CN209795856U - Device for indirectly controlling synchronous rotation through pitching of unmanned aerial vehicle cradle head - Google Patents
Device for indirectly controlling synchronous rotation through pitching of unmanned aerial vehicle cradle head Download PDFInfo
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- CN209795856U CN209795856U CN201920596596.4U CN201920596596U CN209795856U CN 209795856 U CN209795856 U CN 209795856U CN 201920596596 U CN201920596596 U CN 201920596596U CN 209795856 U CN209795856 U CN 209795856U
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Abstract
The utility model discloses a device for indirectly controlling synchronous rotation through pitching of an unmanned aerial vehicle pan-tilt, which comprises a base and a cover plate, wherein the cover plate is arranged above the base, a circuit board is fixedly arranged in the base, a rechargeable battery is arranged on one side of the circuit board, one end of the rechargeable battery is communicated with a charging socket, a rotary interface placing groove is arranged at one end of the base, a motor mounting groove is also arranged in the base, a servo motor is arranged in the motor mounting groove, the output shaft of the servo motor is connected with a rotary interface through a coupler, the rotary interface is positioned in the rotary interface placing groove, a lead screw is arranged at one end of the rotary interface, one end of the rotary interface is connected with a light filling lamp component, an inner thread groove is arranged at one end of the light filling lamp component, the utility model can realize the purpose of controlling the synchronous rotation of the light filling lamp, the work of charging the rechargeable battery is facilitated.
Description
Technical Field
the utility model relates to an unmanned air vehicle technique field specifically is a every single move through unmanned aerial vehicle cloud platform realizes the synchronous pivoted device of indirect control.
Background
The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. The machine has no cockpit, but is provided with an automatic pilot, a program control device and other equipment. The personnel on the ground, the naval vessel or the mother aircraft remote control station can track, position, remotely control, telemeter and digitally transmit the personnel through equipment such as a radar. The aircraft can take off like a common airplane under the radio remote control or launch and lift off by a boosting rocket, and can also be thrown into the air by a mother aircraft for flying. During recovery, the aircraft can land automatically in the same way as the common aircraft landing process, and can also be recovered by a parachute or a barrier net for remote control. Can be repeatedly used for many times. The wide use is in aerial reconnaissance, is kept watch on, is communicated, is anti-dive, electronic interference etc. and when unmanned aerial vehicle was flown at night, there was the light filling lamp.
At present, unmanned aerial vehicle light filling lamp on the market can not realize the synchronous pivoted purpose of control light filling lamp, is not convenient for carry out the work of charging to rechargeable battery, and for this reason, we have proposed a every single move through the unmanned aerial vehicle cloud platform and realize the synchronous pivoted device of indirect control.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a pitching through unmanned aerial vehicle cloud platform realizes the synchronous pivoted device of indirect control, can realize the synchronous pivoted purpose of control light filling lamp, is convenient for carry out the work of charging to rechargeable battery to solve the problem that proposes among the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: a device for indirectly controlling synchronous rotation through pitching of an unmanned aerial vehicle holder comprises a base and a cover plate, wherein the cover plate is arranged above the base, a circuit board is fixedly arranged in the base, a rechargeable battery is arranged on one side of the circuit board, one end of the rechargeable battery is communicated with a charging socket, a rotary interface placing groove is formed in one end of the base, a motor mounting groove is further formed in the base, a servo motor is arranged in the motor mounting groove, an output shaft of the servo motor is connected with a rotary interface through a coupler, the rotary interface is positioned in the rotary interface placing groove, a lead screw is arranged at one end of the rotary interface, one end of the rotary interface is connected with a light supplementing lamp assembly, an inner threaded groove is formed in one end of the light supplementing lamp assembly, a power switch button is arranged on one side of the base, an angle sensor is further mounted inside the base, an inner bolt column is arranged on one side of the angle sensor, a rotary interface placing groove is also formed in one side of the cover plate, bolt holes are formed in the upper portion and the lower portion of the cover plate, a bolt is arranged inside each bolt hole, and the lower end of each bolt is in threaded connection with the inner bolt column.
