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WO2019072009A1 - 一种多用途的导弹无人机 - Google Patents

一种多用途的导弹无人机 Download PDF

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Publication number
WO2019072009A1
WO2019072009A1 PCT/CN2018/099583 CN2018099583W WO2019072009A1 WO 2019072009 A1 WO2019072009 A1 WO 2019072009A1 CN 2018099583 W CN2018099583 W CN 2018099583W WO 2019072009 A1 WO2019072009 A1 WO 2019072009A1
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WO
WIPO (PCT)
Prior art keywords
missile
drone
missiles
purpose missile
pylon
Prior art date
Application number
PCT/CN2018/099583
Other languages
English (en)
French (fr)
Inventor
高原美麟
Original Assignee
高玉宗
李晓旭
高原晨曦
高原美麟
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Filing date
Publication date
Application filed by 高玉宗, 李晓旭, 高原晨曦, 高原美麟 filed Critical 高玉宗
Publication of WO2019072009A1 publication Critical patent/WO2019072009A1/zh

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Classifications

    • A—HUMAN NECESSITIES
    • A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
    • A01G—HORTICULTURE; CULTIVATION OF VEGETABLES, FLOWERS, RICE, FRUIT, VINES, HOPS OR SEAWEED; FORESTRY; WATERING
    • A01G15/00—Devices or methods for influencing weather conditions
    • A—HUMAN NECESSITIES
    • A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
    • A01M—CATCHING, TRAPPING OR SCARING OF ANIMALS; APPARATUS FOR THE DESTRUCTION OF NOXIOUS ANIMALS OR NOXIOUS PLANTS
    • A01M7/00—Special adaptations or arrangements of liquid-spraying apparatus for purposes covered by this subclass
    • A—HUMAN NECESSITIES
    • A62—LIFE-SAVING; FIRE-FIGHTING
    • A62C—FIRE-FIGHTING
    • A62C3/00—Fire prevention, containment or extinguishing specially adapted for particular objects or places
    • A62C3/02—Fire prevention, containment or extinguishing specially adapted for particular objects or places for area conflagrations, e.g. forest fires, subterranean fires
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00—Dropping, ejecting, releasing or receiving articles, liquids, or the like, in flight
    • B64D1/02—Dropping, ejecting, or releasing articles
    • B64D1/04—Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D1/00—Dropping, ejecting, releasing or receiving articles, liquids, or the like, in flight
    • B64D1/02—Dropping, ejecting, or releasing articles
    • B64D1/04—Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
    • B64D1/06—Bomb releasing; Bomb doors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D7/00—Arrangement of military equipment, e.g. armaments, armament accessories or military shielding, in aircraft; Adaptations of armament mountings for aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D7/00—Arrangement of military equipment, e.g. armaments, armament accessories or military shielding, in aircraft; Adaptations of armament mountings for aircraft
    • B64D7/08—Arrangement of rocket launchers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B64U10/13—Flying platforms
    • B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications
    • B64U2101/20—UAVs specially adapted for particular uses or applications for use as communications relays, e.g. high-altitude platforms
    • B64U2101/24—UAVs specially adapted for particular uses or applications for use as communications relays, e.g. high-altitude platforms for use as flying displays, e.g. advertising or billboards
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports

Definitions

  • the utility model relates to the technical field of a drone carrying a missile, in particular to a multi-purpose missile drone.
  • UAVs have been widely used in various fields depending on their own flight characteristics. For example, drones carrying fire-fighting missiles can be used to timely remediate fires in high-rise buildings to avoid artificial high-rise buildings. The fire extinguishing efficiency is low and there may be casualties.
  • the drone launches the missile, the missile will have a certain reaction force to the drone.
  • the drone may also launch the missile. Due to the partial weight reduction, the part of the drone is biased. At this time, the flight direction of the drone may be affected and the task cannot be completed.
  • the technical problem solved by the utility model is to provide a missile drone capable of ensuring that the drone launches the missile without affecting the flight stability of the drone.
  • the utility model provides a multi-purpose missile drone, comprising a frame, a plurality of rotors mounted on the frame, a control system mounted on the frame and controlling the rotor, and being mounted on the frame and A monitoring system for monitoring a flight environment, further comprising a missile pylon suspended from a missile, the missile pylon being disposed directly below a center of the frame, and the plurality of missiles being parallel to each other and vertically arranged in a vertical direction The missile pylon.
  • the missile pylon is a cylinder
  • the missile pylon of the cylinder is provided along the axial direction thereof with a plurality of first through holes for mounting a plurality of the missiles, and the axial directions of the plurality of first through holes are mutually parallel.
