CN209471376U - A kind of UAV Flight Control device and unmanned plane - Google Patents
A kind of UAV Flight Control device and unmanned plane Download PDFInfo
- Publication number
- CN209471376U CN209471376U CN201920545367.XU CN201920545367U CN209471376U CN 209471376 U CN209471376 U CN 209471376U CN 201920545367 U CN201920545367 U CN 201920545367U CN 209471376 U CN209471376 U CN 209471376U
- Authority
- CN
- China
- Prior art keywords
- shell
- mainboard
- control device
- uav flight
- flight control
- 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.)
- Active
Links
Landscapes
- Selective Calling Equipment (AREA)
Abstract
The utility model discloses a kind of UAV Flight Control device and unmanned plane.UAV Flight Control device includes: shell, mainboard, remote-control receiver, data radio station and water-proof connector；Interior of shell includes closed cavity, and side wall is equipped with connecter hole；Mainboard is mounted in the cavity of shell, and mainboard, which is fixedly connected with, flies control module；Remote-control receiver is mounted in the cavity of shell, and remote-control receiver connects mainboard, and the antenna of remote-control receiver is located at the outside of shell；Data radio station is mounted in the cavity of shell, and data radio station connects mainboard, and the antenna of data radio station is located at the outside of shell；Water-proof connector is fixed on the outer wall of shell, covers connecter hole, and water-proof connector connects mainboard.The UAV Flight Control device of the utility model, has the function of waterproof, can simplify the structure of unmanned plane.
Description
Technical field
The utility model belongs to aircraft field more particularly to a kind of UAV Flight Control device and unmanned plane.
Background technique
Unmanned machine operation will carry out in the rain in many cases small, and plant protection drone operation needs that pesticide is avoided to invade
Electronic equipment damages.Existing unmanned plane mostly uses greatly the form of equipment compartment waterproof, i.e., integrally carries out the shell of unmanned plane
Waterproofing design.It is larger that such design will cause aircraft weight, influences cruise duration.
The dynamical system of unmanned plane, such as cable, brushless motor, electron speed regulator and propeller can itself waterproofs.
Many unmanned aerial vehicle onboard task devices also have the function of water proof equipment, such as gondola, pesticide spraying system etc..If airborne core
Control device can itself waterproof, then aircraft monolithic case can not consider using totally enclosed waterproofing design.
Utility model content
To solve the above-mentioned problems, the utility model proposes a kind of UAV Flight Control device and unmanned planes, and flight is controlled
The associated components of system are integrated in the controller, and the shell of controller uses waterproofing design, and unmanned plane is allowed to be exposed to water mist
In.
The utility model provides a kind of UAV Flight Control device, comprising:
Shell, the interior of shell include closed cavity, and side wall is equipped with connecter hole；
Mainboard is mounted in the cavity of the shell, and the mainboard, which is fixedly connected with, flies control module；
Remote-control receiver is mounted in the cavity of the shell, and the remote-control receiver connects the mainboard, the remote control
The antenna of receiver is located at the outside of the shell；
Data radio station is mounted in the cavity of the shell, and the data radio station connects the mainboard, the data radio station
Antenna be located at the outside of the shell；
Water-proof connector, the water-proof connector are fixed on the outer wall of the shell, cover the connecter hole, described
Water-proof connector connects the mainboard.
As the optional scheme of the utility model, the shell includes upper casing and lower casing, and the upper casing and lower casing, which are fixed, to be connected
It connects to form the cavity.
As the optional scheme of the utility model, UAV Flight Control device further includes position module, the position module
Through-hole seal closure installs the upper surface of the shell, and the position module is connect with the mainboard.
As the optional scheme of the utility model, the water-proof connector is located at the front of the winged control module, the number
The platform that conducts electricity is located at the rear of the winged control module.
As the optional scheme of the utility model, the antenna amount of the remote-control receiver is two, is located at described
The two sides of water-proof connector.