Preferably, the light supplementing lamp assembly is in threaded connection with the rotating interface through the matching of the inner thread groove and the lead screw, the length of the lead screw is consistent with the depth of the inner thread groove, and the light supplementing lamp assembly is in threaded connection with the rotating interface through the matching of the inner thread groove and the lead screw.
Preferably, the inner diameter of the rotary interface placing groove is consistent with the diameter of the rotary interface, and the length of the rotary interface placing groove is smaller than the height of the rotary interface.
Preferably, the bolt holes and the inner bolt columns are provided with six groups, and the six groups of bolt holes respectively correspond to the inner bolt columns of the foothold.
Preferably, the inner diameter of the motor mounting groove is consistent with the diameter of the servo motor, and the length of the motor mounting groove is consistent with the length of the servo motor.
Preferably, a power supply groove is formed in one side of the base, and the power switch button is installed inside the power supply groove.
Compared with the prior art, the beneficial effects of the utility model are that:
1. By turning on a power switch, the unmanned aerial vehicle can control pitching of a lens to shoot when an airplane shoots in the flying process, an angle sensor can detect the change of the rotation of the angle of the lens of the unmanned aerial vehicle, the angle sensor can transmit a signal to a chip on a circuit board, after the chip receives the signal transmitted by the angle sensor, a program in the chip is started to transmit the signal and control a servo motor to work, the servo motor can drive a rotating interface to correspondingly rotate by the same angle, the rotating interface can drive a light supplement lamp assembly to rotate, so that pitching of an unmanned aerial vehicle holder can be realized, the view range of the light supplement lamp can synchronously rotate along with the view range of the lens of the unmanned aerial vehicle, and the purpose of controlling the;
2. when the rechargeable battery is not used, the rechargeable battery can be stored after the power switch is turned off, and the rechargeable battery can be charged through the data line for the charging socket under the condition that the rechargeable battery does not have electricity, so that the rechargeable battery can be charged conveniently.
Drawings
Fig. 1 is a schematic diagram of the explosion structure of the present invention;
Fig. 2 is a schematic view of the structure of the rotary interface of the present invention;
Fig. 3 is the utility model discloses a light filling lamp subassembly schematic structure.
In the figure: the device comprises a base 1, a cover plate 2, a circuit board 3, a rechargeable battery 4, a rotary interface 5, a light supplementing lamp assembly 6, a servo motor 7, an angle sensor 8, a power switch button 9, a bolt 10, a lead screw 11, an internal thread groove 12, a bolt hole 13, an internal bolt column 14, a motor mounting groove 15, a rotary interface placing groove 16, a power supply groove 17 and a charging socket 18.
