CN105857607A - Multi-rotor unmanned aerial vehicle - Google Patents
Multi-rotor unmanned aerial vehicle Download PDFInfo
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- CN105857607A CN105857607A CN201610223212.5A CN201610223212A CN105857607A CN 105857607 A CN105857607 A CN 105857607A CN 201610223212 A CN201610223212 A CN 201610223212A CN 105857607 A CN105857607 A CN 105857607A
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- aerial vehicles
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- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 43
- 229910052742 iron Inorganic materials 0.000 claims abstract description 22
- 238000010276 construction Methods 0.000 claims description 4
- 238000012544 monitoring process Methods 0.000 abstract description 5
- 230000007613 environmental effect Effects 0.000 abstract description 2
- 238000000034 method Methods 0.000 abstract 2
- 238000011835 investigation Methods 0.000 abstract 1
- 238000007726 management method Methods 0.000 abstract 1
- 230000002035 prolonged effect Effects 0.000 abstract 1
- 230000000630 rising effect Effects 0.000 abstract 1
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- 241001465754 Metazoa Species 0.000 description 4
- 239000002917 insecticide Substances 0.000 description 4
- 230000002411 adverse Effects 0.000 description 3
- 150000002505 iron Chemical class 0.000 description 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 2
- 230000007812 deficiency Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000010865 sewage Substances 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 241000282472 Canis lupus familiaris Species 0.000 description 1
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 244000000626 Daucus carota Species 0.000 description 1
- 206010038743 Restlessness Diseases 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 241000282898 Sus scrofa Species 0.000 description 1
- 238000003915 air pollution Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 235000005770 birds nest Nutrition 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000003344 environmental pollutant Substances 0.000 description 1
- 239000011152 fibreglass Substances 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 229910001172 neodymium magnet Inorganic materials 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 231100000719 pollutant Toxicity 0.000 description 1
- 229910052761 rare earth metal Inorganic materials 0.000 description 1
- 150000002910 rare earth metals Chemical class 0.000 description 1
- 238000001179 sorption measurement Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 230000032258 transport Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 235000005765 wild carrot Nutrition 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
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- 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
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Electric Cable Installation (AREA)
Abstract
The invention discloses a multi-rotor unmanned aerial vehicle and belongs to the technical field of unmanned aerial vehicles. The multi-rotor unmanned aerial vehicle comprises a vehicle body, vehicle arms, motors, rotors, foot supports and the like and has the characteristics that the vehicle body is further provided with a hanging rack connector and a hanging rack; the hanging rack connector is provided with an iron sheet; a magnet is arranged at the lower end of the hanging rack; the hanging rack is attracted to the hanging rack connector through magnetic force; the upper portion of the hanging rack is provided with a hook or a hanging rod. The multi-rotor unmanned aerial vehicle can be hung on an object in a high position through the hook or the hanging rod on the multi-rotor unmanned aerial vehicle in the using process. No electric energy is needed for providing lift force for the multi-rotor unmanned aerial vehicle in the hung state, and most battery electric energy can be all supplied to equipment carried by the multi-rotor unmanned aerial vehicle to be used so that working time of the working equipment in one rising and landing process can be prolonged greatly. The multi-rotor unmanned aerial vehicle can be widely applied to the fields such as air fixed-point surveillance, monitoring, shooting, environmental protection monitoring, field scientific investigation, case reconnaissance, urban management, courtyard security, vehicle antitheft working, express delivery and the like.
Description
Technical field
The present invention relates to unmanned vehicle technical field, be specifically related to a kind of many rotor wing unmanned aerial vehicles.