As the optional scheme of the utility model, UAV Flight Control device further includes data card slot, the data card slot
It in the cavity of the shell, is connect with the mainboard, data card is installed in the data card slot.
As the optional scheme of the utility model, UAV Flight Control device further includes wide piezoelectricity source module, the wide pressure
Power module is located in the cavity of the shell, and the width piezoelectricity source module connects the water-proof connector and mainboard.
As the optional scheme of the utility model, the remote-control receiver is located at the lower section of the mainboard.
As the optional scheme of the utility model, the shell is equipped with USB interface, and the USB interface connects the master
Plate.
The utility model also provides a kind of unmanned plane, which includes above-mentioned UAV Flight Control device.
The UAV Flight Control device and unmanned plane of the utility model are made by carrying out waterproofing design to flight controller
Obtaining unmanned plane has water-proof function, can be rinsed with water；The hardware configuration for simplifying unmanned plane, avoids to unmanned plane
Shell is sealed waterproof, convenient for the maintenance of unmanned plane；Unmanned plane cable arrangements are simplified, flight is integrated in flight controller
Associated components are controlled, reduction conducting wire is exposed, improves the reliability of unmanned plane.
Detailed description of the invention
Fig. 1 is the structure chart of the utility model embodiment UAV Flight Control device.
Fig. 2 is the explosive view of the utility model embodiment UAV Flight Control device.
Specific embodiment
Below in conjunction with drawings and examples, specific embodiment of the present utility model is described in more details, with
Just the advantages of better understood when the embodiment of the utility model and its various aspects.However, specific implementations described below side
Formula and embodiment are for illustrative purposes only, rather than limitations of the present invention.
" connection " described in the utility model unless otherwise specific regulation or limits, should broadly understood, can be
It is connected directly, is also possible to be connected by intermediary or be electrically connected.In the description of the present invention, it is understood that
It is that the orientation or positional relationship of the instructions such as "upper", "lower", "front", "rear", "left", "right", " top ", " bottom end " is based on attached
Orientation or positional relationship shown in figure, is merely for convenience of describing the present invention and simplifying the description, rather than indication or suggestion
Signified device or element must have a particular orientation, be constructed and operated in a specific orientation, therefore should not be understood as to this
The limitation of utility model.
As illustrated in fig. 1 and 2, the utility model embodiment provides a kind of UAV Flight Control device, comprising: shell 1, mainboard
2, remote-control receiver 3, data radio station 4, water-proof connector 5.Flight controller is integrated with the associated components of control unmanned plane during flying.
It include closed cavity inside shell 1, cavity is for placing other component.Shell 1 is metalwork, and shape is similar to
Cuboid is protected convenient for waterproof and to internal part.The side wall of shell 1 is equipped with connecter hole 13, and connecter hole 13 is used
In installation water-proof connector.
Mainboard 2 is mounted in the cavity of shell 1, and mainboard, which is fixedly connected with, flies control module 21.Fly control module 21 for receiving
The signal of other component controls the flight of unmanned plane, such as controls nobody landing, direction of advance, flying speed.
Remote-control receiver 3 is mounted in the cavity of shell 1, and remote-control receiver 3 connects mainboard 2.Preferably, remote-control receiver
3 are fixed on mainboard 2, and remote-control receiver 3 is connect by mainboard 2 with control module 21 is flown.Remote-control receiver 3 is for receiving remote controler
Signal, and the signal received is sent to and flies control module 21, fly control module 21 according to the signal of remote controler to adjusting nobody
The flight of machine.The antenna 31 of remote-control receiver passes through SMA(Sub-Miniature-A) connector is mounted on the outside of shell 1, SMA
The junction of connector and shell 1 is sealed, and prevents leak, and sub-miniature A connector is waterproof connector.Remote-control receiver will by patchcord
Coaxial signal is connected to the sub-miniature A connector on shell.
