Airborne infrared focusing radiation detection structure of multi-rotor unmanned aerial vehicle

Abstract

The utility model discloses an airborne infrared focusing radiation detection structure of a multi-rotor unmanned aerial vehicle, and belongs to the technical field of an unmanned aerial vehicle airborne infrared detection system. Comprising a quad-rotor unmanned aerial vehicle and infrared detection equipment, the infrared detection equipment comprises an infrared radiation sensor, an acquisition control and transmission module and a directional mechanical module, the acquisition control and transmission module comprises a sampling control mainboard, a display screen, function keys, a data radio station and a sampling mechanical arm, and the top of the sampling mechanical arm is provided with a quick-mounting buckle; the bottom of the quad-rotor unmanned aerial vehicle is provided with a fast-assembly clamping seat, and the quad-rotor unmanned aerial vehicle is connected with the fast-assembly clamping seat in a matched mode through the fast-assembly buckle. According to the utility model, the infrared detection equipment is miniaturized and lightened, a special small sampling control system is developed, and control, GPS and data transmission interfaces and the like are integrated, so that the infrared detection equipment can be remotely controlled during high-altitude flight, and the safe operation of the infrared detection equipment under the unmanned aerial vehicle-mounted condition is ensured.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV)-borne infrared detection system technology, and in particular to an airborne infrared focusing radiation detection structure for a multi-rotor UAV. Background Technology

[0002] With the development of remote sensing technology, drones have been widely used in various measurement tasks. However, existing drone-borne measurement systems mostly focus on radiation measurement in visible light or other bands, and rarely use drone platforms to measure infrared radiation. Using drones to carry infrared detection equipment can significantly improve the efficiency, accuracy and safety of infrared radiation measurement. Combined with the drone's flight control system, it can accurately scan the measurement area for infrared radiation according to mission requirements and acquire infrared radiation distribution data of a large area in real time.

[0003] Most existing infrared detection devices use static measurement, rely on fixed positions, and cannot perform dynamic or large-scale measurement. They also have certain limitations in integration with UAV platforms, mainly in how to effectively monitor equipment and ensure its safe operation under high-altitude conditions, and how to ensure the stability of data acquisition under the condition of rapid UAV movement.

[0004] Therefore, it is necessary to miniaturize and lighten infrared detection equipment to make it more suitable for UAV flight platforms, optimize UAV mounting and equipment power supply systems, ensure safety during high-altitude flight operations, and develop directional mechanical modules specifically for infrared detection equipment to ensure stable and controllable measurement angles. Utility Model Content

[0005] Purpose of the utility model: The purpose of this utility model is to provide a solution to the problems mentioned in the background art.

[0006] Technical solution: A multi-rotor UAV airborne infrared focusing radiation detection structure, comprising a quadcopter UAV and an infrared detection device; the infrared detection device includes an infrared radiation sensor, a data acquisition, control and transmission module and a directional mechanical module;

[0007] The acquisition control and transmission module includes a sampling control motherboard, a display screen, function buttons, a data transmission radio, and a sampling robotic arm. The top of the sampling robotic arm is equipped with a quick-release buckle, and the bottom of the quadcopter drone is equipped with a quick-release bracket. The quick-release buckle and the quick-release bracket are connected through the quick-release buckle. There are 5 function buttons, and a power switch is provided on one side of the sampling robotic arm.

[0008] The orientation mechanical module includes an orientation robotic arm, which contains a lateral swing force unit, a pitch power unit, and an orientation control mainboard. The infrared radiation sensor is fixedly connected to the orientation robotic arm, and the orientation robotic arm is fixedly connected to the sampling robotic arm. The sampling robotic arm is connected to the quadcopter UAV via a quick-release structure.

[0009] Furthermore, a battery compartment is installed on one side of the quadcopter drone's fuselage, with a power interface 1 located above the battery compartment, and a power interface 2 located on the other side of the quadcopter drone's fuselage.

[0010] Furthermore, the sampling control motherboard is used for sampling control, data storage and transmission control of the infrared detection device.

[0011] Furthermore, the display screen, the function buttons, and the data transmission radio are used to realize human-computer interaction. The display screen and the multiple function buttons enable direct operation and control of the infrared detection device, and the data transmission radio communicates with the ground radio to enable remote control of the infrared detection device on the PC.