Background technology
Many rotor wing unmanned aerial vehicles generally have 3～9 rotors, especially most commonly seen with 4 rotors.The functions such as many rotor wing unmanned aerial vehicles possess VTOL, hovering, low-speed operations, inverted flight, side fly, 360 degree of rotations, take photo by plane (take pictures in the air, image) at near-earth, monitor, scout, radio signal relaying, high-voltage line, bridge, dam and road surface inspection, search and rescue aid, transports the aspects such as express delivery and is applied.Existing many rotor wing unmanned aerial vehicles mainly have following deficiency: owing to the battery loaded on dependence machine when hovering is aerial is to provide electric energy, therefore cruising time is short, great majority rely on many rotor wing unmanned aerial vehicles of battery powers work once can only follow-on mission 10～about 30 minutes, the typically only 10～30 minutes time that the most rotor wing unmanned aerial vehicles aloft work, can not meet far away people use many rotor wing unmanned aerial vehicles to carry out long-time air surveillance, shoot, propaganda directed to communicate, transmit, signal relay, deploy troops on garrison duty, the actual demand such as await orders.It addition, existing many rotor wing unmanned aerial vehicles aloft hover when carrying out fixed point supervision, shooting, its attitude is affected relatively big by wind-force and position sensor signal, and stability is difficult to ensure；Many rotor wing unmanned aerial vehicles aloft hover work time, flight control system needs to control its attitude in real time and adjust, both the electric energy of battery had been consumed, there is also no small potential safety hazard, just in case there is fault mechanical, automatically controlled or misoperation, just easily cause air crash accident (aircraft bombing), even fall down from the air and injure people by a crashing object；When many rotor wing unmanned aerial vehicles are used for transporting express delivery, after flight to destination, if picking people does not also arrive, many rotor wing unmanned aerial vehicles just can only drop to ground (otherwise battery electric quantity will quickly exhaust), and cannot rest on aerial wait；Many rotor wing unmanned aerial vehicles are when field observation research animal, birds, insecticide, animal, birds, insecticide can be caused scaring and interference by the sound and the air-flow of generation that its rotor sends, and once take off and be typically only capable to stay aloft 10～30 minutes, use requirement can not be met at all.
Summary of the invention
It is an object of the invention to provide one and can rest on many rotor wing unmanned aerial vehicles that " in the air " works or await orders for a long time, to solve the deficiency that existing many rotor wing unmanned aerial vehicles airborne period is short, cannot the most aloft work.
The technical scheme is that: a kind of many rotor wing unmanned aerial vehicles, including fuselage, horn (propeller bracket), motor, rotor (propeller), foot rest (leg) etc.；Drive the motor of rotor wing rotation and the rotor of correspondence to be typically respectively arranged with 3～9, and be installed on fuselage surrounding by horn；Foot rest is arranged on below fuselage, is also equipped with the battery for powering to consuming parts and flies to control unit in fuselage；Additionally, be additionally provided with hanger interface and hanger (erecting by overhang) on fuselage, the hanger interface on fuselage is provided with iron plate or magnet；Being shaped as of hanger is J-shaped, question mark shaped or 7 fonts, and the lower end of hanger is provided with magnet or iron plate, and the upper part of hanger is provided with hook or peg；Hanger is adsorbed onto on the hanger interface of fuselage by the suction between magnet and iron plate, or magnet and magnet, and this suction is more than the weight of many rotor wing unmanned aerial vehicles complete machine.This many rotor wing unmanned aerial vehicles are in use, can be hung on pinnacled object by the hook above hanger or peg, such as hang skyborne electric wire, branch, steel tower, electric pole, traffic mark board, billboard, the balcony of high building block on bar, and the equipment (such as camera, video camera, loudspeaker, signal relay module, illuminating lamp, gas sensor etc.) that the most rotor wing unmanned aerial vehicles carry just can work the most aloft or await orders.Hang aloft for the ease of manipulating many rotor wing unmanned aerial vehicles, be additionally provided with a camera lens in general above at its fuselage and put video camera (photographic head) on body upper.It addition, in order to alleviate weight, this hanger typically uses hollow-core construction.
