CN106288963A - 小型无人飞机击退装置 - Google Patents
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- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/02—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables
- B64F1/027—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables using net or mesh
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- B64F1/0297—Ground or aircraft-carrier-deck installations for arresting aircraft, e.g. nets or cables adjustable to align with aircraft trajectory
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
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- F41B5/00—Bows; Crossbows
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- F41B—WEAPONS FOR PROJECTING MISSILES WITHOUT USE OF EXPLOSIVE OR COMBUSTIBLE PROPELLANT CHARGE; WEAPONS NOT OTHERWISE PROVIDED FOR
- F41B5/00—Bows; Crossbows
- F41B5/14—Details of bows; Accessories for arc shooting
- F41B5/1484—Bows with special adaptations or devices for special purposes
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- F41—WEAPONS
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- F41H11/00—Defence installations; Defence devices
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
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- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
- B64U70/30—Launching, take-off or landing arrangements for capturing UAVs in flight by ground or sea-based arresting gear, e.g. by a cable or a net
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
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Abstract
提供小型无人飞机击退装置。当小型无人飞机向应该保卫的区域飞来时,快速地击退(捕获)小型无人飞机。本发明的小型无人飞机击退装置(1)由对作为捕获对象的无人机进行捕获的捕获体(2)、以及朝向无人机发射捕获体(2)的捕获体发射装置(3)构成,即使可疑的无人机(6)向应该保卫的区域内飞来,也能够由捕获体发射装置(3)发射捕获体(2)而快速地捕获无人机(6)。因此,能够保卫善良的国民的利益和安全。
Description
技术领域
本发明涉及将向公共的区域飞来的小型无人飞机击退的击退装置。
背景技术
近年来,开发出被称为无人机(drone)的小型无人飞机,使例如航拍、物流等变得容易。无人机在商业用途中以比较便宜的价格销售,普通消费者也能够轻松地获得。预期这样的无人机会活跃在宽范围的领域中。
但是,近来,无人机搭载放射性物质而向首相官邸飞来、以及在寺院(例如,位于长野县的善光寺)的开龛的法事中利用无人机进行航拍这样的恶劣的行为横行。并且,还频繁发生使无人机在这样的公共的区域下落等危险行为。特别是进行使无人机向公共场所飞来而进行航拍等行为会损害善良的国民的利益并且会带来危险,不应该允许对其放任不管。例如,在下述的专利文献1中提出了对捕获对象进行捕获的捕获装置,但即使使用该捕获装置,也很难捕获无人机。
专利文献1:日本特开2002-355323号公报
发明内容
本发明是为了解决上述的问题而完成的,其目的在于,在小型无人飞机向应该保卫的区域内飞来时,能够快速地击退(捕获)小型无人飞机。
根据本发明,提供一种将小型无人飞机击退的小型无人飞机击退装置,其中,该小型无人飞机击退装置具有:捕获体,其捕获小型无人飞机;以及捕获体发射装置,其朝向小型无人飞机发射该捕获体。
