| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 21 | MOTORIZED VEHICLE COMPRISING A DRIVER MODULE WITH V-SHAPED UNDERSIDE AND SIDE MODULE WITH V-SHAPED UNDERSIDE | EP16152455.8 | 2009-12-22 | EP3028928B1 | 2018-12-05 | HALLIDAY, Donald R. |
| A motorized vehicle suitable for military use and adaptable for non-military use, comprising a driver module presenting a v-shaped hull on its underside and a first side module attached to the driver module and presenting a v-shaped hull on its underside, wherein the v-shaped hulls are designed such as to form at least one blast energy dissipation path between the driver module and the first side module. | ||||||
| 22 | Militärisches Fahrzeug, Transportbehälter und Verfahren zum Verstauen von Ausrüstungsgegenständen | EP12187744.3 | 2012-10-09 | EP2587208A2 | 2013-05-01 | Mergard, Tino; Freudenstein, Manfred; Schilling, Martin |
Militärisches Fahrzeug mit einer in Elevation richtbaren Werfereinrichtung, die einen in Elevation richtbaren Höhenrichtteil aufweist, wobei an dem Höhenrichtteil ein Transportbehälter (20) mit einem Stauraum (21) zum Verstauen von Ausrüstungsgegenständen angeordnet ist. Transportbehälter mit einem Stauraum (21) zum Verstauen von Ausrüstungsgegenständen zur Anordnung an einem in Elevation richtbaren Höhenrichtteil einer Werfereinrichtung eines militärischen Fahrzeugs. Verfahren zum Verstauen von Ausrüstungsgegenständen an einer Werfereinrichtung eines militärischen Fahrzeugs, die einen in Elevation richtbaren Höhenrichtteil aufweist, wobei ein Transportbehälter (20), der einen Stauraum (21) zum Verstauen von Ausrüstungsgegenständen aufweist, an dem Höhenrichtteil angeordnet wird.
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| 23 | Vorrichtung und Verfahren zum Richten eines Raketenabschussbehälters | EP11162702.2 | 2011-04-15 | EP2381204A2 | 2011-10-26 | Scheidemann, Georg; Suess, Siegfried; Simon, Alexander |
Die Erfindung betrifft Vorrichtung zum Richten eines Abschussbehälters (2), insbesondere Raketenabschussbehälters, mit einem um eine Elevationsachse (E) richtbaren Höhenrichtteil (4), welches eine Aufnahme (4.1) zur Aufnahme eines oder mehrerer Abschussbehälter (2) aufweist, wobei die Aufnahme (4.1) gegenüber der Elevationsachse (E) verfahrbar angeordnet ist. Einen weiteren Gegenstand der Erfindung bildet ein Verfahren zum Richten eines Abschussbehälters (2), insbesondere eines Raketenabschussbehälters, mit einem um eine Elevationsachse (E) richtbaren Höhenrichtteil (4), welches eine Aufnahme (4.1) zur Aufnahme eines oder mehrerer Abschussbehälter (2) aufweist, |
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| 24 | Méthode de construction, réparation, entretien et transport des engins blindés de combat lourds en plusieurs modules | EP98250302.1 | 1998-08-27 | EP0982560A1 | 2000-03-01 | Wieczorek, Julien |
La méthode des 3 M est un procédé de construction, d'entretien, de réparation, de modernisation et aussi de partage d'un engin blindé lourd, 1 de 120 t à 150 t maxi pour l'engin 2, en trois modules, méthode basée sur l'utilisation de trois semi-remorques 4 placés côte à côte, parallèlement, sur lesquels sont fixés les modules 8 avant, 5 + 6 central, 9 arrière moteur, pour l' assemblage, comme pour leur séparation. Les engins de la 4-ème génération devront avoir beaucoup d'équipements nouveaux, comme un mât télescopique 54 pour l'observation lointaine. Les chars lourds, divisés en trois modules, seront facils à transporter, à grande vitesse, par ces semi-remorques tractés par un camion 3. |
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| 25 | Kampffahrzeug sowie Transportsystem zu seiner Verladung in Transportflugzeuge | EP94107517.8 | 1994-05-14 | EP0664431A2 | 1995-07-26 | Baus, Rüdiger, Dipl.-Ing.; Linge, Reiner |