The invention has the beneficial effects as follows, can hang due to many rotor wing unmanned aerial vehicles and work aloft, and when being in hanging state, lift is provided without rotor, the motor now driving rotor wing rotation quits work, battery power will not be consumed, battery power makes a return voyage in addition to consumption except the many rotor wing unmanned aerial vehicles of reservation, remaining can all supply airborne equipment work, therefore the time that airborne equipment works can greatly be extended in " in the air ", and under hanging state, attitude and the position of many rotor wing unmanned aerial vehicles are the most highly stable, without additionally controlling, affected the least by wind-force.Additionally, if many rotor wing unmanned aerial vehicles in use need not hang aloft, can first be taken off from fuselage by hanger before use, the many rotor wing unmanned aerial vehicles of such present invention just can use as common many rotor wing unmanned aerial vehicles, and its performance and purposes are not resulted in adverse effect.
Accompanying drawing explanation
Fig. 1 is the schematic front view of the present invention one embodiment of many rotor wing unmanned aerial vehicles.
Fig. 2 is the schematic perspective view of the many rotor wing unmanned aerial vehicles of Fig. 1 embodiment.
Fig. 3 is Fig. 1 embodiment many rotor wing unmanned aerial vehicles use view when hanging aloft.
Fig. 4 is the schematic perspective view after the many rotor wing unmanned aerial vehicles of Fig. 1 embodiment take off hanger.
Fig. 5, Fig. 6 are the generalized section of two kinds of hangers used in the many rotor wing unmanned aerial vehicles of the present invention respectively.
Fig. 7 is the schematic perspective view of the present invention second embodiment of many rotor wing unmanned aerial vehicles.
Fig. 8, Fig. 9, Figure 10 are Fig. 7 embodiment many rotor wing unmanned aerial vehicles use view when hanging aloft.
Figure 11 is the schematic perspective view of the 3rd embodiment of the many rotor wing unmanned aerial vehicles of the present invention.
Figure 12 is Figure 11 embodiment many rotor wing unmanned aerial vehicles use view when hanging aloft.
Figure 13, Figure 14 are the schematic perspective view of the 4th, the 5th embodiment of the many rotor wing unmanned aerial vehicles of the present invention respectively.
In figure: 1. hanger, 1A. hook, 1B. magnet, 1C. hook tip, 1D. peg, 2. fuselage, 2A.2B. hanger interface, 3. horn, 4. motor, 5. rotor, 6. foot rest, 7. video camera, 8. guard ring, 9. on put video camera, 10. electric wire, 11. plate objects.
Detailed description of the invention
Below in conjunction with the accompanying drawings, by embodiment, the invention will be further described.
nullWith reference to Fig. 1、Fig. 2、Fig. 3，The many rotor wing unmanned aerial vehicles of the present invention include fuselage (2) in terms of mechanical realization、Horn (3)、Motor (4)、Rotor (5)、Foot rest (6)，Horn (3) is connected to fuselage (2) upper (can also use the structure of fuselage horn integration)，The outer end of horn (3) is provided with motor (4)，Rotor (5) is connected to (or on variator) in the rotating shaft of motor (4)，Foot rest (6) is arranged at fuselage (2) below，The Cloud Terrace and video camera (7) or other working equipment it is further typically provided with below fuselage、Parts，In addition，Fuselage (2) is also equipped with battery and flies to control unit，It is characterized in that: on fuselage (2), be additionally provided with hanger interface and hanger (1)，Hanger interface on fuselage is provided with iron plate or magnet，Being shaped as of hanger (1) is J-shaped，The lower end of hanger (1) is provided with magnet or iron plate，The upper part of hanger (1) is provided with hook (1A)，Hanger (1) passes through magnet and iron plate，Or the suction between magnet and magnet is adsorbed onto on the hanger interface of fuselage (2).
With reference to Fig. 3, the many rotor wing unmanned aerial vehicles of the present invention are in use, if desired it long-time (the most several hours even one day) aloft work or awaits orders, the most just can control its eminence underbelly (the most aerial electric wire flying to be suitable for hanging, branch, ferrum tower, electric pole, traffic mark board, billboard, the balcony of high building blocks the lower section of the positions such as bar), then hung on pinnacled object by the hook (1A) on hanger (1), such as hang skyborne electric wire (10), cable, branch, ferrum tower, traffic mark board cross bar, billboard, high building balcony, in roof outer rim.After hanging is good, the motor (4) driving rotor (5) to rotate just can quit work, and the most rotor wing unmanned aerial vehicles just can be hung for a long time and work aloft or await orders, and its video camera carried (7) just can monitor the most aloft, image.
