CN210072355U - Four-rotor aircraft control device - Google Patents
Four-rotor aircraft control device Download PDFInfo
- Publication number
- CN210072355U CN210072355U CN201920196171.4U CN201920196171U CN210072355U CN 210072355 U CN210072355 U CN 210072355U CN 201920196171 U CN201920196171 U CN 201920196171U CN 210072355 U CN210072355 U CN 210072355U
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- module
- control signal
- controller body
- rotor aircraft
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Abstract
The utility model discloses a four rotor aircraft controlling means, including controller body, microprocessor, control signal receiving module and control signal transmitting module, be provided with operating panel on the controller body lateral wall, the last operation button that is provided with of operating panel, be provided with display screen between the operation button, the operating panel top is provided with the pilot lamp. Has the advantages that: the utility model discloses a set up bluetooth module and cell phone stand, can be fixed the cell-phone to controlling means on, then be connected with controlling means through the bluetooth, can expand controlling means's service function, easy operation, convenient to use through setting up solitary control signal emission module and control signal receiving module, can ensure that controlling means is more stable to four rotor craft's control process, improves control process's stability.
Description
Technical Field
The utility model relates to an aircraft controlling means technical field, concretely relates to four rotor aircraft controlling means.
Background
The unmanned aircraft is an unmanned aircraft operated by utilizing radio remote control equipment and a self-contained program control device, is widely applied to military and civil fields in recent years, is mainly used for activities such as military reconnaissance, national ecological environment monitoring and protection, geographical mapping, target tracking, commercial aerial photography and the like, is a relatively universal mobile aircraft, and can not be separated from the control device in the use process of the four-rotor aircraft.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
In order to overcome the defects of the prior art, the four-rotor aircraft control device is provided, and the problems that the service function of the existing four-rotor aircraft control device is single, the function expansion is inconvenient, and the control process is not stable enough due to the fact that the integrated control signal transmitter-receiver is adopted for wireless control are solved.
(II) technical scheme
The utility model discloses a following technical scheme realizes: the utility model provides a four-rotor aircraft control device, which comprises a controller body, a microprocessor, a control signal receiving module and a control signal transmitting module, wherein an operating panel is arranged on one side wall of the controller body, operating buttons are arranged on the operating panel, a display screen is arranged between the operating buttons, an indicator lamp is arranged above the operating panel, one side of the indicator lamp is provided with a direction handle, the other side of the indicator lamp is provided with a functional handle, the functional handle and one side opposite to the direction handle are both provided with stunt function buttons, a lithium battery is arranged in the controller body, a main control board is arranged above the lithium battery, the microprocessor is arranged in the middle of the main control board, a work indicating module is arranged on one side of the microprocessor, the control signal receiving module is arranged on one side of the work indicating module, control signal receiving module one side is provided with control signal emission module, control signal emission module one side is provided with bluetooth module, controller body top middle part is provided with radio signal transceiver, radio signal transceiver top is provided with cell phone stand, cell phone stand includes the bottom support, sets up the support of bottom support one side, set up and be in top support on the support and setting are in top support with hasp between the bottom support, the inside cell-phone that is provided with of cell phone stand.
Further, the operation panel is connected with the controller body through a clamping groove, and the direction handle and the function handle are connected with the controller body through the clamping groove.
Furthermore, the display screen is connected with the operation panel through a clamping groove, the operation keys are connected with the operation panel through screws, and the special effect function keys are connected with the controller body through a clamping groove.
Furthermore, the mobile phone support is connected with the controller body through a screw, and the mobile phone is connected with the mobile phone support in a clamping and pressing mode.
Furthermore, the lithium battery is connected with the controller body through screws, and the main control board is connected with the controller body through screws.
Furthermore, the microprocessor, the work indication module and the main control board are connected through soldering, the wireless signal transmitting and receiving device is plugged with the main control board, the model of the main control board is ECM20170304-V06, the model of the microprocessor is MK-AOB3202405T, the model of the work indication module is GF22005-10, and the model of the wireless signal transmitting and receiving device is RTL8811 CU.
Further, the control signal receiving module, the control signal transmitting module and the bluetooth module are all connected with the main control board through soldering, the model of the control signal receiving module is LR43B, the model of the control signal transmitting module is KL-BT01, and the model of the bluetooth module is HM-11.
(III) advantageous effects
Compared with the prior art, the utility model, following beneficial effect has:
1. in order to solve the problems that the existing four-rotor aircraft control device has single use function and inconvenient function expansion, the utility model can fix the mobile phone on the control device by arranging the Bluetooth module and the mobile phone bracket, and then is connected with the control device by Bluetooth, so that the use function of the control device can be expanded, the operation is simple and the use is convenient;
2. because the control signal transceiver that adopts the integration carries out wireless control for solving current four rotor aircraft controlling means, the problem that control process is not stable enough, the utility model discloses a set up solitary control signal transmitting module and control signal receiving module, can ensure that controlling means is more stable to four rotor aircraft's control process, improve control process's stability.
