Reinforcing structure for wing lower wall plate of unmanned aerial vehicle

Abstract

The utility model discloses an unmanned aerial vehicle wing lower wall plate reinforcing structure, which belongs to the technical field of unmanned aerial vehicles and comprises a vehicle body, wings are fixedly mounted on two sides of the vehicle body, mounting plates are arranged on lower wall plates at the bottoms of the wings and on side walls of the vehicle body, and a reinforcing rib is fixedly connected between the two mounting plates. Sliding grooves are formed in one sides of the wings, auxiliary wings are installed in the sliding grooves in a sliding mode, and adjusting assemblies enabling the sliding grooves to stretch out and draw back are arranged on the wings. Therefore, by installing the reinforcing ribs between the wings and the aircraft body, the strength of the wings can be improved, the stability of the wings is improved, the lead screws are driven by the driving motors to rotate, the auxiliary wings can enter the sliding grooves through transmission of the lead screws and the threaded grooves, and after the wings are shortened, the wings can be conveniently placed in a hangar.

Description

Technical Field

[0001] This utility model relates to a reinforcement structure for the lower wing panel of an unmanned aerial vehicle (UAV), belonging to the field of UAV technology. Background Technology

[0002] Heavy-duty drones: such as logistics delivery and agricultural spraying drones, need to carry a large weight, and the wings and fuselage are subjected to large bending moments and shear forces, so the wings are unstable.

[0003] Meanwhile, because heavy-duty drones are generally large in size and have wide wings in order to increase their payload, they are not convenient to store in a hangar when not in use. Utility Model Content

[0004] To solve the above-mentioned technical problems, this utility model provides a reinforcement structure for the lower wing panel of a drone, which can reinforce the fuselage and wings, and the wings can be extended and retracted, making it convenient to place in the hangar after the width is reduced.

[0005] The technical solution adopted by this utility model to solve its technical problem is:

[0006] A reinforcement structure for the lower wing panel of a drone includes: a fuselage, on both sides of which wings are fixedly installed; mounting plates are provided at the bottom lower wing panel and the side wall of the fuselage; a reinforcing rib is fixedly connected between the two mounting plates; a sliding groove is provided on one side of the wing; an auxiliary wing is slidably installed in the sliding groove; and an adjustment component for extending and retracting the sliding groove is provided on the wing.

[0007] Preferably, the adjustment assembly includes a lead screw, which is rotatably mounted in a slide groove. One side of the auxiliary wing has a threaded groove that is threadedly connected to the lead screw. The top side of the wing has a groove, and one side of the lead screw passes through the groove and is connected to the output end of the drive motor.

[0008] Preferably, a guide rod is installed in the groove, and a sliding hole is provided on one side of the auxiliary wing to be slidably connected to the guide rod.

[0009] Preferably, the top of the groove is provided with a cover plate.

[0010] Preferably, the cover plate and the wing are detachably installed by bolts.

[0011] Preferably, the reinforcing rib is made of carbon fiber reinforced polymer matrix composite material.

[0012] Compared with the prior art, the beneficial effects of this utility model are as follows: by installing reinforcing ribs between the wing and the fuselage, the strength of the wing can be increased and the stability of the wing can be improved. Furthermore, by driving the lead screw to rotate through the drive motor, the transmission between the lead screw and the threaded groove can allow the aileron to enter the slide groove, thereby shortening the length of the wing and making it easier to place in the hangar. Attached Figure Description

[0013] To more clearly illustrate the technical solutions in the embodiments of this utility model or the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on the structures shown in these drawings without creative effort.

[0014] Figure 1 This is a schematic diagram of the main structure of this utility model;

[0015] Figure 2 This is a schematic diagram of the reinforcing rib structure of this utility model;

[0016] Figure 3 This is a schematic diagram of the adjustment component structure of this utility model;

[0017] Figure 4 This is a schematic diagram of the auxiliary wing structure of this utility model.

