Unmanned aerial vehicle load combination

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle load combination which comprises an unmanned aerial vehicle body, a searchlight and a megaphone, a butt joint port is arranged on the surface of the top end of the unmanned aerial vehicle body, a butt joint port is arranged on the surface of the bottom end of a searchlight control box, and the megaphone is arranged on the surface of the top end of the searchlight control box. The inner side of the top end surface of the connecting piece and the inner sides of the lower portions of the surfaces of the two ends of the megaphone shell are provided with hand screws, through the combined design of the searchlight body and the megaphone body, the unmanned aerial vehicle can have the lighting function and the megaphone function at the same time, the unmanned aerial vehicle can be easily and conveniently disassembled, and the lighting function or the megaphone function can be independently used; and the functional diversity and task execution capability of the unmanned aerial vehicle are greatly improved. In complex environments such as night search and rescue, safety patrol and the like, the unmanned aerial vehicle can provide illumination by using the searchlight, and meanwhile, instruction transmission or information communication is performed through the megaphone, so that the task execution efficiency and accuracy are remarkably improved.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, in particular to a load combination of unmanned aerial vehicles. Background Art

[0002] After searching the Chinese patent document with the existing announcement number CN217563747U, a drone combination loudspeaker is disclosed, including a loudspeaker body and a drone body. The loudspeaker body includes a loudspeaker horn, a heat dissipation back cover, a control bottom box, a pan / tilt bracket, a quick-release bracket and a compression transducer. The interior of the compression transducer includes U iron, neodymium magnet, washer, PCB board, voice coil bracket and diaphragm. A horn unit is installed at one end of the loudspeaker horn. The interior of the horn unit includes a throat plug, a sound cavity, a horn throat, a horn wall and a horn mouth. The device adopts high-performance strong neodymium magnets and high magnetic permeability U iron to effectively shield the leakage of the magnetic field while reducing the size and weight of the transducer. After reducing the size of a single transducer and horn, two or more compression transducers and horn unit combinations are set to achieve a multiple increase in power and sound pressure level, and reduce the power load and heat generation of a single transducer.

[0003] With the rapid development of drone technology, its application in many fields such as agricultural monitoring, search and rescue, and security inspections has become more and more extensive. When performing these tasks, drones usually need to carry different payloads, such as searchlights and loudspeakers, to adapt to different operating environments and needs. However, existing drone systems have certain limitations in the configuration and use of payloads. Most drone designs can only support the installation of a single payload, which limits the flexibility of drone applications in complex tasks. For example, in rescue missions that require nighttime lighting and voice communication at the same time, traditional drone systems cannot be equipped with searchlights and loudspeakers at the same time, which affects the efficiency and effectiveness of mission execution; most drones only provide a single SDK data interface, which limits scenarios that require the simultaneous use of multiple payloads. Data communication and coordination between payloads become complex and inefficient, limiting the combined use and functional expansion of drone payloads; even if some drone systems allow the installation of multiple payloads, the lack of effective payload management and communication mechanisms makes it difficult for devices to work together, which not only increases the complexity of operation, but also reduces the reliability and efficiency of mission execution. Utility Model Content

[0004] The technical problem to be solved by the utility model is to overcome the defects of the prior art and provide a UAV payload combination, aiming to solve the obvious deficiencies in the prior art in the combined use, data communication and management of UAV payload equipment, which limits the performance and efficiency of UAVs in multi-load and multi-functional application scenarios.

[0005] In order to solve the above technical problems, the utility model provides the following technical solutions:

[0006] The utility model discloses a drone load combination, comprising a drone body, a searchlight and a loudspeaker, wherein a docking port is arranged on the top surface of the drone body, screw holes are arranged on both sides of the docking port, a searchlight control box is arranged on the top surface of the drone body, a docking port is arranged on the bottom surface of the searchlight control box, connecting pieces are arranged on the lower parts of the two side surfaces of the searchlight control box, connecting blocks are arranged on the rear parts of the top ends of the two side surfaces of the searchlight control box, shaft arms are arranged on the front ends of the two side surfaces of the searchlight control box, a connecting shaft is arranged on the top surface of the shaft arm, a searchlight is arranged on the end of the connecting shaft, a loudspeaker is arranged on the top surface of the searchlight control box, a loudspeaker shell is arranged on one end surface of the loudspeaker, a docking port is arranged on the bottom surface of the loudspeaker shell, and hand screws are arranged on the inner side of the end of the top surface of the connecting piece and the inner side of the lower parts of the two end surfaces of the loudspeaker shell.

[0007] As a further description of the above technical solution:

[0008] The drone body and the docking port are fixedly connected, the docking port is a Type-C port, the screw holes are symmetrically arranged at both ends, and the drone body and the searchlight control box are connected and fixed by hand screws and screw holes.

