CN205632002U - Empty four dual -purpose rotor unmanned aerial vehicle in land - Google Patents
Empty four dual -purpose rotor unmanned aerial vehicle in land Download PDFInfo
- Publication number
- CN205632002U CN205632002U CN201620480899.6U CN201620480899U CN205632002U CN 205632002 U CN205632002 U CN 205632002U CN 201620480899 U CN201620480899 U CN 201620480899U CN 205632002 U CN205632002 U CN 205632002U
- Authority
- CN
- China
- Prior art keywords
- horn
- suspension bracket
- motor
- control chamber
- propeller
- 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.)
- Expired - Fee Related
Links
Landscapes
- Toys (AREA)
Abstract
The utility model relates to an aircraft flight power machinery field, concretely relates to empty four dual -purpose rotor unmanned aerial vehicle in land, it includes the control box its characterized in that, and the control box is the hollow circular cylinder form and can accepts and handle the signal that outside remote control was sent, and control box curved wall center department follows the circumferencial direction and evenly links to each other with four horizontal horn one end are fixed, the horn outside is served surperficial department and all is fixed with a screw motor, all installs a screw on the motor shaft of screw motor, and every horn lower surface locates all to be equipped with a servo motor near the control box and servo motor passes through the motor shaft and the gallows is fixed continuous, the gallows has two, and two gallowss present in the hope of being improved distributing, and the gallows is the L type, can rotate to control box center vertical line one side in servo motor's drive two lower gallows bottoms. The utility model discloses can realize that the land is empty dual -purpose, richen traditional four rotor unmanned aerial vehicle's function, satisfy people's demand more.
Description
[technical field]
This utility model relates to aviation flight field of power machinery, more particularly to a kind of land and air double-used four rotor wing unmanned aerial vehicles.
[background technology]
Unmanned plane is liked by people widely at present, in life, when four general rotor wing unmanned aerial vehicles in execution task or are entertained for people,
Can only aloft fly, and can not walk on the ground, thus waste electric energy, reduce quadrotor flying power, also reduce its joy
Happy property.Existing quadrotor is when delivering article, and the general mode using hook or the clamping of simple mechanical arm delivers article, have impact on and flies
Stability during row device flight and safety, the experience brought inconvenience to people.
[utility model content]
The technical problems to be solved in the utility model is to provide a kind of land and air double-used four rotor wing unmanned aerial vehicles, and it is possible not only to aloft fly, also may be used
To walk on the ground, also there is the function of safe carriage article simultaneously, increase the flying power of unmanned plane, the merit of abundant traditional four rotor wing unmanned aerial vehicles
Can, more meet the demand of people.
In order to achieve the above object, the technical scheme that this utility model provides is: a kind of land and air double-used four rotor wing unmanned aerial vehicles, it is characterised in that it
Including horn, propeller, propeller motor, control chamber, servomotor, suspension bracket, universal wheel；Described control chamber is hollow cylindrical, control chamber
Can accept and process the signal that external remote control sends, control chamber curved wall center is along the circumferential direction uniformly fixedly linked with four horizontal horn one end,
Angle between adjacent horn is 90 degree, is respectively and fixedly provided with a propeller motor, the motor shaft of propeller motor is respectively mounted at horn outboard end upper surface
A propeller, each horn lower surface is had to be equipped with a servomotor at control chamber；Described suspension bracket has two, the top of one of them suspension bracket with
The motor shaft of two servomotors at adjacent two horn lower surfaces is fixedly linked, at the horn lower surface adjacent with another two of the top of another suspension bracket
The motor shaft of two servomotors be fixedly linked, under the drive of servomotor, two suspension bracket bottoms can rotate to control chamber central vertical line side,
Two suspension brackets are in just to distribution, and suspension bracket is L-shaped, and suspension bracket bottom is to control chamber central vertical line one lateral buckling, and suspension bracket bottom is all in Openworks shape, often
At vertical dual-side, a vertical universal wheel all it is respectively provided with on individual suspension bracket.
The beneficial effects of the utility model are: this utility model is possible not only to aloft fly, it is also possible to walk on the ground, also have simultaneously
The function of safe carriage article, increases the flying power of unmanned plane, the function of abundant traditional four rotor wing unmanned aerial vehicles, more meets the demand of people.