Detailed Description
the technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-3, the present invention provides a technical solution: a device for indirectly controlling synchronous rotation through pitching of an unmanned aerial vehicle holder comprises a base 1 and a cover plate 2, wherein the cover plate 2 is arranged above the base 1, a circuit board 3 is fixedly arranged in the base 1, a rechargeable battery 4 is arranged on one side of the circuit board 3, one end of the rechargeable battery 4 is communicated with a charging socket 18, the rechargeable battery can be accommodated after a power switch 9 is closed when not used, and the rechargeable battery 4 can be charged through a data line through the charging socket 18 under the condition that no electricity exists in the rechargeable battery 4, so that the rechargeable battery 4 can be charged conveniently; one end of the base 1 is provided with a rotary interface placing groove 16, a motor installing groove 15 is further arranged inside the base 1, a servo motor 7 is arranged inside the motor installing groove 15, an output shaft of the servo motor 7 is connected with a rotary interface 5 through a coupler, the rotary interface 5 is positioned inside the rotary interface placing groove 16, one end of the rotary interface 5 is provided with a lead screw 11, one end of the rotary interface 5 is connected with a light supplementing lamp assembly 6, one end of the light supplementing lamp assembly 6 is provided with an internal thread groove 12, one side of the base 1 is provided with a power switch button 9, an angle sensor 8 is further arranged inside the base 1, the power switch 9 is turned on, when the unmanned aerial vehicle is shot in the flying process, the unmanned aerial vehicle can control the pitching of a lens to shoot, the angle sensor 8 can detect the change of the rotation of the lens of the unmanned aerial vehicle, and the angle, after the chip receives a signal sent by the angle sensor 8, a program in the chip is started to send the signal and control the servo motor 7 to work, the servo motor 7 can drive the rotating interface 5 to correspondingly rotate by the same angle, the rotating interface 5 can drive the light supplement lamp assembly 6 to rotate, so that the unmanned aerial vehicle holder can pitch to realize synchronous rotation of the light supplement lamp sight range along with the unmanned aerial vehicle lens sight range, and the purpose of controlling the synchronous rotation of the light supplement lamp can be realized; an inner bolt column 14 is arranged on one side of the angle sensor 8, a rotary interface placing groove 16 is also formed in one side of the cover plate 2, bolt holes 13 are formed in the upper portion and the lower portion of the cover plate 2, a bolt 10 is arranged inside each bolt hole 13, and the lower end of each bolt 10 is in threaded connection with the inner bolt column 14.
Further, the light filling lamp assembly 6 is in fixed threaded connection with the rotating interface 5 through the matching of the inner thread groove 12 and the lead screw 11, the length of the lead screw 11 is consistent with the depth of the inner thread groove 12, and the light filling lamp assembly 6 is in fixed threaded connection with the rotating interface 5 through the matching of the inner thread groove 12 and the lead screw 11, so that the light filling lamp assembly 6 and the rotating interface 5 are convenient to connect and detach.
Further, the inner diameter of the rotary interface placing groove 16 is consistent with the diameter of the rotary interface 5, and the length of the rotary interface placing groove 16 is smaller than the height of the rotary interface 5, so that the rotary operation of the rotary interface 5 is facilitated.
Furthermore, six groups of bolt holes 13 and six groups of inner bolt columns 14 are arranged, the six groups of bolt holes 13 correspond to the inner bolt columns 14 of the foothold respectively, and the six groups of bolt holes 13 and the six groups of inner bolt columns 14 are arranged, so that the base 1 and the cover plate 2 can be fixedly connected together more conveniently.
further, the inner diameter of the motor mounting groove 15 is consistent with the diameter of the servo motor 7, the length of the motor mounting groove 15 is consistent with the length of the servo motor 7, and therefore the servo motor 7 can be better fixed.
Furthermore, a power supply groove 17 is formed in one side of the base 1, the power switch button 9 is installed inside the power supply groove 17, and the power switch button 9 is installed inside the power supply groove 17 through the power switch button 9, so that the power switch button 9 can be conveniently installed and fixed.