[0009] As a further description of the above technical solution:

[0010] The docking ports at the bottom of the searchlight control box and the bottom of the loudspeaker housing are both Type-C interface settings, and the searchlight control box and the connecting piece are fixedly connected, and the connecting piece is a support rod setting with a threaded hole on the inner side of the end.

[0011] As a further description of the above technical solution:

[0012] The connecting shaft and the shaft arm are fixedly connected, and the shaft arm is placed at the front end of the two side surfaces of the searchlight control box. The connecting shaft and the searchlight are fixedly connected, and the searchlight is controlled by the internal steering gear of the searchlight control box to rotate the shaft arm to drive the searchlight to rotate.

[0013] As a further description of the above technical solution:

[0014] The searchlight and the loudspeaker are connected and fixed by passing hand screws through the lower parts of the two ends of the loudspeaker shell and the connecting blocks. The searchlight and the loudspeaker can be disassembled into two parts, which are connected to the drone body through hand screws, screw holes and docking ports for separate use.

[0015] The utility model has the following beneficial effects:

[0016] In the utility model, the combination design of the searchlight body and the loudspeaker body enables the drone to have both lighting and loudspeaking functions, and can be easily disassembled, and the lighting or loudspeaking function can be used alone, which greatly improves the functional diversity and task execution capability of the drone. In complex environments such as night search and rescue, security inspections, etc., the drone can use the searchlight to provide lighting, and at the same time use the loudspeaker to convey instructions or communicate information, which significantly improves the execution efficiency and accuracy of the task. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] The accompanying drawings are used to provide a further understanding of the present invention and constitute a part of the specification. Together with the embodiments of the present invention, they are used to explain the present invention and do not constitute a limitation of the present invention. In the accompanying drawings:

[0018] Figure 1 It is a schematic diagram of the overall connection structure of the utility model;

[0019] Figure 2 It is a front view schematic diagram of the searchlight megaphone structure of the utility model;

[0020] Figure 3 It is a rear view schematic diagram of the searchlight megaphone structure of the utility model;

[0021] In the figure: 1. UAV body; 2. Searchlight; 3. Megaphone; 4. Docking port; 5. Screw hole; 6. Searchlight control box; 7. Docking port; 8. Connector; 9. Connecting block; 10. Axis arm; 11. Coupling; 13. Megaphone housing; 14. Thumb screw. DETAILED DESCRIPTION

[0022] The preferred embodiments of the present invention are described below in conjunction with the accompanying drawings. It should be understood that the preferred embodiments described herein are only used to illustrate and explain the present invention, and are not used to limit the present invention.

[0023] In the drawings, the same reference numerals all refer to the same components.

[0024] Example 1

[0025] Reference Figure 1-3The utility model provides an embodiment: a UAV load combination, including a UAV body 1, a searchlight 2 and a loudspeaker 3, a docking port 4 is provided on the top surface of the UAV body 1, screw holes 5 are provided on both sides of the docking port 4, a searchlight control box 6 is provided on the top surface of the UAV body 1, a docking port 7 is provided on the bottom surface of the searchlight control box 6, connecting pieces 8 are provided on the lower parts of the surfaces of both sides of the searchlight control box 6, connecting blocks 9 are provided on the rear parts of the top ends of the surfaces of both sides of the searchlight control box 6, shaft arms 10 are provided on the front ends of the surfaces of both sides of the searchlight control box 6, a connecting shaft 11 is provided on the top surface of the shaft arm 10, and a searchlight 2 is provided on the ends of the connecting shaft 11, a loudspeaker 3 is provided on the top surface of the searchlight control box 6, a loudspeaker shell 13 is provided on one end surface of the loudspeaker 3, a docking port 7 is provided on the bottom surface of the loudspeaker shell 13, and hand screws 14 are provided on the inner side of the end of the top surface of the connecting piece 8 and the inner side of the lower parts of the two end surfaces of the loudspeaker shell 13.

[0026] The drone body 1 and the docking port 4 are fixedly connected, the docking port 4 is a Type-C interface, the screw holes 5 are symmetrically arranged at both ends, and the drone body 1 and the searchlight control box 6 are connected and fixed by hand screws 14 and screw holes 5.

[0027] The docking port 7 at the bottom of the searchlight control box 6 and the bottom of the loudspeaker housing 13 are both Type-C interface settings, and the searchlight control box 6 and the connecting piece 8 are fixedly connected, and the connecting piece 8 is a support rod setting, and a threaded hole is set on the inner side of the end.

