CN106114814A - A kind of many rotor wing unmanned aerial vehicles - Google Patents
A kind of many rotor wing unmanned aerial vehicles Download PDFInfo
- Publication number
- CN106114814A CN106114814A CN201610586152.3A CN201610586152A CN106114814A CN 106114814 A CN106114814 A CN 106114814A CN 201610586152 A CN201610586152 A CN 201610586152A CN 106114814 A CN106114814 A CN 106114814A
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- Prior art keywords
- carry
- motor
- central plate
- unmanned aerial
- rotor wing
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- 230000007246 mechanism Effects 0.000 claims abstract description 38
- 239000000725 suspension Substances 0.000 claims abstract description 15
- 230000000694 effects Effects 0.000 abstract description 4
- 238000010276 construction Methods 0.000 abstract description 3
- 238000005516 engineering process Methods 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000004575 stone Substances 0.000 description 1
- 230000007306 turnover Effects 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
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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
- B64C27/10—Helicopters with two or more rotors arranged coaxially
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
-
- 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
- B64D47/02—Arrangements or adaptations of signal or lighting devices
-
- 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
-
- 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
- B64U2101/60—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
Open kind of many rotor wing unmanned aerial vehicles of the present invention, including central plate, foot rest, horn, motor cabinet, motor, propeller and antenna, described foot rest is located at below central plate, described antenna is located at above central plate, described horn one end is connected with central plate by joint portion, the other end is connected with motor cabinet, and motor is arranged on motor cabinet, and propeller is arranged on motor；It is additionally provided with suspension holdfast bottom described central plate, described suspension holdfast arranges 2 parallel carry bars；Carry image mechanism, gondola mechanism and microphone successively on described carry bar.The low altitude flight platform of present invention application SUAV, simple in construction, manipulation convenience, using effect are excellent, expand the application of SUAV.
Description
Technical field
The present invention relates to field of mechanical technique, particularly relate to a kind of multiduty many rotor wing unmanned aerial vehicles.
Background technology
Along with the fast development of the high-and-new science and technology such as automatic control technology, information technology, unmanned air vehicle technique also occurs huge
Much progress.The particularly little MAV in low latitude, have that the lead time is short, expense cost is low, application risk is little, easy and simple to handle easily
Etc. distinguishing feature, is an excellent flying platform, anxious lift-launch product to be developed, expands the commercial neck of little MAV
Territory.Such as, at present in important events such as celebration, commercial propaganda, collective team activities, construction petal is free-and-easy, snow flakes are whirling, publicity
The mode of operation of the scenes such as data granting remains and is completed on ground by manually or mechanically device, and its sense of reality is poor, need staff
Many, etc. shortcoming.For in the emergency disposal of disaster, for the disaster-stricken trapped personnel wanted help, due to conveying arrangement, on-the-spot calamity
The factors such as feelings environment, transportation condition limit, it is impossible to accomplish the response of prestissimo.For fire of high-rise building, earthquake and mountain stone
The disasters such as landslide, transportation condition is inconvenient or by heavy damage, ground even walking is also difficult to pass through, and hinders relief goods
Transport is thrown in.Mode is thrown in the air for existing relief goods, on the one hand, inconvenience set out by aircraft, expend huge, be not suitable for
Non-large-scale disaster-stricken trapped personnel is rescued, the input of the most inapplicable light-duty a small amount of load；On the other hand, for fixed-wing high-altitude
Throwing, it is difficult to be accurately positioned throwing point, throwing goods and materials has bigger waste, and producing level is low；And behaviour is thrown in for helicopter low latitude
Making difficulty big, risk is bigger.
Summary of the invention
The purpose of the present invention is aiming at the defect of above-mentioned prior art, it is provided that a kind of simple in construction, manipulation convenience, use
Many rotor wing unmanned aerial vehicles that effect is excellent, the low altitude flight platform of application SUAV, expand the commercial kitchen area of SUAV.
