Gravity center adjusting assembly of unmanned aerial vehicle and unmanned aerial vehicle

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, and discloses an unmanned aerial vehicle gravity center adjusting assembly and an unmanned aerial vehicle, the unmanned aerial vehicle gravity center adjusting assembly comprises an unmanned aerial vehicle equipment body, adjusting mechanisms are arranged on the outer walls of the left end and the right end, away from each other, of the unmanned aerial vehicle equipment body respectively, and each adjusting mechanism comprises an adjusting supporting block, a balance weight supporting column, a fixed supporting block and a balance weight supporting block; a deploying mechanism is arranged at the bottom end of the unmanned aerial vehicle equipment body, the deploying mechanism comprises a positioning mounting plate and a counterweight transverse plate, the two adjusting supporting blocks are fixedly mounted on the outer walls of the left end and the right end, away from each other, of the unmanned aerial vehicle equipment body correspondingly, and a plurality of adjusting mounting grooves are formed in the top end walls of the two adjusting supporting blocks correspondingly. According to the utility model, through the cooperation of the adjusting support block and the counterweight support column with the positioning support plate and the cooperation of the fixed support block and the counterweight support block, the counterweight of the unmanned aerial vehicle equipment body can be freely adjusted, and the counterweight can be rapidly disassembled and assembled.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles (UAVs), in particular to a gravity center adjustment component of a UAV and the UAV. Background Art

[0002] Unmanned aerial vehicles (UAVs) are aircraft that can perform tasks without the need for direct human control. They can fly and perform tasks via pre-set routes, autonomous control systems, or remote operation.

[0003] The characteristics and applications of drones can be summarized as follows:

[0004] Diverse applications: Drones are widely used in military reconnaissance, intelligence collection, and target strikes. They are also used in the civilian field for various tasks such as aerial photography, disaster monitoring, agricultural plant protection, and logistics distribution.

[0005] Technological innovation: With technological advancements, drones’ flight performance, sensor technology, and autonomous control capabilities are constantly improving, enabling them to cope with more complex tasks and environments.

[0006] Improve efficiency and safety: In agriculture, drones can be used to precisely spray pesticides and fertilizers, improving operational efficiency while reducing the impact of chemicals on the environment and operators.

[0007] Emergency response and disaster management: Drones can be quickly deployed to disaster areas for aerial surveys, providing real-time imagery and data support to aid disaster management and rescue efforts.

[0008] Surveillance and Security: In the security sector, drones are used for border patrols, large-scale event security, and monitoring of important facilities, improving surveillance capabilities and response speed.

[0009] Laws and regulations: With the popularity of drones, countries have formulated relevant laws and regulations to stipulate issues such as drone flight restrictions, privacy protection and flight licenses to ensure their safe and legal use.

[0010] In the prior art, although the center of gravity adjustment assembly of the drone can adjust the center of gravity of the drone when in use, it cannot be quickly disassembled or adjusted, which greatly reduces the practicality and efficiency of the device.

[0011] To this end, we propose a center of gravity adjustment component for a UAV and a UAV. Utility Model Content

[0012] The utility model mainly solves the technical problems existing in the above-mentioned prior art and provides a center of gravity adjustment component for a drone and a drone.

[0013] In order to achieve the above-mentioned purpose, the present invention adopts the following technical scheme: the center of gravity adjustment component of the drone includes a drone equipment body, and adjustment mechanisms are respectively provided on the outer walls of the left and right ends of the drone equipment body that are far away from each other. The adjustment mechanism includes an adjustment support block and a counterweight pillar and a fixed support block and a counterweight support block. The bottom end of the drone equipment body is provided with a deployment mechanism, and the deployment mechanism includes a positioning mounting plate and a counterweight cross plate.

[0014] As a preferred technical solution of the present invention, there are two adjusting support blocks, which are respectively fixedly mounted on the left and right outer walls of the drone equipment body that are away from each other.

[0015] As a preferred technical solution of the present invention, a plurality of adjustment mounting grooves are respectively provided on the top walls of the two adjustment support blocks.

[0016] As a preferred technical solution of the present invention, there are a plurality of counterweight pillars, and the plurality of counterweight pillars are movably installed in a plurality of adjustment installation slots respectively.

[0017] As an optimal technical solution of the present invention, positioning support plates are fixedly installed on the top walls of multiple counterweight pillars. There are multiple fixed support blocks, and the multiple fixed support blocks are fixedly installed on the left and right outer walls of the two adjustment support blocks that are far away from each other.

[0018] As a preferred technical solution of the present invention, counterweight installation grooves are respectively opened on the top walls of the plurality of fixed support blocks. There are a plurality of counterweight support blocks, and the plurality of counterweight support blocks are movably installed in the plurality of fixed support blocks.

[0019] As a preferred technical solution of the present invention, there are two positioning mounting plates, which are respectively fixedly mounted on the bottom end wall of the drone equipment body.

[0020] As a preferred technical solution of the present invention, a plurality of limiting screw grooves are respectively provided on the bottom end walls of the two positioning mounting plates.

[0021] As a preferred technical solution of the present invention, a plurality of limiting screw grooves 2 are respectively provided on the bottom end wall of the counterweight horizontal plate.

[0022] As a preferred technical solution of the present invention, the plurality of second limiting screw grooves are matched with the plurality of first limiting screw grooves, and the counterweight horizontal plate is fitted with the positioning mounting plate.

