Efficient balanced unmanned aerial vehicle construction method

Abstract

The invention relates to an efficient and balanced unmanned aerial vehicle construction method. An unmanned aerial vehicle constructed according to the method comprises an unmanned aerial vehicle body, a propeller propeller * 9, a motor * 9, a plastic interface * 8, a power supply notch * 1, a gyroscope * 1, an accelerometer * 1, a compass * 1, a barometer * 1 and a camera * 1. The method is characterized in that four wings of an unmanned aerial vehicle body constructed according to the method are connected with two lightweight plastic interfaces, the interior of each plastic interface is connected with a wire, and the exterior of each plastic interface is connected with a small motor and further connected with a propeller pusher. And a propeller pusher is also arranged behind the machine body and is used for accelerating the advancing speed. A camera adopting an electronic anti-shake technology is arranged below an unmanned aerial vehicle body and used for obtaining stable and clear images, and a gyroscope, an accelerometer, a compass and a barometer are further arranged below the unmanned aerial vehicle body and used for detecting information such as the posture, the speed, the height and the environment state of the unmanned aerial vehicle, and the information can be fed back to a flight controller to be analyzed and controlled. And finally, a power notch is formed in the lower portion and used for containing a battery, supplying power and ensuring safety and compatibility, and the interior of a power source is connected with a motor through a wire so as to provide power for the propeller thruster to enable the propeller thruster to rotate.

Description

Technical Field

[0001] This invention relates to the field of unmanned aerial vehicle (UAV) technology, and in particular to a method for constructing a highly efficient and balanced UAV. The UAV constructed according to this method possesses rapid movement capabilities while maintaining stability, and provides users with clear and stable real-time video, thereby further improving user work efficiency. This invention can be effectively applied to various fields, such as meteorological observation, search and rescue, geological exploration, and aerial photography. Background Technology

[0002] Currently, for many high-risk or dangerous missions, such as search and rescue, disaster monitoring, battlefield reconnaissance, and exploration of confined areas like caves and karst formations where humans cannot or face significant danger, the use of drones can greatly reduce casualties and life-threatening risks. Furthermore, drones offer high efficiency and low cost. However, as mission requirements become increasingly complex, simple drones are no longer sufficient for certain specific application needs, and their functionality is limited in emergency situations.

[0003] Traditionally constructed drones only offer flight capabilities and rudimentary camera recording, failing to guarantee rapid movement or stable and clear images. Therefore, drones built using traditional methods are unsuitable for certain emergency situations. This proposed method addresses these shortcomings of traditional drones by developing a highly efficient and balanced drone construction method with strong propulsion and the ability to transmit clear and stable images. This method can be widely applied in various emergency situations, significantly improving mission processing efficiency. Summary of the Invention

[0004] The purpose of this invention is to provide a highly efficient and balanced method for constructing unmanned aerial vehicles (UAVs). UAVs constructed using this method can be effectively applied to various scenarios, such as search and rescue, exploration, monitoring, and reconnaissance. This significantly enhances mission completion efficiency while ensuring user safety.

[0005] This application provides a method for constructing an efficient and balanced unmanned aerial vehicle (UAV). The UAV structure constructed according to this method includes: a UAV body, characterized by having two plastic interfaces above each of the four wings of the UAV body, the interfaces connecting to motors and subsequently to propeller thrusters. A power supply, camera, gyroscope, accelerometer, compass, and barometer are placed below the body. A propeller thruster is placed at the rear of the body.

[0006] The propeller thruster is powered by a motor connected to a power source via internal wires. The plastic interface is hollow, allowing for internal wire connections and external motor housing. Made of lightweight carbon fiber composite material, the interface is lightweight, rigid, and impact-resistant. The gyroscope, accelerometer, compass, and barometer are all powered by the flight control board inside the drone's fuselage. The camera uses Electronic Image Stabilization (EIS) to counteract image shake and improve image stability as much as possible. All components below the fuselage are secured to the drone's body with screws to prevent damage during flight. The drone is designed to withstand drops; the propeller thruster is made of streamlined, curved metal material for durability; the motor has an intelligent sensing system that detects when a user approaches or holds the drone and disconnects the power supply to prevent accidental activation and injury; the power supply slot is made of copper alloy to ensure stable and reliable power transmission; the gyroscope's core component, the gyroscope wheel, is made of aluminum alloy, offering advantages such as light weight, high tensile strength, and good corrosion resistance; the accelerometer is manufactured using microelectromechanical systems (MEMS) technology, incorporating silicon, polycrystalline silicon, metal, and insulating materials; the compass's core component, the magnetic field sensor, is made of permanent magnets, possessing excellent magnetic properties. The compass casing is made of lightweight plastic to reduce the drone's payload; the barometer is made of silicon, exhibiting excellent mechanical properties and chemical stability.

[0007] The propeller thruster is activated by a button on the flight controller, and can be either activated when the propeller thruster is not activated, or activated when the propeller thruster is activated, or deactivated when the propeller thruster is activated.

