CN205707333U - A kind of four-axle aircraft - Google Patents
A kind of four-axle aircraft Download PDFInfo
- Publication number
- CN205707333U CN205707333U CN201620495038.5U CN201620495038U CN205707333U CN 205707333 U CN205707333 U CN 205707333U CN 201620495038 U CN201620495038 U CN 201620495038U CN 205707333 U CN205707333 U CN 205707333U
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- China
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- rotor
- upper cover
- aircraft
- camera lens
- machine body
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Abstract
This utility model is specifically related to a kind of four-axle aircraft, and including main machine body, rotor and the electric control gear being built in main machine body, described main machine body is connected as one by supporting and mounting bracket with rotor；Described main machine body is made up of upper cover and the lower cover that matches with upper cover, and upper cover constitutes a build-in cavities with lower cover, is equiped with and fixes the lens bracket being connected with upper cover, be equiped with camera lens module at the front end of described lens bracket in cavity at upper cover front end；A kind of four-axle aircraft of this utility model design, this aircraft is connected with smart device communication by WiFi, WiFi is utilized to transmit data, at smart machine, APP is installed, directly aircraft is controlled by APP interface, the front end of aircraft is provided with camera lens module and the wide-angle camera of high pixel, and aircraft has multi-functional and high stability, enriches the use function of aircraft simultaneously.
Description
Technical field
This utility model relates to a kind of flight equipment field, a kind of four-axle aircraft.
Background technology
At present, four-axle aircraft is a kind of most commonly seen multi-rotor aerocraft, and it is to install four at grade
The rotor that inclination angle is fixing, compared with traditional single-rotor helicopter, four-axle aircraft can use less rotor, so that flying
Row becomes safer, and the thrust that the more single rotor of thrust of four rotor generations produces can preferably realize aircraft
Static state is spiraled.
Four-axle aircraft, produces the lift needed for aircraft flight by the rotating speed size changing four rotors and moment of torsion comes
Realize sustained turn and accurate flying, in terms of kinestate, four-axle aircraft there is space six-freedom degree and four controlled
Basic exercise state, four basic exercise states are respectively vertical flight, Longitudinal Flight, horizontal flight and horizontally rotate, existing
Most aircraft all can only realize simply flying, and is manipulated aircraft by control handle, and do not possess and be wirelessly transferred
Function.
Therefore, it is necessary to propose a kind of technical scheme, this Technical Design one four-axle aircraft, four-axle aircraft leads to
Cross Radio Transmission Technology and make aircraft and smart machine wireless connections, thus realize smart machine manipulation aircraft and image biography
Defeated, shooting.
Summary of the invention
(1) to solve the technical problem that
For disadvantage mentioned above, the utility model proposes a kind of technical scheme, this Technical Design effectively solves existing skill
Some defects in art, thus a kind of four-axle aircraft is provided.
(2) technical scheme
For solving above-mentioned technical problem, a kind of four-axle aircraft described in this utility model offer, including main machine body, rotor
And the electric control gear being built in main machine body, described main machine body is connected as one by supporting and mounting bracket with rotor；Described master
Fuselage is made up of upper cover and the lower cover that matches with upper cover, and upper cover constitutes a build-in cavities with lower cover, in cavity before upper cover
It is equiped with at end and fixes the lens bracket being connected with upper cover, at the front end of described lens bracket, be equiped with camera lens module；
Described rotor includes the rotating forward motor being installed in rotor and reverse motor and is arranged on rotating forward motor and reversion
Blade on motor, the rotary shaft of blade passes rotor top, and blade is placed in the upper end of rotor；
Described electric control gear is installed in the cavity between upper cover and lower cover, and electric control gear includes mainboard, WiFi plate, battery
Assembly, described battery component is powered to electric control gear and rotor.
Further, the top of described upper cover is provided with top cover, is provided with camera lens protecgulum at the front lens module of upper cover, described
Camera lens module is made up of high pixel camera lens sum word image stabilization system.
Further, described rotor is provided with LED, and the lampshade material of described LED uses transparent ABS material.
Further, described electric control gear is provided with six axle gyroscopes, the fixed high module of barometer and compass, the fixed height of barometer
Module sets takes off preset height, and described battery component is provided with battery protection cover.
Further, the material of described upper cover and lower cover uses ABS+PS material, and ABS+PS material is by ABS material and PS material
Material mixes, and the material of described camera lens protecgulum, lens bracket, top cover and battery protection cover uses ABS material.
Further, the material of described blade uses turning property PS material.
Further, the low side of described rotor is provided with callosity, and it is anti-that the inside of rotor is provided with motor bump protection ring, callosity and motor
The material of shake circle uses silica gel material.
The beneficial effects of the utility model are:
A kind of four-axle aircraft of this utility model design, this aircraft is connected with smart device communication by WiFi, utilizes
WiFi transmission data and video, installed APP at smart machine, be directly controlled aircraft by APP interface, aircraft
Front end is provided with camera lens module and the wide-angle camera of high pixel, in the image real-time storage that can be arrived by captured in real-time to fuselage
Depositing or real-time Transmission is to App, aircraft has multi-functional and high stability, enriches the use function of aircraft simultaneously.