  • the bottom surface of the missile pylon extends outwardly in a circumferential direction thereof to form a circular chassis belt.
  • the frame is provided with a plurality of second through holes symmetrical about a center of the frame, the axial direction of the second through holes is a vertical direction, and the number of the second through holes is equal to that of the rotor The number of the rotors is installed in the second through hole in one-to-one correspondence.
  • the number of the second through holes is four.
  • the drone further sets a sharing module, and the mobile phone client or controller can control the drone through the sharing module.
  • the utility model also provides a multi-purpose missile drone, wherein the drone is the multi-purpose missile drone described above, and the plurality of missiles are missiles filled with fire extinguishing agent internally, and the plurality of missiles are A broken armor used to break doors and windows.
  • the utility model also provides a multi-purpose missile drone, wherein the drone is the multi-purpose missile drone described above, and the plurality of missiles are missiles filled with dry ice inside.
  • the utility model also provides a multi-purpose missile drone, wherein the unmanned aerial vehicle is the multi-purpose missile drone described above, and a plurality of the missiles are missiles filled with a smoke agent inside.
  • the utility model also provides a multi-purpose missile drone, wherein the drone is the multi-purpose missile drone described above, and the plurality of missiles are missiles filled with a cloud generating agent inside.
  • the utility model also provides a multi-purpose missile drone, wherein the drone is the multi-purpose missile drone described above, and the plurality of missiles are missiles filled with a color smoke agent.
  • the utility model also provides a multi-purpose missile drone, wherein the drone is the multi-purpose missile drone described above, and the plurality of missiles are missiles filled with medicament inside.
  • the utility model also provides a multi-purpose missile drone, wherein the unmanned aerial vehicle is the multi-purpose missile drone described above, and the plurality of the missiles are pyrotechnic bombs filled with medicament inside.
  • the utility model also provides a multi-purpose missile drone, wherein the drone is the multi-purpose missile drone described above, and the plurality of missiles are missiles with internal sound equipment.
  • the utility model also provides a multi-purpose missile drone, wherein the drone is the multi-purpose missile drone described above, and the plurality of missiles are missiles with laser or/and light emitters arranged inside. Several of the missiles are capable of emitting lasers or/and lights.
  • the utility model also provides a multi-purpose missile drone, wherein the drone is the multi-purpose missile drone described above, and the shape of the drone is a cartoon character or an animal shape.
  • the utility model also provides a multi-purpose missile drone, wherein the unmanned aerial vehicle is the multi-purpose missile drone described above, and the missile is a missile with an internal coal mine detector, the coal mine detector The detection result can be transmitted to a terminal display wirelessly connected to the drone.
  • the multi-purpose missile drone of the utility model has the following beneficial effects:
  • the missile pylon is installed directly below the center of the rack, and several missiles are vertically arranged and mounted in the same direction on the missile pylon, and several vertically arranged missiles are all along the rack.
  • the center direction gives the frame a vertical downward pulling force.
  • the missile pylon is a cylinder. During the flight of the drone, the air resistance generated by the outside air to the drone can be reduced.
  • the missile pylon can also be used as a support frame to support the drone placed on the ground, simplifying the structure of the drone, facilitating production and reducing costs.
  • the missile is filled with different materials, so that the multi-purpose missile drone can be used for different working situations such as fire extinguishing, artificial rainfall, artificial cloud making, aerial lighting, playing audio, etc. to complete the corresponding work, so that one can
  • the multi-purpose machine saves costs.
  • the missile drones working in different occasions can always maintain a smooth flight to better complete the corresponding work.
  • Its shape can be a variety of cartoon characters or a variety of animal shapes to enhance its ornamental and adaptability.
  • FIG. 1 is a front elevational view of a specific embodiment of a multi-purpose missile drone provided by the present invention
  • FIG. 2 is a top plan view of a specific embodiment of a multi-purpose missile drone provided by the present invention
  • the purpose of the utility model is to provide a multi-purpose missile drone, which provides a multi-purpose missile drone capable of ensuring that the drone does not affect the flight stability of the drone when the missile is launched and after the missile is launched.
  • FIG. 1 is a front view of a specific embodiment of a multi-purpose missile drone provided by the present invention
  • FIG. 2 is a multi-purpose missile provided by the present invention.
  • a multi-purpose missile drone includes a frame 1, a plurality of rotors 2 mounted on the frame 1, and a plurality of rotors 2 rotating.
  • the drone uses the rotation of the rotor 2 to fly or change the direction of travel generated by the drone.
