| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 161 | COQUE DE NAVIRE COMPORTANT AU MOINS UN FLOTTEUR | EP06794309.2 | 2006-08-08 | EP1917180B1 | 2009-12-30 | GOUBAULT, Philippe; FUMERY, Benoît |
| The inventive ship hull comprises at least one float (10) and a centre of buoyancy (CB) situated behind the centre of flotation (CF), the distance between said centre of buoyancy and centre of flotation is greater by 5 % than the waterline length L of the hull. | ||||||
| 162 | NAVIRE ARME DE SURFACE FURTIF | EP06794324.1 | 2006-08-10 | EP1917182B1 | 2009-10-07 | PHILIPPE, Serge; GOUBAULT, Philippe; MERVIN, Yves; BARDES, Claudia; LE GAC, Christian |
| The invention relates to an armed stealth surface vessel (1) comprising a hull (2), a deck (5, 6) and superstructures (3). The inventive vessel is equipped with sensors, transmitters, arms and, optionally, handling means. The invention is characterised in that the outer casing (4) of the deadworks comprises walls which are all inclined inwards such that the outer faces thereof are oriented upwards and form an angle that is greater than or equal to 20° with the vertical at least above a line located 5 m above the waterline and, along at least 50 % of the length of the vessel, above a line located less than one metre above the waterline. The invention is also characterised in that that the essentially-vertical joint lines between two adjacent walls are inclined inwards and form an angle of more than 20° with the vertical. The invention is further characterised in that the sensors and transmitters, the arms and the handling means are concealed or can be concealed in or under the outer casing of the deadworks. | ||||||
| 163 | Foldable ramp for missile launchers | EP07119060.7 | 2007-10-23 | EP2053337A1 | 2009-04-29 | Onuk, Ekber I. N. ONUK Tasit Sanayi Limited Sirketi |
The foldable ramp (1) is intended to store, carry and launch relatively large size tube- launched missiles typically on board of relatively small sized naval surface ships. Accordingly, the foldable ramp (1) comprises a frame (10) suitable for carrying one or more canisters (11) for launching rockets or missiles and support elements (12,13), which are pivotably attached to the frame (10) and which are adapted to pivotably connect to the launching platform so as to allow rotary movement of the frame (10) with respect to the launching platform. A lifting device (14) lifts the front end of the frame (10) whereby the rear end of the canisters (11) displace a horizontal distance towards the rear of the ramp (1) as said lifting device (14) lifts the frame (10). Adverse effects of the aft flame of the launched rocket or missile is securely displaced to the outside of the vehicle while foldability of the ramp (1) enables to prevent or reduce radar and eye visibility of the launcher, particularly when mounted on a naval surface ship.
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| 164 | NAVIRE ARME DE SURFACE FURTIF | EP06794324.1 | 2006-08-10 | EP1917182A1 | 2008-05-07 | PHILIPPE, Serge; GOUBAULT, Philippe; MERVIN, Yves; BARDES, Claudia; LE GAC, Christian |
| The invention relates to an armed stealth surface vessel (1) comprising a hull (2), a deck (5, 6) and superstructures (3). The inventive vessel is equipped with sensors, transmitters, arms and, optionally, handling means. The invention is characterised in that the outer casing (4) of the deadworks comprises walls which are all inclined inwards such that the outer faces thereof are oriented upwards and form an angle that is greater than or equal to 20° with the vertical at least above a line located 5 m above the waterline and, along at least 50 % of the length of the vessel, above a line located less than one metre above the waterline. The invention is also characterised in that that the essentially-vertical joint lines between two adjacent walls are inclined inwards and form an angle of more than 20° with the vertical. The invention is further characterised in that the sensors and transmitters, the arms and the handling means are concealed or can be concealed in or under the outer casing of the deadworks. | ||||||
| 165 | ADAPTIVE MODIFICATION OF SURFACE PROPERTIES TO ALTER THE PERCEPTION OF ITS UNDERLYING STRUCTURE | EP05807761.1 | 2005-03-08 | EP1856768A1 | 2007-11-21 | Snaper, Alvin A. |
| Adaptive modification of surface properties such as color, temperature and reflective properties by adjustably varying the temperature of a surface perceived by an observer, utilizing Peltier devices (60) at the surface for temperature adjustment. | ||||||
| 166 | AUSRÜSTUNGSSYSTEM-SCHIFFSTYP "KORVETTE" | EP03747834.4 | 2003-09-12 | EP1537016B1 | 2007-01-17 | SCHULZE, Matthias; RZADKI, Wolfgang; SADLER, Karl-Otto; SCHULZE HORN, Hannes |