With reference to Fig. 4, on many rotor wing unmanned aerial vehicles fuselage (2), being provided with hanger interface (2A), this hanger interface (2A) is that (this iron plate can directly adhere to or be screwed in above fuselage one piece of iron plate sticking on fuselage, it is possible to adheres to or is positioned in the recess preset above fuselage；This iron plate also includes that other can be by the material of magnet absorption, such as nickel sheet), this iron plate is for the magnet absorption with hanger lower end together.In general, if the hanger interface (2A) on fuselage (2) is iron plate, then the lower end of hanger then sets magnet；Whereas if the hanger interface (2A) on fuselage (2) is magnet, then hanger lower end then sets iron plate；Or hanger interface (2A) and hanger lower end all set magnet, want the most between the two mutually to adsorb.Utilizing magnetic force to be attached together between hanger on the many rotor wing unmanned aerial vehicles of the present invention and fuselage, therefore hanger can be taken off at any time from fuselage.After hanger is taken off from fuselage, the weight of many rotor wing unmanned aerial vehicles can be alleviated and be easy to manipulation.Many rotor wing unmanned aerial vehicles of hanger are taken off with existing compared with type unmanned plane, in overall appearance, occupation mode and functionally, the most the same (as shown in Figure 4), that is, the many rotor wing unmanned aerial vehicles of the present invention are after taking off hanger, can use as existing same type unmanned plane, its function, performance will not be brought adverse effect.
With reference to Fig. 5, hanger (1) used by the many rotor wing unmanned aerial vehicles of the present invention is J-shaped, hanger is provided with hook (1A), the lower end of hanger is embedded with magnet (1B), this magnet (1B) mutually can adsorb with the iron plate of fuselage upper hanger interface or magnet, so can be achieved with the connection of hanger (1) and fuselage.
With reference to Fig. 6, hanger (1) used by the many rotor wing unmanned aerial vehicles of the present invention is provided with hook (1A), the top of hook (1A) is hook tip (1C), the lower end of hanger (1) is bonded with magnet (1B) (this magnet also can be secured to hanger lower end by screw), this magnet (1B) mutually can adsorb with the iron plate of fuselage upper hanger interface or magnet, so can be achieved with the connection of hanger (1) and fuselage.
With reference to Fig. 7, hanger interface (2B) in the present invention many rotor wing unmanned aerial vehicles fuselage (2) is cylindric, it is provided with iron plate (or magnet) at bottom of cylinder, after hanger (1) lower end is inserted in this cylinder, the magnet (or iron plate) of hanger (1) lower end is just adsorbed on the iron plate (or magnet) of bottom of cylinder, it is achieved hanger (1) and the connection of fuselage (2).In addition; be additionally provided with guard ring (8) in rotor (5) periphery, this guard ring (8) plays the effect of protection rotor (5), when many rotor wing unmanned aerial vehicles can be avoided awing to meet other object; rotor (5) is damaged, it is also possible to avoid the rotor (5) of high speed rotating to hurt sb.'s feelings.Hang aloft for the ease of manipulating many rotor wing unmanned aerial vehicles, be additionally provided with a camera lens in general above at its fuselage (2) and put video camera (9) on body upper.
With reference to Fig. 8, Fig. 9, the personnel of manipulation (unmanned plane driver) control many rotor wing unmanned aerial vehicles hang aloft on object time, the image transmission system of many rotor wing unmanned aerial vehicles can pass the image putting the body upper that video camera (9) photographs in real time back, so manipulation personnel just can see the object above many rotor wing unmanned aerial vehicles in real time clearly, the such as electric wire (10) of top, in order to utilize the hook (1A) on hanger (1) to be hung on eminence object by many rotor wing unmanned aerial vehicles.After many rotor wing unmanned aerial vehicles are hung aloft on object, such as hang skyborne electric wire (10) upper after, its video camera carried (7) just can monitor the most for a long time or shoot.
