CN205440865U - Multi -rotor -wing aircraft - Google Patents
Multi -rotor -wing aircraft Download PDFInfo
- Publication number
- CN205440865U CN205440865U CN201620232601.XU CN201620232601U CN205440865U CN 205440865 U CN205440865 U CN 205440865U CN 201620232601 U CN201620232601 U CN 201620232601U CN 205440865 U CN205440865 U CN 205440865U
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- China
- Prior art keywords
- rotor
- rotor aerocraft
- frame
- substrate
- wing aircraft
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- 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.)
- Expired - Fee Related
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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- Manufacture Of Motors, Generators (AREA)
Abstract
The utility model discloses a multi -rotor -wing aircraft, include: frame, frame include base plate, two curb plates, a plurality of horn and roofs, and two curb plates set up respectively in the base plate both sides, and a plurality of horns set up in base plate and two curb plates, and the roof sets up in two curb plates, drive arrangement sets up in a plurality of horns, and drive arrangement includes a plurality of motors and a plurality of rotor, and a plurality of rotors set up respectively in a plurality of motors, and controlling means, set up in the base plate. The utility model discloses a multi -rotor -wing aircraft has simplified the mechanical structure of aircraft, and part quantity is less, and the production equipment is quick, a plurality of motors are convenient for control, and the rotational speed keeps unanimous, and flight is stable, and the frame adopts the carbon plate material to make, multi -rotor -wing aircraft light in weight, and electronic governor and power supply integration reduce occupation space on a PCB board, the maintenance of being convenient for, its aircraft bonnet accords with the air current design, and multi -rotor -wing aircraft flight in -process reduces aerodynamic drag.
Description
Technical field
This utility model relates to a kind of aircraft, particularly relates to a kind of multi-rotor aerocraft.
Background technology
Along with the fast development of science and technology, the use of flight equipment is more extensive, and the equipment of taking photo by plane that flies also arises at the historic moment.At present, existing flight is taken photo by plane equipment, its complicated in mechanical structure, and production and assembly are more due to part, and operation is more, assembles finished product efficiency slow；The corresponding motor of the single rotor of existing driving means drives, and the rotating speed of multiple motors is variant, it is impossible to keep consistent, causes flight to take photo by plane equipment flight instability；The equipment of taking photo by plane that flies uses material uneven, uses material heavy, is formed without unified specification and material；The take photo by plane picture pick-up device shooting of equipment of flight is fuzzy, and image is unintelligible, controls electronic component many, and does not install concentratedly, causes maintenance and changes difficulty.
Utility model content
For deficiency of the prior art, the purpose of this utility model is to provide a kind of multi-rotor aerocraft.
For solving the problems referred to above, this application discloses a kind of multi-rotor aerocraft, including: frame, frame includes substrate, two side plates, multiple horn and top board, two side plates are respectively arranged at substrate both sides, and multiple horns are arranged at substrate and two side plates, and top board is arranged at two side plates；Driving means, is arranged at multiple horn, and driving means includes multiple motor and multiple rotor, and multiple rotors are respectively arranged at multiple motor；And control device, it is arranged at substrate.
An embodiment according to the application, above-mentioned multi-rotor aerocraft includes that camera head, described camera head are arranged at substrate and two side sheet rooms.
An embodiment according to the application, above-mentioned camera head includes photographic head and transmitter, and photographic head is arranged at substrate and two side sheet rooms, and transmitter is arranged at top board, and electrically connects photographic head.
An embodiment according to the application, above-mentioned control device includes pcb board, electron speed regulator and power supply unit, and pcb board is arranged at substrate, and electron speed regulator is arranged at pcb board, power supply unit is arranged at pcb board, and power supply unit electrically connects multiple motors, photographic head and transmitter.
An embodiment according to the application, above-mentioned multi-rotor aerocraft includes that hood, hood are arranged at frame.
An embodiment according to the application, above-mentioned frame is carbon plate material.
An embodiment according to the application, above-mentioned multiple motors are brushless electric machine.
Compared with prior art, this utility model can obtain and include techniques below effect:
Multi-rotor aerocraft of the present utility model simplifies the frame for movement of aircraft, and number of parts is less, and production and assembly are quick；Multiple motors are easy to control, and rotating speed keeps consistent, flight stability, and frame uses carbon plate material to make, and multi-rotor aerocraft is lightweight, and electron speed regulator and power supply unit are integrated on one piece of pcb board, and minimizing takes up room, it is simple to maintenance；Its hood meets air flow design, reduces air drag in multi-rotor aerocraft flight course.
