CN106809379A - A kind of unmanned aerial vehicle - Google Patents
A kind of unmanned aerial vehicle Download PDFInfo
- Publication number
- CN106809379A CN106809379A CN201610958300.XA CN201610958300A CN106809379A CN 106809379 A CN106809379 A CN 106809379A CN 201610958300 A CN201610958300 A CN 201610958300A CN 106809379 A CN106809379 A CN 106809379A
- Authority
- CN
- China
- Prior art keywords
- fuselage
- propeller
- unmanned aerial
- aerial vehicle
- module
- 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- Withdrawn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
Classifications
-
- 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
- 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
- B64C27/32—Rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S19/00—Satellite radio beacon positioning systems; Determining position, velocity or attitude using signals transmitted by such systems
- G01S19/38—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system
- G01S19/39—Determining a navigation solution using signals transmitted by a satellite radio beacon positioning system the satellite radio beacon positioning system transmitting time-stamped messages, e.g. GPS [Global Positioning System], GLONASS [Global Orbiting Navigation Satellite System] or GALILEO
- G01S19/42—Determining position
- G01S19/48—Determining position by combining or switching between position solutions derived from the satellite radio beacon positioning system and position solutions derived from a further system
- G01S19/49—Determining position by combining or switching between position solutions derived from the satellite radio beacon positioning system and position solutions derived from a further system whereby the further system is an inertial position system, e.g. loosely-coupled
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/20—Remote controls
Abstract
The present invention relates to a kind of unmanned aerial vehicle, it include fuselage, propeller and fuselage be connected with propeller together with connecting rod, described fuselage head sets camera and searchlight, searchlight causes to provide illumination in night flight, fuselage upper end sets both wings breath light, fuselage bottom sets alignment system emitter window and foot pad, and fuselage is built-in with power module, control mainboard, satellite positioning navigation module, acousto-optic alignment system, sensor, photographing module, wireless module and storage module.Described propeller is symmetrically connected to around fuselage at least provided with four, and propeller mount outside is additionally provided with blade guard circle, effectively effect and safety coefficient of lifting paddle.The built-in acousto-optic alignment system of the present invention solves the problems, such as precisely hover and balance flight indoors, and built-in wireless module is connected with mobile phone and carries out Remote operation；Body design path type fuselage effectively reduces air drag enhancing flying quality.
Description
Technical field
The present invention relates to a kind of unmanned aerial vehicle, especially it is connected with propeller by fuselage, four propellers and fuselage
The unmanned aerial vehicle of connecting rod composition together.
Background technology
Nowadays with development in science and technology, small miniature pilotless plane has incorporated us and has lived central, is applied in every profession and trade.
Therefore；There are various unmanned aerial vehicles in the market, and general unmanned aerial vehicle is the remote controller operation by matching, and takes nothing
People's aircraft takes remote control again simultaneously, and will seem trouble；The also common built-in GPS of unmanned aerial vehicle and GLONASS satellite
Navigation system carries out location navigation, if it is desired to being flown indoors, be just interfered cannot normal flight.Therefore, it is just to solve
Certainly above mentioned problem, a kind of unmanned aerial vehicle of present invention offer, can carry out remote control by connecting mobile phone；The built-in acousto-optic positioning of fuselage
System, easily realizes the fixed high, fixed point of indoor and outdoor, hovering.
The content of the invention
The technical problems to be solved by the invention are to provide a kind of unmanned aerial vehicle, fuselage built-in satellite positioning navigation module,
It is also equipped with acousto-optic alignment system and solves the problems, such as that interior cannot precisely hover and smooth flight.
In order to solve the above technical problems, unmanned aerial vehicle of the present invention, including fuselage, propeller and fuselage is connected with propeller
Connect connecting rod together；At least provided with four, its propeller mount outside is additionally provided with propeller blade guarantor to described propeller
Guard ring, described connecting rod sets at least to four groups, every group of at least two connecting rods, and connecting rod one end is fixedly connected on fuselage
Side, the other end is connected with plastics plate；Described propeller is arranged on plastics plate so that propeller is symmetrically disposed in
The fuselage left and right sides.
Described fuselage head sets camera and searchlight, and fuselage upper end sets both wings breath light, and fuselage bottom is set
Alignment system emitter window and foot pad, fuselage are built-in with power module, satellite positioning navigation module, the sound electrically connected with control mainboard
Light-seeking system, sensor, photographing module, wireless module and storage module.Support mobile phone, two kinds of modes of operation of remote control, one
Key takes off and realizes that low electricity is maked a return voyage, lost contact is maked a return voyage, emergency stop function.Built-in satellite positioning navigation module, easily realizes indoor
Outer fixed high, fixed point, hovering.
Further, described propeller include paddle and spiral base, spiral chassis interior set motor, motor with
Control mainboard is electrically connected, and is started motor and is driven blade to rotate.
Further, described sensor includes three axle magnetic compasses, three-axis gyroscope, 3-axis acceleration sensor and air pressure
Sensor.