[0008] The propeller thruster is activated via a control button on the flight controller. The steps are as follows: the control button on the flight controller transmits a signal wirelessly to the UAV's flight control system; upon receiving the control signal, the UAV's flight control system forwards it to the electronic speed controller (ESC); the ESC, upon receiving the control signal, starts the motor according to the signal's instructions. The ESC provides appropriate current and voltage to the motor, causing it to rotate; once started, the motor drives the propeller thruster to begin rotating. The motor generates torque through the interaction of internal coils and a magnetic field, thus causing the propeller thruster to rotate.

[0009] The steps to stop the propeller thruster rotation via the control button on the flight controller are as follows: The control button on the flight controller transmits a signal to the UAV's flight control system via wireless communication; after receiving the control signal, the flight control system parses the command and determines that it is a command to stop rotation; once the flight control system parses the command to stop rotation, it transmits the corresponding command to the ESC; after receiving the command to stop rotation, the ESC reduces or interrupts the current supply to the motor, thereby stopping the motor rotation; when the motor stops rotating, the propeller thruster also stops rotating; the propeller provides the UAV with propulsion for movement, increasing its speed. When the UAV starts, the propellers under the wings and fuselage rotate, providing strong thrust to make the UAV take off quickly while maintaining stability. When moving forward or backward, the propeller at the rear of the fuselage rotates, further increasing the movement speed; in this embodiment, after the propeller thruster is activated, the UAV slowly ascends, and after reaching the set altitude, the UAV can be controlled to move using the control joystick on the flight controller. Attached Figure Description

[0010] To more clearly describe the embodiments of this application, the design drawings of this application will be briefly introduced below.

[0011] Figure 1 is a top view of the UAV structure constructed according to the method of the present invention; Figure 2 is a bottom view of the UAV structure constructed according to the method of the present invention; Figure 3 is a side view of the UAV structure constructed according to the method of the present invention. Explanation of the labels in the diagram: The drone body (1), plastic interface (2), propeller thruster (3), motor (4), camera (5), gyroscope (6), accelerometer (7), compass (8), barometer (9), power supply slot (10). Detailed Implementation

[0012] To make the objectives, technical solutions, and advantages of this application clearer, the following detailed description is provided in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative and not intended to limit the scope of this application.

[0013] Please refer to Figures 1 to 3. This application provides a method for constructing an efficient and balanced unmanned aerial vehicle (UAV). The UAV structure constructed according to this method includes: a UAV body, characterized by having two plastic interfaces above each of the four wings of the UAV body, with the interfaces connecting to motors and subsequently to propeller thrusters. A power supply, camera, gyroscope, accelerometer, compass, and barometer are placed below the body. A propeller thruster is placed at the rear of the body.

[0014] In this embodiment, the propeller actuator obtains power by being connected to a power source via a motor and internal wires.

[0015] In this embodiment, the plastic interface is hollow inside, allowing for the connection of wires inside and the placement of a motor on the outside.

[0016] In this embodiment, the plastic interface is made of lightweight carbon fiber composite material, which has the characteristics of being lightweight, having good rigidity, and having strong impact resistance.

[0017] In this embodiment, the gyroscope, accelerometer, compass, and barometer are all powered by the flight control main control board inside the UAV body.

[0018] In this embodiment, the camera uses Electronic Image Stabilization (EIS) to counteract image shake and improve image stability as much as possible.

[0019] In this embodiment, all components below the fuselage are fixed to the drone fuselage with screws to prevent them from falling off during flight.

[0020] In this embodiment, the propeller thruster is made of a curved, streamlined metal material, which is highly durable.

[0021] In this embodiment, the motor has an intelligent sensing system that can sense when a user approaches or holds the drone and disconnect the current supply to prevent accidental injury from touching the drone's switch.

[0022] In this embodiment, the power supply slot is made of copper alloy to ensure the stability and reliability of power transmission.

[0023] In this embodiment, the core component of the gyroscope, the gyroscope wheel, is made of aluminum alloy, which has the advantages of being lightweight, having high tensile strength, and being corrosion resistant.

[0024] In this embodiment, the accelerometer is manufactured using microelectromechanical systems (MEMS) technology and comprises silicon, polycrystalline silicon, metal, and insulating materials.

[0025] In this embodiment, the core component of the compass, the magnetic field sensor, is made of a permanent magnet, possessing excellent magnetic properties. Meanwhile, the compass casing is made of lightweight plastic, reducing the payload of the drone.

[0026] In this embodiment, the barometer is made of silicon, which has excellent mechanical properties and chemical stability.

[0027] In this embodiment, the propeller thruster is activated by a button on the flight controller, which can be either: the propeller thruster is not activated but is started by the control button; or the propeller thruster is activated but is stopped by the control button.

[0028] In this embodiment, the propeller thruster is activated via a control button on the flight controller. The steps are as follows: the control button on the flight controller transmits a signal wirelessly to the UAV's flight control system; upon receiving the control signal, the UAV's flight control system forwards the signal to the electronic speed controller (ESC); the ESC receives the control signal and activates the motor according to the signal's instructions. The ESC provides appropriate current and voltage to the motor, thereby inducing the motor to rotate; after the motor starts, it drives the propeller thruster to begin rotating. The motor generates torque through the interaction of internal coils and magnetic fields, thus causing the propeller thruster to rotate.

