| 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 | 远程多管灭火发射架及其灭火火箭弹系统 | CN200710066253.9 | 2007-09-30 | CN101130133A | 2008-02-27 | 杨国俊 |
| 远程多管灭火发射架及其灭火火箭弹系统，本发明由不少于一根的发射管(2)横竖排列设置在发射架体(1)内，发射架为一箱体结构；在发射架与平衡基座(3)之间的正中设置有一液压电动升降机(5)；在平衡基座上还设置有发射点火系统(6)、定位终端系统(7)、充电控制器(8)和蓄电池(9)；火箭弹(4)的弹体结构为，传感器(10)、红外测感仪(11)、引爆装置(12)、压缩灭火干粉(13)、隔热板(14)、燃烧室(15)、点火门(16)、前弹盖(17)和弹壳体(18)；其中弹壳体(18)材料为纸筒或塑料，隔热板为耐高温纤维材料及陶瓷隔热材料；本发明控制可靠，应急迅速，不受火场远近距离所限，灭火效能极高，打击火场精准，尤其对大面积强势火场灭火有特殊效果，更具有能将初燃的火势在最短的时间内扑灭的显著优点。 | ||||||
| 2 | 다연장 발사장치 | KR1020140174255 | 2014-12-05 | KR1020160068460A | 2016-06-15 | 송철호 |
| 본발명은동일방향배치되는복수개의발사관을수용하며상기발사관과정렬되는발사구를포함하는몸체부; 상기발사구를덮는덮개부;및상기발사구둘레를따라상기덮개부와접촉하여상기몸체부에결합하는플랜지부와, 상기플랜지부에서상기발사관의길이방향을기준으로발사방향으로돌출형성되며상기발사구의둘레를따라형성되는화염차단부를포함하는덮개클램프부를포함하는다연장발사장치를제공하여, 인접하는발사관에서발사되는발사체의화염에의해해당발사구의덮개부가파손되는것을방지하는유리한효과를제공한다. | ||||||
| 3 | SYSTEM AND METHOD FOR ARMORING VEHICLES USING A HULL HAVING A BLAST VENT | US13733652 | 2013-01-03 | US20140013936A1 | 2014-01-16 | 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. | ||||||
| 4 | Deformable armored land vehicle | US13293271 | 2011-11-10 | US08430196B2 | 2013-04-30 | Donald R. Halliday |
| An armored land vehicle comprising a first hull portion and an engine compartment which form a central chassis (CC) adapted to receive second hull portions on both sides and the rear of the CC. The CC and hull portions have generally V-shaped undersides with slanted, upwardly extending sides to create multiple blast venting paths to deflect blast energy away from the vehicle occupants. These blast paths comprise one or more blast vents through the vehicle for further reducing occupant exposure to blast energy. The engine compartment and front and rear tractive units can comprise an open framework, allowing significant under vehicle blast venting between the hull portions, through the engine compartment, and around the hull portions, thereby increasing survivability of the crew. The hull portions can be designed to rotate and/or be frangible to increase the blast-venting through the vehicle. | ||||||
| 5 | System and method for armoring vehicles using a hull having a blast vent | US13461841 | 2012-05-02 | US08347997B2 | 2013-01-08 | 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. | ||||||
| 6 | Deformable modular armored combat system | US12344630 | 2008-12-29 | US08205703B2 | 2012-06-26 | 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. | ||||||
| 7 | Mobile carrier for a projectile launcher | US11475380 | 2006-06-27 | US07707922B1 | 2010-05-04 | Ehud Dekel |
| A mobile projectile launcher is disclosed having a tiltable launching platform for supporting a plurality of canisters in each of which projectiles to be launched are stored and fired, a support plate pivotally connected to a horizontal cargo bed, and at least one linear actuator by which the support plate is swingable from a closed position substantially perpendicular to the cargo bed to an open position substantially parallel to the cargo bed. The support plate is made of a material that is resistant to the projectile plume following launching and is sufficiently sturdy to support a technician during the loading of projectiles when set in an open position, yet is adapted to protect and hide the loaded canisters when set in a closed position. | ||||||
| 8 | Anti-tank guided missile weapon | US10097814 | 2002-03-13 | US07086318B1 | 2006-08-08 | Larry N. Darnall |
| An anti-tank guided missile (ATGM) weapon system with an overhead mounted, electrically driven, remote controlled weapon station that supports a tube-launched optically-tracked wire-guided (TOW) missile launcher and a machine gun, typically the caliber .50 M2, on a single traversing and elevating platform. Above-deck assemblies include the TOW and gun cradle, a dual pod missile launcher, the Improved Target Acquisition System (ITAS), target acquisition subsystem (TAS), elevation and traverse motors and gear transmissions and drive electronics, and an ammunition case. Below-deck assemblies include the ATGM weapon system control handles, biocular display, control panel, ITAS fire control system (FCS), ITAS battery power source (BPS), slip-ring, and gunner's seat. Electrical cables connecting the two assemblies penetrate the vehicle deck directly below the weapon System. | ||||||
| 9 | Missile container support rack | US455537 | 1995-05-31 | US5682005A | 1997-10-28 | David R. Crowley |
| A rack system (10) is disclosed for use on a vehicle (12) which carries weapons containers (48, 50) containing one or more missiles or rockets (52). A crane mounted on the system pivots each weapons container independently from a storage position to a vertical launch position. Locking devices lock the weapons containers in the storage position for transport and in the vertical, launch position. | ||||||
| 10 | Combat vehicle and system for transporting it for loading onto aircraft | US361267 | 1994-12-21 | US5461961A | 1995-10-31 | Rudiger Baus; Reiner Linge |