Drawings
Fig. 1 is a front view of a quad-rotor aircraft control device according to the present invention;
fig. 2 is a front cross-sectional view of a controller body in the control device of a quad-rotor aircraft according to the present invention;
fig. 3 is a left side view of a handset cradle in a quad-rotor aircraft control apparatus according to the present invention;
fig. 4 is a circuit block diagram of a control device for a quad-rotor aircraft according to the present invention.
The reference numerals are explained below:
1. a controller body; 2. a direction handle; 3. a functional handle; 4. a trick function key; 5. an operation panel; 6. operating a key; 7. a display screen; 8. an indicator light; 9. a mobile phone support; 901. a bottom bracket; 902. a support; 903. a top support; 904. locking; 10. a wireless signal transmitter-receiver; 11. a mobile phone; 12. A lithium battery; 13. a main control board; 14. a microprocessor; 15. a work indication module; 16. a control signal receiving module; 17. a control signal transmitting module; 18. and a Bluetooth module.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more clearly understood, the present invention is further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
As shown in fig. 1-4, a control device for a four-rotor aircraft comprises a controller body 1, a microprocessor 14, a control signal receiving module 16 and a control signal transmitting module 17, wherein an operation panel 5 is disposed on a side wall of the controller body 1, operation keys 6 are disposed on the operation panel 5, a display screen 7 is disposed between the operation keys 6, the display screen 7 can display electric quantity and operation information of the four-rotor aircraft, an indicator light 8 is disposed above the operation panel 5, the indicator light 8 is used for displaying a working state of the four-rotor aircraft, a direction handle 2 is disposed on one side of the indicator light 8, the direction handle 2 is used for controlling a flight direction of the four-rotor aircraft, a function handle 3 is disposed on the other side of the indicator light 8, a trick function key 4 is disposed on both opposite sides of the function handle 3 and the direction handle 2, the function handle 3 and the trick function key 4 can be used for controlling the four-rotor aircraft, the controller body 1 is internally provided with a lithium battery 12, the lithium battery 12 supplies power for the control device, a main control board 13 is arranged above the lithium battery 12, a microprocessor 14 is arranged in the middle of the main control board 13, a work indication module 15 is arranged on one side of the microprocessor 14, a control signal receiving module 16 is arranged on one side of the work indication module 15, the control signal receiving module 16 is used for receiving a control signal, a control signal transmitting module 17 is arranged on one side of the control signal receiving module 16, the control signal transmitting module 17 is used for transmitting a control signal, a Bluetooth module 18 is arranged on one side of the control signal transmitting module 17, the Bluetooth module 18 is used for carrying out Bluetooth connection with the mobile phone 11, a wireless signal transmitting and receiving device 10 is arranged in the middle of the upper part of the controller body 1, a mobile phone support 9 is arranged above the wireless signal transmitting and receiving device, The mobile phone comprises a support 902 arranged on one side of a bottom support 901, a top support 903 arranged on the support 902, and a lock catch 904 arranged between the top support 903 and the bottom support 901, wherein a mobile phone 11 is arranged in a mobile phone support 9.
Wherein, the operation panel 5 is connected with the controller body 1 through a card slot, the direction handle 2 and the function handle 3 are connected with the controller body 1 through a card slot, the display screen 7 is connected with the operation panel 5 through a card slot, the operation key 6 is connected with the operation panel 5 through a screw, the special effect function key 4 is connected with the controller body 1 through a card slot, the mobile phone support 9 is connected with the controller body 1 through a screw, the mobile phone 11 is connected with the mobile phone support 9 through a card pressing mode, the lithium battery 12 is connected with the controller body 1 through a screw, the main control board 13 is connected with the controller body 1 through a screw, the microprocessor 14, the work indication module 15 is connected with the main control board 13 through tin soldering, the wireless signal transmitting receiver 10 is inserted with the main control board 13, the model of the main control board 13 is ECM20170304-V06, the model of the microprocessor 14 is MK-AOB3202405T, the model of the work indication module 15 is GF, the wireless signal transmitting and receiving device 10 is RTL8811CU, the control signal receiving module 16, the control signal transmitting module 17 and the Bluetooth module 18 are all connected with the main control board 13 by soldering, the control signal receiving module 16 is LR43B, the control signal transmitting module 17 is KL-BT01, and the Bluetooth module 18 is HM-11.
