CN220809831U - Unmanned aerial vehicle for industrial transportation - Google Patents

Abstract

The utility model discloses an unmanned aerial vehicle for industrial transportation, which belongs to the technical field of unmanned aerial vehicles for industry, and comprises the following components: the device comprises a machine body, a mechanical arm arranged below the machine body and a flight control system arranged in the machine body; the flying control system comprises a chassis, the chassis is arranged at the bottom of the machine body, a storage bin is formed between the machine body and the chassis, and a power supply module for integrally supplying power to the flying control system and the mechanical arm and a control module for controlling the flying of the unmanned aerial vehicle and the clamping of the mechanical arm are arranged in the storage bin. Preferably, the control module comprises a communication module for receiving instructions and sending data, a navigation module for providing position and posture information and a camera module for transmitting image data, wherein the camera module is arranged to shoot materials, and the load module transmits images to the holder, so that a manager can conveniently monitor the whole body of the unmanned aerial vehicle in real time, and the transportation efficiency and the safety of surrounding personnel are improved.

Description

A drone for industrial transportation

Technical Field

The utility model relates to the technical field of industrial unmanned aerial vehicles, in particular to a unmanned aerial vehicle used for industrial transportation.

Background technique

Industrial transport drones refer to drone systems used for cargo transportation in the industrial field. They usually have a large load capacity and a long flight time, and can efficiently transport goods in industrial environments. Existing industrial transport drones include multi-rotor drones, fixed-wing drones, and vertical take-off and landing drones, which are often used in various cargo transportation tasks such as logistics, warehousing, mining, and construction.

Existing industrial transport drones may cause safety problems to workers around the materials during the material transportation process. Due to the high degree of automation of drones, operators may not be able to detect and respond to unexpected situations in time, such as material falling or collision. In particular, the flight altitude and speed of drones may pose potential safety risks to the surrounding environment and personnel. Therefore, a drone for industrial transportation is proposed.

Utility Model Content

The utility model aims to solve at least one of the technical problems existing in the prior art. To this end, one purpose of the utility model is to provide a drone for industrial transportation.

In order to achieve the above purpose, the utility model provides the following technical solutions:

A drone for industrial transportation, comprising: a fuselage, a mechanical arm installed under the fuselage, and a flight control system arranged inside the fuselage;

Among them, the flight control system includes a chassis, which is installed at the bottom of the fuselage. A storage compartment is formed between the fuselage and the chassis. The interior of the storage compartment is provided with a power supply module for powering the flight control system and the robotic arm as a whole, and a control module for controlling the flight of the drone and the clamping of the robotic arm.

Preferably, the control module includes a communication module for receiving instructions and sending data, a navigation module for providing position and posture information, a camera module for transmitting image data, a payload module for transmitting data, and an obstacle avoidance module for providing obstacle detection information. The communication module, camera module, payload module and obstacle avoidance module are all electrically connected to the control module through wires, and the navigation module is connected to the control module through an interface.

Preferably, the power supply module includes a battery pack and a motor.

Preferably, the fuselage includes a fuselage frame and wings.

Preferably, the flight control system includes an inertial measurement unit, a GPS compass module, an LED indicator light module, a freeRTOS system, a gyroscope, and pid control.

Preferably, the camera module includes a camera, an image transmission device and an image processing unit.

Preferably, the obstacle avoidance module includes an ultrasonic sensor, an infrared sensor and a radar.

Compared with the prior art, the beneficial effects of the utility model are:

In the utility model, by arranging a mechanical arm under the fuselage, the versatility and applicability of the drone are improved by identifying and classifying different materials placed in the area and transporting the materials to the designated area;

In the utility model, a camera module is provided to shoot materials, and a load module transmits images to a gimbal, so that managers can conduct real-time monitoring and clearly control the whole body of the drone, thereby improving the efficiency of transportation and the safety of surrounding personnel.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG1 is a schematic diagram of the external three-dimensional structure of the utility model;

FIG2 is a front view of the structure of the utility model;

FIG3 is a schematic structural diagram of the flight control system of the present invention.

In the figure: 1. Body; 2. Robotic arm; 3. Power supply module; 4. Control module; 5. Communication module; 6. Navigation module; 7. Camera module; 8. Payload module; 9. Obstacle avoidance module.

Detailed ways

The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

In the description of the present invention, it should be noted that the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inside", "outside" and the like indicate positions or positional relationships based on the positions or positional relationships shown in the drawings, which are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific position, be constructed and operated in a specific position, and therefore cannot be understood as limiting the present invention; the terms "first", "second" and "third" are only used for descriptive purposes, and cannot be understood as indicating or implying relative importance. In addition, unless otherwise clearly specified and limited, the terms "installed", "connected" and "connected" should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be an indirect connection through an intermediate medium, or it can be a connection between the two elements. For those of ordinary skill in the art, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.

Please refer to Figures 1 to 3. The utility model provides a technical solution:

A drone for industrial transportation comprises: a fuselage 1, a mechanical arm 2 installed below the fuselage 1, and a flight control system arranged inside the fuselage 1; the fuselage 1 comprises a fuselage frame and wings.