For reaching above-mentioned purpose, the present invention realizes by the following technical solutions: a kind of many rotor wing unmanned aerial vehicles, including in
Core, foot rest, horn, motor cabinet, motor, propeller and antenna, described foot rest is located at below central plate, during described antenna is located at
Above core, described horn one end is connected with central plate by joint portion, and the other end is connected with motor cabinet, and motor is arranged on motor
On seat, propeller is arranged on motor；It is additionally provided with suspension holdfast bottom described central plate, described suspension holdfast arranges 2 and puts down
The carry bar of row；Carry image mechanism, gondola mechanism and microphone successively on described carry bar.
Further, described motor cabinet is provided with two motors, same end face and the bottom surface being located in motor cabinet, and the two
Turn to contrary, synchronization.
Further, described image mechanism include carry part, carry plate, X-axis brushless electric machine, The Cloud Terrace support, shooting support,
Y-axis brushless electric machine and camera head, the upper end of carry part is provided with bayonet socket, and carry part is sticked on carry bar by bayonet socket, hangs
The lower end of holder is affixed with carry plate, and the bottom of carry plate is connected with X-axis brushless electric machine, and X-axis brushless electric machine controls The Cloud Terrace support
Rotate；One end of described The Cloud Terrace support is connected with Y-axis brushless electric machine, and Y-axis brushless electric machine controls shooting support and rotates；Described shooting
Device is fixed on shooting support.
Further, described gondola mechanism includes that hanger, nacelle, hatch door, 4 hangers are located at the end face of nacelle, are sleeved on
On carry bar, two fan hatch doors are located at nacelle bottom surface, and hatch door is hinged with the intermediate parting strips of nacelle bottom surface, by being located at the bottom of nacelle side
The electrical switch in portion realizes Guan Bi and the unlatching of hatch door.
Further, described microphone is affixed with installing plate, is sleeved on carry bar by 2 through holes on installing plate.
Compared with prior art, advantages of the present invention and good effect are:
The image mechanism of many rotor wing unmanned aerial vehicles, gondola mechanism and the microphone carry that the present invention provides is being arranged at suspension
Carry bar on frame, it is possible to multiple special in the environment of, it is ensured that image mechanism can provide stable, clearly picture pass ground back
Face, can communicate information to ground staff in real time by microphone, hovers in the low latitude possessed, and improves throwing accurate of goods and materials
Degree and utilization ratio, especially for a small amount of load that is lightweight and that be badly in need of, have the more prominent using value of ratio, be greatly improved
Work efficiency.It addition, the suspension holdfast bottom unmanned plane is located at by carry bar, under non-working condition, can quickly remove shooting
Mechanism, gondola mechanism and microphone；Be flexibly connected between horn with central plate, can quick unmarshaling, transport, easy to carry, real
Strong by property.
Accompanying drawing explanation
Fig. 1 is the structural representation of the many rotor wing unmanned aerial vehicles of the present invention；
Fig. 2 is carry bar carry image mechanism, gondola mechanism and the structural representation of microphone in the present invention；
Fig. 3 is the structural representation of image mechanism in the present invention；
In figure: 1-central plate, 2-antenna, 3-horn, 4-propeller, 5-motor, 6-motor cabinet, 7-carry bar, 8-images
Mechanism, 9-suspension holdfast, 10-foot rest, 11-gondola mechanism, 12-microphone, 81-carry part, 82-carry plate, 83-X axle is brushless
Motor, 84-The Cloud Terrace support, 85-images support, 86-Y axle brushless electric machine, 87-camera head,.111-hanger, 112-electronic cutting
Close, 121-installing plate.
Detailed description of the invention
In order to make the purpose of the present invention, technical scheme and advantage clearer, below in conjunction with accompanying drawing, the present invention is entered
Row further describes.