[0028] The connecting shaft 11 and the shaft arm 10 are fixedly connected, and the shaft arm 10 is placed at the front end of the surface of both sides of the searchlight control box 6. The connecting shaft 11 and the searchlight 2 are fixedly connected. The searchlight 2 is controlled by the internal servo of the searchlight control box 6 to rotate the shaft arm 10 to rotate the searchlight 2.

[0029] The searchlight 2 and the loudspeaker 3 are connected and fixed by inserting the hand screws 14 through the lower parts of the two ends of the loudspeaker housing 13 and the connecting block 9. The searchlight 2 and the loudspeaker 3 can be disassembled into two parts, which can be connected to the drone body 1 through the hand screws 14, the screw holes 5 and the docking port 7 for separate use.

[0030] Specifically, its structure is composed of a drone body 1, a searchlight 2, a megaphone 3, a docking port 4, a screw hole 5, a searchlight control box 6, a docking port 7, a connector 8, a connecting block 9, an axis arm 10, a connecting shaft 11, a megaphone housing 13 and a hand screw 14 to form a drone load combination. The drone load combination allows the user to flexibly combine or split the searchlight and the megaphone according to actual needs, so that it can be used as a whole device or separately. This flexibility enables the drone to adapt to more application scenarios and meet the needs of different tasks. Furthermore, by introducing a unified data exchange protocol and an intelligent recognition mechanism, efficient communication and collaborative work between load devices are achieved. Complex data exchange and command transmission can be carried out between devices, ensuring the accuracy of data and the efficiency of transmission. This not only improves the communication efficiency between the drone and the load device, but also provides strong support for the precise operation and task execution of the drone. In addition, the modular design makes the installation, disassembly and replacement of the load device simple and quick, reduces maintenance costs, and improves the reliability and stability of the equipment. At the same time, the mechanism of multi-load equipment working together ensures that the UAV can automatically coordinate the working sequence and power distribution of each device when carrying multiple load equipment, optimizes energy utilization, and prolongs the endurance of the UAV. The searchlight 2 and the loudspeaker 3 adopt a combined design, and are firmly connected by hand screws 14 to ensure that they will not loosen or fall off during flight. The docking interface 4 and the docking ports 7 of the searchlight 2 and the loudspeaker 3 are both Type-C interfaces as electrical connection parts, with a foolproof structural design, which effectively prevents mis-insertion and damage. The screw hole 5 is used to fix the UAV body 1 and the searchlight 2 and the loudspeaker 3 as a whole. The searchlight control box 6 accommodates internal components such as the steering gear and the circuit board, and the shaft arm 10 and the connecting shaft 11 are used to connect and fix the searchlight 2. At the same time, the searchlight 2 can be rotated by the steering gear. The searchlight 2 and the loudspeaker 3 both have intelligent recognition functions and can automatically recognize whether they are in a combined state. To achieve this function, the utility model designs a unified data exchange protocol, which supports multiple data types and transmission rates, ensuring efficient and stable data transmission between different load devices. Through this protocol, the drone body 1 can obtain the working status of the searchlight 2 and the loudspeaker 3 in real time, and flexibly adjust the working mode of the load device according to the task requirements. In addition, a mechanism for the coordinated work of multiple load devices has been developed. It is ensured that when the drone body 1 is equipped with multiple load devices, the load devices can automatically coordinate the working timing and power distribution of each load device, ensuring that sufficient energy supply can be obtained when used alone or in combination, and ensuring that the efficiency and effect of task execution are optimized. The drone load combination can be widely used in agricultural monitoring, search and rescue, safety inspections and other fields. Through a simple installation process, the searchlight 2 and the loudspeaker 3 can form an integrated connection and be fixed on the drone body 1.The drone body 1 can flexibly combine different payloads according to mission requirements, such as using searchlights 2 and loudspeakers 3 at the same time to adapt to complex scenarios such as night search and rescue. By introducing a unified data protocol and intelligent identification mechanism, efficient communication and collaborative work between payloads are achieved, improving the mission execution capability and practicality of the drone body 1. At the same time, the modular design simplifies the installation, disassembly and replacement process of payloads, reduces maintenance costs, and provides a strong guarantee for the rapid deployment and mission adaptability of drones.