[0012] Furthermore, the lateral swing force unit is used to drive the directional robotic arm to swing left and right, thereby driving the infrared radiation sensor to sample the roll angle, and the pitch power unit is used to drive the infrared radiation sensor to sample the pitch angle.

[0013] Beneficial effects: This utility model miniaturizes and lightens the infrared detection equipment, and develops a special small sampling control system that integrates control, GPS and data transmission interfaces, enabling remote control of the infrared detection equipment even during high-altitude flight, ensuring its safe operation in the case of unmanned aerial vehicles.

[0014] This invention develops a directional mechanical module specifically designed for infrared detection equipment, enabling it to be oriented during infrared radiation measurement and ensuring a stable and controllable measurement angle during flight. It is also integrated with a matching UAV system, wherein the UAV platform and the infrared detection equipment have a quick-release function, allowing for rapid installation and removal. Attached Figure Description

[0015] Figure 1 This is a schematic diagram of the overall structure of this utility model;

[0016] Figure 2 This is a schematic diagram of the overall structure of the quadcopter drone of this utility model;

[0017] Figure 3 This is a schematic diagram of the overall structure of the infrared detection device of this utility model.

[0018] In the diagram: 1. Quadcopter UAV; 11. Quick-release mounting bracket; 12. Battery compartment; 121. Power interface one; 122. Power interface two; 2. Infrared detection equipment; 21. Infrared radiation sensor; 22. Data acquisition, control and transmission module; 222. Display screen; 223. Function buttons; 225. Sampling robotic arm; 226. Quick-release buckle; 228. Power switch; 23. Orientation mechanical module; 231. Orientation robotic arm; 232. Lateral swing force unit; 233. Pitch power unit. Detailed Implementation

[0019] To make the technical solution of this utility model clearer, the present utility model will be further described in detail below with reference to the accompanying drawings and specific embodiments.

[0020] Example:

[0021] like Figures 1-3 As shown, a multi-rotor UAV airborne infrared focusing radiation detection structure is provided, including a quadcopter UAV 1 and an infrared detection device 2; the infrared detection device 2 includes an infrared radiation sensor 21, a data acquisition, control and transmission module 22 and a directional mechanical module 23;

[0022] The data acquisition, control and transmission module 22 includes a sampling control motherboard, a display screen 222, function buttons 223, a data transmission radio and a sampling robotic arm 225. The top of the sampling robotic arm 225 is equipped with a quick-release buckle 226, and the bottom of the quadcopter drone 1 is equipped with a quick-release bracket 11. The quick-release buckle 226 is connected to the quick-release bracket 11. There are 5 function buttons 223. A power switch 228 is provided on one side of the sampling robotic arm 225.

[0023] The orientation mechanical module 23 includes an orientation mechanical arm 231, which contains a side swing force unit 232, a pitch power unit 233 and an orientation control motherboard. An infrared radiation sensor 21 is fixedly connected to the orientation mechanical arm 231. The orientation mechanical arm 231 is fixedly connected to a sampling mechanical arm 225. The sampling mechanical arm 225 is connected to the quadcopter UAV 1 through a quick-release structure.

[0024] A battery compartment 12 is installed on one side of the fuselage of the quadcopter drone 1. A power interface 121 is located above the battery compartment 12. A power interface 122 is located on the other side of the fuselage of the quadcopter drone 1.

[0025] First, connect the quadcopter drone 1 and the infrared detection device 2 via quick-release buckles 226 and quick-release brackets 11. Install the dedicated power supply battery for the infrared detection device 2 in the small battery compartment 12 on the drone. Connect the battery power cable to power interface 121 at the battery compartment 12. Connect the power cable for the infrared detection device 2 to the power interface and power interface 222 at the sampling robotic arm 225. Press and hold the power switch 228 on the sampling robotic arm 225 to power on and start the infrared detection device 2. The display screen 222 shows the main operation interface. Through the prompts on the LCD screen 222, operate the five function buttons 223 to view relevant information of the infrared detection device 2, set the working mode, adjust the rotation angle of the orientation mechanical module 23, etc.

