CN210662628U

CN210662628U - Unmanned aerial vehicle navigation searchlighting device

Info

Publication number: CN210662628U
Application number: CN201922230258.1U
Authority: CN
Inventors: 张玮航
Original assignee: Individual
Current assignee: Individual
Priority date: 2019-12-11
Filing date: 2019-12-11
Publication date: 2020-06-02
Anticipated expiration: 2029-12-11

Abstract

The utility model discloses an unmanned aerial vehicle navigation searchlighting device, including the electron base, be equipped with the cavity on the electron base, install lithium cell, distribution board, inertia guidance module and controller in the cavity, control switch is installed to one side lateral wall of electron base. The utility model discloses in, this navigation lamp subassembly is by the information of inertia guidance module real-time detection aircraft flight three-dimensional direction, and with real-time detection's information feedback to controller, the controller is with the flight state data processing back that inertia measuring unit detected, convert the cloud platform control signal into, with this control triaxial stabilizes the cloud platform and rotates, thereby realize the orientation that changes the searchlight on the searchlight device in the automatic and real-time change of in-process of unmanned aerial vehicle at the flight, thereby make searchlight orientation and aircraft three-dimensional moving direction synchronous completely, be favorable to unmanned aerial vehicle operator to judge unmanned aerial vehicle's flight direction in real time in practical application, find the barrier on the airline, guarantee flight safety.

Description

Unmanned aerial vehicle navigation searchlighting device

Technical Field

The utility model relates to an unmanned aerial vehicle navigation auxiliary device technical field, more specifically say, in particular to unmanned aerial vehicle navigation searchlighting device.

Background

Along with the rapid development of unmanned aerial vehicle technique, unmanned aerial vehicle's application mode is more and more, and the task and the flight condition that unmanned aerial vehicle will face are more and more complicated, and the condition that leads to the crash on striking the barrier when unmanned aerial vehicle is flown at the complex condition often can appear, especially night.

Therefore, the unmanned aerial vehicle navigation searchlight device is provided to solve the problems.

SUMMERY OF THE UTILITY MODEL

The utility model aims at solving the problem that exists among the prior art, and the unmanned aerial vehicle navigation searchlighting device who possesses direction, searchlighting, avoid etc. multiple flight obstacle function that provides.

In order to achieve the above purpose, the utility model adopts the following technical scheme:

the utility model provides an unmanned aerial vehicle navigation searchlighting device, includes electronic base, the last cavity that is equipped with of electronic base, install lithium cell, distributor plate, inertia guidance module and controller in the cavity, control switch is installed to one side lateral wall of electronic base, one side that electronic base is close to control switch is equipped with the mouth that charges, the top of electronic base is stabilized the cloud platform through the triaxial and is connected with the shell, be equipped with mounting groove on the shell, mounting groove's interior bottom fixedly connected with circuit board, the electric connection has two LED luminescent plates, two lamp cups and a set of laser emitter on the circuit board, the LED luminescent plate is located the lamp cup, the shell is close to one side fixedly connected with of mounting groove opening part and the lens set up with the shell matching, install detachable lens on the lens set shell.

Preferably, the installation is in the mouth that charges and the rubber buffer that the mouth matched with that charges set up.

Preferably, the laser emitter is located between two LED light boards.

Preferably, the lens holder case is in contact with the outer case through a packing.

The embodiment of the utility model provides a technical scheme can include following beneficial effect:

the utility model discloses in, this navigation lamp subassembly is by the information of inertia guidance module real-time detection aircraft flight three-dimensional direction, and with real-time detection's information feedback to controller, the controller is with the flight state data processing back that inertia measuring unit detected, convert the cloud platform control signal into, with this control triaxial stabilizes the cloud platform and rotates, thereby realize the orientation that changes the searchlight on the searchlight device in the automatic and real-time change of in-process of unmanned aerial vehicle at the flight, thereby make searchlight orientation and aircraft three-dimensional moving direction synchronous completely, be favorable to unmanned aerial vehicle operator to judge unmanned aerial vehicle's flight direction in real time in practical application, find the barrier on the airline, guarantee flight safety.

