| 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 | Self-propelled cannon-shaped | JP2000576228 | 1999-09-29 | JP2002527712A | 2002-08-27 | イーグルストーン、デビッド・アンドリュー; ハーバート、フレデリック; ビーン、マービン・レスリー |
| (57)【要約】 自走式大砲（２）は一次動力源（６）を処理するビークル（４）と該ビークルに移動可能に取付けられた大砲アッセンブリイ（８）とを含む。 大砲アッセンブリイ（８）はベース（１０）と、該ベースに軸動可能にマウントされたクレードル（１４）と、該クレードル（１４）に摺動可能にマウントされたバレル（１６）とを備えて、第１のランアウト位置から第２のリコイルド（反動）位置まで発砲でのバレル（１６）の反動の結果として変位が摺動でとれるようにしている。 大砲アッセンブリイ（８）はビークル（４）に移動可能にマウントされており、好ましいのはビークル（４）とベース（１０）との間のピボット構成（２４，２６）によって移動可能であって、第１の“モビリティ（可動性）”モードでは大砲アッセンブリイ（８）が大地（４２）と何らの直接接触をされない状態にあり、また前記バレル（１６）は第１の方向を向いていて前記ビークル（４）が駆動できるようにされ、かつ第２の“ファイヤリング（発射）”モードの動作では、大砲アッセンブリイが発射位置に展開されて、この位置ではベースが大地（４２）に向ってそこと係合するように移動する。 大砲アッセンブリイ（８）の展開の際に、バレル（１６）は少くとも９０度だけは前記第１の方向から違っている仰角にわたって展開可能となっている。 | ||||||
| 22 | JPH0467114B2 - | JP9638687 | 1987-04-21 | JPH0467114B2 | 1992-10-27 | KURUTO UAI; UARUTERU FUON KEENERU |
| 23 | JPS63502369A - | JP50551986 | 1986-10-14 | JPS63502369A | 1988-09-08 | |
| 24 | JPS5514999B2 - | JP13446873 | 1973-12-03 | JPS5514999B2 | 1980-04-19 | |
| 25 | 사격 가능조건 판단방법 | KR1020160112410 | 2016-09-01 | KR1020180025577A | 2018-03-09 | 김건국; 김석환; 배재만 |
| 본발명은사격가능조건판단방법에관한것이다. 본발명의일 실시예에따르면, (a) 지상전투차량의시스템보정완료여부를판단하는단계, (b) 지상전투차량에서무장장치를운용하는사용자가누구인지판단하는단계, (c) 지상전투차량의무장장치가구동가능한지판단하는단계, (d) 지상전투차량의무장장치중 적어도하나를선택하는단계, (e) 지상전투차량에서표적을탐지및 조준하기위한시계를판단하는단계, (f) 탐지된표적의정지영상전시여부를판단하는단계, (g) 지상전투차량에서조준용차선의전시여부를판단하는단계, (h) 무장장치의사격금지구간여부를판단하는단계, (i) 탄의장전여부를판단하는단계, (j) 표적과의거리를판단하는단계, (k) 지상전투차량의조준장치와무장장치의표적조준위치의차이를검출하는단계, 및 (l) 교전준비완료를판단하는단계를포함하는, 사격가능조건판단방법을제공한다. | ||||||
| 26 | 차량 상의 소형화기용 포지셔닝 구조물 | KR1020137025607 | 2012-03-13 | KR1020140008421A | 2014-01-21 | 이알델라,카를로,알베르토; 아리기,파올로 |
| 기갑 조종석(A)이 장착된 차량 상의 무기용 포지셔닝 구조물로서, 상기 무기는 차량의 상부에 구속된다. 이러한 포지셔닝 구조물은 차량의 프레임에, 특히 전형적으로 기갑 조종석을 형성하는 롤-바로 불리는 보강 바(B)에 직접 결합된다.