Data radio station 4 is mounted in the cavity of shell 1, and data radio station 4 connects mainboard 2.Data radio station 4 is for emitting, connecing
Data information is received, the data information includes image information.In an other embodiment, the data radio station 4 can also be used to connect
Remote controler information is received, in this embodiment, remote-control receiver 3 can be alternative.Preferably, data radio station 4 can be fixed on mainboard 2
On, data radio station 4 is connect by mainboard 2 with control module 21 is flown.The antenna 41 of data radio station is mounted on shell 1 by sub-miniature A connector
Outside, the junction of sub-miniature A connector and shell 1 is sealed, and prevents leak.
Water-proof connector 5 is fixed on the outer wall of shell 1, covers connecter hole 13, and the partial insertion of water-proof connector 5 connects
In device hole 13.Water-proof connector 5 connects mainboard 2, and the connection of flight controller and external power supply and the transmission of wire signal are logical
Cross the progress of water-proof connector 5.The external wired input of the flight controller of the present embodiment and output by water-proof connector 5 into
Row simplifies cable design, and reduction conducting wire is exposed, improves the waterproof performance of unmanned plane.
Optionally, shell 1 includes upper casing 11 and lower casing 12, and upper casing 11 and lower casing 12 are fixed by screw, and upper casing 11 is under
The connection of shell 12 forms cavity.Semicircular hole is offered on upper casing 11 and lower casing 12, upper casing 11 and lower casing 12 connect, the company of being formed
Connect device hole 13.
Optionally, UAV Flight Control device further includes position module 6.Position module 6 is in real time carrying out unmanned plane
Positioning, position module 6 are connect with mainboard 2, are sent position signal to by mainboard 2 and are flown control module 21.The position of the present embodiment
Module 6 is GPS module, and GPS module needs to receive satellite-signal, so being placed on the surface of entire flight controller.Because of GPS
Module antenna cannot block, and you must use an independent cabin.6 through-hole seal closure 61 of position module installs the upper of shell 1
Surface, the material of seal closure 61 are plastics, and plastics will not influence position module 6 and receive signal, and can block water mist.Position module
The shell 1 of 6 lower sections is metal material, it is ensured that other devices are completely in the range of metallic shield.
In the present embodiment, for the space in 1 cavity of reasonable arrangement shell, mainboard 2 is arranged in the middle of cavity.Fly
Control module 21 is mounted on the top of mainboard 2, and water-proof connector 5 and the line of mainboard 2 are more, to reduce electric wire the space occupied,
Water-proof connector 5 is located at the front for flying control module 21.5 occupied space of data radio station is larger, is mounted on after flying control module 21
Side.
Optionally, 31 quantity of antenna of remote-control receiver is two, is located at the two sides of water-proof connector 5.In this way may be used
The connection electric wire of the antenna 31 of remote-control receiver is set to connect the remaining space of electric wire using water-proof connector 5.
It is easily installed for the ease of the antenna 31 of remote-control receiver, the antenna 31 of remote-control receiver need to be mounted on lower casing 12
Near bottom surface, so remote-control receiver 3 to be arranged in the lower section of mainboard 2.
In the present embodiment, UAV Flight Control device further includes data card slot (not shown), and data slot is in outer
It in the cavity of shell, is connect with mainboard, data card is installed in data card slot.Data card can be TF data card, for recording nothing
Man-machine operation data.
Optionally, UAV Flight Control device further includes wide piezoelectricity source module (not shown), wide piezoelectricity source module position
In in the cavity of shell, wide piezoelectricity source module connects water-proof connector and mainboard.The power supply of external power supply passes through water-proof connector
It is transmitted to wide piezoelectricity source module, is transmitted to mainboard later, mainboard is powered according to the demand assignment of all parts.The width of the present embodiment
Piezoelectricity source module is 60V wide voltage source.
