CN107150796A - A kind of multi-rotor unmanned aerial vehicle - Google Patents

A kind of multi-rotor unmanned aerial vehicle Download PDF

Info

Publication number
CN107150796A
CN107150796A CN201710185144.2A CN201710185144A CN107150796A CN 107150796 A CN107150796 A CN 107150796A CN 201710185144 A CN201710185144 A CN 201710185144A CN 107150796 A CN107150796 A CN 107150796A
Authority
CN
China
Prior art keywords
unmanned aerial
aerial vehicle
rotor unmanned
rotor
fuselage
Prior art date
Legal status (The legal status 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 status listed.)
Withdrawn
Application number
CN201710185144.2A
Other languages
Chinese (zh)
Inventor
周良勇
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CN201710185144.2A priority Critical patent/CN107150796A/en
Publication of CN107150796A publication Critical patent/CN107150796A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/08Helicopters with two or more rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00Equipment not otherwise provided for
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/10Rotorcrafts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00UAVs specially adapted for particular uses or applications

Abstract

A kind of multi-rotor unmanned aerial vehicle, belong to unmanned vehicle technical field, including fuselage, horn, motor, rotor, foot stool, one end connection fuselage of horn, motor is arranged on horn, and rotor is arranged in the rotating shaft of motor, foot stool is connected to below fuselage, in addition horizontal hanger is additionally provided with fuselage, the outer end of the hanger is provided with sucker and support, and support is located at the lower section of sucker.Multi-rotor unmanned aerial vehicle can be adsorbed on the cladding glass of high building or the window-glass in house by the sucker on the hanger.After adsorbing on pinnacled glass, multi-rotor unmanned aerial vehicle just provides lift without battery power, and its working equipment carried aloft can work or await orders for a long time.Multi-rotor unmanned aerial vehicle of the present invention can be widely applied to pinpoint the fields such as shooting, monitoring, live, environment monitoring, case scouting, city management, garden security protection, vehicle anti-theft in the air.