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| 27 | 방향 제한 방법 및 방향 제한 시스템 | KR1020167015729 | 2014-11-12 | KR1020160095659A | 2016-08-11 | 트룰손퍼; 니가드에릭; 팜로브울프; 브요른라스-고란 |
| 본발명은, 발사시스템의방향제한을위한중복방법으로서, 제1 계산유닛이발사시스템을제어하고, (a) 방향제한위치가제1 계산유닛에의해알려지며, 발사시스템의높이를측정하는단계, (b) 발사시스템의가로이동을측정하는단계, (c) 측정된높이및 가로이동을기초로하여제1 계산유닛에서발사시스템의위치를계산하는단계, (d) 측정된높이및 가로이동을기초로하여제2 계산유닛에서발사시스템의위치를계산하는단계, (e) 계산된발사시스템의위치를방향제한위치와비교하는단계, 및 (f) 발사시스템이방향제한위치이외에위치설정되었는지의여부를결정하는단계를포함하는발사시스템의방향제한을위한중복방법에관한것이다. 본발명은또한, 발사시스템을위한방향제한시스템으로서, 발사시스템의높이를측정하기위한적어도하나의센서, 발사시스템의가로이동을측정하기위한적어도하나의센서및 발사시스템을제어하기위한제1 계산유닛을포함하며, 제1 계산유닛이측정된가로이동및 높이를기초로하여발사시스템의위치를계산하고, 제1 세트의방향제한위치가제1 계산유닛에의해알려지며, 발사시스템은, 발사시스템의위치를제1 세트의방향제한위치를비교하는제1 계산유닛과, 가로이동및 높이를측정하여, 발사시스템의위치와제2 세트의방향제한위치를비교하는제2 계산유닛에의해방향제한되는것인발사시스템을위한방향제한시스템에관한것이다. | ||||||
| 28 | 지지대 어셈블리 | KR1020120078960 | 2012-07-19 | KR1020140012349A | 2014-02-03 | 오승률; 천성준 |
| The present invention relates to a support assembly and more specifically, a support assembly which is suitable for geographical features. The present invention includes a body unit; a support plate installed in the body unit; and a first fixing plate connected to the support plate to be able to be replaced and having a first fixing protrusion on one side. | ||||||
| 29 | 회전 포탑이 장착된 차량 | KR1020100021123 | 2010-03-10 | KR1020110101833A | 2011-09-16 | 아도르니,안드리아; 치아피니,안드리아 |
| 장갑판 구조의 조종실(2)과 중앙 회전 포탑(4)의 움직임을 위한 시스템을 포함한 회전 포탑이 제공된 차량이 제공되며, 상기 중앙 회전 포탑 상에 주포(5)가 장착될 수 있다. 이러한 포탑은 원주방향 5륜(8)에 의해 차량의 장갑판 구조의 조종실로 연결되며, 상기 원주방향 5륜에 따라 포탑은 상기 5륜의 중심을 관통하는 실질적으로 수직인 축 주위에서 회전가능하다. 이러한 포탑의 기저부(9)는 차량의 조종실(2)의 내부와 포탑의 내부 사이에 연통을 위한 해치(10)가 제공된다.
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| 30 | 중장비 차량의 해치와 연동되는 측면쉴드 및 건쉴드 | KR1019990058135 | 1999-12-16 | KR1020010056601A | 2001-07-04 | 송병륜; 송병근 |
| PURPOSE: Side shields and a gun shield are simultaneously opened and closed as a hatch is opened and closed to protect a combatant taking charge of firearms against firearms of enemy from all directions. CONSTITUTION: Side shields and a gun shield comprise a hatch(20), a left side shield(26) and a right side shield(28) and a gun shield(38). The hatch(20) is installed on a rear side of a rotary frame(18) rotatably installed on the upper part of a turret shell(10) with a hinge(22) to be opened and closed. The left side shield(26) and the right side shield(28) are installed on the left side and the right side of the rotary frame(18) facing with each other with hinges, placed on the hatch(20) overlapping with each other to be interlocked with the opening and closing of the hatch(20) and has curved slide grooves guided with the opening and closing operation by slider balls installed on both ends of the hatch(20). The gun shield(38) is installed on the front side of the rotary frame(18) with a hinge(36), placed folded on the left side and right side shields(26, 28) to be interlocked with the opening and closing operation of the hatch(20) and has curved slide grooves guided with the opening and closing operation by slider balls installed on the left side and the right side shields(26, 28). | ||||||
| 31 | Weapons platform, military vehicle comprising a weapons platform and method for operating a weapons platform | US14415749 | 2013-07-15 | US09649903B2 | 2017-05-16 | Matthias Raczek; Matthias Czok; Roman Wiche; Volker Crede |
| A weapons platform including an undercarriage (11, 111) and a weapon (13, 113) that is positioned in a directable manner on the undercarriage (11, 111). The undercarriage (11, 111) may be supported in relation to the ground beneath by a supporting device (16, 116) that is damped in order to absorb firing recoil forces, the damping characteristics of the supporting device (16, 116) being adjustable in accordance with the firing recoil forces that are to be expected from the weapon (13, 113). The weapons platform (10, 110) may be mounted on a military vehicle (1). A method for operating such a weapons platform (10, 110) is also disclosed. | ||||||
| 32 | PROJECTILE SIGHTING AND LAUNCHING CONTROL SYSTEM | US13925620 | 2013-06-24 | US20160069644A1 | 2016-03-10 | John Curtis Bell |
| A remote controlled projectile sighting and launching system (RCPSLS) is disclosed. In some embodiments, such a system can be compliant with the Americans with Disabilities Act (ADA) and can automatically facilitate moving targets, unmanned operation of a projectile launching device and automatic friendly-fire over-ride. In some embodiments, such a system can include network-linked components such as a plurality of auto-adjusting aiming units (AAAU), gimbaled robotic apparatuses (GRA), trigger activation devices (TAD), and transport vehicles (TRV). In some implementations, a plurality of shooters and/or command centers that are able to view and operate a plurality of AAAUs, TADs, GRAs, and TRVs from a remote location(s). The system can be configured to be capable of discerning friendly confirmed target coordinates (CTC) from enemy CTC and is able to launch a plurality of preselected projectiles (PP) from a plurality of preselected projectile launching devices (PPLD). | ||||||