In the present embodiment, shell 1 is equipped with USB interface, and USB interface connects 2 mainboards.USB interface is for carrying out unmanned plane
Debugging and flying quality downloading.Preferably, USB interface is Mini USB interface, is protected using serum cap, can be with waterproof.
The utility model embodiment also provides a kind of unmanned plane, which includes above-mentioned UAV Flight Control device.
The UAV Flight Control device and unmanned plane of the present embodiment, flight controller are integrated with flight and control relevant portion
Part, and there is water-proof function, so that no longer needing to carry out waterproofing design to the monolithic case of unmanned plane.Simplify the hard of unmanned plane
Part structure, is easy for installation and maintenance.
It should be noted that each embodiment above by reference to described in attached drawing is only to illustrate the utility model rather than limits
The scope of the utility model processed, those skilled in the art should understand that, in the spirit and model for not departing from the utility model
The modification or equivalent replacement carried out under the premise of enclosing to the utility model, should all cover within the scope of the utility model.
In addition, signified outer unless the context, the word occurred in the singular includes plural form, and vice versa.In addition, except non-specifically
Illustrate, then any embodiment all or part of in combination with any other embodiment all or part of come using.
Claims (10)
1. a kind of UAV Flight Control device characterized by comprising
Shell, the interior of shell include closed cavity, and side wall is equipped with connecter hole；
Mainboard is mounted in the cavity of the shell, and the mainboard, which is fixedly connected with, flies control module；
Remote-control receiver is mounted in the cavity of the shell, and the remote-control receiver connects the mainboard, the remote control reception
The antenna of machine is located at the outside of the shell；
Data radio station is mounted in the cavity of the shell, and the data radio station connects the mainboard, the day of the data radio station
Line is located at the outside of the shell；
Water-proof connector, the water-proof connector are fixed on the outer wall of the shell, cover the connecter hole, the waterproof
Connector connects the mainboard.
2. UAV Flight Control device according to claim 1, which is characterized in that the shell includes upper casing and lower casing,
The upper casing and lower casing are fixedly connected to form the cavity.
3. UAV Flight Control device according to claim 1, which is characterized in that it further include position module, the position
Module throughbore seal closure installs the upper surface of the shell, and the position module is connect with the mainboard.
4. UAV Flight Control device according to claim 1, which is characterized in that the water-proof connector is located at described fly
The front of module is controlled, the data radio station is located at the rear of the winged control module.
5. UAV Flight Control device according to claim 1, which is characterized in that the antenna amount of the remote-control receiver
It is two, is located at the two sides of the water-proof connector.
6. UAV Flight Control device according to claim 1, which is characterized in that further include data card slot, the data
Card slot is located in the cavity of the shell, connect with the mainboard, is equipped with data card in the data card slot.
7. UAV Flight Control device according to claim 1, which is characterized in that it further include wide piezoelectricity source module, it is described
Wide piezoelectricity source module is located in the cavity of the shell, and the width piezoelectricity source module connects the water-proof connector and mainboard.
8. UAV Flight Control device according to claim 1, which is characterized in that the remote-control receiver is located at the master
The lower section of plate.
9. UAV Flight Control device according to claim 1, which is characterized in that the shell is equipped with USB interface, institute
It states USB interface and connects the mainboard.
