Quick-release connecting structure of unmanned aerial vehicle module

Abstract

The utility model discloses an unmanned aerial vehicle module quick release connecting structure, which comprises a fuselage, a motor and wings, two mounting rods are symmetrically and fixedly mounted on each of two sides of the fuselage, and a slot is formed in one end, far away from the fuselage, of each mounting rod; one end of the wing is inserted into the slot at one end of the mounting rod, the electromagnet and the magnet block are attracted together, so that the assembly between the wing and the mounting rod is completed, and then the motor can be clamped and mounted in the arc-shaped slot formed by the wing, the arc-shaped plate and the anti-collision frame, so that the assembly between the motor and the wing is completed; the whole unmanned aerial vehicle is convenient to assemble, the assembling process is simplified, the assembling efficiency is improved, meanwhile, it is ensured that the unmanned aerial vehicle can normally and stably run after being assembled, standardized interfaces and connecting pieces are adopted between the modules, complex debugging and calibration are not needed in the assembling process, and the assembling efficiency is improved. And the convenience and high efficiency of overall assembly of the unmanned aerial vehicle are successfully realized.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles (UAVs), and in particular to a quick-detachable connection structure of an UAV module. Background Art

[0002] Drones are a general term for unmanned aerial vehicles (UAVs). These are equipped with flight controllers, GPS, and other equipment, allowing them to be tracked and located by ground stations or pilots. Compared to manned aircraft, UAVs offer advantages such as small size, low cost, and ease of use. They can be launched and recovered by radio remote control and are reusable.

[0003] Most drones currently on the market have complex interconnections between components, making disassembly and reassembly difficult. This not only impacts the user experience but also creates challenges for precise management and maintenance. This inconvenience, particularly in complex environments or over long distances, further reduces operational efficiency and increases safety risks. Utility Model Content

[0004] The purpose of the present invention is to provide a quick-release connection structure for a drone module to solve the problems raised in the above-mentioned background technology.

[0005] To achieve the above-mentioned purpose, the present invention provides the following technical solutions: a quick-release connection structure of a drone module, comprising a fuselage, a motor and wings, two mounting rods are symmetrically fixedly installed on both sides of the fuselage, a slot is provided inside the mounting rod at one end away from the fuselage, a clamping rod is fixedly installed inside the slot, an electromagnet is fixedly installed at one end of the clamping rod, a support seat is fixedly installed at the bottom of the motor, an annular groove is provided on the outer side of the top of the support seat, a propeller is fixedly installed at the output end of the motor, an arc plate is fixedly installed at one end of the wing, an anti-collision frame is fixedly installed at the end of the arc plate away from the wing, an arc block is fixedly installed on the inner side of the arc plate, a clamping groove is provided inside the end of the wing away from the arc plate, and a magnet block is fixedly installed inside the clamping groove.

[0006] Preferably, the specifications of the outer diameter of the wing match the specifications of the inner diameter of the slot, and the specifications of the outer diameters of the clamping rod and the electromagnet match the specifications of the inner diameter of the clamping slot.

[0007] Preferably, the magnetic poles of the electromagnet and the opposite surface of the magnet block are opposite.

[0008] Preferably, the specifications and dimensions of the outer contour of the arc block are adapted to the specifications and dimensions of the inner contour of the annular groove, and the position of the arc block corresponds to the position of the annular groove, and the inner contour of the arc formed by the wing, arc plate and anti-collision frame is adapted to the outer contour of the motor.

[0009] Preferably, an electric pan-tilt head is fixedly mounted on the bottom of the fuselage, and a camera is mounted inside the electric pan-tilt head.

[0010] Preferably, a fluorescent block is fixedly mounted on the outer side of the support seat, and an anti-collision rod is fixedly mounted on the top of the anti-collision frame away from the end of the arc-shaped plate.

[0011] Compared with the prior art, the beneficial effect of the present invention is that by inserting one end of the wing into the slot at one end of the mounting rod, the electromagnet and the magnet block are adsorbed together, thereby completing the assembly between the wing and the mounting rod, and then the motor can be clamped and installed inside the arc groove composed of the wing, the arc plate and the anti-collision frame, thereby completing the assembly between the motor and the wing, facilitating the assembly of the entire drone, simplifying the assembly process, and improving the assembly efficiency. At the same time, it ensures that the drone can operate normally and stably after assembly. Standardized interfaces and connectors are used between modules, so that complicated debugging and calibration are not required during assembly, successfully achieving the convenience and efficiency of the overall assembly of the drone. BRIEF DESCRIPTION OF THE DRAWINGS

[0012] Figure 1 This is a schematic diagram of the three-dimensional appearance structure of the utility model.