With reference to Figure 10, the many rotor wing unmanned aerial vehicles of the present invention are in use, in addition to can hanging pinnacled bar-shaped object (such as electric wire, horizontal branch etc.) and be upper, it is possible to hang on pinnacled plate object (11), such as, hang in the outer rim of tall building roof balcony, the outer rim etc. of building balcony.When the present invention many rotor wing unmanned aerial vehicles pinnacled plate object of hanging (11) are upper, the hook tip (1C) on hook (1A) top just stings on plate object (11), so can ensure that stablizing of many rotor wing unmanned aerial vehicles position, even if being also not easy by wind to slide and drop.After the present invention many rotor wing unmanned aerial vehicles pinnacled plate object of hanging (11) are upper, its video camera carried (7) just can monitor the most for a long time or shoot.
With reference to Figure 11, Figure 12, the hook (1A) in the present invention many rotor wing unmanned aerial vehicles hanger (1) be double hooks, when the most rotor wing unmanned aerial vehicles are hung aloft on object, such as hang on skyborne electric wire, or time on the plate object (11) of eminence, be just not easy to rotate, attitude stability is more preferable.Additionally; guard ring (8) is circle shape; rotor (5) can be protected to avoid meeting other object during many rotor wing unmanned aerial vehicles use and damage, it is possible to so that many rotor wing unmanned aerial vehicles are hanging and departing from during from hanging object, rotor (5) avoids encountering hanging object.After the many rotor wing unmanned aerial vehicles of the present invention are hung on pinnacled plate object (11) or other object, its video camera carried (7) just can monitor the most for a long time or shoot.
After the hanging of the present invention many rotor wing unmanned aerial vehicles completes task aloft, if to depart from return ground from the eminence object (electric wire as aerial) hung, as long as restarting rotor motor, allow many rotor wing unmanned aerial vehicles slightly raise and deviate from hanging object side and fly, hanging object can be departed from, the most just can normally return to ground.
With reference to Figure 13, the present invention many rotor wing unmanned aerial vehicles fuselage (2) being provided with the hanger (1) of question mark shaped, and this hanger (1) is provided with hook (1A), many rotor wing unmanned aerial vehicles can pass through the hook (1A) on hanger (1) and hang aloft on object.
With reference to Figure 14, the present invention many rotor wing unmanned aerial vehicles fuselage (2) being provided with the hanger (1) of 7 fonts, this hanger (1) is provided with peg (1D), and many rotor wing unmanned aerial vehicles can pass through the peg (1D) on hanger (1) and hang aloft on object.Such as, controlling many rotor wing unmanned aerial vehicles and make this peg (1D) be inserted under outdoor air-conditioner in space, after closing down rotor motor, many rotor wing unmanned aerial vehicles just can be hung aloft.
Hanger (1) on the many rotor wing unmanned aerial vehicles of the present invention generally J-shaped, question mark shaped or 7 fonts, simple in construction, low cost, and weight is also light, and (general employing fiberglass or carbon fiber equal strength material high, lightweight make, and generally use hollow-core construction), the landing of many rotor wing unmanned aerial vehicles will not be brought adverse effect, the consumption of the battery electric quantity thus increased can also be ignored；And be connected by magnetic-adsorption between hanger (1) with fuselage (2), either hanger is installed on fuselage, or from fuselage, take off hanger, the most very convenient.