| A combat vehicle with a driver's cab mounted on its chassis along with a weapon incorporating a rocket launcher, wherein the rocket launcher rests on a carriage and is elevated and leveled by electrically powered mechanisms between it and the carriage, and the carriage pivots in azimuth on an intermediate structure that rotates on a collar on the chassis. The weapon is an independent assembly incorporating the rocket launcher, the carriage, the intermediate structure, and the collar and is attached to the chassis only by a mount, and by electrical connections if any, accessible from outside the vehicle. To load the motor vehicle onto aircraft, the rocket launcher is rotated at elevation 0.degree. into a position 90.degree. to the length of the vehicle. A carrier that travels on at least three wheel-mounted upright rack-and-pinion mechanisms is advanced over the vehicle to above the weapon, the weapon is attached to the carrier, the weapon is detached from the chassis by releasing the mount and by disconnecting any electrical connections, the rack-and-pinion mechanisms lift the weapon, the chassis is removed, the rack-and-pinion mechanisms lower the weapon to carrying height, the weapon is carried onto the aircraft by the carrier, and the chassis is loaded onto another aircraft. | ||||||
| 11 | Side-mounted rolling airframe missile launcher | US739262 | 1991-08-01 | US5129307A | 1992-07-14 | R. Neal Cain; Gary L. Carle; Walter H. Klaus |
| An integrated sidemounting of a rolling airframe missile launcher with a 54 MK-45 gun mount is provided. The integrated gun-missile system permits simultaneous tracking of the missile system and gun system and, through software systems, allows the ship's defensive system to automatically sequence through weapons as required. Chaff, decoys and flares may also be launched using the side-mounted missile launcher. | ||||||
| 12 | Armored vehicle with a laterally alignable mortar | US34046773 | 1973-03-12 | US3818794A | 1974-06-25 | MAYER C; BURKHART R |
| An armored vehicle with a laterally alignable mortar which can be operated by a gunner or firing personnel and encompassing launching barrels each possessing a propellant charge chamber for shells loaded at the muzzles. The launching barrels are rigidly mounted at a laterally alignable turret housing which houses the firing personnel or gunner of the armored vehicle. The muzzles of the launching barrels are located at the wall of the turret. An annular compartment concentric to the axis of rotation of the turret and accommodating an infeed or delivery mechanism for the shells stored in magazines is arranged about the turret and protected by a hood. The magazines are movable relative to the turret by means of the infeed mechanism into a position in alignment with the launching barrels.
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| 13 | Device for launching flying bodies | US3595127D | 1965-07-26 | US3595127A | 1971-07-27 | STANGL ARNOLD; PFISTER FRANZ |
| 1. A device for launching flying bodies particularly reactiondriven missiles, comprising a substantially ball-shaped pivot member, means pivotally mounting said pivot member for pivotal movement about a first normally horizontal axis and about a second normally vertical axis, at least one first and one second flying body launching tube rotatably mounted on said pivot member, control means operatively connected to said pivotal mounting means for said pivot member for pivoting said pivot member about said first and second axes, said pivot member having a loading opening defined therethrough below the pivotal mounting of said launching tubes thereon, said first and second launching tubes being rotatable between a firing position at which one of said first and second launching tubes extends above said ball member and a loading position at which one of said first and second loading tubes extends in alignment with the loading opening defined in said ball member, and a closure flap carried by said ball member and movable between a position closing said opening and a position opening said opening.
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| 14 | Space vehicle and launching means therefor | US3437285D | 1966-08-04 | US3437285A | 1969-04-08 | MANFREDI DARIO; RAITI ANGELO |
| 15 | Missile launcher and loading system | US49518065 | 1965-10-12 | US3316808A | 1967-05-02 | FRANK MAIS |
| 16 | Vehicle with elevating platform | US71622358 | 1958-02-19 | US2926798A | 1960-03-01 | WALLACE HAMILTON |
| 17 | Missile launcher | US25297051 | 1951-10-24 | US2826960A | 1958-03-18 | SCHIAVI FERDINAND J |
| 18 | Multiple rocket launcher | US26113051 | 1951-12-11 | US2720818A | 1955-10-18 | SWIPP STANLEY W; KOEPER CASPER J; KESTER ARNOLD A; OLSON EDWIN O |
| 19 | Gun and gun carriage | US61471545 | 1945-09-06 | US2489749A | 1949-11-29 | DENNISTOUN BURNEY CHARLES |
| 20 | Barrage rocket projector | US58295445 | 1945-03-15 | US2429021A | 1947-10-14 | GOULD ALBERT S; LINDVALL FREDERICK C |
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