| 33 | Cannon and Military Vehicle | US14119182 | 2012-05-15 | US20150075358A1 | 2015-03-19 | Matthias Raczek; Jens Koester; Matthias Czok |
| A cannon and a military vehicle having such a cannon, which includes a support, a turret that is rotatable relative to the support and is provided with an opening, and a closure element disposed on the support and configured for the closing off of the opening of the turret. | ||||||
| 34 | Powered Ride-On Vehicle of an Airplane Design With Steer and Tilt Combination and Simulated Combat Capabilities. | US13846886 | 2013-03-18 | US20140265204A1 | 2014-09-18 | Jerry L. Lanser |
| A motor powered riding vehicle with an airplane appearance consisting of a chassis, body and shell. The chassis is in contact with the ground via the wheels. The body includes a seat for the operator and an area to accommodate the controls and battery, if electric power is used. The shell surrounds the body, and gives form to the type of plane being imitated. The body/shell combination are connected to the chassis at two longitudinal pivot points which allow the body to simulate a banking motion as the rear wheel is turned. In addition, the body can contain a bracket to which a toy gun or some electronic “shooting” device is attached to allow two or more planes to engage in simulated combat. | ||||||
| 35 | Field gun aim | US13708605 | 2012-12-07 | US08726784B2 | 2014-05-20 | Keith Dawson; Frederick Herbert; John Michael Webb |
| A howitzer suitable for deployment on a ground plane, the howitzer having an ordnance for firing a projectile. The ordnance can include a barrel defining a barrel axis and having a muzzle towards the front end of the howitzer and a breech assembly at the back end of the barrel; a cradle for holding the ordnance at a traverse and an elevation; two trunnion pins located on the cradle, which co-locate with receiving trunnion bearings on a saddle, wherein in a first position said breech is located forward of the trunnion, in a second position, at the end of the recoil stroke, the breech is retracted substantially behind the trunnion, wherein a recoil stroke is variable depending on the selection of the elevation. | ||||||
| 36 | FIELD GUN AIM | US13708605 | 2012-12-07 | US20140102286A1 | 2014-04-17 | Keith DAWSON; Frederick Herbert; John Michael Webb |
| A howitzer suitable for deployment on a ground plane, the howitzer having an ordnance for firing a projectile. The ordnance can include a barrel defining a barrel axis and having a muzzle towards the front end of the howitzer and a breech assembly at the back end of the barrel; a cradle for holding the ordnance at a traverse and an elevation; two trunnion pins located on the cradle, which co-locate with receiving trunnion bearings on a saddle, wherein in a first position said breech is located forward of the trunnion, in a second position, at the end of the recoil stroke, the breech is retracted substantially behind the trunnion, wherein a recoil stroke is variable depending on the selection of the elevation. | ||||||
| 37 | 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. | ||||||
| 38 | Orbital device with stowable mount | US12931600 | 2011-02-03 | US08584573B2 | 2013-11-19 | Paul Prado; Larry Lopez; Eric Beazer |
| A weapon/recon mount device, comprising: a base ring fixable to a vehicle; a slewing ring concentric with and rotatable relative to the base ring; a pivot mount attached to the slewing ring and having a stowed state and a deployed state; and a back rest attached to the slewing ring and having a stowed state and a deployed state. | ||||||
| 39 | 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. | ||||||
| 40 | Vehicle with space utilization | US12050048 | 2008-03-17 | US08167072B2 | 2012-05-01 | Joshua J. Leonard; Richard Raymond Maki; Eric Bjerketvedt; Michael D. Schneider; Bradley Robert Morisch; Brian D. Krosschell; Louis J. Brady; James Bergman; Larry Holter; Richard Nelson; Lionel Hoff; Doug Moman; Mitchell D. Johnson |
| A utility vehicle with space utilization features is disclosed. The space utilization features provide storage and access to components. | ||||||
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