[accompanying drawing explanation]
With embodiment, this utility model is further illustrated below in conjunction with the accompanying drawings.
Fig. 1 is structural representation of the present utility model.
Wherein, 1-horn, 2-propeller, 3-propeller motor, 4-control chamber, 5-servomotor, 6-suspension bracket, 7-universal wheel.
[detailed description of the invention]
In example shown in the drawings, a kind of land and air double-used four rotor wing unmanned aerial vehicles, it is characterised in that it includes horn, propeller, propeller electricity
Machine, control chamber, servomotor, suspension bracket, universal wheel；Described control chamber is hollow cylindrical, and control chamber can accept and process what external remote control sent
Signal, control chamber curved wall center is along the circumferential direction uniformly fixedly linked with four horizontal horn one end, and the angle between adjacent horn is 90 degree,
It is respectively and fixedly provided with a propeller motor at horn outboard end upper surface, the motor shaft of propeller motor is mounted on a propeller, each horn lower surface
It is equipped with a servomotor at control chamber；Described suspension bracket has two, the top of one of them suspension bracket and two at adjacent two horn lower surfaces
The motor shaft of servomotor is fixedly linked, and the motor shaft of two servomotors at the horn lower surface adjacent with another two of the top of another suspension bracket is fixed
Being connected, under the drive of servomotor, two suspension bracket bottoms can rotate to control chamber central vertical line side, two suspension brackets in just to distribution, suspension bracket in
L-type, and suspension bracket bottom is to control chamber central vertical line one lateral buckling, suspension bracket bottom is all in Openworks shape, equal at vertical dual-side on each suspension bracket
It is respectively provided with a vertical universal wheel.
When using this utility model, switching on power, propeller electric machine rotation also drives propeller to rotate, thus is produced upwards by propeller
Lift, people can give this utility model indication signal by remote-control transmitting end, makes this utility model aloft fly by the purpose of manipulator, this
Outer this utility model can also roll walking on the ground by the universal wheel on suspension bracket, saves the electricity that flight consumes, and increases flying power；Work as people
Want with this utility model delivery article time, can by control private take motor by suspension bracket bottom to control chamber central vertical line side rotate, and then produce
The crawl campaign of raw mechanical arm type, thus by article clip in the middle of suspension bracket.This utility model is possible not only to aloft fly, it is also possible to go on the ground
Walk, also there is the function of safe carriage article simultaneously, increase the flying power of unmanned plane, enrich the function of traditional four rotor wing unmanned aerial vehicles, more satisfied
The use demand of people.
Claims (1)
1. land and air double-used four rotor wing unmanned aerial vehicles, it is characterised in that it include horn, propeller, propeller motor, control chamber, servomotor,
Suspension bracket, universal wheel；Described control chamber is hollow cylindrical, and control chamber can accept and process the signal that external remote control sends, control chamber curved wall center
Place is along the circumferential direction uniformly fixedly linked with four horizontal horn one end, and the angle between adjacent horn is 90 degree, the most solid at horn outboard end upper surface
Surely having a propeller motor, the motor shaft of propeller motor is mounted on a propeller, each horn lower surface is equipped with one at control chamber and watches
Take motor；Described suspension bracket has two, and phase is fixed with the motor shaft of two servomotors at adjacent two horn lower surfaces in the top of one of them suspension bracket
Even, the motor shaft of two servomotors at the horn lower surface adjacent with another two of the top of another suspension bracket is fixedly linked, in the drive of servomotor
Lower two suspension bracket bottoms can rotate to control chamber central vertical line side, and two suspension brackets are in just to distribution, and suspension bracket is L-shaped, and suspension bracket bottom is to control