Accompanying drawing explanation
Accompanying drawing described herein is used for providing further understanding of the present application, constitutes the part of the application, and the schematic description and description of the application is used for explaining the application, is not intended that the improper restriction to the application.In the accompanying drawings:
Fig. 1 is the axonometric chart of the multi-rotor aerocraft of the application one embodiment；
Fig. 2 is the partial enlarged drawing of the multi-rotor aerocraft of the application one embodiment；
Fig. 3 is the side view of the multi-rotor aerocraft of the application one embodiment.
Detailed description of the invention
To schematically disclose multiple embodiments of the application below, as clearly stated, the details in many practices will be explained in the following description.It should be appreciated, however, that the details in these practices is not applied to limit the application.It is to say, in the some embodiments of the application, the details in these practices is non-essential.Additionally, for simplify graphic for the sake of, some known usual structures and assembly will illustrate it in the drawings in the way of simply illustrative.
Refer to the axonometric chart that Fig. 1, Fig. 1 are the multi-rotor aerocrafts 1 of the application one embodiment.As it can be seen, the multi-rotor aerocraft 1 of the application mainly includes frame 11, driving means 12 and controls device 13.Frame 11 includes 111, two side plates 112 of substrate, multiple horn 113 and top board 114, two side plates 112 are arranged at the both sides of substrate 111, and two side plates 112 are in parastate, multiple horns 113 are arranged at substrate 111 and run through the bottom of two side plates 112, top board 114 is arranged at two side plates 112, and is in parastate with substrate 111.Driving means 12 includes that multiple motor 121 and multiple rotor 122, multiple motors 121 are correspondingly arranged in multiple horn 113 respectively, and multiple rotors 122 are correspondingly arranged in the top of multiple motor 121 respectively, controls device 13 and is arranged at substrate 111.
Multi-rotor aerocraft 1 also includes that camera head 14, camera head 14 include photographic head 141 and transmitter 142, and photographic head 141 is arranged between substrate 111 and two side plates 112, and transmitter 142 is arranged at top board 114, and electrically connects photographic head 141.Photographic head 141 scalable camera angle, produces the first visual angle picture.Transmitter 142, for transmitting the image that the photographic head 141 of multi-rotor aerocraft 1 shoots and records, also can transmit the operation conditions of multi-rotor aerocraft 1 and the command set control command for multi-rotor aerocraft 1.Above-mentioned transmitter 142 is 5.8G600mw32CH transmitter, naturally it is also possible to for other transmitter, do not repeating with this.
It is the partial enlarged drawing of the multi-rotor aerocraft 1 of the application one embodiment the most in the lump refering to Fig. 2, Fig. 2.As shown in the figure, control device 13 and include pcb board 131, electron speed regulator 132 and power supply unit 133, pcb board 131 is arranged at substrate 111, electron speed regulator 132 and power supply unit 133 and is arranged at pcb board, and power supply unit 133 electrically connects with multiple motors 121, photographic head 141 and transmitter 142.Electron speed regulator 132 can be used for controlling the rotating speed of multiple motor 121, reaches to control flight speed and the purpose of flight angle of multi-rotor aerocraft 1.Above-mentioned frame 11 is carbon plate material, naturally it is also possible to other material, is not repeating with this；Above-mentioned multiple motors 121 are brushless electric machine, naturally it is also possible to for other motor, do not repeating with this.
It is the side view of the multi-rotor aerocraft 1 of the application one embodiment the most in the lump refering to Fig. 3, Fig. 3.As it can be seen, in the another embodiment of the application, the multi-rotor aerocraft 1 of the application includes that hood 15, hood 15 are arranged at the top of frame 11.Hood 15 is as the shell of multi-rotor aerocraft 1, and it meets air flow design, reduces air drag, and play pcb board 131, electron speed regulator 132 and the effect of power supply unit 133 in protection multi-rotor aerocraft 1 in multi-rotor aerocraft 1 flight course.
The function mode of the multi-rotor aerocraft 1 of the application is, command set inputs control signal of taking off, transmitter 142 receives and takes off control signal and be sent to multiple motor 121, multiple motors 121 start, the most multiple motors 121 drive multiple rotor 122 to rotate, and multiple rotors 122 drive multi-rotor aerocraft 1 to take off.In flight course, control electron speed regulator 132 and reach to control the rotating speed of multiple motor 121, thus control flight speed and the flight angle of multi-rotor aerocraft 1.