[0013] Figure 2 It is a schematic diagram of the three-dimensional structure of the fuselage of the utility model.

[0014] Figure 3 It is a schematic diagram of the partial three-dimensional structure of the utility model.

[0015] Figure 4 This is a schematic diagram of the three-dimensional structure of the wing of the utility model.

[0016] In the figure: 1. Fuselage; 2. Motor; 3. Wing; 4. Propeller; 5. Support base; 6. Anti-collision bar; 7. Electric gimbal; 8. Camera; 9. Mounting rod; 10. Arc plate; 11. Slot; 12. Electromagnet; 13. Snap-on rod; 14. Annular groove; 15. Fluorescent block; 16. Snap-on groove; 17. Magnet block; 18. Arc block; 19. Anti-collision frame. DETAILED DESCRIPTION

[0017] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0018] See also Figure 1-Figure 4The utility model provides a technical solution: a quick-release connection structure of a drone module, including a fuselage 1, a motor 2 and a wing 3. Two mounting rods 9 are symmetrically fixedly installed on both sides of the fuselage 1. A slot 11 is provided inside the mounting rod 9 at one end away from the fuselage 1. A clamping rod 13 is fixedly installed inside the slot 11. An electromagnet 12 is fixedly installed at one end of the clamping rod 13. A support seat 5 is fixedly installed at the bottom of the motor 2. An annular groove 14 is provided on the outer side of the top of the support seat 5. A propeller 4 is fixedly installed at the output end of the motor 2. An arc plate 10 is fixedly installed at one end of the wing 3. An anti-collision frame 19 is fixedly installed at the end of the arc plate 10 away from the wing 3. An arc block 18 is fixedly installed on the inner side, and a snap-in groove 16 is opened inside the end of the wing 3 away from the arc plate 10, and a magnet block 17 is fixedly installed inside the snap-in groove 16. The specifications and dimensions of the outer diameter of the wing 3 match the specifications and dimensions of the inner diameter of the slot 11, and the specifications and dimensions of the outer diameter of the snap-in rod 13 and the electromagnet 12 match the specifications and dimensions of the inner diameter of the snap-in groove 16. The magnetic poles of the opposite surfaces of the electromagnet 12 and the magnet block 17 are opposite, and the specifications and dimensions of the outer contour of the arc block 18 match the specifications and dimensions of the inner contour of the annular groove 14, and the position of the arc block 18 corresponds to the position of the annular groove 14. The inner contour of the arc formed by the wing 3, the arc plate 10 and the anti-collision frame 19 is adapted to the outer contour of the motor 2.

[0019] The working principle of the above technical solution is: when the drone needs to be assembled, one end of the wing 3 can be first inserted into the slot 11 at one end of the mounting rod 9, and the clamping rod 13 and the electromagnet 12 inside the slot 11 can be inserted into the clamping slot 16 at one end of the wing 3. At this time, the switch button on the top of the fuselage 1 can be pressed to make the battery inside the fuselage 1 supply power to the electromagnet 12, so that the electromagnet 12 and the magnet block 17 are adsorbed together, thereby completing the assembly between the wing 3 and the mounting rod 9, and then the motor 2 can be clamped and installed in the arc groove formed by the wing 3, the arc plate 10 and the anti-collision frame 19, and the arc block 18 can be clamped and installed in the annular groove 14, thereby completing the assembly between the motor 2 and the wing 3, making it convenient to assemble the drone as a whole, simplifying the assembly process, and improving the assembly efficiency. At the same time, it ensures that the drone can operate normally and stably after assembly. Standardized interfaces and connectors are used between modules, so that complicated debugging and calibration are not required during assembly, successfully achieving the convenience and efficiency of the overall assembly of the drone.

[0020] In another embodiment, Figure 1-Figure 4 As shown, an electric pan-tilt head 7 is fixedly installed on the bottom of the fuselage 1, and a camera 8 is installed inside the electric pan-tilt head 7.