The robot arm 2 is provided with a clamping device for grabbing objects, which is used to clamp the objects and then move them to a specified position. The flight control system is arranged at the inner center of the fuselage 1 .

The flight control system includes a chassis, which is installed at the bottom of the fuselage 1. A storage compartment is formed between the fuselage 1 and the chassis. A power supply module 3 for supplying power to the flight control system and the robotic arm 2 as a whole and a control module 4 for controlling the flight of the UAV and the clamping of the robotic arm 2 are arranged inside the storage compartment. The control module 4 is used to sense the environment, control the flight attitude and execute flight instructions. The flight control system calculates and sends control instructions to the control module 4 based on this information to control the flight of the UAV.

The control module 4 includes a communication module 5 for receiving instructions and sending data, a navigation module 6 for providing position and posture information, a camera module 7 for transmitting image data, a load module 8 for transmitting data, and an obstacle avoidance module 9 for providing obstacle detection information;

The communication module 5 , the camera module 7 , the payload module 8 and the obstacle avoidance module 9 are all electrically connected to the control module 4 through wires, and the navigation module 6 is connected to the control module 4 through an interface.

The power supply module 3 includes a battery pack and a motor, which are used to provide power to drive the drone to fly. The battery pack is connected to the motor and the electric regulator through wires to convert electrical energy into mechanical energy to drive the rotor of the drone to rotate.

The flight control system includes an inertial measurement unit, a GPS compass module, an LED indicator module, a freeRTOS system, a gyroscope, and a pid control system; it is used to realize the positioning, navigation, and attitude control of the UAV. The GPS module determines the position of the UAV by receiving satellite signals, and the inertial measurement unit estimates the attitude of the UAV by measuring acceleration and angular velocity. The GPS compass module is used to provide the direction information of the UAV. The positioning and navigation information is transmitted to the control module 4 to assist the UAV in achieving precise flight control.

The camera module 7 includes a camera, an image transmission device and an image processing unit; it is used to take photos and videos and transmit them in real time, collect data sets and perform post-processing through machine learning algorithms. The camera is connected to the control module 4 and the communication module 5 through wires to transmit image data.

The obstacle avoidance module 9 includes an ultrasonic sensor, an infrared sensor and a radar; it is used to detect and avoid obstacles to ensure flight safety. The obstacle avoidance module 9 is connected to the control module 4 through a wire to provide obstacle detection information.

The load module 8 is used for data collection and environmental perception. The load module 8 is connected to the control module 4 through an interface to transmit the collected data.

The communication module 5 is used for communication and data transmission with the gimbal or other drones. Through wireless connection, the user sends instructions to the drone through the gimbal, and the drone transmits the sensed data and images back to the gimbal.

Parts not involved in the present invention are the same as the prior art or can be implemented by the prior art. Although the embodiments of the present invention have been shown and described, it is understood by those skilled in the art that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principles and spirit of the present invention, and the scope of the present invention is defined by the attached claims and their equivalents.

Claims (7)

1. A drone for industrial transportation, characterized in that it comprises: a fuselage (1), a mechanical arm (2) installed below the fuselage (1), and a flight control system arranged inside the fuselage (1); The flight control system comprises a chassis, which is installed at the bottom of a fuselage (1), and a storage compartment is formed between the fuselage (1) and the chassis. A power supply module (3) for supplying power to the flight control system and the mechanical arm (2) as a whole, and a control module (4) for controlling the flight of the unmanned aerial vehicle and the clamping of the mechanical arm (2) are arranged inside the storage compartment. 2. The unmanned aerial vehicle for industrial transportation according to claim 1 is characterized in that the control module includes a communication module (5) for receiving instructions and sending data, a navigation module (6) for providing position and posture information, a camera module (7) for transmitting image data, a payload module (8) for transmitting data, and an obstacle avoidance module (9) for providing obstacle detection information, wherein the communication module (5), the camera module (7), the payload module (8) and the obstacle avoidance module (9) are all electrically connected to the control module (4) through wires, and the navigation module (6) is connected to the control module (4) through an interface. 3. The unmanned aerial vehicle for industrial transportation according to claim 1, characterized in that the power supply module (3) includes a battery pack and a motor. 4. The unmanned aerial vehicle for industrial transportation according to claim 1, characterized in that the fuselage (1) comprises a fuselage frame and wings. 5. The unmanned aerial vehicle for industrial transportation according to claim 1 is characterized in that the flight control system includes an inertial measurement unit, a GPS compass module, an LED indicator light module, a freeRTOS system, a gyroscope, and pid control. 6. The unmanned aerial vehicle for industrial transportation according to claim 2, characterized in that the camera module (7) comprises a camera, an image transmission device and an image processing unit. 7. The unmanned aerial vehicle for industrial transportation according to claim 2, characterized in that the obstacle avoidance module (9) comprises an ultrasonic sensor, an infrared sensor and a radar.