  • control system 3 mounted to the frame 1 and controlling the rotor 2 and a monitoring system 4 mounted to the frame 1 and monitoring the environment of the flight, wherein the control system 3 controls a number of rotors 2, such as
  • the control system 3 increases the rotational speed of a certain rotor 2 and reduces the rotational speed of the rotor 2 corresponding to the rotor 2, and the speed difference between the rotational speeds of the rotor 2 makes the rotor 2 to the drone Different lifts are generated. Under the drive of different lifts, the drone can realize steering.
  • the monitoring system 4 is used to monitor the environment of the drone and transmit it to the ground, and the operator can monitor it in real time.
  • a missile pylon 7 that suspends a missile 6, wherein the missile pylon 7 is disposed directly below the center of the gantry 1, and a plurality of the missiles 6 are vertically aligned with each other and mounted to the missile in the same direction Hanger 7, in this embodiment, the missile pylon 7 is installed directly below the center of the frame 1, and a plurality of missiles 6 are vertically arranged and mounted in the same direction on the missile pylon 7, and a plurality of vertically arranged missiles 6 are The center direction of the frame 1 gives the frame 1 a vertical downward pulling force.
  • the overall weight of the frame 1 is reduced, and the weight reduction position is the center of the frame 1, so the frame 1 does not cause the position of the frame 1 to be biased or light, so that the branch is not stable.
  • the missile pylon 7 is a cylinder, and the cylindrical missile pylons 7 are disposed along the axial direction thereof in parallel with each other in the axial direction and are used for mounting a plurality of the missiles 6 .
  • a through hole 8 A plurality of missiles 6 are disposed in a plurality of first through holes 8 which are parallel to each other in the axial direction, and can simultaneously fire missiles to a certain position at the same time.
  • the missile pylon 7 is selected as a cylinder, which can minimize the air resistance generated by the outside air to the drone during the flight of the drone.
  • the structure of the missile pylon 7 is not limited thereto, and may be, for example, a rectangular parallelepiped.
  • the bottom surface of the missile pylon 7 extends outward in a circumferential direction thereof to form a circular chassis 71.
  • the circular chassis 71 is merely an embodiment, on the one hand, a circle The space occupied by the chassis 71 is small, which makes the drone more compact.
  • the design of the circular chassis 71 is firmer. It is not damaged by touching the trunk or the branch.
  • the circular chassis 71 contacts the ground to support the drone.
  • the circular chassis 71 can also be provided with a support. The legs support the ground.
  • the missile pylon 7 can also serve as the support frame 5. This arrangement simplifies the structure of the drone, facilitates fabrication, and reduces costs.
  • the frame 1 is provided with a plurality of second through holes 9 symmetrically about the center of the frame 1, and the axial direction of some of the second through holes 9 is a vertical direction, the second The number of through holes 9 is equal to the number of the rotors 2, and the rotors 2 are mounted in the second through holes 9 one by one.
  • a plurality of rotors 2 are respectively disposed in the corresponding second through holes 9 because the environment in which the drone is in the execution of the mission may be a harsh environment, so that the rotor 2 is disposed in the second through hole 9 It is not directly exposed to the outside of the frame 1, so that the rotation of the rotor 2 can be prevented by the rotor 2 being touched by other items in the environment, and the rotor 2 can be well protected.
  • the number of the second through holes 9 is four.
  • the frame 1 is provided with four rotors 2, and the four rotors 2 are respectively arranged one by one.
  • four rotors 2 are arranged symmetrically about the center of the frame 1.
  • the structure is simple and can ensure the smooth flight of the drone. It should be understood that the number of the rotors 2 is selected as four not unique settings. the way.
  • the drone is further provided with a sharing module, and the mobile phone client or the controller can control the drone through the sharing module. Sharing drones can get more people into contact with drones.
  • the utility model also provides a multi-purpose missile drone, wherein the drone is the multi-purpose missile drone described above, wherein a plurality of the missiles 6 are missiles 6 filled with fire extinguishing agent inside, a plurality of The missile 6 is an armor-piercing projectile for breaking doors and windows.
  • the operator passes the monitoring system 4 and the control system 3, firstly, the armor-piercing projectile destroys the door and window, and secondly, the missile 6 containing the fire-extinguishing agent can be fired to the fire extinguishing place.
  • the utility model also provides a multi-purpose missile drone, wherein the drone is the multi-purpose missile drone described above, wherein a plurality of the missiles 6 are missiles 6 filled with dry ice inside, which can be completed Local artificial rainfall.
  • the operator can launch the missile 6 containing dry ice to a certain position through the monitoring system 4 and the control system 3 to complete the artificial rainfall work, because several of the missiles 6 containing dry ice are vertically arranged.