[0029] In this embodiment, the propeller thruster is stopped by a control button on the flight controller. The steps are as follows: the control button on the flight controller transmits a signal to the UAV's flight control system via wireless communication; after receiving the control signal, the flight control system parses the command and determines that it is a command to stop rotation; once the flight control system parses the command to stop rotation, it transmits the corresponding command to the ESC; after receiving the command to stop rotation, the ESC reduces or interrupts the current supply to the motor, thereby stopping the motor from rotating; when the motor stops rotating, the propeller thruster also stops rotating.

[0030] In this embodiment, after the propeller thruster is activated, the drone slowly ascends into the air. Once it reaches the set altitude, the drone can be controlled to move using the control joystick on the flight controller. As the drone moves, the propeller at the rear of the drone rotates accordingly, further increasing the drone's speed.

[0031] Propellers provide the thrust for drones, increasing their speed. When a drone takes off, the propellers on its wings rotate, providing powerful thrust to lift it into the air while maintaining stability. As it moves, the propellers at the rear of the drone rotate, further increasing its speed.

[0032] The above-described specific embodiments are merely preferred embodiments of this invention and are not intended to limit this invention. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of this invention should be included within the protection scope of this invention.

Claims

1. A method for constructing an efficient and balanced unmanned aerial vehicle (UAV), characterized in that... The structure constructed according to this method includes: a drone fuselage, characterized by two plastic interfaces above each of the four wings of the drone fuselage, the interfaces connecting to motors and subsequently to propeller thrusters. A power supply, camera, gyroscope, accelerometer, compass, and barometer are placed below the fuselage. A propeller thruster is placed at the rear of the fuselage.

2. The efficient and balanced UAV construction method according to claim 1, characterized in that, The propeller thruster is powered by a motor connected to a power source via internal wires. The plastic interface is hollow, allowing for internal wire connections and external motor housing. Made of lightweight carbon fiber composite material, the plastic interface is lightweight, rigid, and impact-resistant. The gyroscope, accelerometer, compass, and barometer are all powered by the flight control board inside the drone's fuselage. The camera uses Electronic Image Stabilization (EIS) to counteract image shake and improve image stability as much as possible. Components below the fuselage are secured to the drone body with screws to prevent them from falling off during flight. The propeller thruster is made of streamlined, curved metal material, ensuring durability.

3. The efficient and balanced UAV construction method according to claim 1, characterized in that... The motor has an intelligent sensing system that can sense when a user approaches or holds the drone and disconnect the current supply to prevent accidental injury from touching the drone's switch. The power supply slot is made of copper alloy to ensure the stability and reliability of power transmission. The gyroscope's core component, the gyroscope wheel, is made of aluminum alloy, which has advantages such as light weight, high tensile strength, and good corrosion resistance. The accelerometer is manufactured using microelectromechanical systems (MEMS) technology and includes silicon, polycrystalline silicon, metals, and insulating materials.

4. The efficient and balanced UAV construction method according to claim 1, characterized in that... The core component of the compass, the magnetic field sensor, is made of permanent magnets and possesses excellent magnetic properties. The compass housing is made of lightweight plastic, reducing the drone's payload; the barometer is made of silicon, offering excellent mechanical properties and chemical stability. The propeller thrusters are controlled by buttons on the flight controller, with the following modes: the propeller thrusters are not activated but are started via the control button; the propeller thrusters are already activated but are stopped via the control button.

5. A method for constructing an efficient and balanced unmanned aerial vehicle according to claim 15, characterized in that... The propeller thruster is activated via a control button on the flight controller. The steps are as follows: the control button on the flight controller transmits a signal wirelessly to the UAV's flight control system; upon receiving the control signal, the UAV's flight control system forwards it to the electronic speed controller (ESC); the ESC, upon receiving the control signal, starts the motor according to the signal's instructions. The ESC provides appropriate current and voltage to the motor, causing it to rotate; once started, the motor drives the propeller thruster to begin rotating. The motor generates torque through the interaction of internal coils and a magnetic field, thus causing the propeller thruster to rotate.

6. A method for constructing an efficient and balanced unmanned aerial vehicle according to claim 15, characterized in that... To stop the propeller thruster from rotating via a control button, the steps are as follows: The control button on the flight controller transmits a signal wirelessly to the UAV's flight control system. Upon receiving the control signal, the flight control system analyzes the command and determines if it is a stop-rotation command. Once the flight control system determines the stop-rotation command, it transmits the corresponding command to the electronic speed controller (ESC). Upon receiving the stop-rotation command, the ESC reduces or interrupts the current supply to the motor, thus stopping the motor's rotation. When the motor stops rotating, the propeller thruster also stops rotating. After the propeller thruster is activated, the UAV slowly ascends. Once it reaches the set altitude, the UAV can be controlled to move using the control stick on the flight controller.

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