Description

A kind of multi-rotor unmanned aerial vehicle
Technical field
The present invention relates to unmanned vehicle technical field, and in particular to a kind of multi-rotor unmanned aerial vehicle.
Background technology
Multi-rotor unmanned aerial vehicle generally has 3~8 rotors, especially most commonly seen with 4 rotors.Multi-rotor unmanned aerial vehicle possesses vertically Landing, hovering, low-speed operations, inverted flight, side fly, 360 degree rotate etc. function, take pictures, image, monitor, detect in the air Examine, radio signal is relayed, high-voltage line, bridge, dam inspection Check, search and rescue aid are applied in terms of transport express delivery.It is existing Multi-rotor unmanned aerial vehicle mainly have following deficiency:Electric energy is provided by the battery loaded on machine during due to hovering in the air, because This cruising time is short, and most of multi-rotor unmanned aerial vehicles worked by battery powers once can only follow-on mission about 10~30 minutes Left and right, that is to say, that typically only 10~30 minutes time that multi-rotor unmanned aerial vehicle works in the air, people far can not be met The reality such as long-time is monitored, shot, propagandaing directed to communicate, transmitting in the air, signal is relayed, deployed troops on garrison duty, awaited orders are carried out using multi-rotor unmanned aerial vehicle Demand.In addition, existing multi-rotor unmanned aerial vehicle is hovered in the air when the monitoring of progress fixed point, shooting, its posture is by wind-force and position Put sensor signal influence larger, stability is difficult to ensure;Multi-rotor unmanned aerial vehicle hover in the air work when, flight control system need Its posture is carried out to control and adjust in real time, the electric energy of battery had both been consumed, there is also no small potential safety hazard, just in case occur machine Tool, automatically controlled failure or misoperation, just easily cause air crash accident(Aircraft bombing), or even from aerial fall down injure people by a crashing object.
The content of the invention
It is an object of the invention to provide it is a kind of can stop for a long time many rotors for working or await orders on aloft object without It is man-machine, to solve the deficiency that existing multi-rotor unmanned aerial vehicle airborne period is short, can not work in the air for a long time.
The technical scheme is that:A kind of multi-rotor unmanned aerial vehicle, including fuselage, horn, motor, rotor(Propeller), pin Frame(Leg), one end connection fuselage of horn, motor is on horn, and rotor is arranged in the rotating shaft of motor(Or speed changer On), foot stool is connected to below fuselage, and typically head and video camera or other working equipments, part are additionally provided with below fuselage, Battery is also equipped with fuselage and flies control unit, is generally additionally provided with rotor protective frame to protect what is rotated at a high speed in rotor periphery Rotor is damaged from encountering foreign object, in addition, being additionally provided with horizontal hanger on fuselage, is looked up from Vertical Square(Overlook), should Hanger is stretched out outside each rotor wing rotation scope line, and sucker and support are provided with the outer end of hanger, and support is located under sucker Side.By the sucker and support on hanger, multi-rotor unmanned aerial vehicle rests against cladding glass, window of the sucker suction in high building On glass.After absorption is on the cladding glass, window-glass of high building, the working equipment carried in multi-rotor unmanned aerial vehicle(Such as phase Machine, video camera, megaphone, signal trunk module, illuminating lamp, gas sensor etc.)Just can be for a long time(It is general reachable several small When, or even more than 24 hours)Aloft work or await orders.
The beneficial effects of the invention are as follows because multi-rotor unmanned aerial vehicle can be adsorbed by the sucker on hanger in curtain wall glass Worked on glass and window-glass, and the multi-rotor unmanned aerial vehicle under adsorbed state, lift is provided without rotor, now driving rotation The motor of wing rotation is stopped, and will not consume battery power, make a return voyage consumption of the battery power except retaining multi-rotor unmanned aerial vehicle Outside, remaining can all supply airborne equipment work, therefore can greatly extend time of the airborne equipment in " aerial " work, and And under adsorbed state, the posture of multi-rotor unmanned aerial vehicle and position are all highly stable, without control in addition, influenceed by wind-force It is very small.
Brief description of the drawings