  • the UAV launches the missile 6 and launches the missile 6 containing dry ice without affecting the smoothness of the UAV flight.
  • the utility model also provides a multi-purpose missile drone, wherein the drone is the multi-purpose missile drone described above, wherein a plurality of the missiles 6 are missiles 6 filled with a smoke agent inside, which can As a smoke bomb, at this time, the operator can make a smoke screen on important targets through the monitoring system 4 and the control system 3, preventing enemy missiles and satellite positioning from being attacked, due to several of the described missiles containing the smoke agent 6 respectively Vertically arranged in the missile pylon 7, so that the UAV does not affect the stability of the UAV flight when launching the missile and after launching the missile.
  • the utility model also provides a multi-purpose missile drone, wherein the unmanned aerial vehicle is the multi-purpose missile drone described above, wherein a plurality of the missiles 6 are missiles 6 filled with a cloud generating agent inside,
  • the cloud generating agent may be liquid nitrogen or atomized water.
  • the operator creates a cloud over the scenic spot through the monitoring system 4 and the control system 3 to beautify the landscape, because several of the missiles 6 containing the cloud generating agent are respectively vertical. It is arranged directly in the missile pylon 7, so it ensures that the UAV does not affect the stability of the UAV flight when it launches the missile and after launching the missile.
  • the utility model also provides a multi-purpose missile drone, wherein the drone is the multi-purpose missile drone described above, wherein a plurality of the missiles 6 are missiles 6 filled with a color smoke agent.
  • the operator can launch the missile 6 through the monitoring system 4 and the control system 3 to perform performances for the grand festival, because several of the missiles 6 containing the colored smoke agent are vertically arranged on the missile pylon 7 respectively. Therefore, it is guaranteed that the UAV launches the missile at 6 o'clock and launches the missile 6 without affecting the stability of the UAV flight.
  • the utility model also provides a multi-purpose missile drone, wherein the unmanned aerial vehicle is the multi-purpose missile drone described above, wherein a plurality of the missiles 6 are missiles 6 filled with medicaments, which can be The crops enter the new plant protection work.
  • the operator can launch the missile 6 containing the medicament through the detection system 4 and the control system 3 to complete the corresponding plant protection work, because several of the missiles 6 containing the medicament are vertically arranged.
  • the missile pylon 7 it ensures that the UAV launches the missile at 6 o'clock and launches the missile 6 without affecting the stability of the UAV flight.
  • the utility model also provides a multi-purpose missile drone, wherein the unmanned aerial vehicle is the multi-purpose missile drone described above, and the plurality of the missiles 6 are pyrotechnic bombs filled with medicaments, which can be discharged in the air. Fireworks, firecrackers.
  • the utility model also provides a multi-purpose missile drone, wherein the unmanned aerial vehicle is the multi-purpose missile drone described above, and the plurality of the missiles 6 are internally provided with an audio device for playing audio in the air.
  • the utility model also provides a multi-purpose missile drone, wherein the drone is the multi-purpose missile drone described above, and the plurality of missiles 6 may be laser or light generators in the air. Launch a laser or illumination light.
  • the utility model also provides a multi-purpose missile drone, the shape of the drone being cartoon characters, animals and other shapes that can be used for aerial display, such as flying turtles, eagle, birds, apples, moons , stars, etc.
  • the utility model also provides a multi-purpose missile drone, the multi-purpose missile drone described above, the missile 6 is a missile with a coal mine detector inside, and the coal mine detector can transmit the detection result To the terminal display that is wirelessly connected to the drone.
  • the multi-purpose missile UAV of the structure can ensure that the UAV launches the missile 6 without affecting the stability of the UAV flight during use.

