CN105836113A - A multi-rotor unmanned aerial vehicle - Google Patents
A multi-rotor unmanned aerial vehicle Download PDFInfo
- Publication number
- CN105836113A CN105836113A CN201610220907.8A CN201610220907A CN105836113A CN 105836113 A CN105836113 A CN 105836113A CN 201610220907 A CN201610220907 A CN 201610220907A CN 105836113 A CN105836113 A CN 105836113A
- Authority
- CN
- China
- Prior art keywords
- unmanned aerial
- hanger
- rotor wing
- aerial vehicles
- wing unmanned
- 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- Withdrawn
Links
- 238000010276 construction Methods 0.000 claims description 5
- 238000012544 monitoring process Methods 0.000 abstract description 6
- 230000005611 electricity Effects 0.000 abstract 2
- 238000011835 investigation Methods 0.000 abstract 1
- 238000007726 management method Methods 0.000 abstract 1
- 238000000034 method Methods 0.000 abstract 1
- 230000002265 prevention Effects 0.000 abstract 1
- 230000001681 protective effect Effects 0.000 abstract 1
- 241001465754 Metazoa Species 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 239000002917 insecticide Substances 0.000 description 4
- 230000002411 adverse Effects 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 230000007812 deficiency Effects 0.000 description 2
- 239000012634 fragment 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
- 230000007613 environmental effect Effects 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
- 239000000463 material Substances 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 231100000719 pollutant Toxicity 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/006—Safety devices
-
- 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
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- 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
-
- 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
-
- 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
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Electric Cable Installation (AREA)
Abstract
The invention relates to 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, rotary wings and foot supports. The vehicle body is provided with a hanging support. The hanging support is provided with a hook. The lower part of the hook is provided with protective bars used for protecting the rotary wings. The hanging support is connected to a hanging support connecting port in the vehicle body through a hanging support connecting head at the lower end of the hanging support. During using, the multi-rotor unmanned aerial vehicle can be hung to an object on high through the hook, for example the multi-rotor unmanned aerial vehicle can be hung to electric wires in the air. Electricity is not needed to supply the lift force of the multi-rotor unmanned aerial vehicle in a hung state, and most of electricity of a battery can be supplied to devices carried by the multi-rotor unmanned aerial vehicle, thus greatly prolonging the working time of working devices in a descending and lifting process. The multi-rotor unmanned aerial vehicle can be widely used for fixed-point monitoring in the air, monitoring, camera shooting, environment protection monitoring, field scientific investigation, case reconnaissance, city management, courtyard security and protection, vehicle thievery prevention, express delivery, and other fields.
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 (erecting by overhang) on fuselage, being provided with hook on hanger, the bottom of hanger is additionally provided with the fender rod for protecting rotor, and hanger is connected with the hanger interface on fuselage by the hanger joint of its lower end.This many rotor wing unmanned aerial vehicles are in use, can be hung on pinnacled object by the hook on hanger, 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, the hanger being connected on many rotor wing unmanned aerial vehicles fuselage is the most dismountable, if in use need not hang aloft many rotor wing unmanned aerial vehicles, hanger can be disassembled from fuselage；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 pulled down 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 pull down hanger.
Fig. 5 is the schematic perspective view of the present invention second embodiment of many rotor wing unmanned aerial vehicles.
Fig. 6 is Fig. 5 embodiment many rotor wing unmanned aerial vehicles use view when hanging aloft.
Fig. 7 is the schematic perspective view of the 3rd embodiment of the many rotor wing unmanned aerial vehicles of the present invention.
Fig. 8 is Fig. 7 embodiment many rotor wing unmanned aerial vehicles use view when hanging aloft.
Fig. 9 is the schematic front view of a kind of hanger on the many rotor wing unmanned aerial vehicles of the present invention.
Figure 10, Figure 11 are the schematic perspective view of the other two kinds of hangers on the many rotor wing unmanned aerial vehicles of the present invention respectively.
In figure: 1. hanger, 1A. hook, 1B. fender rod, 1C. hanger joint, 1D. hook tip, 2. fuselage, 2A. hanger interface, 3. horn, 4. motor, 5. rotor, 6. foot rest, 7. video camera, 8. electric wire, 9. plate object.
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，Fuselage (2) is provided with battery and flies to control unit，In addition，Hanger (1) it is additionally provided with on fuselage (2)，This hanger (1) is arranged above with hook (1A)，Bottom is provided with fender rod (1B)，Hanger (1) is connected with the hanger interface on fuselage (2) by hanger joint.
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.During many rotor wing unmanned aerial vehicles are hung on eminence object; and during departing from from the eminence object of hanging; fender rod (1B) on hanger (1) can protect rotor (5), it is to avoid rotor (5) is encountered hanging object (electric wire as aerial) and damaged.