Kampffahrzeug sowie Transportsystem zu seiner Verladung in Transportflugzeuge. Das Kampffahrzeug besitzt ein Fahrzeuguntergestell, auf dem eine Abschußvorrichtung für Artillerieraketen angeordnet ist. Die Schnittstelle zwischen Fahrzeug und Abschußvorrichtung ist so ausgewählt, daß die gesamte Abschußvorrichtung als selbständige Einheit ausgebildet ist, welche mit dem Fahrzeuguntergestell über von der Fahrzeugaußenseite her bedienbare Verriegelungsvorrichtungen gekoppelt ist. Die Verladung geschieht mittels eines fahrbaren Transportgestells (8), durch welches das Fahrzeug im Bereich der Abschußvorrichtung überfahren wird. Das Transportgestell (8) besitzt einen Oberrahmen (9.1-9.2-9.3) zur Aufhängung des Werferrahmens (3) und einen Unterrahmen (9.7-9.11) zur Abstützung der Oberlafette (4). Die Abschußvorrichtung (3, 4) wird am Transportgestell (8) befestigt und vom Fahrzeuguntergestell getrennt. Das Transportgestell wird mittels an ihm angeordneter Hub- Fahrstützen (10.1, 10.3) angehoben und nach Entfernen des Fahrzeuguntergestells wieder abgesenkt. Jede Hub- Fahrstütze (10.1, 10.3) besitzt eine Säule (12), an der ein Räderpaar (11) verschwenkbar angeordnet ist und an der über einen Tragarm (13.1, 13.3) das Transportgestell (8) anheb- und absenkbar geführt ist. Das Transportgestell (8) wird zum Transportflugzeug gefahren und zusammen mit der Abschußvorrichtung (3, 4) verladen. |
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| 26 | Kippbarer Aufbau für ein Militärfahrzeug | EP93118482.4 | 1993-11-16 | EP0612969A1 | 1994-08-31 | Ennenga, Luitjen, Dipl.-Ing. |
Bei einem geländegängigen Fahrzeug (10) mit Fahrerhaus (13) und Ladefläche (14) und mit einem auf der Ladefläche (14) montierten, das Fahrerhaus (13) überragenden Gerät (15), insbesondere zur Flugabwehr, ist zur Sicherstellung der Luftverbringbarkeit und der guten Fahreigenschaften des Fahrzeugs trotz des aufgesetzten Gerätes (15) das Gerät (15) auf einer Plattform (23) angeordnet, die auf einem auf der Ladefläche (14) fest verankerten Gestell (24) um eine quer zur Fahrzeuglängsachse sich erstreckende Schwenkachse (25) aus einer im wesentlichen parallel zur Ladefläche (14) unterhalb der Dachkontur (26) liegenden, etwa horizontalen Gebrauchsstellung in eine sich entlang der Fahrerhausrückwand erstreckende, etwa vertikale Transportstellung und umgekehrt schwenkbar gehalten ist. Die Schwenkachse (25) ist so angeordnet, daß in der Transportstellung der Plattform (23) der Masseschwerpunkt des Geräts (15) vor der Fahrzeughinterachse (12) und möglichst nahe der Ladefläche (14) liegt. |
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| 27 | System and method for armoring vehicles using a hull having a blast vent | US13733652 | 2013-01-03 | US08662227B2 | 2014-03-04 | Donald R. Halliday |
| A modular, wheeled vehicle suitable for military use, includes a driver module having a width for seating one person and having length for seating a second (and optional third) person therebehind, and an engine module disposed behind the driver module containing an engine for powering the modular vehicle. The engine module has a rear surface adapted to receive a storage module. The driver module and the engine module form a central element having a pair of sides, a bottom, and a top. The central element is adapted to receive the modules on both of the central element sides. The central element has air inlet for personnel and for the engine disposed atop the central element. The bottom of the central element and troop side pods generally are V-shaped with slanted, upward extending sides. | ||||||
| 28 | System and Method for Armoring Vehicles Using A Hull Having A Blast Vent | US13461841 | 2012-05-02 | US20120240759A1 | 2012-09-27 | Donald R. Halliday |
| A modular, wheeled vehicle suitable for military use, includes a driver module having a width for seating one person and having length for seating a second (and optional third) person therebehind, and an engine module disposed behind the driver module containing an engine for powering the modular vehicle. The engine module has a rear surface adapted to receive a storage module. The driver module and the engine module form a central element having a pair of sides, a bottom, and a top. The central element is adapted to receive the modules on both of the central element sides. The central element has air inlet for personnel and for the engine disposed atop the central element. The bottom of the central element and troop side pods generally are V-shaped with slanted, upward extending sides. | ||||||
| 29 | Mobile vertical missile launcher | US12931635 | 2011-02-01 | US08266999B1 | 2012-09-18 | Carl L. Sisemore; Myron Lyn Thomas, II |