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Abstract

本实用新型公开了一种多用途的导弹无人机，包括机架、安装于机架的多个旋翼、安装于机架并控制旋翼的控制系统和安装于机架并对飞行的环境进行监测的监测系统，还包括悬挂导弹的导弹挂架，导弹挂架设置于机架的中心的正下方，若干导弹彼此平行且沿竖直方向排列安装于导弹挂架。该多用途的导弹无人机的导弹安装方式，能保证无人机发射导弹时而不影响无人机的飞行的平稳性。

Description

一种多用途的导弹无人机 技术领域
本实用新型涉及携带导弹的无人机技术领域，具体涉及一种多用途的导弹无人机。
背景技术
无人机依靠其自身的飞行特点，已被广泛的用于各个领域中，比如，携带灭火导弹的无人机可用于对高层建筑所突发的火灾进行及时的补救，以避免人为对高层建筑灭火效率低且可能会发生人员伤亡的情况的发生，而无人机在发射导弹时，导弹会对无人机产生一定的反作用力，同时，无人机在射出导弹的情况下，可能还会由于部分重量的减少而导致无人机出现部分部位偏重的情况，此时，无人机的飞行方向可能会受到影响而使得其无法完成任务。
因此，如何提供一种能保证无人机发射导弹时及发射导弹后不影响无人机的飞行平稳性的导弹无人机便成为了本领域技术人员急需解决的技术问题。
发明内容
本实用新型解决的技术问题在于能够提供一种能保证无人机发射导弹时而不影响无人机的飞行平稳性的导弹无人机。
本实用新型提供的多用途的导弹无人机，包括机架、安装于所述机架的多个旋翼、安装于所述机架并控制所述旋翼的控制系统和安装于所述机架并对飞行的环境进行监测的监测系统，还包括悬挂导弹的导弹挂架，所述导弹挂架设置于所述机架的中心的正下方，若干所述导弹彼此平行且沿竖直方向排列安装于所述导弹挂架。
作为优选，所述导弹挂架为圆柱体，圆柱体的所述导弹挂架沿其轴向设置有用于安装若干所述导弹的若干第一通孔，所述若干第一通孔的轴向彼此平行。
作为优选，所述导弹挂架的底面沿其周向方向向外延伸形成圆形底盘带。
作为优选，所述机架设有关于所述机架的中心对称的若干第二通孔，所述第二通孔的轴向为竖直方向，所述第二通孔的数量等于所述旋翼的数量，所述旋翼一一对应安装于所述第二通孔内。
作为优选，所述第二通孔的数量为四个。
作为优选，所述无人机还设置共享模块，手机客户端或者控制器通过所述共享模块可以控制所述无人机。
本实用新型还提供一种多用途的导弹无人机，所述无人机为上述所述的多用途的导弹无人机，若干所述导弹为内部填充灭火剂的导弹，若干所述导弹为用于破开门窗的破甲弹。
本实用新型还提供一种多用途的导弹无人机，所述无人机为上述所述的多用途的导弹无人机，若干所述导弹为内部填充干冰的导弹。
本实用新型还提供一种多用途的导弹无人机，所述无人机为上述所述的多用途的导弹无人机，若干所述导弹为内部填充烟幕剂的导弹。
本实用新型还提供一种多用途的导弹无人机，所述无人机为上述所述的多用途的导弹无人机，若干所述导弹为内部填充云朵生成剂的导弹。
本实用新型还提供一种多用途的导弹无人机，所述无人机为上述所述的多用途的导弹无人机，若干所述导弹为内部填充彩色烟幕剂的导弹。
本实用新型还提供一种多用途的导弹无人机，所述无人机为上述所述的多用途的导弹无人机，若干所述导弹为内部填充药剂的导弹。
本实用新型还提供一种多用途的导弹无人机，所述无人机为上述所述的多用途的导弹无人机，若干所述导弹为内部填充药剂的烟火弹。
本实用新型还提供一种多用途的导弹无人机，所述无人机为上述所述的多用途的导弹无人机，若干所述导弹为内部设置音响设备的导弹。
本实用新型还提供一种多用途的导弹无人机，所述无人机为上述所述的多用途的导弹无人机，若干所述导弹为内部设置激光或/和灯光发射器的导弹，若干所述导弹能够发射激光或/和灯光。
本实用新型还提供一种多用途的导弹无人机，所述无人机为上述所述的多用途的导弹无人机，所述无人机的外形为卡通人物或者动物的外形。
本实用新型还提供一种多用途的导弹无人机，所述无人机为上述所述的多用途的导弹无人机，所述导弹为内部设置煤矿探测器的导弹，所述煤矿探测器能够将探测结果传输至与所述无人机无线相连的终端显示器上。
本实用新型的多用途导弹无人机与现有技术相比，具有以下有益效果：