优选本发明的小型无人飞机击退装置还具有检测单元,该检测单元检测距上述小型无人飞机的距离和方向。优选在本发明中,该小型无人飞机击退装置包含判定单元,该判定单元根据该检测单元的信息来判定该小型无人飞机是否处于射程内,当该判定单元判定为处于射程内时,上述捕获体发射装置朝向该小型无人飞机发射上述捕获体。
优选上述捕获体由捕获上述小型无人飞机的捕获弹、连结于该捕获体的线、以及对该线进行卷绕的电动卷轴构成。
优选上述捕获弹具有缠绕于上述小型无人飞机的网以及使该小型无人飞机的下落速度减缓的降落伞。
由于本发明的小型无人飞机击退装置由捕获小型无人飞机的捕获体、以及朝向小型无人飞机发射捕获体的捕获体发射装置构成,因此即使可疑的小型无人飞机向应该保卫的区域内飞来,也能够由捕获体发射装置发射捕获体而快速地捕获小型无人飞机。因此,能够保卫善良的国民的利益和安全。
本发明的小型无人飞机击退装置在具有检测距上述小型无人飞机的距离和方向的检测单元的情况下,能够确定向应该保卫的区域内飞来的小型无人飞机的位置。并且,小型无人飞机击退装置在包含根据该检测单元的信息来判定该小型无人飞机是否处于射程内的判定单元的情况下,构成为当该判定单元判定为处于射程内时,上述捕获体发射装置朝向该小型无人飞机发射上述捕获体,因此能够可靠地捕获小型无人飞机。
由于上述捕获体由捕获上述小型无人飞机的捕获弹、连结于该捕获体的线、以及对该线进行卷绕的电动卷轴构成,因此在利用捕获弹捕获上述小型无人飞机之后,利用该电动卷轴卷绕该线,能够将该小型无人飞机向该小型无人飞机击退装置侧拉近。
由于上述捕获弹具有缠绕于上述小型无人飞机的网、以及使该小型无人飞机的下落速度减缓的降落伞,因此在利用该网捕获到该小型无人飞机之后,通过打开降落伞而能够防止该小型无人飞机下落而撞击到地上。
附图说明
图1是示出小型无人飞机击退装置的一例的结构的侧视图。
图2是示出在捕获体发射装置中装配了捕获体的状态下的小型无人飞机击退装置的结构的俯视图。
图3是示出捕获体的捕获弹的结构的侧视图。
图4的(a)、(b)是对使捕获弹的网放出的方法进行说明的说明图。
图5是示出朝向小型无人飞机发射捕获体并且使捕获弹的网放出的状态的侧视图。
图6是示出小型无人飞机被捕获体捕获并且降落伞已打开的状态的侧视图。
标号说明
1:小型无人飞机击退装置;2:捕获体;20:捕获弹;200:收纳器;201:网;202:锤;203:降落伞;203a:伞体;203b:吊索;204:气体产生材料;205:点火材料;21:线;22:电动卷轴;23:电动机;23’:固定托架;24:距离传感器;3:捕获体发射装置;30:发射台;31:弓;32:弦;33:钩挂部;33a:端部;34:空气活塞;4:检测单元;40:固定部;5:判定单元;6:无人机;7:设置台;8:旋转台;9:支承部;10:支点轴。
具体实施方式
图1所示的小型无人飞机击退装置1由对作为捕获对象的小型无人飞机(以下,称为“无人机”)进行捕获的捕获体2、以及朝向无人机发射捕获体2的捕获体发射装置3构成。
如图1和图2所示,捕获体发射装置3具有:像枪弩那样构成的发射台30,其用于装配并发射捕获体2;弓31,其安装于发射台30的前端;弦32,其张设在弓31的两端之间;以及钩挂部33,其钩挂住弦32。钩挂部33的端部33a与固定于发射台30的下表面的气缸34的活塞连结。是如下的结构:在向后方侧牵拉弦32而将其钩挂于钩挂部33的状态下,气缸34的活塞将端部33a拉向后方侧而将钩挂部33释放,由此弦32借助弓31的复原力而朝向前方高速移动。
图1所示的捕获体发射装置3配设于设置台7,在设置台7的上表面上配设有能够旋转的旋转台8。当使旋转台8旋转时,能够使捕获体发射装置3旋转。在旋转台8上配设有对发射台30的后部侧进行支承的支承部9。在将捕获体2装配于发射台30的状态下,使发射台30的后部侧以支点轴10为支点转动,由此能够使发射台30的前部侧上下摇动,调整捕获体2的瞄准。捕获体发射装置3不限于本实施方式的结构,也可以由空气枪、弹珠、气枪等构成。
小型无人飞机击退装置1具有检测单元4,该检测单元4对距向应该保卫的区域飞来的无人机的距离和方向进行检测。检测单元4借助固定部40而固定在发射台30上。检测单元4由例如雷达构成,具有抛物面天线。检测单元4通过与旋转台8一同旋转并朝向空中发射电波并且接收由无人机反射的反射波,由此能够检测距无人机的距离和方向。检测单元4既可以采用根据包含在接收到的反射波中的相位信息进行图像处理而能够识别无人机的方向和距离的结构,也可以使用观测器(scope)等。
如图2所示,小型无人飞机击退装置1在设置台7中具有判定单元5,该判定单元5使用由检测单元4检测到的信息来判定无人机是否在射程内。是如下的结构:如果判定单元5判定为无人机处于射程范围内,捕获体发射装置3朝向无人机发射捕获体2。
如图1和图2所示,捕获体2由如下部件构成:捕获弹20,其捕获无人机;线21,其与捕获体2连结;电动卷轴22,其卷绕线21;以及距离传感器24,其检测距无人机的距离而识别能够捕获的位置。电动机23与电动卷轴22连接。电动机23被固定托架23’固定于旋转台8,当电动机23驱动时,利用电动卷轴22卷绕线21,能够将捕获体2拉近小型无人飞机击退装置1。
如图3所示,捕获弹20具有:网201,其缠绕于无人机;多个锤202,其等间隔地安装在网201的周缘部;收纳器200,其在网201折叠的状态下进行收纳且能够开闭;以及降落伞203,其使无人机的下落速度减缓。