| A mobile terrestrial vertical missile launch system is provided for relocatable ballistic missile deployment. The system is connectable to a transport truck and includes a trailer, a pivotable canister, a plurality of stabilizing legs, and an equipment module. The trailer has a hitch for connecting to the truck, a base for supporting wheels for road travel, and a flatbed platform having a transverse hinge. The canister contains launcher for at least one missile and is configurable by rotation at the hinge for disposal in either a longitudinal position for stowage or an erected position for deployment. The stabilizing legs are disposed along a periphery of the trailer. The legs can be disposed in one of an elevated position for stowage and a retarded position for ground engagement. The equipment container supplies electrical power, environmental conditioning, tracking, communication and control for the missile. | ||||||
| 30 | MOBILE MISSILE LAUNCH SYSTEM AND METHOD THEREOF | US13260731 | 2010-01-11 | US20120036987A1 | 2012-02-16 | Siddalingappa Guruprasad; Shreedhar Aravind Katti; Alasani Prasad Goud; Vikas Narayan Waghmare; Sanjay Kumar; Atul Gupta; Ravindra Sudhakar Khire; Tushar Kant Santosh; Bimal Gautam; Paras Ram |
| The present invention relates to launching system, more particularly relates to mobile launching system for missiles. The mobile missile launch system comprising a vehicle (14) having a chassis structure adapted to carry the launch system; a mounting frame (16) comprising predetermined truss framework mounted onto the chassis structure; plurality of sliding mechanisms mounted at rear end of the mounting frame (16); plurality of canisters (43) mounted onto said beam (22) and plurality of missiles (11) ensconced within the canisters (43); plurality of containers (42) enclosing said canisters (43) and are connected to the saddles (32, 34) for linear movement; plurality of resting units (27) abutting to rear end of the canisters (43) and are adapted to move linearly to transfer reaction forces from said missiles (11) to ground. | ||||||
| 31 | Deformable Modular Armored Combat System | US12344630 | 2008-12-29 | US20100163330A1 | 2010-07-01 | Donald R. Halliday |
| A modular, wheeled vehicle suitable for military use, includes a driver module having a width for seating one person and having length for seating a second (and optional third) person therebehind, and an engine module disposed behind the driver module containing an engine for powering the modular vehicle. The engine module has a rear surface adapted to receive a storage module. The driver module and the engine module form a central element having a pair of sides, a bottom, and a top. The central element is adapted to receive the modules on both of the central element sides. The central element has air inlet for personnel and for the engine disposed atop the central element. The bottom of the central element and troop side pods generally are V-shaped with slanted, upward extending sides. | ||||||
| 32 | Multiple tube pneumatic launcher | US10503625 | 2004-03-29 | US20060086241A1 | 2006-04-27 | Stephen Miller; Steven Fox; David Feild; Richard Bauernschub; Justin Mettee |
| A launcher includes a plurality of launch tubes for stowing and launching a plurality of air vehicles. A central air manifold is operatively connected to an air storage tank; a first launch tube air manifold is operatively connected to a first group of the launch tubes and operatively connected to the central air manifold. The first launch tube air manifold has a separate port corresponding to each launch tube of the first group of launch tubes. A release valve mechanism is removably mounted in one of the ports of the first launch tube air manifold, the release valve mechanism controlling the passage of launch air between the first launch tube air manifold and the launch tube corresponding to the port in which the release valve mechanism is mounted. A plug is removably mounted in each of the ports not occupied by the release valve mechanism. | ||||||
| 33 | Multi-purpose missile launcher system for a military land vehicle | US10316476 | 2002-12-11 | US06691600B2 | 2004-02-17 | David R. Boudreau; Stan Bovee; Philip Matteson; Bruce Gaedke; Dennis Borgwarth |
| A multi-purpose missile launcher system for a military land vehicle that has the capability for direct targeting both short and medium range land targets, as well launching missiles against longer-range land targets or air targets using indirect targeting. The multi-purpose missile launcher system is deployed as part of a modular weapon system that mates with a modular bed of the military land vehicle. | ||||||
| 34 | Multi-purpose missile launcher system for a military land vehicle | US09817490 | 2001-03-26 | US06584881B1 | 2003-07-01 | David R. Boudreau; Stan Bovee; Philip Matteson; Bruce Gaedke; Dennis Borgwarth |