[0018] In the diagram: 1. Airframe; 2. Wing; 3. Mounting plate; 4. Reinforcing rib; 5. Slide groove; 6. Auxiliary wing; 7. Adjustment assembly; 701. Lead screw; 702. Threaded groove; 703. Groove; 704. Drive motor; 705. Guide rod; 706. Slide hole; 707. Cover plate; 708. Bolt. Detailed Implementation

[0019] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0020] Please see Figure 1-4 This utility model provides a technical solution:

[0021] A reinforcement structure for the lower wing panel of a drone includes: a body 1, wings 2 fixedly mounted on both sides of the body 1, mounting plates 3 on the lower wing panel and the side wall of the body 1, a reinforcing rib 4 fixedly connected between the two mounting plates 3, a sliding groove 5 on one side of the wing 2, an auxiliary wing 6 slidably mounted in the sliding groove 5, and an adjustment component 7 on the wing 2 to extend and retract the sliding groove 5. By installing the reinforcing rib 4 between the lower wing panel and the body 1, the stability of the wing 2 can be improved.

[0022] In this embodiment: the adjustment assembly 7 includes a lead screw 701, which is rotatably installed in the slide groove 5. A threaded groove 702 is provided on one side of the auxiliary wing 6, which is threadedly connected to the lead screw 701. A groove 703 is provided on one side of the top of the wing 2. One side of the lead screw 701 passes through the groove 703 and is connected to the output end of the drive motor 704. The drive motor 704 drives the lead screw 701 to rotate. Through the transmission of the lead screw 701 and the threaded groove 702, the auxiliary wing 6 can slide in the slide groove 5.

[0023] In this embodiment: a guide rod 705 is installed in the slide groove 5, and a sliding hole 706 is opened on one side of the auxiliary wing 6 to be slidably connected with the guide rod 705. The auxiliary wing 6 slides in the slide groove 5, and the guide rod 705 slides in the sliding hole 706, which plays a limiting role for the auxiliary wing 6.

[0024] In this embodiment: The top of the groove 703 is provided with a cover plate 707, which can protect the drive motor 704 and reduce the dust accumulation on the drive motor 704.

[0025] In this embodiment: the cover plate 707 and the wing 2 are detachably installed by bolts 708. The detachability of the cover plate 707 and the wing 2 facilitates the maintenance of the drive motor 704.

[0026] In this embodiment: the material of the reinforcing rib 4 is carbon fiber reinforced polymer matrix composite material, which has the advantages of being lightweight and having high strength.

[0027] The workflow of this embodiment is as follows: The stability between the body 1 and the wing 2 can be improved by the reinforcing rib 4. When the UAV is not in use in the hangar, the drive motor 704 can be started to rotate the lead screw 701. The lead screw 701, through the transmission with the threaded groove 702, causes the auxiliary wing 6 to retract into the slide groove 5, reducing the overall width and making it easier to store in the hangar.

[0028] Although 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 alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.

Claims

1. A UAV wing lower panel stiffening structure, characterized by, The device includes a fuselage, on both sides of which wings are fixedly mounted. Mounting plates are provided on the bottom lower wall of the wings and on the side wall of the fuselage. A reinforcing rib is fixedly connected between the two mounting plates. A sliding groove is provided on one side of the wings, and an auxiliary wing is slidably mounted in the sliding groove. An adjustment component for extending and retracting the sliding groove is provided on the wings.

2. The unmanned aerial vehicle wing lower panel reinforcing structure of claim 1, wherein, The adjustment assembly includes a lead screw, which is rotatably mounted in a slide groove. One side of the auxiliary wing has a threaded groove that is threadedly connected to the lead screw. The top side of the wing has a groove, and one side of the lead screw passes through the groove and is connected to the output end of the drive motor.

3. The unmanned aerial vehicle wing lower panel stiffening structure of claim 2, wherein, A guide rod is installed in the groove, and a sliding hole is opened on one side of the auxiliary wing to slide and connect with the guide rod.

4. The unmanned aerial vehicle wing lower panel stiffening structure of claim 2, wherein, The top of the groove is provided with a cover plate.

5. The unmanned aerial vehicle wing lower panel stiffening structure of Claim 4, wherein, The cover plate and the wing are detachably installed by bolts.

6. The unmanned aerial vehicle wing lower panel stiffening structure of Claim 1, wherein, The reinforcing rib is made of carbon fiber reinforced polymer matrix composite material.

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