网201优选由无人机缠结于网201时网201不会被切断的程度的高强度的材料构成。并且,锤202的材质或个数等无特别限定。通过将多个锤202安装于网201的周缘部,而能够使收纳在收纳器200内的状态下的网201在从收纳器200放出时容易展开,并且在无人机缠结于网201时封锁无人机的动作。
这里,作为使网201从收纳器200放出的方法,能够利用例如气囊的放出原理。例如,在构成捕获弹20的网201的后方侧配置充气机(气体产生装置)。即,如图4的(a)所示,在各锤202的后方侧配置气体产生材料204,并且配置使气体产生材料204爆炸的点火材料205。通过将点火材料205点火、使气体产生材料204爆炸,从而能够利用气体的压力使网201从收纳器200放出。如图4的(b)所示,优选配置气体产生材料204以使得各个锤202向相互背离的方向(放射方向)吹散。由此,能够使网201可靠地向放射方向展开,覆盖无人机。另外,点火材料和气体产生材料无特别限定,但优选使用由不适用火药类监管法的非火药组成物构成的材料。
降落伞203具有半球形状的伞体203a、以及与伞体203a连接并且与捕获体2连结的吊索203b。在利用捕获体2捕获了无人机的状态下伞体203a打开,由此能够使无人机的下落速度减缓。
接着,对小型无人飞机击退装置1的动作例进行说明。首先,如图2所示,将捕获体2装配于捕获体发射装置3的发射台30。小型无人飞机击退装置1的设置场所无特别限定,但优选主要设置于公共的区域。该公共的区域并不是指特别限定的区,例如广泛包含首相官邸、皇居、寺院、公园、公共设施、历史性建筑物等区域。
利用检测单元4对小型无人飞机击退装置1的周围进行检测。检测单元4一边借助图1所示的旋转台8而旋转一边朝向空中发送电波,例如当由图5所示的无人机6反射并接收反射波时,能够检测出从小型无人飞机击退装置1到无人机6的距离和方向,能够确定无人机6的位置。接着,判定单元5根据检测单元4所检测的信息,判定飞行中的无人机6是否处于射程内。在通过判定单元5识别出无人机6的位置处于射程范围内之后,使图2所示的发射台30的后部侧在支承部9处以支点轴10为支点旋转,并使装配于发射台30的捕获体2的瞄准器与无人机6的位置对准。
捕获体发射装置3将钩挂部33释放,向后方侧牵拉弦32而借助钩挂于钩挂部33的弓31的复原力使弦32朝向前方高速地移动,朝向无人机6发射捕获体2。伴随着捕获体2的发射,与捕获体2连结的线21也从电动卷轴22送出。
如图5所示,当捕获体2接近无人机6而距离传感器24识别为已到达能够利用捕获体2捕获无人机6的位置之后,捕获弹20的收纳器200打开,向前方放出网201。即,通过将图4的(a)所示的点火材料205点火,而使气体产生材料204爆炸从而吹散各锤202,使网201向放射方向展开。
如图6所示,当网201覆盖并缠绕住无人机6时,无人机6的动作被封锁而被捕获。然后,图2所示的电动机23驱动,利用电动卷轴22来卷绕所送出的线21,将捕获了无人机6的捕获体2向小型无人飞机击退装置1拉近。此时,降落伞203的伞体203a打开,使无人机6的下落速度减缓,能够防止无人机6撞击到地上。并且,在无人机6的下落地点周边有人的情况下,也能够将事故的产生防患于未然。
这样,由于本发明的小型无人飞机击退装置1由捕获无人机的捕获体2以及朝向无人机发射捕获体2的捕获体发射装置3构成,因此即使无人机6向应该保卫的公共的区域飞来,也能够由捕获体发射装置3发射捕获体2而快速地捕获无人机6。因此,能够保卫善良的国民的利益和安全。
小型无人飞机击退装置1的设置台数能够根据需要而任意设定。因此,如果在公共的区域设置多台小型无人飞机击退装置1,即使多个可疑的无人机向公共的区域内飞来,也能够高效地捕获。
另外,实施方式所示的捕获体2优选构成为不会错误地捕获无人机以外的物体(例如,鸟兽类),也可以在捕获弹20中配设识别单元(例如,热传感器)。
Claims (5)
1.一种小型无人飞机击退装置,其将小型无人飞机击退,其中,该小型无人飞机击退装置具有:
捕获体,其捕获小型无人飞机;以及
捕获体发射装置,其朝向小型无人飞机发射该捕获体。
2.根据权利要求1所述的小型无人飞机击退装置,其中,
该小型无人飞机击退装置还具有检测单元,该检测单元检测距所述小型无人飞机的距离和方向。
3.根据权利要求2所述的小型无人飞机击退装置,其中,
该小型无人飞机击退装置包含判定单元,该判定单元根据所述检测单元的信息来判定所述小型无人飞机是否处于射程内,
当该判定单元判定为处于射程内时,该捕获体发射装置朝向该小型无人飞机发射所述捕获体。
4.根据权利要求1或2所述的小型无人飞机击退装置,其中,
所述捕获体由捕获所述小型无人飞机的捕获弹、连结于该捕获体的线、以及对该线进行卷绕的电动卷轴构成。
5.根据权利要求4所述的小型无人飞机击退装置,其中,
所述捕获弹具有缠绕于所述小型无人飞机的网以及使该小型无人飞机的下落速度减缓的降落伞。
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US20160376029A1 (en) | 2016-12-29 |
JP2017009244A (ja) | 2017-01-12 |
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