Drawings

Fig. 1 is a schematic structural view of an unmanned aerial vehicle navigation searchlighting device provided by the present invention;

fig. 2 is a schematic diagram of a right-view structure of the unmanned aerial vehicle navigation searchlighting device provided by the utility model;

fig. 3 is a schematic diagram of a connection structure of a housing, a circuit board, a photosensitive sensor, an LED light-emitting panel, a lamp cup and a laser emitter in the navigation searchlighting device of the unmanned aerial vehicle according to the present invention;

fig. 4 is a schematic view of a connection structure of a lens fixing shell, a sealing ring and a shell in the navigation and searchlighting device of the unmanned aerial vehicle provided by the utility model;

fig. 5 is a schematic view of a connection structure of an electronic base, a lithium battery, a distributor plate, a controller, an inertial guidance module, a charging port, a rubber plug and a control switch in the unmanned aerial vehicle navigation searchlighting device provided by the utility model;

fig. 6 is the utility model provides a supply circuit diagram of outage control and information control circuit among unmanned aerial vehicle navigation searchlighting device.

In the figure: 1. an electronic base; 2. a three-axis stabilizing pan-tilt; 3. a lens fixing case; 4. a lens; 5. a laser transmitter; 6. an LED light emitting panel; 7. a circuit board; 8. a lamp cup; 9. a charging port; 10. a seal ring; 11. a housing; 12. a lithium battery; 13. a distributor plate; 14. an inertial guidance module; 15. a controller; 16. a control switch; 17. and a rubber plug.

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.

Referring to fig. 1-6, an unmanned aerial vehicle navigation searchlighting device comprises an electronic base 1, a cavity is arranged on the electronic base 1, a lithium battery 12, a distributor 13, an inertia guidance module 14 and a controller 15 are arranged in the cavity, a control switch 16 is arranged on the outer side wall of one side of the electronic base 1, a charging port 9 is arranged on one side of the electronic base 1 close to the control switch 16, a rubber plug 17 matched with the charging port 9 is arranged in the charging port 9, the bottom of the electronic base 1 is smooth, a plurality of fixing holes are formed in the electronic base 1, the electronic base 1 is convenient to fix on an unmanned aerial vehicle, the lithium battery 12 is used for providing electric energy for each component, the inertia guidance module 14 has the functions of detecting attitude data of the unmanned aerial vehicle and the distance between the unmanned aerial vehicle and a flight obstacle in real time, and aims to transmit the attitude data of the unmanned aerial vehicle in, 2 adjustment housing 11's orientation of cloud platform is stabilized to controller 15 control triaxial, be convenient for control light shines the direction that removes to the unmanned aerial vehicle aircraft in real time, the effect of the mouth 9 that charges is convenient for charge lithium cell 12, the mouth 9 that charges is plugged up in rubber buffer 17's effect, avoid in the water stain cavity that enters into on the electron base 1, lead to installing the component part damage in the cavity, control switch 16 effect is the break-make of control lithium cell 12 to each component part supply circuit.

Wherein, the top of electron base 1 is connected with shell 11 through triaxial stabilization pan-tilt 2, it is required to explain that, triaxial stabilization pan-tilt 2 is prior art, do not do too much narration here, and triaxial stabilization pan-tilt 2 can control the three-dimensional all-round rotation of shell 11, is convenient for carry out real-time detection to the environment around the unmanned aerial vehicle aircraft, avoids the unmanned aerial vehicle aircraft to hit and damages on the flight barrier, and in addition, triaxial stabilization pan-tilt 2 can also replace with the pan-tilt of single face side arm.