1、提供的多用途导弹无人机中，导弹挂架安装于机架中心的正下方，若干导弹竖直排列且沿同一方向安装于导弹挂架，若干竖直排列的导弹均沿机架的中心方向给予机架竖直向下的拉力，当导弹发出时，机架整体的重量会减轻，而重量减轻的位置为机架的中心，所以机架不会发生因为非中心位置重量的变化而受力不均，也就不会出现飞行不平稳的情况。
2、导弹挂架为圆柱体，无人机飞行过程中可以减少外界空气对无人机产生的空气阻力。
3、导弹挂架也可以作为支撑架用于支撑放置于地面的无人机，简化了无人机的结构，方便制作，降低成本。
4、导弹内填充不同的材料，以使该多用途导弹无人机能够用于灭火、人工降雨、人工造云、空中照明、播放音频等不同的工作场合以完成相应的工作，如此，可一机多用，节约成本，同时，又因为该多用途导弹无人机的结构，可使在不同场合工作中的导弹无人机一直可以保持平稳的飞行，以更好的完成相应的工作。其外形可以是各种卡通人物外形或者各种动物外形，提高其观赏性和适应性。
附图说明
图1为本实用新型所提供的多用途的导弹无人机的一种具体实施方式的主视图；
图2为本实用新型所提供的多用途的导弹无人机的一种具体实施方式的俯视图；
图1-2中的附图标记说明如下：
1机架，2旋翼，3控制系统，4监测系统，5支撑架，6导弹，7导弹挂架，71圆形底盘，8第一通孔，9第二通孔。
具体实施方式
本实用新型的目的是提供一种多用途的导弹无人机，所提供的多用途的导弹无人机，能保证无人机发射导弹时及发射导弹后不影响无人机的飞行平稳性。
为了使本领域的技术人员更好地理解本实用新型的技术方案，下面结合附图和具体实施方式对本实用新型作进一步的详细说明。
如图1和图2所示，图1为本实用新型所提供的多用途的导弹无人机的一种具体实施方式的主视图，图2为本实用新型所提供的多用途的导弹无人机的一种具体实施方式的俯视图。
本具体实施方式中，如图1和图2所示，一种多用途的导弹无人机，包括机架1、安装于所述机架1上的多个旋翼2，多个旋翼2旋转，无人机利用旋翼 2旋转对无人机产生的升力进行飞行或者改变运行方向。还包括安装于所述机架1并控制所述旋翼2的控制系统3和安装于所述机架1并对飞行的环境进行监测的监测系统4，其中，控制系统3控制若干旋翼2，比如，当无人机需要改变运行方向时，控制系统3通过提升某一旋翼2的转速和降低与该旋翼2对应的旋翼2的转速，旋翼2之间转速的速度差使得旋翼2对无人机产生不同的升力，在不同升力的驱使下，无人机可实现转向，监测系统4用于监测无人机所在环境，并传输给地面，操作人员可实时监测。
还包括悬挂导弹6的导弹挂架7，其中，所述导弹挂架7设置于所述机架1的中心的正下方，若干所述导弹6彼此平行竖直排列沿同一方向安装于所述导弹挂架7，该具体实施方式中，导弹挂架7安装于机架1中心的正下方，若干导弹6竖直排列且沿同一方向安装于导弹挂架7，若干竖直排列的导弹6均于机架1的中心方向给予机架1竖直向下的拉力，当导弹6发出时，机架1整体的重量会减轻，而重量减轻的位置为机架1的中心，所以机架1不会发生因为非中心位置重量的变化而受力不均，也不会出现机架1某一处偏重或者偏轻的情况，因此也就不会出现分行不平稳的情况。
本具体实施方式中，如图1所示，导弹挂架7为圆柱体，圆柱体的导弹挂架7沿其轴向设有轴向方向彼此平行且用于安装若干所述导弹6的若干第一通孔8。若干导弹6设置安装于轴向方向彼此平行的若干第一通孔8内，可同时向某一处连续发射导弹。导弹挂架7选为圆柱体，可以最大限度的减少无人机飞行过程中外界空气对无人机产生的空气阻力，当然，导弹挂架7的结构不限于此，比如还可以为长方体等。
本具体实施方式中，如图1所示，所述导弹挂架7的底面沿其周向方向向外延伸形成圆形底盘71，设置为圆形底盘71只是一种实施方式，一方面，圆形底盘71所占的空间较小，使得无人机更为小巧，另一方面，当无人机进入比较恶劣的环境执行任务时，比如树木较多的森林，圆形底盘71的设计更加牢固，其不会因触碰到树干或树枝而被损坏，同时，无人机置于地面时，所述圆形底盘71接触地面以支撑无人机，当然，圆形底盘71上也可以设置支腿，以支撑地面，而本实施方式中，导弹挂架7也可以作为支撑架5，该设置简化了无人机的结构，方便制作，降低成本。