[0026] The sampling control motherboard receives commands from the PC via a data transmission radio, including sampling start and stop commands, roll and pitch angle setting commands. The sampling control motherboard drives the infrared detection device 2 to perform sampling start and stop operations. The sampling control motherboard 221 transmits the roll and pitch angle setting commands to the orientation control motherboard. The orientation control motherboard drives the side swing force unit 232 and the pitch power unit 233 to perform the corresponding angle rotation.

[0027] like Figure 2 and Figure 3 As shown, the sampling control motherboard is used for sampling control, data storage and transmission control of the infrared detection device 2.

[0028] like Figure 3 As shown, the display screen 222, function buttons 223, and data transmission radio are used to realize human-computer interaction. The display screen 222 and multiple function buttons 223 enable direct operation and control of the infrared detection device 2. The data transmission radio communicates with the ground radio to realize remote control of the infrared detection device 2 on the PC.

[0029] like Figure 3 As shown, the side swing force unit 232 is used to drive the directional robotic arm 231 to swing left and right, thereby driving the infrared radiation sensor 21 to sample the roll angle, and the pitch power unit 233 is used to drive the infrared radiation sensor 21 to sample the pitch angle.

[0030] The embodiments described above are merely illustrative of several implementations of this utility model, and while the descriptions are relatively specific and detailed, they should not be construed as limiting the scope of this utility model patent. It should be noted that those skilled in the art can make various modifications and improvements without departing from the concept of this utility model, and these all fall within the protection scope of this utility model. Therefore, the protection scope of this utility model patent should be determined by the appended claims.

Claims

1. A multi-rotor unmanned aerial vehicle (UAV) airborne infrared focusing radiation detection structure, comprising a quadcopter UAV (1) and an infrared detection device (2); characterized in that: The infrared detection device (2) includes an infrared radiation sensor (21), an acquisition, control and transmission module (22), and a directional mechanical module (23). The acquisition control and transmission module (22) includes a sampling control motherboard, a display screen (222), function buttons (223), a data transmission radio and a sampling robotic arm (225). The top of the sampling robotic arm (225) is equipped with a quick-release buckle (226), and the bottom of the quadcopter drone (1) is equipped with a quick-release bracket (11). The quick-release buckle (226) and the quick-release bracket (11) are connected in cooperation. The number of function buttons (223) is 5. A power switch (228) is provided on one side of the sampling robotic arm (225). The orientation mechanical module (23) includes an orientation mechanical arm (231), which is equipped with a side swing force unit (232), a pitch power unit (233) and an orientation control motherboard (234). The infrared radiation sensor (21) is fixedly connected to the orientation mechanical arm (231), and the orientation mechanical arm (231) is fixedly connected to the sampling mechanical arm (225). The sampling mechanical arm (225) is connected to the quadcopter UAV (1) through a quick-release structure.

2. The airborne infrared focusing radiation detection structure for a multi-rotor unmanned aerial vehicle according to claim 1, characterized in that: The quadcopter drone (1) has a battery compartment (12) installed on one side of its fuselage. A power interface (121) is provided above the battery compartment (12), and a power interface (122) is provided on the other side of the fuselage of the quadcopter drone (1).

3. The airborne infrared focusing radiation detection structure for a multi-rotor unmanned aerial vehicle according to claim 1, characterized in that: The sampling control motherboard is used for sampling control, data storage and transmission control of the infrared detection device (2).

4. The airborne infrared focusing radiation detection structure for a multi-rotor unmanned aerial vehicle according to claim 1, characterized in that: The display screen (222), the function buttons (223) and the data transmission radio are used to realize human-computer interaction. The display screen (222) and the multiple function buttons (223) are used to realize direct operation and control of the infrared detection device (2). The data transmission radio communicates with the ground radio and realizes remote control of the infrared detection device (2) on the PC.

5. The airborne infrared focusing radiation detection structure for a multi-rotor unmanned aerial vehicle according to claim 1, characterized in that: The side swing force unit (232) is used to drive the directional robotic arm (231) to swing left and right, thereby driving the infrared radiation sensor (21) to perform roll angle sampling. The pitch power unit (233) is used to drive the infrared radiation sensor (21) to perform pitch angle sampling.

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