With reference to Fig. 4, the hanger on the many rotor wing unmanned aerial vehicles of the present invention is the most dismountable.On many rotor wing unmanned aerial vehicles fuselage (2), it is provided with hanger interface (2A), for hanger being connected to fuselage (2).The structure of hanger interface (2A), shape match with the hanger joint on hanger used.Such as, hanger joint is bolt shape, and hanger interface (2A) is just provided with the female thread matched；Hanger joint is provided with bayonet socket, and hanger interface (2A) is just provided with the dead bolt or lock screw matched.When using many rotor wing unmanned aerial vehicles, if need not be hung aloft, hanger can be removed from fuselage (2), to alleviate the weight of many rotor wing unmanned aerial vehicles and to be easy to manipulation.Many rotor wing unmanned aerial vehicles (as shown in Figure 4) of hanger are pulled down with existing compared with type unmanned plane, in overall appearance, occupation mode and functionally, the most the same, that is, the many rotor wing unmanned aerial vehicles of the present invention are after pulling down hanger, can use as existing same type unmanned plane, its function, performance will not be brought adverse effect.
With reference to Fig. 5, Fig. 6; fender rod (1B) on hanger (1) used by the many rotor wing unmanned aerial vehicles of the present invention is decussate texture; and it is positioned at the top of rotor (5), can be that rotor (5) provides preferably protection, it is to avoid rotor damages because encountering hanging object (electric wire as aerial).
With reference to Fig. 6, 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 (9), such as outer rim of the outer rim of tall building roof balcony, building balcony etc..After the present invention many rotor wing unmanned aerial vehicles pinnacled plate object of hanging (9) are upper, its video camera carried (7) just can monitor the most for a long time or shoot.
With reference to Fig. 7, Fig. 8, the hook (1A) on hanger (1) used by the many rotor wing unmanned aerial vehicles of the present invention be double hooks, when the most rotor wing unmanned aerial vehicles are hung aloft on object, such as hang on skyborne electric wire (8), or time on the plate object of eminence, be just not easy to rotate, attitude stability is more preferable.After the many rotor wing unmanned aerial vehicles of the present invention are hung on pinnacled electric wire (8) or other object, its video camera carried (7) just can monitor the most for a long time or shoot.
With reference to Fig. 9, hanger (1) used by the many rotor wing unmanned aerial vehicles of the present invention is provided with hook (1A), the bottom of hanger (1) is provided with a fender rod (1B), lower end is hanger joint (1C), this hanger joint (1C) is provided with bayonet socket, after hanger joint (1C) is inserted in the hanger interface above many rotor wing unmanned aerial vehicles fuselage, locked by the dead bolt (or locking bolt, screw, shell fragment) in hanger interface, it is possible to realize the connection of hanger (1) and fuselage.
With reference to Figure 10, 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 (1D), the bottom of hanger (1) is provided with cross fender rod (1B), lower end is hanger joint (1C), this hanger joint (1C) is provided with hole clipping, after hanger joint (1C) is inserted in the hanger interface above many rotor wing unmanned aerial vehicles fuselage, locked by the latch (or locking bolt, screw, shell fragment) in hanger interface, it is possible to realize the connection of hanger (1) and fuselage.The hook tip (1D) on hook (1A) top can be when the many rotor wing unmanned aerial vehicles pinnacled plate object of hanging (9) be upper (as shown in Figure 6), thorn is on plate object (9), 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.
With reference to Figure 11, hook (1A) on hanger (1) used by the many rotor wing unmanned aerial vehicles of the present invention is double hook, the top of hook (1A) is hook tip (1D), the bottom of hanger (1) is provided with shape fender rod (1B), lower end is hanger joint (1C), this hanger joint (1C) is provided with screw thread, is tightened to by hanger joint (1C) above many rotor wing unmanned aerial vehicles fuselage with after in female hanger interface, it is possible to realize the connection of hanger (1) and fuselage.
The hanger joint (1C) of hanger (1) lower end used by the many rotor wing unmanned aerial vehicles of the present invention is in addition to using bayonet socket, hole clipping, helicitic texture and realizing the connection with fuselage (2) upper hanger interface (2A), structure and the mode that can also use other connect, and clamp for example with clip, hook catches on, by the rope mode such as binding.
Hang aloft for the ease of manipulating many rotor wing unmanned aerial vehicles; it is additionally provided with a camera lens in general above at its fuselage (2) and puts video camera (or photographic head) on body upper; 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 photographs on this in real time back, and such manipulation personnel just can see the object above many rotor wing unmanned aerial vehicles and position in real time clearly.
Hanger (1) on the many rotor wing unmanned aerial vehicles of the present invention generally uses hollow-core construction, so can alleviate its weight.
Hanger (1) simple in construction on the many rotor wing unmanned aerial vehicles of the present invention, 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.
The many rotor wing unmanned aerial vehicles of the present invention can work (after hanger is disassembled, 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).