The working principle is as follows: the device for indirectly controlling synchronous rotation through pitching of the unmanned aerial vehicle holder controls pitching of a lens to shoot when an unmanned aerial vehicle plane shoots in the flying process by turning on the power switch 9, the angle sensor 8 detects the change of the rotation corresponding to the angle of the lens of the unmanned aerial vehicle, the angle sensor 8 transmits a signal to the chip on the circuit board 3, the chip receives the signal sent by the angle sensor 8, the program in the chip is started to send the signal and controls the servo motor 7 to work, the servo motor 7 works to drive the rotating interface 5 to correspondingly rotate by the same angle, the rotating interface 5 drives the light supplement lamp component 6 to rotate, further the pitching of the unmanned aerial vehicle holder can realize synchronous rotation of the light supplement lamp sight range along with the lens sight range of the unmanned aerial vehicle, the power switch 9 can be turned off when the unmanned aerial vehicle holder is not used, and then the rechargeable battery 4 is stored under the, charging may be performed with the data line through the charging jack 18.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides a pitch through unmanned aerial vehicle cloud platform realizes synchronous pivoted device of indirect control, includes base (1) and apron (2), its characterized in that: the solar charging device is characterized in that a cover plate (2) is arranged above the base (1), a circuit board (3) is fixedly arranged inside the base (1), a rechargeable battery (4) is arranged on one side of the circuit board (3), one end of the rechargeable battery (4) is communicated with a charging socket (18), a rotary interface placing groove (16) is formed in one end of the base (1), a motor mounting groove (15) is further formed in the base (1), a servo motor (7) is arranged inside the motor mounting groove (15), an output shaft of the servo motor (7) is connected with a rotary interface (5) through a coupling, the rotary interface (5) is located inside the rotary interface placing groove (16), a lead screw (11) is arranged at one end of the rotary interface (5), and a light supplementing lamp component (6) is connected with one end of the rotary interface (5), interior thread groove (12) have been seted up to the one end of light filling banks spare (6), one side of base (1) is equipped with switch power button (9), just angle sensor (8) are still installed to the inside of base (1), one side of angle sensor (8) is equipped with interior bolt post (14), rotation interface standing groove (16) have also been seted up to one side of apron (2), just bolt hole (13) have been seted up from top to bottom in apron (2), the inside of bolt hole (13) is equipped with bolt (10), the lower extreme and interior bolt post (14) threaded connection of bolt (10) are in the same place.
2. The device of claim 1, wherein the device for indirectly controlling synchronous rotation through pitching of the pan/tilt head of the unmanned aerial vehicle comprises: the light supplementing lamp assembly (6) is fixedly connected with the rotary interface (5) through the matching of the internal thread groove (12) and the screw rod (11) in a threaded manner, and the length of the screw rod (11) is consistent with the depth of the internal thread groove (12).
3. The device of claim 1, wherein the device for indirectly controlling synchronous rotation through pitching of the pan/tilt head of the unmanned aerial vehicle comprises: the inner diameter of the rotary interface placing groove (16) is consistent with the diameter of the rotary interface (5), and the length of the rotary interface placing groove (16) is smaller than the height of the rotary interface (5).
4. The device of claim 1, wherein the device for indirectly controlling synchronous rotation through pitching of the pan/tilt head of the unmanned aerial vehicle comprises: six groups of bolt holes (13) and six groups of inner bolt columns (14) are arranged, and the six groups of bolt holes (13) correspond to the inner bolt columns (14) of the foothold respectively.
5. The device of claim 1, wherein the device for indirectly controlling synchronous rotation through pitching of the pan/tilt head of the unmanned aerial vehicle comprises: the inner diameter of the motor mounting groove (15) is consistent with the diameter of the servo motor (7), and the length of the motor mounting groove (15) is consistent with the length of the servo motor (7).
6. The device of claim 1, wherein the device for indirectly controlling synchronous rotation through pitching of the pan/tilt head of the unmanned aerial vehicle comprises: a power supply groove (17) is formed in one side of the base (1), and the power switch button (9) is installed inside the power supply groove (17).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920596596.4U CN209795856U (en) | 2019-04-28 | 2019-04-28 | Device for indirectly controlling synchronous rotation through pitching of unmanned aerial vehicle cradle head |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920596596.4U CN209795856U (en) | 2019-04-28 | 2019-04-28 | Device for indirectly controlling synchronous rotation through pitching of unmanned aerial vehicle cradle head |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209795856U true CN209795856U (en) | 2019-12-17 |
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ID=68831386
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920596596.4U Active CN209795856U (en) | 2019-04-28 | 2019-04-28 | Device for indirectly controlling synchronous rotation through pitching of unmanned aerial vehicle cradle head |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209795856U (en) |
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2019
- 2019-04-28 CN CN201920596596.4U patent/CN209795856U/en active Active
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