| The invention relates to a corvette ship-type equipment system comprising standard-equipment segments, such as an energy generator, an energy distributor, a drive and an automation segment, and a hull (1) which is adapted to the size and specific requirements on the corvette ship-type equipment system. According to the invention, in order to construct standard equipment-segments for a corvette ship-type equipment system which is technically and constructively simple and economical in terms of cost, at least one of the standard-equipment segments, such as the energy generator and/or the energy distributor and/or the drive and/or the automation segment is constructed from standard units or components which correspond to the requirements of the corvette ship-type equipment system and which are arranged in the hull of the boat (1) and which can be built into the hull of the boat according to different boat or ship-type equipment systems. | ||||||
| 167 | RETROFITTING VESSELS TO DEFLECT RADAR SIGNALS | EP00945463.8 | 2000-07-26 | EP1210562B1 | 2006-10-04 | STAFFORD, Philip, K. |
| The radar signature of a vessel is reduced by retrofitting it with an array (10) of elements (15) fastened to surfaces (14b) of the vessel. The elements (15) have planar faces (11-12) so oriented that incident radar signal (20) is reflected away from its angle of incidence. | ||||||
| 168 | Radar-getarnter Werfer | EP03025308.2 | 2003-11-03 | EP1426726B1 | 2006-08-23 | Folgmann, Uwe; Fegg, Martin |
| 169 | ADAPTIVE COMPLIANT WING AND ROTOR SYSTEM | EP04749349.9 | 2004-03-03 | EP1603798A1 | 2005-12-14 | KOTA, Sridhar; HETRICK, Joel, A. |
| Variation in the contours of first and second compliant surfaces is produced by a compliant frame having a first resiliently variable frame element ( 120 ) having a corresponding first outer surface ( 122 ) and a first inner surface ( 124 ), and a second resiliently variable frame element ( 130 ) having a corresponding second outer surface ( 132 ) and a second inner surface ( 134 ). The first and second outer surfaces ( 122, 132 ) communicate with respective ones of the first and second compliant surfaces. A linkage element ( 141 - 144 ) having a predetermined resilience characteristic is coupled at a first end thereof to the first inner surface ( 124 ) and at a second end thereof to the second inner surface ( 134 ). A frame coupler ( 151 ) couples the first resiliently variable frame element ( 120 ) to a support element ( 150 ). An actuator ( 106 ) applies a force to the second resiliently variable frame element ( 130 ) with respect to the support element (150), resulting in a corresponding variation in the contour of the first and second compliant surfaces. | ||||||
| 170 | Radar-getarnter Werfer | EP03025308.2 | 2003-11-03 | EP1426726A1 | 2004-06-09 | Folgmann, Uwe; Fegg, Martin |
Die vorliegende Erfindung betrifft eine Vorrichtung zum Ausbringen von Munition, wobei eine vorgesehene Aussparung (2) in der Außenhülle (1) eines Fahrzeuges, insbesondere eines Schiffes mit einer Abdeckeinrichtung (4) abgedeckt ist, so daß eine durch diese Aussparung (2) verursachte, sich negativ auswirkende Erhöhung der Radarsignatur vermindert wird. |
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| 171 | Einrichtung zur Verringerung der Infrarot-Emission bei amphibischen Fahrzeugen, insbesondere Panzerfahrzeugen | EP03450234.4 | 2003-10-23 | EP1424223A1 | 2004-06-02 | Strassgürtl, Anton, Ing.; Koleszar, Béla, Dipl.- Ing. |
Eine Einrichtung zur Verringerung der Infrarot-Emission bei amphibischen Fahrzeugen (1), insbesondere Panzerfahrzeugen zeichnet sich dadurch aus, daß bei einem amphibischen Einsatz der Auspuffstrom gegen die Wasseroberfläche gerichtet ist, wobei das Ausströmende (8) des Auspuffs knapp oberhalb der Wasseroberfläche angeordnet ist. |
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| 172 | RETROFITTING VESSELS TO DEFLECT RADAR SIGNALS | EP00945463 | 2000-07-26 | EP1210562A4 | 2004-03-24 | STAFFORD PHILIP K |
| The radar signature of a vessel is reduced by retrofitting it with an array (10) of elements (15) fastened to surfaces (14b) of the vessel. The elements (15) have planar faces (11-12) so oriented that incident radar signal (20) is reflected away from its angle of incidence. | ||||||
| 173 | Schwingungsdämpfungsvorrichtung für Antriebsaggregate von Schiffsantriebsanlagen von Über- und Unterwasserschiffen | EP03011252.8 | 2003-05-16 | EP1366984A1 | 2003-12-03 | Bechtold, Mario; Schulze, Matthias |