本具体实施方式中，所述机架1设有关于所述机架1的中心对称的若干第二通孔9，若干所述第二通孔9的轴向为竖直方向，所述第二通孔9的数量等于所述旋翼2的数量，所述旋翼2一一对应安装于所述第二通孔9内。若干旋翼2分别置于相对应的第二通孔9内，是因为无人机在执行任务时，所处的环境有 可能是恶劣的环境，所以将旋翼2设置于第二通孔9内而不是直接的全部裸露于机架1的外侧，这样一来，可避免旋翼2触碰到环境中的其他物品而致使旋翼2损坏的情况的发生，可以很好的保护旋翼2。
如图2所示，本具体实施方式中，所述第二通孔9的数量为四个，相应的，机架1上设有四个旋翼2，四个旋翼2分别一一对应设置于第二通孔9内，设置四个关于机架1的中心中心对称的旋翼2，结构简单且可以保证无人机平稳的飞行，应当理解的是，旋翼2的数量选为四个不是唯一的设置方式。
本具体实施方式中，无人机还设置共享模块，手机客户端或者控制器通过共享模块可以控制无人机。共享化无人机，可以使更多的人接触到无人机。
本实用新型还提供一种多用途的导弹无人机，所述无人机为上述所述的多用途的导弹无人机，其中，若干所述导弹6为内部填充灭火剂的导弹6，若干所述导弹6为用于破开门窗的破甲弹，此时，操作人员通过监测系统4和控制系统3，首先，破甲弹破坏门窗，其次可以向灭火处发射含有灭火剂的导弹6，以完成灭火工作，尤其是对一些高层建筑物或人员较难进入的灭火场所，由于若干所述的灭火导弹6分别竖直排列于导弹挂架7内，所以保证了该无人机发射灭火导弹6时及发射灭火导弹6后不影响无人机飞行的平稳性。
本实用新型还提供一种多用途的导弹无人机，所述无人机为上述所述的多用途的导弹无人机，其中，若干所述导弹6为内部填充干冰的导弹6，可以完成局部人工降雨，此时，操作人员通过监测系统4和控制系统3，可以向某一位置发射含有干冰的导弹6，以完成人工降雨工作，由于若干所述的含有干冰的导弹6分别竖直排列于导弹挂架7内，所以保证了该无人机发射导弹6时及发射含有干冰的导弹6后不影响无人机飞行的平稳性。
本实用新型还提供一种多用途的导弹无人机，所述无人机为上述所述的多用途的导弹无人机，其中，若干所述导弹6为内部填充烟幕剂的导弹6，可以作为烟幕弹使用，此时，操作人员通过监测系统4和控制系统3，可以在重要目标上制造烟幕，防止敌人的导弹、卫星定位，避免遭受袭击，由于若干所述的含有烟幕剂的导弹6分别竖直排列于导弹挂架7内，所以保证了该无人机发射导弹时及发射导弹后不影响无人机飞行的平稳性。
本实用新型还提供一种多用途的导弹无人机，所述无人机为上述所述的多用途的导弹无人机，其中，若干所述导弹6为内部填充云朵生成剂的导弹6，云朵生成剂可以为液氮或雾化水，此时，操作人员通过监测系统4和控制系统3，在景点上空制造云朵，以美化景观，由于若干所述的含有云朵生成剂的导弹6 分别竖直排列于导弹挂架7内，所以保证了该无人机发射导弹时及发射导弹后不影响无人机飞行的平稳性。
本实用新型还提供一种多用途的导弹无人机，所述无人机为上述所述的多用途的导弹无人机，其中，若干所述导弹6为内部填充彩色烟幕剂的导弹6，此时，操作人员通过监测系统4和控制系统3，可以向空中发射该导弹6，为盛大节日进行表演助威，由于若干所述的含有彩色烟幕剂的导弹6分别竖直排列于导弹挂架7内，所以保证了该无人机发射导弹6时及发射导弹6后不影响无人机飞行的平稳性。
本实用新型还提供一种多用途的导弹无人机，所述无人机为上述所述的多用途的导弹无人机，其中，若干所述导弹6为内部填充药剂的导弹6，可以对农作物等进新植保工作，此时，操作人员通过检测系统4和控制系统3，可以发射含有药剂的导弹6，以完成相应的植保工作，由于若干所述的含有药剂的导弹6分别竖直排列于导弹挂架7内，所以保证了该无人机发射导弹6时及发射导弹6后不影响无人机飞行的平稳性。
本实用新型还提供一种多用途的导弹无人机，所述无人机为上述所述的多用途的导弹无人机，若干所述导弹6为内部填充药剂的烟火弹，可在空中燃放烟火、爆竹。
本实用新型还提供一种多用途的导弹无人机，所述无人机为上述所述的多用途的导弹无人机，若干所述导弹6为内部设置音响设备，可在空中播放音频。
本实用新型还提供一种多用途的导弹无人机，所述无人机为上述所述的多用途的导弹无人机，若干所述导弹6可以是雷射激光或灯光发生器，在空中发射激光或照明灯光。