[0021] The flight path of the UAV can be photographed by the provided camera 8, thereby improving the practicality of the UAV. In addition, the direction of the camera 8 can be changed by the provided electric pan-tilt platform 7.

[0022] In another embodiment, Figure 1-Figure 4 As shown, a fluorescent block 15 is fixedly installed on the outer side of the support seat 5, and an anti-collision rod 6 is fixedly installed on the top of the anti-collision frame 19 away from the arc plate 10.

[0023] The fluorescent block 15 is provided to facilitate staff to identify the UAV at night, and the anti-collision frame 19 and the anti-collision rod 6 are provided to protect the propeller 4 to prevent the propeller 4 from being hit when the UAV is flying.

[0024] Working principle: When the drone needs to be assembled, first, one end of the wing 3 can be inserted into the slot 11 at one end of the mounting rod 9, and the clamping rod 13 and the electromagnet 12 inside the slot 11 can be inserted into the clamping slot 16 at one end of the wing 3. At this time, the switch button on the top of the fuselage 1 can be pressed to make the battery inside the fuselage 1 supply power to the electromagnet 12, so that the electromagnet 12 and the magnet block 17 are adsorbed together, thereby completing the assembly between the wing 3 and the mounting rod 9, and then the motor 2 can be clamped and installed in the arc groove formed by the wing 3, the arc plate 10 and the anti-collision frame 19, and the arc block 1 8 is snap-fitted and installed inside the annular groove 14, thereby completing the assembly between the motor 2 and the wing 3, making it convenient to assemble the entire drone, simplifying the assembly process, and improving the assembly efficiency. At the same time, it ensures that the drone can operate normally and stably after assembly. Standardized interfaces and connectors are used between modules, so that complicated debugging and calibration are not required during assembly, and the convenience and efficiency of the overall assembly of the drone are successfully achieved. The flight path of the drone can be photographed through the provided camera 8, thereby improving the practicality of the drone. In addition, the direction of the camera 8 can be changed through the provided electric gimbal 7.

[0025] Although the embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and variations may 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 appended claims and their equivalents.

Claims

1. A quick-release connection structure for a drone module, comprising a fuselage (1), a motor (2) and wings (3), characterized in that: Two mounting rods (9) are symmetrically fixedly installed on both sides of the body (1), a slot (11) is provided inside the mounting rod (9) at one end away from the body (1), a clamping rod (13) is fixedly installed inside the slot (11), an electromagnet (12) is fixedly installed at one end of the clamping rod (13), a support seat (5) is fixedly installed at the bottom of the motor (2), an annular groove (14) is provided on the outer side of the top of the support seat (5), and the motor The output end of (2) is fixedly mounted with a propeller (4), one end of the wing (3) is fixedly mounted with an arc plate (10), the end of the arc plate (10) away from the wing (3) is fixedly mounted with an anti-collision frame (19), the inner side of the arc plate (10) is fixedly mounted with an arc block (18), the interior of the end of the wing (3) away from the arc plate (10) is provided with a clamping groove (16), and the interior of the clamping groove (16) is fixedly mounted with a magnet block (17).

2. The quick-release connection structure of a drone module according to claim 1, characterized in that: The outer diameter of the wing (3) matches the inner diameter of the slot (11), and the outer diameters of the clamping rod (13) and the electromagnet (12) match the inner diameter of the clamping slot (16).

3. The quick-release connection structure of a drone module according to claim 2, characterized in that: The magnetic poles of the electromagnet (12) and the magnet block (17) facing each other are opposite.

4. The quick-release connection structure of a drone module according to claim 3, characterized in that: The specifications and dimensions of the outer contour of the arc block (18) are adapted to the specifications and dimensions of the inner contour of the annular groove (14), and the position of the arc block (18) corresponds to the position of the annular groove (14). The inner contour of the arc formed by the wing (3), the arc plate (10) and the anti-collision frame (19) is adapted to the outer contour of the motor (2).

5. The quick-release connection structure of a drone module according to claim 4, characterized in that: An electric pan-tilt platform (7) is fixedly mounted on the bottom of the fuselage (1), and a camera (8) is mounted inside the electric pan-tilt platform (7).

6. The quick-release connection structure of a drone module according to claim 5, characterized in that: A fluorescent block (15) is fixedly mounted on the outer side of the support seat (5), and an anti-collision rod (6) is fixedly mounted on the top of the anti-collision frame (19) away from one end of the arc plate (10).

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