Fig. 1 is the schematic front view of multi-rotor unmanned aerial vehicle one embodiment of the present invention.
Fig. 2 is the left view schematic diagram of Fig. 1 embodiment multi-rotor unmanned aerial vehicles.
Fig. 3 is the schematic perspective view of Fig. 1 embodiment multi-rotor unmanned aerial vehicles.
Fig. 4, Fig. 5 are the uses that Fig. 1 embodiments multi-rotor unmanned aerial vehicle adsorbs two different visual angles when on cladding glass View.
Fig. 6 is that Fig. 1 embodiment multi-rotor unmanned aerial vehicles pull down the schematic perspective view after hanger.
Fig. 7, Fig. 8 are the schematic perspective views of two different visual angles of second embodiment of multi-rotor unmanned aerial vehicle of the present invention.
In figure:1. fuselage, 2. horns, 3. motors, 4. rotors, 5. foot stools, 6. video cameras, 7. connectors, 8. hangers, 8A. Support, 9. suckers, 10. drawstrings, 11. cladding glass, 12. rotor protective frames put video camera on 13..
Embodiment
Below in conjunction with the accompanying drawings, by embodiment, the invention will be further described.
Reference picture 1, Fig. 2, Fig. 3, multi-rotor unmanned aerial vehicle of the present invention mainly include fuselage in terms of mechanical realization(1), horn (2), motor(3), rotor(4), foot stool(5).Horn(2)One end connection fuselage(1), motor(3)Installed in horn(2)On, Rotor(4)Installed in motor(3)Rotating shaft on, foot stool(5)It is connected to fuselage(1)Below, in fuselage(1)Below typically also set It is equipped with head and video camera(6)Or other working equipments, part, fuselage(1)In be also equipped with battery and fly control unit.This Outside, in fuselage(1)On be additionally provided with horizontal hanger(8), the hanger(8)Pass through connector(7)It is connected to fuselage(1)On, and be It is flexibly connected(Hanger can be on connector axis of rotation);Hanger(8)Outer end stretch out each rotor(4)Rotating range Outside line(In order on sucker suction to glass), in hanger(8)Outer end be provided with sucker(9)And support(8A), and support (8A)Positioned at sucker(9)Lower section.Sucker(9)Use be for adsorbing cladding glass or window-glass in high building, from And multi-rotor unmanned aerial vehicle hanging is aloft worked;Support(8A)In sucker(9)Play a part of fulcrum during in adsorbed state. In order that sucker(9)When absorption is on glass, hanger(8)More stably hang and be located at sucker on multi-rotor unmanned aerial vehicle, hanger (9)The support of lower section(8A)It is commonly made to in-line or arc.For the ease of sucker(9)Spin off, inhaling from adsorbed state The lower edge of disk is typically provided drawstring(10), when the multi-rotor unmanned aerial vehicle in hanging state takes off rise, the drawstring (10)Sucker will be pulled open(9), so that sucker(9)Depart from adsorbed state.
Reference picture 4, Fig. 5, multi-rotor unmanned aerial vehicle of the present invention when in use, are adsorbed pinnacled curtain wall glass if desired Glass(11)Upper work(Such as monitor, shoot, await orders), then just first control its flight to arrive cladding glass(11)Place, and make hanger (8)The sucker of outer end(9)Touch cladding glass(11), such sucker(9)Just can tightly it adsorb in cladding glass(11)On. There is sucker(9)Absorption and support(8A)Support, multi-rotor unmanned aerial vehicle just can be stably hung in cladding glass(11) It is upper, its video camera carried(6)Just can be for a long time aloft downwards or to indoor monitoring, shooting.Multi-rotor unmanned aerial vehicle is removed Can by sucker suction on cladding glass it is outer, can also adsorb in the same way in window-glass, outdoor air-conditioner On.
Reference picture 6, can be first by multi-rotor unmanned aerial vehicle when multi-rotor unmanned aerial vehicle absorption aloft need not work Hanger(And connector)Disassemble.Hanger has been played in dismounting(And connector)Multi-rotor unmanned aerial vehicle with revolving existing same type more Wing unmanned plane is compared, and is substantially not much different, and can be used as existing same type multi-rotor unmanned aerial vehicle.
In reference picture 7, Fig. 8, the present embodiment, the hanger in multi-rotor unmanned aerial vehicle(8)It is connected directly between fuselage(1)On, separately External rotor(4)Periphery be additionally provided with rotor protective frame(12), for preventing multi-rotor unmanned aerial vehicle from use, putting at a high speed The rotor put is encountered foreign object and damaged.In addition, above fuselage, being additionally provided with and putting video camera(13), so as in many rotations of control When wing unmanned plane is adsorbed, for observing adsorbate(Cladding glass or window-glass)Orientation and distance.