Further, described acousto-optic alignment system is by ultrasonic sensor and light stream sensor group into acousto-optic positioning skill
The use of art efficiently solves the problems, such as that interior cannot precisely hover and smooth flight.
Further, described photographing module is made up of image chip, imageing sensor, camera lens, and photo resolution reaches
14000000 pixels, video resolution reaches 1080P；Described camera lens is by 6 groups of glass lens, 1 infrared fileter composition.
Further, described wireless module is the double wireless modules of WIFI, 2.4G, and wireless module range of signal is 100 meters.
Further, described power module is 1600mAh lithium batteries, and described battery is arranged at the battery of fuselage interior
Box.
Further, described storage module is plug type storage module, and Android, IOS systems are supported in wireless video output
Mobile phone or flat board viewing preview, playback and the download recorded video storage of system.
Further, described satellite positioning navigation module includes gps satellite alignment system and GLONASS satellite navigation system
System.
The beneficial effects of the present invention are：
1. present invention design fashion is attractive in appearance, and succinct smooth integrated design, streamline fuselage effectively reduces air drag, increases
Strong flying quality；
2. the double global position systems of the built-in GPS GLONASS of fuselage, and installation acousto-optic alignment system solves interior cannot be accurate
Hovering and the problem of smooth flight；
3. fuselage two sides are respectively provided with two pairs of propellers, and propeller mount outside is additionally provided with blade guard circle, effectively lifting
Effect and safety coefficient of blade.
Brief description of the drawings
The present invention is described in further detail with specific embodiment mode below in conjunction with the accompanying drawings：
Accompanying drawing 1 is the stereochemical structure view of the embodiment of the present invention；
Accompanying drawing 2 is the system logic view of the embodiment of the present invention.
Specific embodiment
Embodiment
It is the dimensional structure diagram for the preferred embodiments of the invention shown in accompanying drawing 1, for one kind, nobody flies the present invention
Machine, including fuselage 1, propeller 2 and fuselage 1 be connected with propeller 2 together with connecting rod 3；Described propeller 2 at least sets
Be equipped with four, described propeller 2 includes blade 5 and spiral base 6, the motor 17 that the inside of spiral base 6 is set, motor 17 with
Control mainboard 12 is electrically connected, and is started motor 17 and is driven blade 5 to rotate.The chassis outer side of propeller 2 is additionally provided with the guard circle of blade 5,
Described connecting rod 3 sets at least to four groups, every group of at least two connecting rods 3, and the one end of connecting rod 3 is fixedly connected on fuselage 1
Side, the other end is connected with plastics plate 10；Described propeller 2 is arranged on plastics plate 10 so that propeller 2 is symmetrically
It is arranged on the body left and right sides of machine 1.
Shown in accompanying drawing 1 to accompanying drawing 2, the described head of fuselage 1 sets camera 8 and searchlight 9, and searchlight 9 was caused at night
Illumination is provided during late flight, the upper end of fuselage 1 sets both wings breath light 7, and the bottom of fuselage 1 sets alignment system emitter window and foot pad,
Fuselage 1 is built-in with power module 11, satellite positioning navigation module, acousto-optic alignment system 15, the biography electrically connected with control mainboard 12
Sensor 16, photographing module 18, wireless module 19 and storage module 20, described acousto-optic alignment system 15 by ultrasonic sensor and
Light stream sensor group is into the use of acousto-optic location technology efficiently solves the problems, such as that interior cannot precisely hover and smooth flight；
Described sensor 16 includes three axle magnetic compasses, three-axis gyroscope, 3-axis acceleration sensor and baroceptor；Photographing module
1 is made up of image chip, imageing sensor, camera lens, and photo resolution reaches 14,000,000 pixels, and video resolution reaches 1080P；
Described camera lens is by 6 groups of glass lens, 1 infrared fileter composition；Mobile phone, two kinds of modes of operation of remote control are supported, a key rises
Fly to realize that low electricity is maked a return voyage, lost contact is maked a return voyage, emergency stop function.Built-in satellite positioning navigation module, acousto-optic alignment system 15, gently
The fixed high, fixed point of the existing indoor and outdoor of pine nut, hovering.
More specifically, described wireless module 19 is the double wireless modules of WIFI, 2.4G, wireless module range of signal is 100
Rice.
More specifically, described power module 11 is 1600mAh lithium batteries, described battery is arranged inside fuselage 1
Battery case.
More specifically, described storage module 20 is plug type storage module, Android, IOS are supported in wireless video output
Mobile phone or flat board viewing preview, playback and the download recorded video storage of system.