The LED illuminating lamp comprises a shell 11, a circuit board 7 is fixedly connected to the inner bottom of the installation groove, two LED illuminating plates 6, two lamp cups 8 and a group of laser emitters 5 are electrically connected to the circuit board 7, the LED illuminating plates 6 are located in the lamp cups 8, a lens fixing shell 3 matched with the shell 11 is fixedly connected to one side, close to an opening of the installation groove, of the shell 11, a detachable lens 4 is installed on the lens fixing shell 3, the laser emitters 5 are located between the two LED illuminating plates 6, the lens fixing shell 3 is in contact with the shell 11 through a sealing ring 10, the LED illuminating plates 6 are used for illuminating light, the lamp cups 8 are used for limiting the light emitted by the LED illuminating plates 6, the light is kept to be illuminated in one direction, and the lamp cups 8 and the LED illuminating plates 6 are matched to form; the laser emitter 5 is used for emitting laser, so that the inertial guidance module 14 can conveniently detect the distance of a flight obstacle, an operator can conveniently operate the unmanned aerial vehicle to avoid the flight obstacle, the damage of the unmanned aerial vehicle caused by the collision of the unmanned aerial vehicle on the flight obstacle is avoided, the lens fixing shell 3 is used for fixing the lens 4 on the shell 11, and the lens 4 can be replaced so as to change the color and the heat dissipation degree of light; the sealing ring 10 is used for keeping the sealing performance between the lens fixing shell 3 and the shell 11 and preventing water from entering the shell 11 to damage the circuit board 7, the LED light-emitting board 6 and the laser emitter 5.

In the utility model, when the unmanned aerial vehicle is operated to fly at night, the control switch 16 is turned on to operate the unmanned aerial vehicle to fly into the air, in the flying process of the unmanned aerial vehicle, the controller 15 controls the three-axis stabilizing pan-tilt 2 to adjust the orientation of the shell 11, so as to control the light and the direction of the laser emitter 5 to irradiate the unmanned aerial vehicle in real time, the inertial guidance module 14 detects the attitude data of the unmanned aerial vehicle according to the condition of irradiation of the laser emitter 5, and transmits the attitude data of the unmanned aerial vehicle in the flying process to the controller 15, so that an operator can conveniently check whether flying obstacles exist around the unmanned aerial vehicle and the distance between the unmanned aerial vehicle and the flying obstacles in real time, and the flight trajectory of the unmanned aerial vehicle is adjusted according to the distance data between the unmanned aerial vehicle and the flight barrier, so that the unmanned aerial vehicle is prevented from colliding with the flight barrier in the flight process and being damaged.

The utility model discloses the standard part that uses all can purchase from the market, and dysmorphism piece all can be customized according to the description with the record of drawing of description, and the concrete connection mode of each part all adopts conventional means such as ripe bolt, rivet, welding among the prior art, and machinery, part and equipment all adopt prior art, and conventional model, including circuit connection adopts conventional connection mode among the prior art, does not detailed here again.

The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.

Claims

1. The utility model provides an unmanned aerial vehicle navigation searchlighting device, includes electronic base (1), its characterized in that, be equipped with the cavity on electronic base (1), install lithium cell (12), distributor plate (13), inertia guidance module (14) and controller (15) in the cavity, control switch (16) are installed to one side lateral wall of electronic base (1), one side that electronic base (1) is close to control switch (16) is equipped with charge mouth (9), the top of electronic base (1) is connected with shell (11) through triaxial stabilized cloud platform (2), be equipped with the mounting groove on shell (11), the interior bottom fixedly connected with circuit board (7) of mounting groove, electrically connected with two LED luminescent plates (6) on circuit board (7), two lamp cups (8) and a set of laser emitter (5), LED luminescent plate (6) are located lamp cup (8), one side fixedly connected with that shell (11) is close to the mounting groove opening part matches lens set casing (3) that sets up with shell (11), install detachable lens (4) on lens set casing (3).

2. The unmanned aerial vehicle navigation searchlighting device of claim 1, wherein a rubber plug (17) is installed in the charging port (9) and is matched with the charging port (9).

3. An unmanned aerial vehicle navigation and searchlighting device according to claim 1, wherein the laser emitter (5) is located between two LED light emitting panels (6).

4. The unmanned aerial vehicle navigation searchlight device of claim 1, characterized in that the lens fixing shell (3) is in contact with the outer shell (11) through a sealing ring (10).