Sucker in multi-rotor unmanned aerial vehicle of the present invention(9)Can be provided with multiple, to increase the reliable of absorption affinity and absorption Property.
Hanger in multi-rotor unmanned aerial vehicle of the present invention(8)It is general using carbon fiber, glass fibre, aluminium alloy equal strength it is high, Lightweight material makes, and its main body generally uses hollow-core construction.Due to lighter in weight, thus will not to many rotors without Man-machine landing and flight brings adverse effect, and the thus consumption of increased battery electric quantity can also ignore.
Fuselage in multi-rotor unmanned aerial vehicle of the present invention(1)And horn(2)Integral structure can also be used(This structure Referred to as frame).
Horn in multi-rotor unmanned aerial vehicle of the present invention(2)It can be fixed or telescopic horn, can store Horn, rotatable horn etc..
Multi-rotor unmanned aerial vehicle of the present invention can work as existing multi-rotor unmanned aerial vehicle, again can be when required by extension Sucker on frame is adsorbed on pinnacled cladding glass or window-glass.When being in adsorbed state due to multi-rotor unmanned aerial vehicle, Lift is provided without battery power so that the working equipment entrained by it(Such as video camera)Or part(For example for detecting sky The gas sensor of gas pollution)Available power greatly increase, " aerial " continuously work several hours even more than 24 hours Will be no longer difficult, therefore the use space of multi-rotor unmanned aerial vehicle will greatly be extended.For example, municipal administration can by many rotors nobody Machine is adsorbed on the window-glass in overlooking house, is monitored that the random pendulum on street is disorderly sold by Airborne camera, disorderly is stopped leaving about, throws out without care Rubbish, the behavior such as spit everywhere, if clashing, can also can not only be recorded down from the picture of on-site law-enforcing is taken in the air in addition Video evidence, can also prevent other people from grabbing apparatus for making a video recording and destroying video evidence very well;When reporter interviews at the scene, it can allow and revolve more Wing unmanned plane is adsorbed and imaged on pinnacled window-glass, and the picture taken from eminence can more attract spectators to watch, if in addition Hit reporter, grab the event of apparatus for making a video recording, the multi-rotor unmanned aerial vehicle of eminence can also take video evidence;Running into burst During event(Such as street rally, demonstration, traffic accident, large-scale activity), the police can adsorb multi rack multi-rotor unmanned aerial vehicle On the cladding glass and window-glass of high building, field conditions are carried out to monitor in real time, recorded a video;Car owner will be many after car has been stopped Rotor wing unmanned aerial vehicle is adsorbed on the window-glass near car, it is possible to pass through the monitoring device pair carried in multi-rotor unmanned aerial vehicle Car monitor and image in real time, if car is stolen, is hit, scraped, and car owner can just receive alert notice, and monitoring in time Video recording can also provide clue to solve the case and evidence;On oneself window-glass, multi-rotor unmanned aerial vehicle can also be adsorbed and come to garden (Or cell)It is monitored, if occurring, injured in garden, the foster dog of child is carried off away by force by people, thief enters the things such as room theft Therefore, monitoring video provides for clue to solve the case and evidence;When multi-rotor unmanned aerial vehicle is used for signal relaying, it can be adsorbed in high building Cladding glass on, due to not needing rotor wing rotation to provide lift, therefore it aloft works(Relaying)Time than always The multi-rotor unmanned aerial vehicle hovered or spiraled in the air is much longer;Come into vogue currently with unmanned plane to enter performing network living broadcast Come, just solve existing multi-rotor unmanned aerial vehicle airborne period using multi-rotor unmanned aerial vehicle of the present invention short(Generally only 10~30 points Clock)Deficiency, can allow multi-rotor unmanned aerial vehicle absorption on window-glass carry out for a long time(Such as several hours, or even one day More than)It is live.
Someone's residence, which is substantially all, has window-glass, and on the high building in city, cladding glass almost everywhere may be used See, that is to say, that be substantially all to have and be adapted to the place that multi-rotor unmanned aerial vehicle of the present invention is adsorbed, thus many rotors of the invention nobody The application places of machine are extremely wide.