More specifically, described satellite positioning navigation module includes gps satellite alignment system and GLONASS satellite navigation system
System
The built-in gps satellite alignment system 13 of unmanned aerial vehicle fuselage 1 of the present invention the double satellite navigation systems 14 of GLONASS, and be provided with
Acousto-optic alignment system 15, can outdoor flight indoors, solves the problems, such as indoor cannot precisely hover and smooth flight；Support hand
Machine, two kinds of modes of operation of remote control, manipulation distance is 500 meters, 120 meters of ceiling altitude, 100 meters of image transmitting distance, most
Big rate of climb 5m/s, maximum falling speed 5m/s, the m/s of maximum horizontal flying speed 13,1 hour charging interval can fly 15
Minute.
Certainly, illustrated above is only better embodiment of the present invention, not limits use scope of the invention with this, therefore,
It is every made in the principle of the invention it is equivalent change should be included within the scope of the present invention.
Claims (10)
1. a kind of unmanned aerial vehicle, including fuselage（1）, propeller（2）And fuselage（1）With propeller（2）The company being connected together
Extension bar（3）, it is characterised in that：Described propeller（2）At least provided with four, its propeller mount（6）Outside is additionally provided with
Blade（5）Guard circle（4）, described connecting rod（3）Set at least to four groups, every group of at least two connecting rods（3）, connecting rod
（3）One end is fixedly connected on fuselage（1）Side, the other end is connected to plastics plate（10）；Described propeller（2）Installed in modeling
Flitch block（10）On so that propeller（2）It is symmetrically disposed in fuselage（1）The left and right sides.
2. the fuselage described in（1）Head sets camera（8）And searchlight（9）, fuselage（1）Upper end sets both wings breath light（7）,
Fuselage（1）Bottom sets alignment system emitter window and foot pad, fuselage（1）It is built-in with and control mainboard（12）The power supply mould of electrical connection
Block（11）, satellite positioning navigation module, acousto-optic alignment system（15）, sensor（16）, photographing module（18）, wireless module（19）
And storage module（20）.
3. a kind of unmanned aerial vehicle according to claim 1, it is characterised in that：Described propeller（2）Including blade（5）And
Spiral base（6）, spiral base（6）The motor that inside is set（17）, motor（17）With control mainboard（12）Electrical connection.
4. a kind of unmanned aerial vehicle according to claim 1, it is characterised in that：Described sensor（16）Including three axle magnetic sieve
Disk, three-axis gyroscope, 3-axis acceleration sensor and baroceptor.
5. a kind of unmanned aerial vehicle according to claim 1, it is characterised in that：Described acousto-optic alignment system（15）By ultrasound
Wave sensor and light stream sensor group into.
6. a kind of unmanned aerial vehicle according to claim 1, it is characterised in that：Described photographing module（18）By image core
Piece, imageing sensor, camera lens composition.
7. a kind of unmanned aerial vehicle according to claim 1, it is characterised in that：Described wireless module（19）For WIFI,
The double wireless modules of 2.4G.
8. a kind of unmanned aerial vehicle according to claim 1, it is characterised in that：Described power module（11）It is 1600mAh
Lithium battery, described battery is arranged at the battery case of fuselage interior.
9. a kind of unmanned aerial vehicle according to claim 1, it is characterised in that：Described storage module（20）It is plug type
Storage module.
10. a kind of unmanned aerial vehicle according to claim 1, it is characterised in that：Described satellite positioning navigation module includes
Gps satellite alignment system（13）With GLONASS satellite navigation system（14）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610958300.XA CN106809379A (en) | 2016-11-03 | 2016-11-03 | A kind of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610958300.XA CN106809379A (en) | 2016-11-03 | 2016-11-03 | A kind of unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106809379A true CN106809379A (en) | 2017-06-09 |
Family
ID=59106771
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610958300.XA Withdrawn CN106809379A (en) | 2016-11-03 | 2016-11-03 | A kind of unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106809379A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107551568A (en) * | 2017-09-03 | 2018-01-09 | 佛山市海茂聚航科技有限公司 | A kind of study course four-axle aircraft of anticollision |
| CN108394563A (en) * | 2018-01-30 | 2018-08-14 | 谢幼环 | Automatic separation device of unmanned aerial vehicle parachute |
| CN109050889A (en) * | 2018-08-17 | 2018-12-21 | 陈霞 | A kind of unmanned plane of new-type freely adjustable protective device |
-
2016
- 2016-11-03 CN CN201610958300.XA patent/CN106809379A/en not_active Withdrawn
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107551568A (en) * | 2017-09-03 | 2018-01-09 | 佛山市海茂聚航科技有限公司 | A kind of study course four-axle aircraft of anticollision |
| CN108394563A (en) * | 2018-01-30 | 2018-08-14 | 谢幼环 | Automatic separation device of unmanned aerial vehicle parachute |
| CN109050889A (en) * | 2018-08-17 | 2018-12-21 | 陈霞 | A kind of unmanned plane of new-type freely adjustable protective device |
| CN109050889B (en) * | 2018-08-17 | 2021-08-20 | 陕西汇成天云智能科技有限公司 | New-type unmanned aerial vehicle that can freely adjust protector |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20170609 |
|
| WW01 | Invention patent application withdrawn after publication |