As it is shown in figure 1, the many rotor wing unmanned aerial vehicles of one that the present invention provides, including central plate 1, foot rest 10, horn 3, motor
Seat 6, motor 5, propeller 4 and antenna 2, described foot rest 10 is located at below central plate 1, and described antenna 2 is located at above central plate 1,
Described horn 3 one end is connected with central plate 1 by joint portion, and the other end is connected with motor cabinet 6, and motor 5 is arranged on motor cabinet 6
On, propeller 4 is arranged on motor 5；It is additionally provided with suspension holdfast 9 bottom described central plate 1, described suspension holdfast 9 arranges 2
Parallel carry bar 7；Carry image mechanism 8, gondola mechanism 11 and microphone 12 successively on described carry bar 7.This structure
Many rotor wing unmanned aerial vehicles, it is possible to multiple special in the environment of perform multiple-task, such as in field such as burst alert, the disaster relief, celebration etc.
Close, improve the precision of throwing for a small amount of load that is lightweight and that be badly in need of and utilization ratio.
Further, described motor cabinet 6 is provided with two motors 5, same end face and the bottom surface being located in motor cabinet 6, and
Turning to of the two is contrary, synchronization.From frame for movement, considerably increase the stability of aircraft, also promote the energy of aircraft simultaneously
Consumption efficiency.
As shown in Figure 2,3, further, described image mechanism 8 includes carry part 81, carry plate 82, X-axis brushless electric machine
83, The Cloud Terrace support 84, shooting support 85, Y-axis brushless electric machine 86 and camera head 87, the upper end of carry part 81 is provided with bayonet socket,
Carry part 81 is sticked on carry bar 7 by bayonet socket, and the lower end of carry part 81 is affixed with carry plate 82, and the bottom of carry plate 82 is solid
Being connected to X-axis brushless electric machine 83, X-axis brushless electric machine 83 controls The Cloud Terrace support 84 and rotates；One end of described The Cloud Terrace support 84 is connected with Y
Axle brushless electric machine 86, Y-axis brushless electric machine 86 controls shooting support 85 and rotates；Described camera head 87 is fixed in shooting support 85
On.Ensure that image mechanism can provide stable, picture clearly.
Further, described gondola mechanism 11 includes that hanger 111, nacelle, hatch door, 4 hangers 111 are located at the top of nacelle
Face, is sleeved on carry bar 7, and two fan hatch doors are located at nacelle bottom surface, and Open Side Down, and hatch door cuts with scissors with the intermediate parting strips of nacelle bottom surface
Connect, realize Guan Bi and the unlatching of hatch door by being located at the electrical switch 112 of nacelle side bottom.When loading load, can be
Carry bar 7 is extracted out from suspension holdfast 9, then makes hatch door open up gondola mechanism 11 upset, in order to filling operation, filling
Terminate, close hatch door, by the locked hatch door of electrical switch 112, afterwards turn over on-hook.
Further, described microphone 12 is affixed with installing plate 121, is sleeved on extension by 2 through holes on installing plate 121
Carry on bar 7.Under non-working condition, can quickly remove, it is simple to transport or collect.
Many rotor wing unmanned aerial vehicles that the present invention provides, the work process in burst alert or the disaster relief is as follows:
Ground prepares: filling gondola, on carry image mechanism 8, gondola mechanism 11 and microphone 12 to unmanned plane；Take off,
Arrive overhead, target location, pass image back with reference to image mechanism 8, control many rotor wing unmanned aerial vehicles flight attitude, accurately adjust hovering
Position, sends voice signal by microphone 12, notifies, reminds reception staff；Control the electrical switch 112 dozens of gondola mechanism 11
Storehouse door opening, load departs from nacelle, completes input action；Now image mechanism 8 monitoring is thrown the reception condition of load and is immediately passed
Returning, commanding may determine that load is received；Make a return voyage landing, complete a duty cycle.
When celebration occasion uses, fly up to overhead, target location, pass image back with reference to image mechanism 8, control many rotors without
Man-machine flight attitude, sends celebrating melody by microphone 12, and door opened by the electrical switch 112 controlling gondola mechanism 11, can
To send out propaganda material, according to the image monitoring flow of personnel situation immediately passed back, dredged by microphone 12, it is to avoid occur
Unexpected.Can be certainly also used to the detection of traffic conditions and dredge.