Claims (6)

1. a kind of multi-rotor unmanned aerial vehicle, including fuselage, horn, motor, rotor, foot stool, one end connection fuselage of horn, motor peace On horn, rotor is arranged in the rotating shaft of motor, and foot stool is connected to below fuselage, it is characterized in that:It is additionally provided with fuselage Horizontal hanger, the hanger is stretched out outside each rotor wing rotation scope line, and sucker and support, and support are provided with the outer end of hanger Positioned at the lower section of sucker.
2. multi-rotor unmanned aerial vehicle according to claim 1, it is characterized in that:Hanger is connected on fuselage by connector, and To be flexibly connected.
3. multi-rotor unmanned aerial vehicle according to claim 1, it is characterized in that:Drawstring is provided with the lower edge of sucker.
4. multi-rotor unmanned aerial vehicle according to claim 1, it is characterized in that:Hanger main body is hollow-core construction.
5. multi-rotor unmanned aerial vehicle according to claim 1, it is characterized in that:Support on hanger is in-line or arc.
6. multi-rotor unmanned aerial vehicle according to claim 1, it is characterized in that:Video camera is put on being additionally provided with fuselage.
CN201710185144.2A 2017-03-25 2017-03-25 A kind of multi-rotor unmanned aerial vehicle Withdrawn CN107150796A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710185144.2A CN107150796A (en) 2017-03-25 2017-03-25 A kind of multi-rotor unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710185144.2A CN107150796A (en) 2017-03-25 2017-03-25 A kind of multi-rotor unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN107150796A true CN107150796A (en) 2017-09-12

Family

ID=59792519

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710185144.2A Withdrawn CN107150796A (en) 2017-03-25 2017-03-25 A kind of multi-rotor unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN107150796A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107618671A (en) * 2017-11-02 2018-01-23 北京嘉寓门窗幕墙股份有限公司 A kind of aerial gluing robot of curtain wall operation maintenance and its method
CN107745806A (en) * 2017-09-25 2018-03-02 南京律智诚专利技术开发有限公司 A kind of assembly type shipping unmanned plane

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107745806A (en) * 2017-09-25 2018-03-02 南京律智诚专利技术开发有限公司 A kind of assembly type shipping unmanned plane
CN107618671A (en) * 2017-11-02 2018-01-23 北京嘉寓门窗幕墙股份有限公司 A kind of aerial gluing robot of curtain wall operation maintenance and its method

Similar Documents

Publication Publication Date Title
CN107117310A (en) A kind of multi-rotor unmanned aerial vehicle
CN105836114A (en) A multi-rotor unmanned aerial vehicle
CN108622385A (en) A kind of multi-rotor unmanned aerial vehicle
CN106956771A (en) A kind of multi-rotor unmanned aerial vehicle
CN106965924A (en) A kind of multi-rotor unmanned aerial vehicle
CN106976557A (en) A kind of multi-rotor unmanned aerial vehicle
CN107150796A (en) A kind of multi-rotor unmanned aerial vehicle
CN107416194A (en) A kind of multi-rotor unmanned aerial vehicle
CN107117309A (en) A kind of multi-rotor unmanned aerial vehicle
CN105799921A (en) Multi-rotor unmanned aerial vehicle
CN105857606A (en) Multi-rotor unmanned aerial vehicle
CN105799922A (en) Multi-rotor unmanned aerial vehicle
CN107054635A (en) A kind of multi-rotor unmanned aerial vehicle
CN105775115A (en) Multi-rotor wing unmanned aerial vehicle
CN107150797A (en) A kind of multi-rotor unmanned aerial vehicle
CN107150800A (en) A kind of multi-rotor unmanned aerial vehicle
CN205707315U (en) A kind of many rotor wing unmanned aerial vehicles
CN105775116A (en) Multi-rotor wing unmanned aerial vehicle
CN106976553A (en) A kind of multi-rotor unmanned aerial vehicle
CN106965925A (en) A kind of multi-rotor unmanned aerial vehicle
CN105857607A (en) Multi-rotor unmanned aerial vehicle
CN106976556A (en) A kind of multi-rotor unmanned aerial vehicle
CN106976555A (en) A kind of multi-rotor unmanned aerial vehicle
CN108327904A (en) A kind of multi-rotor unmanned aerial vehicle
CN105799944A (en) Hanging frame for multi-rotor-wing unmanned aerial vehicle

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
WW01 Invention patent application withdrawn after publication

Application publication date: 20170912

WW01 Invention patent application withdrawn after publication