The many rotor wing unmanned aerial vehicles of the present invention can work (after hanger is taken off above fuselage, it appears that with existing same type unmanned plane does not has much differences) as existing many rotor wing unmanned aerial vehicles, can hang aloft on object when required by hanger again.When being in hanging state due to many rotor wing unmanned aerial vehicles, lift is provided without electric energy, the available power making working equipment (such as video camera) or parts (such as detecting the gas sensor of air pollution) is greatly increased, in " in the air ", work continuously will become usual thing in 24 hours, and therefore the use space of many rotor wing unmanned aerial vehicles will greatly be extended.Such as, municipal administration can use on many rotor wing unmanned aerial vehicles hanging electric wire, electric pole, billboard, trees or high building in overhead, street, by Airborne camera monitor the unrest pendulum on road surface disorderly sell, disorderly stop to leave about, the behavior such as littering, additionally can also be from the picture taking on-site law-enforcing in the air, if clashing, lower video evidence can not only be recorded, also can prevent other people from grabbing apparatus for making a video recording very well and destroy video recording；When running into accident (such as street rally, demonstration, vehicle accident, large-scale activity etc.), situation can be monitored on the hanging of many rotor wing unmanned aerial vehicles building, light pole or aerial electric wire at incident, record a video by the police in real time；During case is scouted, the hanging of many rotor wing unmanned aerial vehicles can be monitored by personnel in charge of the case aloft, not only monitors that angle is better than on ground, and convenient, flexible, quiet；When reporter interviews at the scene, the hanging of many rotor wing unmanned aerial vehicles can be allowed to image aloft, so if it occur that hit reporter, the event of plunder apparatus for making a video recording, hang pinnacled many rotor wing unmanned aerial vehicles and just can take evidence；Law enforcement for environmental protection personnel can allow many rotor wing unmanned aerial vehicles hang the top (such as hang supervision sewage discharge above sewage draining exit, or hanging is monitored gas on chimney in real time and discharged) of discharge of pollutant sources position, carries out supervision and the evidence obtaining of 24 hours；When scientific research personnel carries out zooscopy in the wild, many rotor wing unmanned aerial vehicles can be allowed to hang on branch, such as hang by Bird's Nest, by honeycomb, above wild boar nest etc., thus birds, insecticide, animal etc. can be carried out the long-time close-ups of (such as 24 hours), shooting, and the many rotor wing unmanned aerial vehicles being in hanging state will not send the sound and unusual fluctuation, interfere thus without on the birds of observational study, insecticide, animal and affect；When the many rotor wing unmanned aerial vehicles of the present invention are used for transporting express delivery, after flight to destination, if picking people does not also show up and connects goods, many rotor wing unmanned aerial vehicles can first be hung aloft (such as roof outer rim, aerial electric wire, branch, cross rod of traffic sign etc.) " STOP " (stopping rotor wing rotation) and wait, the most both can avoid that express delivery is stolen robs, it is possible to avoid unmanned plane to be parked in ground and destroyed or snatched away by people；Car owner is after having stopped car, by eminence near many for present invention rotor wing unmanned aerial vehicles hanging car, just can be equipped by the monitoring carried on many rotor wing unmanned aerial vehicles and car be monitored in real time and images, if car is stolen, hit, scraped, car owner just can receive alert notice in time, and monitoring video is also provided that clue to solve the case and evidence；On the roof outer rim of dwelling garden, aerial electric wire or branch, the present invention many rotor wing unmanned aerial vehicles can also be hung garden is monitored, if occurring, child Canis familiaris L. injured when playing in garden, that support is carried off away by force by people, thief enters the accidents such as room theft, and monitoring video provides for clue to solve the case and evidence；When many for present invention rotor wing unmanned aerial vehicles are used for signal relay, can be hung on pinnacled object, such as on communication base station tower, water tower, chimney, high building, treetop, aerial power circuit, thering is provided lift owing to need not rotor wing rotation, therefore the time of its work aloft (relaying) is more much longer than existing many rotor wing unmanned aerial vehicles.
Fuselage and horn in the many rotor wing unmanned aerial vehicles of the present invention can also use integral structure (such structure is also referred to as frame or support), and such structure is it will be also be appreciated that be equal to above-mentioned fuselage (2) and horn (3).
Magnet used by the present invention many rotor wing unmanned aerial vehicles hanger and hanger interface, preferably with the strong rare-earth permanent magnet of unit magnetic force, such as Nd-Fe-B permanent magnet, so can alleviate complete machine weight.
Interest field of the present invention is applicable not only to many rotor wing unmanned aerial vehicles, can equally be well applied to the model plane rotor craft of band remote control.