In sum, in one or more embodiment of the application, multi-rotor aerocraft of the present utility model simplifies the frame for movement of aircraft, and number of parts is less, and production and assembly are quick；Multiple motors are easy to control, and rotating speed keeps consistent, flight stability, and frame uses carbon plate material to make, and multi-rotor aerocraft is lightweight, and electron speed regulator and power supply unit are integrated on one piece of pcb board, and minimizing takes up room, it is simple to maintenance；Its hood meets air flow design, reduces air drag in multi-rotor aerocraft flight course.
Described above illustrate and describes some preferred embodiments of the present utility model, but as previously mentioned, it is to be understood that this utility model is not limited to form disclosed herein, it is not to be taken as the eliminating to other embodiments, and can be used for other combinations various, amendment and environment, and can be modified by above-mentioned teaching or the technology of association area or knowledge in utility model contemplated scope described herein.And the change that those skilled in the art are carried out and change are without departing from spirit and scope of the present utility model, the most all should be in the protection domain of this utility model claims.
Claims (7)
1. a multi-rotor aerocraft, it is characterised in that including:
Frame, described frame includes substrate, two side plates, multiple horn and top board, and described two side plates are respectively arranged at described substrate both sides, and the plurality of horn is arranged at described substrate and described two side plates, and described top board is arranged at described two side plates；
Driving means, is arranged at the plurality of horn, and described driving means includes multiple motor and multiple rotor, and the plurality of rotor is respectively arranged at the plurality of motor；And
Control device, be arranged at described substrate.
2. multi-rotor aerocraft as claimed in claim 1, it is characterised in that described multi-rotor aerocraft includes that camera head, described camera head are arranged at described substrate and described two side sheet rooms.
3. multi-rotor aerocraft as claimed in claim 2, it is characterised in that described camera head includes that photographic head and transmitter, described photographic head are arranged at described substrate and described two side sheet rooms, and described transmitter is arranged at described top board, and electrically connects described photographic head.
4. multi-rotor aerocraft as claimed in claim 1, it is characterized in that, described control device includes pcb board, electron speed regulator and power supply unit, described pcb board is arranged at described substrate, described electron speed regulator is arranged at described pcb board, described power supply unit is arranged at described pcb board, and described power supply unit electrically connects the plurality of motor, photographic head and transmitter.
5. multi-rotor aerocraft as claimed in claim 1, it is characterised in that described multi-rotor aerocraft includes that hood, described hood are arranged at described frame.
6. multi-rotor aerocraft as claimed in claim 1, it is characterised in that described frame is carbon plate material.
7. multi-rotor aerocraft as claimed in claim 1, it is characterised in that the plurality of motor is brushless electric machine.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620232601.XU CN205440865U (en) | 2016-03-23 | 2016-03-23 | Multi -rotor -wing aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620232601.XU CN205440865U (en) | 2016-03-23 | 2016-03-23 | Multi -rotor -wing aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205440865U true CN205440865U (en) | 2016-08-10 |
Family
ID=56574920
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620232601.XU Expired - Fee Related CN205440865U (en) | 2016-03-23 | 2016-03-23 | Multi -rotor -wing aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205440865U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107069361A (en) * | 2017-05-10 | 2017-08-18 | 中科新松有限公司 | A kind of power distribution device and unmanned plane |
| CN112498672A (en) * | 2020-11-03 | 2021-03-16 | 中国直升机设计研究所 | Unmanned aerial vehicle |
| CN113353269A (en) * | 2021-07-26 | 2021-09-07 | 惠州市翼飞智能科技有限公司 | Unmanned aerial vehicle |
-
2016
- 2016-03-23 CN CN201620232601.XU patent/CN205440865U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107069361A (en) * | 2017-05-10 | 2017-08-18 | 中科新松有限公司 | A kind of power distribution device and unmanned plane |
| CN112498672A (en) * | 2020-11-03 | 2021-03-16 | 中国直升机设计研究所 | Unmanned aerial vehicle |
| CN113353269A (en) * | 2021-07-26 | 2021-09-07 | 惠州市翼飞智能科技有限公司 | Unmanned aerial vehicle |
| CN113353269B (en) * | 2021-07-26 | 2022-07-19 | 惠州市翼飞智能科技有限公司 | Unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160810 Termination date: 20170323 |