本实用新型还提供一种多用途的导弹无人机，所述无人机外形为卡通人物、动物及其他可以用于空中展示的各种形状，比如飞行的乌龟、老鹰、鸟、苹果、月亮、星星等等。
本实用新型还提供一种多用途的导弹无人机，无人机为上述所述的多用途的导弹无人机，导弹6为内部设置煤矿探测器的导弹，煤矿探测器能够将探测结果传输至与无人机无线相连的终端显示器上。
由此可见，该结构的多用途的导弹无人机，在使用过程中，可保证该无人机发射导弹6时而不影响无人机飞行的平稳性。
以上实施方式仅为本实用新型的示例性实施方式，不用于限制本实用新型，本实用新型的保护范围由权利要求书限定。本领域技术人员在本实用新型的实 质和保护范围内，对本实用新型做出的各种修改或等同替换也落在本实用新型的保护范围内。

Claims (17)

  1. 一种多用途的导弹无人机，包括机架、安装于所述机架的多个旋翼、安装于所述机架并控制所述旋翼的控制系统和安装于所述机架并对飞行的环境进行监测的监测系统，还包括悬挂导弹的导弹挂架，其特征在于，所述导弹挂架设置于所述机架的中心的正下方，若干所述导弹彼此平行且沿竖直方向排列安装于所述导弹挂架。
  2. 根据权利要求1所述的多用途的导弹无人机，其特征在于，所述导弹挂架为圆柱体，圆柱体的所述导弹挂架沿其轴向设置有用于安装若干所述导弹的若干第一通孔，所述若干第一通孔的轴向彼此平行。
  3. 根据权利要求2所述的多用途的导弹无人机，其特征在于，所述导弹挂架的底面沿其周向方向向外延伸形成圆形底盘。
  4. 根据权利要求2所述的多用途的导弹无人机，其特征在于，所述机架设有关于所述机架的中心对称的若干第二通孔，所述第二通孔的轴向为竖直方向，所述第二通孔的数量等于所述旋翼的数量，所述旋翼一一对应安装于所述第二通孔内。
  5. 根据权利要求4所述的多用途的导弹无人机，其特征在于，所述第二通孔的数量为四个。
  6. 根据权利要求1所述的多用途的导弹无人机，其特征在于，所述无人机还设置共享模块，手机客户端或者控制器通过所述共享模块可以控制所述无人机。
  7. 一种多用途的导弹无人机，其特征在于，所述无人机为上述权利要求1-6任一项所述的多用途的导弹无人机，若干所述导弹为内部填充灭火剂的导弹，若干所述导弹为用于破开门窗的破甲弹。
  8. 一种多用途的导弹无人机，其特征在于，所述无人机为上述权利要求1-6任一项所述的多用途的导弹无人机，若干所述导弹为内部填充干冰的导弹。
  9. 一种多用途的导弹无人机，其特征在于，所述无人机为上述权利要求1-6任一项所述的多用途的导弹无人机，若干所述导弹为内部填充烟幕剂的导弹。
  10. 一种多用途的导弹无人机，其特征在于，所述无人机为上述权利要求1-6任一项所述的多用途的导弹无人机，若干所述导弹为内部填充云朵生成剂的导弹。
  11. 一种多用途的导弹无人机，其特征在于，所述无人机为上述权利要求1-6任一项所述的多用途的导弹无人机，若干所述导弹为内部填充彩色烟幕剂的导弹。
  12. 一种多用途的导弹无人机，其特征在于，所述无人机为上述权利要求1-6任一项所述的多用途的导弹无人机，若干所述导弹为内部填充药剂的导弹。
  13. 一种多用途的导弹无人机，其特征在于，所述无人机为上述权利要求1-6任一项所述的多用途的导弹无人机，若干所述导弹为内部填充药剂的烟火弹。
  14. 一种多用途的导弹无人机，其特征在于，所述无人机为上述权利要求1-6任一项所述的多用途的导弹无人机，若干所述导弹为内部设置音响设备的导弹。
  15. 一种多用途的导弹无人机，其特征在于，所述无人机为上述权利要求1-6任一项所述的多用途的导弹无人机，若干所述导弹为内部设置激光或/和灯光发射器的导弹，若干所述导弹能够发射激光或/和灯光。
  16. 一种多用途的导弹无人机，其特征在于，所述无人机为上述权利要求1-6任一项所述的多用途的导弹无人机，所述无人机的外形为卡通人物或者动物的外形。
  17. 一种多用途的导弹无人机，其特征在于，所述无人机为上述权利要求1-6任一项所述的多用途的导弹无人机，所述导弹为内部设置煤矿探测器的导弹，所述煤矿探测器能够将探测结果传输至与所述无人机无线相连的终端显示器上。
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