10. a kind of unmanned plane, which is characterized in that including any UAV Flight Control device of claim 1 ~ 9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920545367.XU CN209471376U (en) | 2019-04-22 | 2019-04-22 | A kind of UAV Flight Control device and unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920545367.XU CN209471376U (en) | 2019-04-22 | 2019-04-22 | A kind of UAV Flight Control device and unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209471376U true CN209471376U (en) | 2019-10-08 |
Family
ID=68093564
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920545367.XU Active CN209471376U (en) | 2019-04-22 | 2019-04-22 | A kind of UAV Flight Control device and unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209471376U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111198575A (en) * | 2020-02-27 | 2020-05-26 | 西北工业大学 | Unmanned aerial vehicle flight controller |
| CN112774218A (en) * | 2020-12-28 | 2021-05-11 | 连云港杰瑞电子有限公司 | Hand-held type vehicle exterior control method |
-
2019
- 2019-04-22 CN CN201920545367.XU patent/CN209471376U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111198575A (en) * | 2020-02-27 | 2020-05-26 | 西北工业大学 | Unmanned aerial vehicle flight controller |
| CN112774218A (en) * | 2020-12-28 | 2021-05-11 | 连云港杰瑞电子有限公司 | Hand-held type vehicle exterior control method |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN209471376U (en) | A kind of UAV Flight Control device and unmanned plane | |
| CN109070759A (en) | For being able to carry out the docking recharging station of the unmanned vehicle of ground moving | |
| CN203191778U (en) | A mobile unmanned plane ground comprehensive control station | |
| JP6830187B2 (en) | Electric rotary wing unmanned aerial vehicle with multiple connected aircraft | |
| CA2728025A1 (en) | Flight recorder having integral reserve power supply within form factor of enclosure and method therefor | |
| KR102201550B1 (en) | Wireless Fuel Sensor System | |
| CN204956923U (en) | Intelligent Mobile Terminal's flying suit and intelligence flight system thereof | |
| WO2020135639A1 (en) | Unmanned aerial vehicle base station and unmanned aerial vehicle communication system | |
| CN106468775A (en) | Aircraft tracking and equipment and installation method | |
| JP2021504810A (en) | Unmanned aerial vehicle and its avionics system | |
| CN107201843A (en) | A kind of integrated system set for unmanned plane | |
| CN206885325U (en) | Unmanned vehicle device layout structure | |
| CN206107573U (en) | Unmanned aerial vehicle who possesses waterproof function | |
| CN206906894U (en) | A kind of UAV Flight Control management system | |
| CN205524950U (en) | Use miniature real time monitoring unmanned aerial vehicle based on police | |
| CN111731465B (en) | Fuselage frame rack construction and unmanned aerial vehicle for unmanned aerial vehicle | |
| CN209728523U (en) | A kind of unmanned machine automatic drive system | |
| CN209055987U (en) | A kind of unmanned plane data logger | |
| CN209553497U (en) | A kind of new energy unmanned plane | |
| CN210112002U (en) | Unmanned aerial vehicle signal relay box for distribution line | |
| CN211943737U (en) | Waterproof dirt-proof unmanned aerial vehicle aircraft nose assembly | |
| CN109319104B (en) | Unmanned aerial vehicle | |
| CN109983857B (en) | Heat radiation structure, camera and moving platform | |
| CN212829064U (en) | Unmanned aerial vehicle integrated avionics module and unmanned aerial vehicle thereof | |
| CN207346087U (en) | A kind of unmanned plane |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: 830000 room 6-5a, floor 6, No. 567, Dongrong street, North District, high tech Zone (new urban area), Urumqi, Xinjiang Uygur Autonomous Region Patentee after: Xinjiang glory Jiutian Technology Co.,Ltd. Address before: 211200 Building 5, No. 36 Huatang Road, Honglan Industrial Park, Lishui District, Nanjing City, Jiangsu Province Patentee before: JIANGSU GLORY ROC AERO SCIENCE & TECH Co.,Ltd. |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20220701 Address after: No. 1911, block C, Times Square, Wuyi East Road, Changji City, Changji Hui Autonomous Prefecture, Xinjiang Uygur Autonomous Region 831100 Patentee after: Xinjiang jiuyu Technology Co.,Ltd. Address before: 830000 room 6-5a, floor 6, No. 567, Dongrong street, North District, high tech Zone (new urban area), Urumqi, Xinjiang Uygur Autonomous Region Patentee before: Xinjiang glory Jiutian Technology Co.,Ltd. |