Schwingungsdämpfungsvorrichtung für Antriebsaggregate von Schiffsantriebsanlagen von Über- und Unterwasserschiffen Eine Schwingungsdämpfungsvorrichtung für Antriebsaggregate (2) von Schiffsantriebsanlagen von Über- und Unterwasserschiffen hat Schockdämpfungselemente (14), die in Lagerungen (11, 12) des Antriebsaggregats (2) integriert sind. Um mittels der Schockdämpfungselemente (14) nicht kompensierbare Schwingungen und Geräusche des Antriebsaggregats (2) zu kompensieren, wird vorgeschlagen, dass die Schwingungsdämpfungsvorrichtung (1) Körperschalldämpfungselemente (3) aufweist, die in die Lagerungen (11, 12) des Antriebsaggregats (2) integriert sind. |
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| 174 | EXHAUST MIXER AND APPARATUS USING SAME | EP00902303 | 2000-01-04 | EP1141534A4 | 2003-04-23 | SIEFKER ROBERT G; VITTAL BAILY RAMACHANDRA; BAKER VON DAVID; KHALID SYED ARIF; LOEBIG JAMES CARL |
| Disclosed is an exhaust mixer (50) including a passage (54) extending from an inlet (56) to an outlet (58) that is coincident with a centerline axis of mixer (50). Several ridges (68) are circumferentially disposed about the axis and each flare away from the centerline axis relative to a direction along the centerline axis from inlet (56) toward outlet (58). Ridges (68) each define a corresponding one of several inner channels (74) radially disposed about passage (54) that each intersect passage (54) between inlet (56) and outlet (58). Several outer channels (84) are also radially disposed about passage (54) and are each positioned between a corresponding pair of inner channels (74). Ridges are each shaped to turn inner channels (74) and outer channels (84) about the axis as ridges (68) extend along the indicated direction. Inner channels (74) diverge away from the axis and one another in this direction while outer channels (84) converge toward the axis and one another in this direction. | ||||||
| 175 | Dispositif antidétection par radar d'une superstructure aplatie de navire | EP02290749.7 | 2002-03-26 | EP1245485A1 | 2002-10-02 | Aknin, Bernard |
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| 176 | RETROFITTING VESSELS TO DEFLECT RADAR SIGNALS | EP00945463.8 | 2000-07-26 | EP1210562A1 | 2002-06-05 | STAFFORD, Philip, K. |
| The radar signature of a vessel is reduced by retrofitting it with an array (10) of elements (15) fastened to surfaces (14b) of the vessel. The elements (15) have planar faces (11-12) so oriented that incident radar signal (20) is reflected away from its angle of incidence. | ||||||
| 177 | METHOD OF REDUCING INFRARED VIEWABILITY OF OBJECTS | EP99965716.6 | 1999-08-13 | EP1104387A2 | 2001-06-06 | COLVIN, David, P.; MCKINNEY, Richard, A.; BRYANT, Yvonne, G. |
| A method of camouflaging an object which emits infrared radiation by forming a binder (30) upon a substrate (S) wherein microcapsules which absorb infrared radiation are (10) are submersed within the binder. | ||||||
| 178 | METHOD OF GENERATING A LIQUID MIST | EP98930015.7 | 1998-06-18 | EP0988224A1 | 2000-03-29 | PERSSON, Rolf |
| Method of generating a liquid mist for producing phantom targets or camouflage, whereupon liquid is launched by means of a water cannon (1) at so high velocity that initially the liquid is held together in a liquid packet (2) in order to decompose after a certain distance, under the effect of the air resistance, and atomise into small liquid drops to form a liquid mist (3). | ||||||
| 179 | Exhaust gas discharge system and method | EP97308106.0 | 1997-10-13 | EP0836987A3 | 1999-08-11 | Wood, David William |
A method of treating exhaust gases discharged from a combustion engine (1) of a marine vessel (2) includes injecting into the exhaust gases a cloud of water droplets. The exhaust gases are removed from the engine (1) along a tubular member (3) and thence discharged to the atmosphere just above the water line (4) of the vessel (2). The cloud of water droplets is injected through a plurality of nozzles (5) in the periphery of the tubular member (3). Because of the high surface area of the water cloud, the exhaust gases passing along the tubular member (3) are cooled down such that the final discharge (6) has a sufficiently low temperature to make thermal detection difficult. |
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| 180 | Composite material structure able to absorb and dissipate incident electromagnetic radiation power, in particular for air, water and land craft and for fixed ground installations | EP96200720.9 | 1996-03-15 | EP0742095A2 | 1996-11-13 | Sgherri, Roberto; Simonini, Stefano |
A composite material structure is described able to absorb and dissipate the power of the electromagnetic radiation incident on the structure. The main characteristic of said structure is that the absorbent layers (12, 12A), of which it is composed, consist of resins, plastics or polyurethane foams mixed with carbon fibre dipoles, in order to improve the electrical, electromagnetic and mechanical properties of the structure compared with the known art. |
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