| A multi-purpose missile launcher system for a military land vehicle that has the capability for direct targeting both short and medium range land targets, as well launching missiles against longer-range land targets or air targets using indirect targeting. The mulit-purpose missile launcher system is deployed as part of a modular weapon system that mates with a modular bed of the military land vehicle. | ||||||
| 35 | System for upending/reclining launch vehicles | US943454 | 1997-10-03 | US5924648A | 1999-07-20 | James William Ellinthorpe |
| An improved system is disclosed for upending/reclining an extraterrestrial vehicle. In one embodiment, first and second trunnion supports may be positioned on opposing sides of a u-shaped opening provided at the rearward end of a mobile support platform. A launch vehicle may be pivotably supported via trunnions received by the first and second trunnion supports for pivotal movement between a reclined position on top of the support platform to an upended position. In the upended position a launch vehicle will extend through the u-shaped opening. A bridge assembly may be selectively interconnected to the launch vehicle to facilitate handling, transport and storage therewith. | ||||||
| 36 | Armored missile launch/shipping container | US405484 | 1982-08-05 | US4470336A | 1984-09-11 | Lynn J. Swann; Larry D. Wedertz |
| A missile launch system includes a missile launch support structure mounted on a launch platform and including a pair of spaced apart rails having longitudinal slots formed therein, and a cooperating missile launch container having a cylindrical bore for receiving and supporting a missile for launching includes radially extending ribs spaced and oriented to engage and slide along the slots in the rails for supporting the missile launch container for launching of the missile. | ||||||
| 37 | Fire control mechanism | US189980 | 1980-09-22 | US4361071A | 1982-11-30 | Donald J. Carlson; Martin J. Neumeyer; Glenn O'Rourke; Roger K. Waid |
| A TOW (Tube-launched, Optically tracked, Wire-guided) missile system is mted on a combat vehicle turret for greater combat effectiveness. Before the missile is launched, the gunner keeps the target in his sights in azimuth by powering the turret through a movable sight to which the turret is slaved by a lock mechanism. Missile launch energizes certain electrical devices which unlock the mechanism to make sight movement independent of the turret, open the turret drive motor power switch, and set a brake on the motor which locks the turret against movement to provide a stable platform for tracking the target during missile flight. After a preset time to allow for on-target impact, the devices are automatically reset and the turret drive is again slaved to the sight in azimuth. | ||||||
| 38 | Driving mechanism for the cover of an ammunition magazine on armored land vehicles | US628771 | 1975-11-04 | US4010672A | 1977-03-08 | Hans Kolbinger; Ulf Wossagk |
| A driving mechanism for controllably opening and closing the cover of an ammunition storage magazine of an armored land vehicle operates to enable the cover to be opened in an essentially vertical position by automatic hydraulic means when the ammunition, which may comprise rockets or the like, is to be loaded into a launcher located above the magazine. When it is desired to reload the magazine itself, the cover may be detached from the driving mechanism and manually opened into a horizontal position extending generally flush with the opening of the magazine itself to facilitate loading of ammunition into the magazine. | ||||||
| 39 | Armoured vehicle | US3800659D | 1972-06-22 | US3800659A | 1974-04-02 | KUIPER C |
| An armoured vehicle or vessel has a device for launching guided projectiles, such as rockets, with the aid of a training apparatus. A launching tube and the training apparatus are positioned in the interior and under the armour of the vehicle or vessel during normal transport. The holding means for the launching tube is pivotably attached to a supporting means provided under the top of the armour which is provided with an opening that can be shut off.
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| 40 | Automatic repeating rocket launcher | US38846653 | 1953-10-26 | US2933981A | 1960-04-26 | ANDERSON PAUL E; CROMP THEODORE Q; EVANS PAUL I; MAURICE RANSOM |