Many rotor wing unmanned aerial vehicles that the present invention provides, are being arranged at suspension image mechanism, gondola mechanism and microphone carry
Carry bar on support, it is possible to multiple special in the environment of, it is ensured that image mechanism can provide stable, clearly picture pass back
Ground, can communicate information to ground staff in real time by microphone, and hovering in the low latitude possessed, improves the essence of the throwing of goods and materials
Accuracy and utilization ratio, especially for a small amount of load that is lightweight and that be badly in need of, have than more prominent using value.It addition,
The suspension holdfast bottom unmanned plane is located at by carry bar, under non-working condition, can extract out, it is simple to quickly tear open from suspension holdfast
Except image mechanism, gondola mechanism and microphone；Be flexibly connected between horn with central plate, can quick unmarshaling, transport, the side of carrying
Just, practical.
Certainly, the present invention also can have other various embodiments, in the case of without departing substantially from present invention spirit and essence thereof, ripe
Know those skilled in the art and can make various corresponding change and deformation according to the present invention, but these change and deformation accordingly
All should belong to the protection domain of appended claims of the invention.
Claims (5)
1. a rotor wing unmanned aerial vehicle more than, including central plate (1), foot rest (10), horn (3), motor cabinet (6), motor (5), spiral
Oar (4) and antenna (2), it is characterised in that: central plate (1) lower section is located at by described foot rest (10), and central plate is located at by described antenna (2)
(1) top, described horn (3) one end is connected with central plate (1) by joint portion, and the other end is connected with motor cabinet (6), motor
(5) being arranged on motor cabinet (6), propeller (4) is arranged on motor (5)；Described central plate (1) bottom is additionally provided with suspension holdfast
(9), described suspension holdfast (9) is arranged 2 parallel carry bars (7)；Carry image mechanism successively on described carry bar (7)
(8), gondola mechanism (11) and microphone (12).
Many rotor wing unmanned aerial vehicles the most according to claim 1, it is characterised in that: described motor cabinet (6) is provided with two motors
(5), with being located in end face and the bottom surface of motor cabinet (6), and the two turn to contrary, synchronization.
Many rotor wing unmanned aerial vehicles the most according to claim 1, it is characterised in that: described image mechanism (8) includes carry part
(81), carry plate (82), X-axis brushless electric machine (83), The Cloud Terrace support (84), shooting support (85), Y-axis brushless electric machine (86) and taking the photograph
As device (87), the upper end of carry part (81) is provided with bayonet socket, and carry part (81) is sticked on carry bar (7) by bayonet socket, hangs
The lower end of holder (81) is affixed with carry plate (82), and the bottom of carry plate (82) is connected with X-axis brushless electric machine (83), and X-axis is brushless
Motor (83) controls The Cloud Terrace support (84) and rotates；One end of described The Cloud Terrace support (84) is connected with Y-axis brushless electric machine (86), Y-axis
Brushless electric machine (86) controls shooting support (85) and rotates；Described camera head (87) is fixed in shooting support (85).
Many rotor wing unmanned aerial vehicles the most according to claim 1, it is characterised in that: described gondola mechanism (11) includes hanger
(111), nacelle, hatch door, 4 hangers (111) are located at the end face of nacelle, are sleeved on carry bar (7), and two fan hatch doors are located at nacelle
Bottom surface, and Open Side Down, hatch door is hinged with the intermediate parting strips of nacelle bottom surface, by being located at the electrical switch of nacelle side bottom
(112) Guan Bi and the unlatching of hatch door are realized.