Accompanying drawing explanation
Fig. 1 is the system structure schematic diagram of a kind of four-axle aircraft of this utility model preferred embodiment；
Wherein, 1, main machine body, 2, rotor, 3, electric control gear, 4, supporting and mounting bracket, 5, upper cover, 6, lower cover, 7, top cover, 8,
Camera lens protecgulum, 9, lens bracket, 10, camera lens module, 11, rotate forward motor, 12, reverse motor, 13, blade, 14, mainboard, 15,
WiFi plate, 16, battery component, 17, battery protection cover, 18, LED, 19, callosity, 20, motor bump protection ring.
Detailed description of the invention
For making the purpose of this utility model, technical scheme and advantage of greater clarity, below in conjunction with detailed description of the invention
And referring to the drawings, this utility model is further described.It should be understood that these describe the most exemplary, and do not really want
Limit scope of the present utility model.Additionally, in the following description, the description to known features and technology is eliminated, to avoid not
Obscure concept of the present utility model necessarily.
With reference to shown in Fig. 1, a kind of four-axle aircraft, including main machine body 1, rotor 2 and be built in main machine body 1 automatically controlled
Device 3, described main machine body 1 is connected as one by supporting and mounting bracket 4 with rotor 2；Described main machine body 1 is by upper cover 5 and with upper
The lower cover 6 that lid 5 matches is constituted, and upper cover 5 and lower cover 6 constitute a build-in cavities, are equiped with upper in cavity at upper cover 5 front end
The fixing lens bracket 9 connected of lid 5, is equiped with camera lens module 10 at the front end of described lens bracket 9；
Described rotor 2 includes the rotating forward motor 11 being installed in rotor 2 and reverse motor 12 and is arranged on rotating forward motor
11 and reverse motor 12 on blade 13, the rotary shaft of blade 13 pass rotor 2 top, blade 13 is placed in the upper end of rotor 2；
Described electric control gear 3 is installed in the cavity between upper cover 5 and lower cover 6, and electric control gear 3 includes mainboard 14, WiFi
Plate 15, battery component 16, described battery component 16 is powered to electric control gear 3 and rotor 2.
Described rotor 2 is provided with LED 18, and the lampshade material of described LED 18 uses transparent ABS material；Described automatically controlled
Device 3 is provided with six axle gyroscopes, the fixed high module of barometer and compass, and the fixed high module sets of barometer takes off preset height, institute
State battery component 16 and be provided with battery protection cover 17；The material of described upper cover 5 and lower cover 6 uses ABS+PS material, described camera lens
The material of protecgulum 8, lens bracket 9, top cover 7 and battery protection cover 17 uses ABS material；The material of described blade 13 uses turning property
PS material；The low side of described rotor 2 is provided with callosity 19, and the inside of rotor 2 is provided with motor bump protection ring 20, and callosity 19 and motor are shockproof
The material of circle 20 uses silica gel material.
The top of described upper cover 5 is provided with top cover 7, is provided with camera lens protecgulum 8, described mirror at the front lens module 10 of upper cover 5
Head mould group 10 is made up of high pixel camera lens sum word image stabilization system；Camera lens uses 115 Radix Rumiciss, a diameter of 18mm, and 3,000,000
Pixel A R0330 Sensor.
Rotate forward motor 11 and reverse motor 12 and driven four groups of motors by PWM, control flight attitude and the height of product；Built-in
The fixed high function of barometer, degree of accuracy need to control within ± 10CM, and the built-in compass of product can lock heading and make a return voyage
(degree of accuracy ± 2 meter)；Using Micro USB port to be charged, within charging current is limited in 1A, the battery for 700mAh fills
Electricity, the deadline should be within 1 hour；
Described battery component 16 is made up of 700mAh 20C lithium battery, uses plastic shell to be packaged, can plug,
Charging interval should be less than 45 minutes；Need to insert fuselage battery compartment rear can charge, during charging, mainboard 14 sends out a warning, and is full of viride nitens
Lamp；Single battery uses the time to be not less than 7 minutes；
Function describes: this utility model is a to be shot for the four-axle aircraft of major function, uses WIFI to connect, makes
With APP manipulation flight and shooting, camera lens module 10 is the Sensor of 3,000,000 pixels, carries digital image stabilization system, connect away from
From more than 50 meters, product is suitable for indoor and outdoor and uses, specific as follows: 1. use 4*8520 motor, directly push away 66mm blade 13, promote
Product flies, and the flight time is about 6-7 minute；2. the built-in six axle gyroscopes of product；3. the fixed high module of the built-in barometer of product,
There is a key to take off to default height (2m ± 10CM), and be stably maintained at current altitude, until promoting throttle at APP
Button changes current height.4. the built-in compass of product, can lock heading and make a return voyage (degree of accuracy ± 2 meter),
APP sets Headless mode/free flight pattern.5. product has preposition 3,000,000 pixel wide-angle photographic head, can shoot maximum
Photograph 12M(4M/8M/12M) and 1080P(1080P 30FPS/720P 30FPS/720P 60FPS) video, camera lens
Sensor carries image stabilization system, shoots photograph or the video of more preferably quality, product tape while four axles self fly
Micro SD draw-in groove, can be saved in the photograph of shooting and video in SD card in real time.6. product built-in WIFI AP, can make
Connect product by the WIFI signal of smart mobile phone/panel computer, after entering APP, control flight and shooting, and can be by SD card internal memory
The file download of storage stores to APP.7.APP can (video size be as 640* with real time inspection product camera lens live view video
480), the photograph of shooting synchronizes to store to SD card and APP, and video only stores and exists in SD card, preserves thumbnail in APP, permissible
Preview, it is possible to foradownloaded video to APP；In the range of 30 meters, time delay cannot be greater than 300ms, and signal connects distance not lower than
50 meters.8. the built-in pluggable plastic packaging lithium battery of product, battery capacity is 700mAh 20C, uses Micro USB port to carry out
Charging (is charged for battery, battery need to be pushed completely into product battery compartment).