[0031] Working principle: Align and connect the docking port 7 Type-C port at the bottom of the megaphone 3 and the docking port 7 Type-C port at the top of the searchlight 2, and then align the hand screws 14 on both sides of the megaphone housing 13 with the screw holes 5 of the connecting blocks 9 on both sides of the searchlight control box 6, and tighten them through threaded connection to complete the stable connection, and then the combination is completed, so that the searchlight 2 and the megaphone 3 are combined together to form a structural design of an integral device. Then align the docking port 7 Type C port at the bottom of the searchlight 2 with the docking port 4 Type C port at the top of the drone body 1, and then align the hand screws 14 on the inside of the connector 8 with the screw holes 5 on the drone body 1, and tighten them through threaded connection to complete the connection and fixation. The drone body 1 can use the searchlight 2 and the megaphone 3 at the same time. The design allows the user to combine the searchlight 2 and the megaphone 3 according to actual needs, or to separate them and use them separately, which greatly improves the flexibility and adaptability of the searchlight 2 and the megaphone 3. When the devices are used together, they can automatically identify the combination state. Through the customized unified data protocol, efficient data transmission can be carried out between the devices to achieve complex data exchange and command transmission. Whether used in combination or alone, the device can communicate with the drone through the SDK data interface provided by the drone. The communication mechanism ensures accurate transmission and efficient processing of data, so that the drone body 1 can perform precise operations and task execution according to the data provided by the load device. The modular design concept is adopted to make the combination, splitting and installation of the load device faster and more convenient, which not only reduces the time cost of equipment replacement and upgrading, but also provides strong support for the multi-scenario application of the drone body 1. In order to support the efficient operation of the load device, a mechanism for the coordinated work of multiple load devices is designed. It ensures that when the drone is equipped with multiple load devices, the load devices can automatically coordinate the working sequence and power distribution of each, ensure that sufficient energy supply can be obtained when used alone or in combination, and ensure that the efficiency and effect of the drone in task execution are optimized. The overall technology of UAV payload combination not only improves the usage flexibility and communication efficiency of UAV payload equipment, but also provides strong technical support for the multi-functional application and mission execution of UAV.

[0032] Finally, it should be noted that the above description is only a preferred embodiment of the utility model and is not intended to limit the utility model. Although the utility model is described in detail with reference to the above embodiments, those skilled in the art can still modify the technical solutions recorded in the above embodiments or replace some of the technical features therein by equivalents. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the utility model shall be included in the protection scope of the utility model.

Claims

1. A drone load combination, comprising a drone body (1), a searchlight (2) and a loudspeaker (3), characterized in that: The top surface of the drone body (1) is provided with a docking port (4), and screw holes (5) are provided on both sides of the docking port (4). The top surface of the drone body (1) is provided with a searchlight control box (6), and the bottom surface of the searchlight control box (6) is provided with a docking port (7). Connectors (8) are provided at the lower part of the two side surfaces of the searchlight control box (6), and connecting blocks (9) are provided at the rear part of the top of the two side surfaces of the searchlight control box (6). The front end of the two side surfaces of the searchlight control box (6) is provided with There is an arm (10), the top surface of the arm (10) is provided with a connecting shaft (11), the ends of the connecting shaft (11) are provided with searchlights (2), the top surface of the searchlight control box (6) is provided with a loudspeaker (3), one end surface of the loudspeaker (3) is provided with a loudspeaker shell (13), the bottom surface of the loudspeaker shell (13) is provided with a docking port (7), and the inner side of the end of the top surface of the connecting piece (8) and the inner side of the lower part of the two end surfaces of the loudspeaker shell (13) are provided with hand screws (14).

2. The UAV load combination according to claim 1, characterized in that: The drone body (1) and the docking interface (4) are fixedly connected, the docking interface (4) is a Type-C interface, the screw holes (5) are symmetrically arranged at both ends, and the drone body (1) and the searchlight control box (6) are connected and fixed by hand screws (14) cooperating with the screw holes (5).

3. The UAV load combination according to claim 1, characterized in that: The docking ports (7) at the bottom of the searchlight control box (6) and the bottom of the loudspeaker housing (13) are both provided with Type-C interfaces, and the searchlight control box (6) and the connecting piece (8) are fixedly connected, wherein the connecting piece (8) is provided with a support rod, and a threaded hole is provided on the inner side of the end.

4. The UAV load combination according to claim 1, characterized in that: The connecting shaft (11) and the shaft arm (10) are fixedly connected, and the shaft arm (10) is placed at the front ends of the surfaces on both sides of the searchlight control box (6). The connecting shaft (11) and the searchlight (2) are fixedly connected, and the searchlight (2) is controlled by the steering gear inside the searchlight control box (6) to rotate the shaft arm (10) to rotate the searchlight (2).

5. The UAV load combination according to claim 1, characterized in that: The searchlight (2) and the megaphone (3) are connected and fixed by inserting hand screws (14) through the lower parts of both ends of the megaphone housing (13) and the connecting block (9). The searchlight (2) and the megaphone (3) can be disassembled into two parts, which can be connected to the drone body (1) through the hand screws (14), the screw holes (5) and the docking port (7) for separate use.

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