26 | US09062941B2 | 2015-06-23 | Johannes Grundler; Juergen Hofmann; Rainer Gaisbauer; Markus Jung; Michael Koepf |
| An effect body is encapsulated in such a way that the encapsulation or casing supports the ignition behavior of the effect body or of the components. The effect body has a casing for accommodating the components of the effect body, which differ with regard to the chemical composition and the properties thereof. An additional component is located in the casing as an ignition aid. The effect body can be ignited through the top/side surface of the casing or by an internal ignition mixture located inside the effect body. | ||||||