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: on fuselage (2), be additionally provided with hanger (1), this hanger is provided with hook (1A), the bottom of hanger (1) is additionally provided with fender rod (1B), and hanger (1) is connected with the hanger interface (2A) on fuselage (2) by the hanger joint (1C) of its lower end.
Many rotor wing unmanned aerial vehicles the most according to claim 1, is characterized in that: be provided with hanger interface (2A) on many rotor wing unmanned aerial vehicles fuselage (2).
Many rotor wing unmanned aerial vehicles the most according to claim 1, is characterized in that: the fender rod (1B) of hanger (1) bottom is decussate texture.
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 (1D).
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 hollow-core construction.
7. according to the many rotor wing unmanned aerial vehicles described in claim 3,4,5 or 6, it is characterized in that: on the hanger joint (1C) of hanger (1) lower end, be provided with bayonet socket, hole clipping or screw thread.
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 on body upper.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610220907.8A CN105836113A (en) | 2016-04-11 | 2016-04-11 | A multi-rotor unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610220907.8A CN105836113A (en) | 2016-04-11 | 2016-04-11 | A multi-rotor unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105836113A true CN105836113A (en) | 2016-08-10 |
Family
ID=56598053
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610220907.8A Withdrawn CN105836113A (en) | 2016-04-11 | 2016-04-11 | A multi-rotor unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105836113A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106308692A (en) * | 2016-10-17 | 2017-01-11 | 罗智诚 | Intelligent cleaning device for UAV (unmanned aerial vehicle) |
| CN106394915A (en) * | 2016-11-11 | 2017-02-15 | 深圳市智璟科技有限公司 | All-in-one mission load of unmanned aerial vehicle |
| CN106892098A (en) * | 2017-03-13 | 2017-06-27 | 广东工业大学 | A kind of fence type loading unmanned plane |
| CN107521711A (en) * | 2017-09-25 | 2017-12-29 | 南京律智诚专利技术开发有限公司 | A kind of transport unmanned plane |
-
2016
- 2016-04-11 CN CN201610220907.8A patent/CN105836113A/en not_active Withdrawn
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106308692A (en) * | 2016-10-17 | 2017-01-11 | 罗智诚 | Intelligent cleaning device for UAV (unmanned aerial vehicle) |
| CN106394915A (en) * | 2016-11-11 | 2017-02-15 | 深圳市智璟科技有限公司 | All-in-one mission load of unmanned aerial vehicle |
| CN106394915B (en) * | 2016-11-11 | 2019-08-23 | 深圳市智璟科技有限公司 | Unmanned plane All-in-One mission payload |
| CN106892098A (en) * | 2017-03-13 | 2017-06-27 | 广东工业大学 | A kind of fence type loading unmanned plane |
| CN106892098B (en) * | 2017-03-13 | 2023-10-31 | 广东工业大学 | Fence type object carrying unmanned aerial vehicle |
| CN107521711A (en) * | 2017-09-25 | 2017-12-29 | 南京律智诚专利技术开发有限公司 | A kind of transport unmanned plane |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105836114A (en) | A multi-rotor unmanned aerial vehicle | |
| CN105799922A (en) | Multi-rotor unmanned aerial vehicle | |
| CN107117310A (en) | A kind of multi-rotor unmanned aerial vehicle | |
| CN105836113A (en) | A multi-rotor unmanned aerial vehicle | |
| CN105775115A (en) | Multi-rotor wing unmanned aerial vehicle | |
| CN105857606A (en) | Multi-rotor unmanned aerial vehicle | |
| CN105799921A (en) | Multi-rotor unmanned aerial vehicle | |
| CN105857607A (en) | Multi-rotor unmanned aerial vehicle | |
| CN105775116A (en) | Multi-rotor wing unmanned aerial vehicle | |
| CN205707315U (en) | A kind of many rotor wing unmanned aerial vehicles | |
| CN107416194A (en) | A kind of multi-rotor unmanned aerial vehicle | |
| CN205707311U (en) | A kind of many rotor wing unmanned aerial vehicles | |
| CN106976557A (en) | A kind of 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 | |
| CN106976555A (en) | A kind of multi-rotor unmanned aerial vehicle | |
| CN107150797A (en) | A kind of multi-rotor unmanned aerial vehicle | |
| CN107054635A (en) | A kind of multi-rotor unmanned aerial vehicle | |
| CN105799920A (en) | Multi-rotor unmanned aerial vehicle | |
| CN108327904A (en) | A kind of multi-rotor unmanned aerial vehicle | |
| CN108298086A (en) | A kind of multi-rotor unmanned aerial vehicle suspender | |
| CN205707316U (en) | A kind of many rotor wing unmanned aerial vehicles | |
| CN205707314U (en) | A kind of many rotor wing unmanned aerial vehicles | |
| CN107150795A (en) | A kind of multi-rotor unmanned aerial vehicle | |
| CN108622386A (en) | A kind of multi-rotor unmanned aerial vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | 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 | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20160810 |