It should be appreciated that above-mentioned detailed description of the invention of the present utility model is used only for exemplary illustration or explains this reality
By novel principle, and do not constitute restriction of the present utility model.Therefore, without departing from spirit and scope of the present utility model
In the case of any modification, equivalent substitution and improvement etc. done, within should be included in protection domain of the present utility model.Additionally,
This utility model claims are intended to fall into scope and border or this scope and border
Whole in equivalents change and modifications example.
Claims (7)
1. a four-axle aircraft, including main machine body, rotor and the electric control gear being built in main machine body, described main machine body with
Rotor is connected as one by supporting and mounting bracket；It is characterized in that: described main machine body is by upper cover and under matching with upper cover
Lid is constituted, and upper cover constitutes a build-in cavities with lower cover, is equiped with and fixes the camera lens being connected with upper cover in cavity at upper cover front end
Support, is equiped with camera lens module at the front end of described lens bracket；
Described rotor includes the rotating forward motor being installed in rotor and reverse motor and is arranged on rotating forward motor and reverse motor
On blade, the rotary shaft of blade pass rotor top, blade is placed in the upper end of rotor；
Described electric control gear is installed in the cavity between upper cover and lower cover, and electric control gear includes mainboard, WiFi plate, set of cells
Part, described battery component is powered to electric control gear and rotor.
A kind of four-axle aircraft the most according to claim 1, it is characterised in that the top of described upper cover is provided with top cover, on
Being provided with camera lens protecgulum at the front lens module of lid, described camera lens module is by high pixel camera lens sum word image stabilization system group
Become.
A kind of four-axle aircraft the most according to claim 1, it is characterised in that described rotor is provided with LED, described
The lampshade material of LED uses transparent ABS material.
A kind of four-axle aircraft the most according to claim 1, it is characterised in that described electric control gear is provided with six axle gyros
The fixed high module of instrument, barometer and compass, the fixed high module sets of barometer takes off preset height, and described battery component is provided with electricity
Pond protective cover.
A kind of four-axle aircraft the most according to claim 1, it is characterised in that described camera lens protecgulum, lens bracket, top cover
ABS material is used with the material of battery protection cover.
A kind of four-axle aircraft the most according to claim 1, it is characterised in that the material of described blade uses turning property PS material
Material.
A kind of four-axle aircraft the most according to claim 1, it is characterised in that the low side of described rotor is provided with callosity, rotation
The inside of the wing is provided with motor bump protection ring, and the material of callosity and motor bump protection ring uses silica gel material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620495038.5U CN205707333U (en) | 2016-05-27 | 2016-05-27 | A kind of four-axle aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620495038.5U CN205707333U (en) | 2016-05-27 | 2016-05-27 | A kind of four-axle aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205707333U true CN205707333U (en) | 2016-11-23 |
Family
ID=57299747
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620495038.5U Expired - Fee Related CN205707333U (en) | 2016-05-27 | 2016-05-27 | A kind of four-axle aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205707333U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018209770A1 (en) * | 2017-05-19 | 2018-11-22 | 深圳市大疆创新科技有限公司 | Barometer assembly and drone |
| CN109383776A (en) * | 2017-08-02 | 2019-02-26 | 百润红科技有限公司 | H.D unmanned plane is determined with air pressure |
-
2016
- 2016-05-27 CN CN201620495038.5U patent/CN205707333U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018209770A1 (en) * | 2017-05-19 | 2018-11-22 | 深圳市大疆创新科技有限公司 | Barometer assembly and drone |
| CN109843717A (en) * | 2017-05-19 | 2019-06-04 | 深圳市大疆创新科技有限公司 | Barometer component and unmanned plane |
| CN109843717B (en) * | 2017-05-19 | 2021-11-26 | 深圳市大疆创新科技有限公司 | Barometer subassembly and unmanned aerial vehicle |
| CN109383776A (en) * | 2017-08-02 | 2019-02-26 | 百润红科技有限公司 | H.D unmanned plane is determined with air pressure |
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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: 20161123 Termination date: 20170527 |