Case central vertical line one lateral buckling, suspension bracket bottom, all in Openworks shape, each suspension bracket is all respectively provided with a vertical universal wheel at vertical dual-side.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620480899.6U CN205632002U (en) | 2016-05-20 | 2016-05-20 | Empty four dual -purpose rotor unmanned aerial vehicle in land |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620480899.6U CN205632002U (en) | 2016-05-20 | 2016-05-20 | Empty four dual -purpose rotor unmanned aerial vehicle in land |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205632002U true CN205632002U (en) | 2016-10-12 |
Family
ID=57052099
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620480899.6U Expired - Fee Related CN205632002U (en) | 2016-05-20 | 2016-05-20 | Empty four dual -purpose rotor unmanned aerial vehicle in land |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205632002U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106892098A (en) * | 2017-03-13 | 2017-06-27 | 广东工业大学 | A kind of fence type loading unmanned plane |
| CN107639983A (en) * | 2017-10-10 | 2018-01-30 | 南京工程学院 | A kind of land and air double-used quadrotor |
| CN109999515A (en) * | 2019-04-26 | 2019-07-12 | 西北工业大学明德学院 | A kind of multi-functional quadrotor |
| CN113370729A (en) * | 2021-07-08 | 2021-09-10 | 河北工业大学 | Air-ground deformable four-footed reconnaissance robot |
| CN114537065A (en) * | 2022-02-28 | 2022-05-27 | 重庆交通大学 | Air-ground dual-purpose multifunctional unmanned aerial vehicle |
-
2016
- 2016-05-20 CN CN201620480899.6U patent/CN205632002U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN107639983A (en) * | 2017-10-10 | 2018-01-30 | 南京工程学院 | A kind of land and air double-used quadrotor |
| CN109999515A (en) * | 2019-04-26 | 2019-07-12 | 西北工业大学明德学院 | A kind of multi-functional quadrotor |
| CN113370729A (en) * | 2021-07-08 | 2021-09-10 | 河北工业大学 | Air-ground deformable four-footed reconnaissance robot |
| CN113370729B (en) * | 2021-07-08 | 2022-04-08 | 河北工业大学 | Air-ground deformable four-footed reconnaissance robot |
| CN114537065A (en) * | 2022-02-28 | 2022-05-27 | 重庆交通大学 | Air-ground dual-purpose multifunctional unmanned aerial vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205632002U (en) | Empty four dual -purpose rotor unmanned aerial vehicle in land | |
| CN204822090U (en) | Unmanned aerial vehicle | |
| CN204895855U (en) | Many rotors of oil -electricity hybrid vehicle unmanned vehicles | |
| CN204979218U (en) | Many rotors of oil -electricity hybrid vehicle unmanned vehicles | |
| CN102285449A (en) | Coaxial double-rotor wing ducted aircraft | |
| CN204802086U (en) | Single -person aircraft | |
| CN105109677A (en) | Composite aircraft composed of fixed wings and multi-rotary wings and control method of composite aircraft | |
| CN205396531U (en) | Electric control oil moves many rotor unmanned aerial vehicle | |
| CN107161334A (en) | A kind of flapping wing helicopter | |
| CN108516084B (en) | Unmanned aerial vehicle | |
| CN206750143U (en) | A kind of electronic compound rotor aircraft | |
| CN205044954U (en) | Coaxial two thick liquid hybrid gyroplane | |
| CN205022854U (en) | Deformable compound aircraft | |
| CN204895853U (en) | Compound aircraft that stationary vane and deformable electronic many rotors are constituteed | |
| CN213168519U (en) | Air-ground dual-purpose unmanned aerial vehicle | |
| CN203958614U (en) | Integral type multi-rotor aerocraft | |
| CN204895856U (en) | Many rotors of oil -electricity hybrid vehicle unmanned vehicles | |
| CN205273856U (en) | Multiaxis horn pesticide sprinkling system | |
| CN205168896U (en) | Horizontal acceleration rate system of gyroplane | |
| CN103043211A (en) | Vertically lifting aircraft | |
| CN106986005A (en) | A kind of structure of verting of the dynamic tilt rotor aircraft of oil | |
| CN205396527U (en) | Many heligyro of letter way formula power | |
| CN205589510U (en) | Novel unmanned aerial vehicle sprays insecticide | |
| CN202219839U (en) | Omnidirectional flight wing structure of vertically taking-off and landing aircraft | |
| CN205554583U (en) | Multi -functional rotor craft |
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 |
Granted publication date: 20161012 Termination date: 20170520 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |