WO2019072009A1 - Véhicule aérien sans pilote consistant en un missile guidé à usages multiples - Google Patents

Véhicule aérien sans pilote consistant en un missile guidé à usages multiples 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
Authority
WO
WIPO (PCT)
Prior art keywords
missile
drone
missiles
purpose missile
pylon
Prior art date
Application number
PCT/CN2018/099583
Other languages
English (en)
Chinese (zh)
Inventor
高原美麟
Original Assignee
高玉宗
李晓旭
高原晨曦
高原美麟
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
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/fr

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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; Bombs 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—Arrangements 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—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft
    • B64D7/08—Arrangements of rocket launchers or releasing means
    • 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
    • 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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  • Life Sciences & Earth Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Environmental Sciences (AREA)
  • Biodiversity & Conservation Biology (AREA)
  • Pest Control & Pesticides (AREA)
  • Wood Science & Technology (AREA)
  • Zoology (AREA)
  • Insects & Arthropods (AREA)
  • Ecology (AREA)
  • Forests & Forestry (AREA)
  • Health & Medical Sciences (AREA)
  • Public Health (AREA)
  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Atmospheric Sciences (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

Le présent modèle d'utilité est un véhicule aérien sans pilote consistant en un missile guidé à usages multiples, comprenant un bâti, une pluralité d'ailes de rotor montées sur le bâti, un système de commande monté sur le bâti pour commander les ailes de rotor, et un système de surveillance monté sur le bâti pour surveiller l'environnement pendant le vol, et comprenant en outre un cadre de suspension de missile guidé auquel sont suspendus des missiles guidés, le cadre de suspension de missile guidé étant disposé juste au-dessous du centre du bâti, plusieurs missiles guidés étant parallèles les uns aux autres, disposés dans une direction verticale, et montés sur le cadre de suspension de missile guidé. La manière de monter le missile guidé du véhicule aérien sans pilote consistant en un missile guidé à usages multiples peut garantir que la stabilité de vol du véhicule aérien sans pilote n'est pas affectée lorsque le véhicule aérien sans pilote lance un missile guidé.
PCT/CN2018/099583 2017-10-13 2018-08-09 Véhicule aérien sans pilote consistant en un missile guidé à usages multiples WO2019072009A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN201721320548.XU CN207737504U (zh) 2017-10-13 2017-10-13 一种多用途的导弹无人机
CN201721320548.X 2017-10-13

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Publication Number Publication Date
WO2019072009A1 true WO2019072009A1 (fr) 2019-04-18

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CN (1) CN207737504U (fr)
WO (1) WO2019072009A1 (fr)

Cited By (1)

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CN117898156A (zh) * 2024-03-07 2024-04-19 成都润联科技开发有限公司 基于无人机的人工天气干预***

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CN111388928A (zh) * 2020-03-18 2020-07-10 高原晨曦 基于无人机的灭火方法及智能消防***
CN112802287B (zh) * 2020-12-16 2022-08-30 广东电网有限责任公司电力科学研究院 一种输电线路山火监测预警和定位***及其方法

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117898156A (zh) * 2024-03-07 2024-04-19 成都润联科技开发有限公司 基于无人机的人工天气干预***
CN117898156B (zh) * 2024-03-07 2024-05-31 成都润联科技开发有限公司 基于无人机的人工天气干预***

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