The utility model provides a four rotor aircraft controlling means's theory of operation: when the controller is used, the mobile phone 11 is fixed inside the mobile phone support 9, then the mobile phone 11 is connected with the controller through Bluetooth, meanwhile, the four-rotor aircraft is connected with the mobile phone 11 through a wireless network, then the four-rotor aircraft can be opened through the operation keys 6 on the operation panel 5 to start, the direction handle 2 can transmit a control signal to the four-rotor aircraft through the control signal receiving module 16 and the control signal transmitting module 17 through the wireless signal transmitting and receiving device 10, the flight direction of the four-rotor aircraft is controlled, the function handle 3 and the special effect function handle can transmit the control signal to the four-rotor aircraft through the control signal receiving module 16 and the control signal transmitting module 17 through the wireless signal transmitting and receiving device 10, and the four-rotor aircraft is controlled to perform some functional actions, the mobile phone 11 can watch pictures and video information shot by the four-rotor aircraft in real time, the display screen 7 can display the electric quantity and the running information of the four-rotor aircraft, and the use is extremely convenient.
The above-described embodiments are merely illustrative of the preferred embodiments of the present invention and are not intended to limit the spirit and scope of the present invention. Without departing from the design concept of the present invention, various modifications and improvements made by the technical solution of the present invention by those skilled in the art should fall into the protection scope of the present invention, and the technical contents claimed by the present invention have been fully recorded in the claims.
Claims (7)
1. A four-rotor aircraft control device, its characterized in that: comprises a controller body (1), a microprocessor (14), a control signal receiving module (16) and a control signal transmitting module (17), wherein an operation panel (5) is arranged on one side wall of the controller body (1), operation keys (6) are arranged on the operation panel (5), a display screen (7) is arranged between the operation keys (6), an indicator lamp (8) is arranged above the operation panel (5), a direction handle (2) is arranged on one side of the indicator lamp (8), a function handle (3) is arranged on the other side of the indicator lamp (8), stunt function keys (4) are arranged on the opposite sides of the function handle (3) and the direction handle (2), a lithium battery (12) is arranged inside the controller body (1), a main control board (13) is arranged above the lithium battery (12), and the microprocessor (14) is arranged in the middle of the main control board (13), a work indication module (15) is arranged on one side of the microprocessor (14), a control signal receiving module (16) is arranged on one side of the work indication module (15), a control signal transmitting module (17) is arranged on one side of the control signal receiving module (16), a Bluetooth module (18) is arranged on one side of the control signal transmitting module (17), a wireless signal transmitting and receiving device (10) is arranged in the middle of the upper portion of the controller body (1), a mobile phone support (9) is arranged above the wireless signal transmitting and receiving device (10), the mobile phone support (9) comprises a bottom support (901), a support (902) arranged on one side of the bottom support (901), a top support (903) arranged on the support (902), and a lock catch (904) arranged between the top support (903) and the bottom support (901), the mobile phone support (9) is internally provided with a mobile phone (11).
2. A quad-rotor aircraft control apparatus according to claim 1, wherein: the operation panel (5) is connected with the controller body (1) through a clamping groove, and the direction handle (2) and the function handle (3) are connected with the controller body (1) through the clamping groove.
3. A quad-rotor aircraft control apparatus according to claim 1, wherein: the display screen (7) is connected with the operation panel (5) through a clamping groove, the operation key (6) is connected with the operation panel (5) through a screw, and the special effect function key (4) is connected with the controller body (1) through a clamping groove.
4. A quad-rotor aircraft control apparatus according to claim 1, wherein: the mobile phone support (9) is connected with the controller body (1) through a screw, and the mobile phone (11) is connected with the mobile phone support (9) in a clamping and pressing mode.
5. A quad-rotor aircraft control apparatus according to claim 1, wherein: the lithium battery (12) is connected with the controller body (1) through screws, and the main control board (13) is connected with the controller body (1) through screws.
6. A quad-rotor aircraft control apparatus according to claim 1, wherein: the microprocessor (14), the work indication module (15) with the main control board (13) is connected through the soldering, wireless signal transceiver (10) with the main control board (13) is pegged graft, the model of main control board (13) is ECM20170304-V06, the model of microprocessor (14) is MK-AOB3202405T, the model of work indication module (15) is GF22005-10, the model of wireless signal transceiver (10) is RTL8811 CU.
7. A quad-rotor aircraft control apparatus according to claim 1, wherein: the control signal receiving module (16), the control signal transmitting module (17) and the Bluetooth module (18) are connected with the main control board (13) through soldering, the model of the control signal receiving module (16) is LR43B, the model of the control signal transmitting module (17) is KL-BT01, and the model of the Bluetooth module (18) is HM-11.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920196171.4U CN210072355U (en) | 2019-02-14 | 2019-02-14 | Four-rotor aircraft control device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920196171.4U CN210072355U (en) | 2019-02-14 | 2019-02-14 | Four-rotor aircraft control device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210072355U true CN210072355U (en) | 2020-02-14 |
Family
ID=69432652
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920196171.4U Expired - Fee Related CN210072355U (en) | 2019-02-14 | 2019-02-14 | Four-rotor aircraft control device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210072355U (en) |
-
2019
- 2019-02-14 CN CN201920196171.4U patent/CN210072355U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200214 Termination date: 20210214 |
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| CF01 | Termination of patent right due to non-payment of annual fee |