Many rotor wing unmanned aerial vehicles the most according to claim 1, it is characterised in that: described microphone (12) and installing plate (121)
Affixed, it is sleeved on carry bar (7) by 2 through holes on installing plate (121).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610586152.3A CN106114814A (en) | 2016-07-22 | 2016-07-22 | A kind of many rotor wing unmanned aerial vehicles |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610586152.3A CN106114814A (en) | 2016-07-22 | 2016-07-22 | A kind of many rotor wing unmanned aerial vehicles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106114814A true CN106114814A (en) | 2016-11-16 |
Family
ID=57289380
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610586152.3A Pending CN106114814A (en) | 2016-07-22 | 2016-07-22 | A kind of many rotor wing unmanned aerial vehicles |
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| Country | Link |
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| CN (1) | CN106114814A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107719653A (en) * | 2017-09-25 | 2018-02-23 | 南京律智诚专利技术开发有限公司 | A kind of monitoring unmanned plane |
| CN109229389A (en) * | 2018-08-30 | 2019-01-18 | 西安三翼航空科技有限公司 | A kind of multi-functional mission payload hanger of unmanned plane |
| CN110182363A (en) * | 2019-04-26 | 2019-08-30 | 厦门大学 | It is a kind of for capturing the flying wing type unmanned plane of unmanned plane |
| CN111439386A (en) * | 2020-04-17 | 2020-07-24 | 江苏无国界无人机科技有限公司 | Unmanned aerial vehicle electric power inspection nacelle integrating ultraviolet light, visible light and infrared light |
| CN114104315A (en) * | 2021-12-17 | 2022-03-01 | 国网江西省电力有限公司赣州供电分公司 | Method and device for cooperative surveying and mapping of unmanned aerial vehicle cluster |
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| CN104477399A (en) * | 2014-11-26 | 2015-04-01 | 马鞍山市靓马航空科技有限公司 | Multi-rotor unmanned aerial vehicle (UAV) for searching and rescuing at night |
| CN104527980A (en) * | 2014-12-15 | 2015-04-22 | 青岛欧森系统技术有限公司 | Transportation throwing mechanism of unmanned helicopter |
| CN204507269U (en) * | 2015-03-27 | 2015-07-29 | 马鞍山市赛迪智能科技有限公司 | A kind of unmanned plane tackling airborne aircraft |
| CN205131689U (en) * | 2015-11-16 | 2016-04-06 | 湖南云顶智能科技有限公司 | A carry platform for unmanned aerial vehicle |
| CN205854473U (en) * | 2016-07-22 | 2017-01-04 | 四川克瑞斯航空科技有限公司 | A kind of many rotor wing unmanned aerial vehicles |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN104477399A (en) * | 2014-11-26 | 2015-04-01 | 马鞍山市靓马航空科技有限公司 | Multi-rotor unmanned aerial vehicle (UAV) for searching and rescuing at night |
| CN104527980A (en) * | 2014-12-15 | 2015-04-22 | 青岛欧森系统技术有限公司 | Transportation throwing mechanism of unmanned helicopter |
| CN204507269U (en) * | 2015-03-27 | 2015-07-29 | 马鞍山市赛迪智能科技有限公司 | A kind of unmanned plane tackling airborne aircraft |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107719653A (en) * | 2017-09-25 | 2018-02-23 | 南京律智诚专利技术开发有限公司 | A kind of monitoring unmanned plane |
| CN109229389A (en) * | 2018-08-30 | 2019-01-18 | 西安三翼航空科技有限公司 | A kind of multi-functional mission payload hanger of unmanned plane |
| CN110182363A (en) * | 2019-04-26 | 2019-08-30 | 厦门大学 | It is a kind of for capturing the flying wing type unmanned plane of unmanned plane |
| CN111439386A (en) * | 2020-04-17 | 2020-07-24 | 江苏无国界无人机科技有限公司 | Unmanned aerial vehicle electric power inspection nacelle integrating ultraviolet light, visible light and infrared light |
| CN114104315A (en) * | 2021-12-17 | 2022-03-01 | 国网江西省电力有限公司赣州供电分公司 | Method and device for cooperative surveying and mapping of unmanned aerial vehicle cluster |
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| PB01 | Publication | ||
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Application publication date: 20161116 |