Claims (8)
1. rotor wing unmanned aerial vehicle more than a kind, including fuselage (2), horn (3), motor (4), rotor (5), foot rest (6), it is characterized in that: be arranged above with hanger interface (2A, 2B) and hanger (1) at fuselage (2), hanger interface (2A, 2B) is provided with iron plate or magnet, the lower end of hanger (1) is provided with magnet (1B) or iron plate, and the upper part of hanger (1) is provided with hook (1A) or peg (1D)；Hanger (1) is adsorbed onto on the hanger interface (2A, 2B) of fuselage (2) by the suction between magnet and iron plate, or magnet and magnet.
Many rotor wing unmanned aerial vehicles the most according to claim 1, is characterized in that: the hanger interface (2A) on many rotor wing unmanned aerial vehicles fuselage (2) is iron plate.
Many rotor wing unmanned aerial vehicles the most according to claim 1, is characterized in that: the hanger interface (2B) on many rotor wing unmanned aerial vehicles fuselage (2) is cylindrical shape.
Many rotor wing unmanned aerial vehicles the most according to claim 1, is characterized in that: the top of the upper hook (1A) of hanger (1) is hook tip (1C).
Many rotor wing unmanned aerial vehicles the most according to claim 1, is characterized in that: the hook (1A) on hanger (1) hooks for double.
Many rotor wing unmanned aerial vehicles the most according to claim 1, is characterized in that: the hanger (1) being arranged on many rotor wing unmanned aerial vehicles fuselage is J-shaped, question mark shaped or 7 fonts.
Many rotor wing unmanned aerial vehicles the most according to claim 1, is characterized in that: the hanger (1) being arranged on many rotor wing unmanned aerial vehicles fuselage is hollow-core construction.
Many rotor wing unmanned aerial vehicles the most according to claim 1, is characterized in that: be additionally provided with a camera lens on many rotor wing unmanned aerial vehicles fuselage (2) and put video camera (9) on body upper.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610223212.5A CN105857607A (en) | 2016-04-11 | 2016-04-11 | Multi-rotor unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610223212.5A CN105857607A (en) | 2016-04-11 | 2016-04-11 | Multi-rotor unmanned aerial vehicle |
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| Publication Number | Publication Date |
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| CN105857607A true CN105857607A (en) | 2016-08-17 |
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| CN201610223212.5A Withdrawn CN105857607A (en) | 2016-04-11 | 2016-04-11 | Multi-rotor unmanned aerial vehicle |
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| CN (1) | CN105857607A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106786139A (en) * | 2016-12-08 | 2017-05-31 | 北京国网富达科技发展有限责任公司 | A kind of tele-control system of transmission line of electricity fall coaster |
| CN107783542A (en) * | 2016-08-26 | 2018-03-09 | 深圳光启空间技术有限公司 | The control method and control system of unmanned plane |
| CN111169628A (en) * | 2019-11-22 | 2020-05-19 | 西安理工大学 | Rotor unmanned aerial vehicle ceiling perches mechanism |
| WO2024131617A1 (en) * | 2022-12-19 | 2024-06-27 | 北京天玛智控科技股份有限公司 | Unmanned-aerial-vehicle inspection method |
-
2016
- 2016-04-11 CN CN201610223212.5A patent/CN105857607A/en not_active Withdrawn
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107783542A (en) * | 2016-08-26 | 2018-03-09 | 深圳光启空间技术有限公司 | The control method and control system of unmanned plane |
| CN107783542B (en) * | 2016-08-26 | 2024-05-31 | 云南延奔信息安全技术股份有限公司 | Unmanned aerial vehicle control method and control system |
| CN106786139A (en) * | 2016-12-08 | 2017-05-31 | 北京国网富达科技发展有限责任公司 | A kind of tele-control system of transmission line of electricity fall coaster |
| CN111169628A (en) * | 2019-11-22 | 2020-05-19 | 西安理工大学 | Rotor unmanned aerial vehicle ceiling perches mechanism |
| WO2024131617A1 (en) * | 2022-12-19 | 2024-06-27 | 北京天玛智控科技股份有限公司 | Unmanned-aerial-vehicle inspection method |
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Application publication date: 20160817 |