[0023] The present application also proposes a drone, which includes the drone center of gravity adjustment component as described above.

[0024] Beneficial effects

[0025] The utility model provides a center of gravity adjustment component for a drone and the drone, which has the following beneficial effects:

[0026] 1. When the center of gravity adjustment component of the drone and the drone need to be used, the adjustment block and the counterweight pillar cooperate with the positioning support plate and the fixed block and the counterweight block, so that the drone equipment body can freely adjust its own counterweight and can quickly disassemble and install the counterweight.

[0027] 2. When the center of gravity adjustment component of the drone and the drone need to be used, the device can be quickly disassembled and assembled and the counterweight can be adjusted through the cooperation between the positioning mounting plate and the limiting screw groove 1 and the counterweight cross plate and the limiting screw groove 2. BRIEF DESCRIPTION OF THE DRAWINGS

[0028] The structures, proportions, sizes, etc. depicted in this specification are only used to match the contents disclosed in the specification for people familiar with this technology to understand and read, and are not used to limit the conditions under which the utility model can be implemented, and therefore have no substantive technical significance.

[0029] Figure 1 A diagram showing the overall structure of the utility model;

[0030] Figure 2 This is a diagram showing the utility model's counterweight horizontal plate;

[0031] Figure 3 Utility Model Figure 1 Enlarged view of point A in the middle.

[0032] Legend:

[0033] 10. UAV equipment body; 11. Adjustment support block; 12. Adjustment mounting slot; 13. Counterweight pillar; 14. Positioning support plate; 15. Fixed support block; 16. Counterweight mounting slot; 17. Counterweight support block; 18. Positioning mounting plate; 19. Limit screw groove 1; 20. Counterweight horizontal plate; 21. Limit screw groove 2. DETAILED DESCRIPTION

[0034] To more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the following briefly introduces the drawings required for the embodiments or the description of the prior art. Obviously, the drawings described below are merely illustrative, and those skilled in the art can derive other implementation drawings based on the provided drawings without inventive effort.

[0035] The structures, proportions, sizes, etc. illustrated in this specification are intended solely to complement the contents disclosed herein and to facilitate understanding and reading by persons familiar with the art. They are not intended to limit the conditions under which the present invention may be implemented and therefore have no substantive technical significance. Any structural modifications, changes in proportions, or adjustments in size, without affecting the efficacy and objectives of the present invention, shall remain within the scope of the technical contents disclosed herein.

[0036] It should be noted that similar reference numerals and letters denote similar items in the following drawings, and therefore, once an item is defined in one drawing, it does not need to be further defined or explained in subsequent drawings.

[0037] In the description of the embodiments of the present invention, it should be noted that the terms "center," "upper," "lower," "inner," "outer," and "side" and the like indicate positions or location relationships based on the positions or location relationships shown in the accompanying drawings, or the positions or location relationships in which the product of the present invention is typically placed when in use. These terms are intended solely to facilitate the description of the present invention and to simplify the description, and are not intended to indicate or imply that the device or component referred to must have a specific orientation, be constructed, or operate in a specific orientation. Therefore, they should not be construed as limitations on the present invention. Furthermore, the terms "first," "second," and the like are used solely to distinguish descriptions and should not be construed as indicating or implying relative importance.

[0038] In the description of the embodiments of the present invention, it should also be noted that, unless otherwise expressly specified or limited, the terms "disposed," "installed," "connected," and "connected" should be understood in a broad sense. For example, they can refer to fixed connections, detachable connections, or integral connections; they can refer to mechanical connections or electrical connections; they can refer to direct connections or indirect connections through an intermediate medium; and they can refer to internal connections between two components. Those skilled in the art will understand the specific meanings of the above terms in the embodiments of the present invention based on the specific circumstances.

[0039] The center of gravity adjustment components of the drone, such as Figure 1-3As shown, it includes a drone device body 10, and an adjustment mechanism is respectively provided on the outer walls of the left and right ends of the drone device body 10 that are away from each other. The adjustment mechanism includes an adjustment block 11 and a counterweight pillar 13 and a fixed block 15 and a counterweight block 17. The bottom end of the drone device body 10 is provided with a deployment mechanism, and the deployment mechanism includes a positioning mounting plate 18 and a counterweight cross plate 20. There are two adjustment blocks 11, and the two adjustment blocks 11 are respectively fixedly mounted on the outer walls of the left and right ends of the drone device body 10 that are away from each other. A plurality of adjustment mounting slots 12 are respectively opened on the top walls of the two adjustment blocks 11. There are a plurality of counterweight pillars 13, and the plurality of counterweight pillars 13 are respectively movably mounted in the plurality of adjustment mounting slots 12, and the plurality of counterweight pillars 13 are respectively fixedly mounted on the top walls. There is a positioning support plate 14, and there are multiple fixed support blocks 15. The multiple fixed support blocks 15 are respectively fixedly mounted on the left and right end outer walls of the two adjustment support blocks 11 away from each other. Counterweight mounting grooves 16 are respectively opened on the top walls of the multiple fixed support blocks 15. There are multiple counterweight support blocks 17. The multiple counterweight support blocks 17 are respectively movably installed in the multiple fixed support blocks 15. There are two positioning mounting plates 18. The two positioning mounting plates 18 are respectively fixedly mounted on the bottom end walls of the drone equipment body 10. A plurality of limiting screw grooves 19 are respectively opened on the bottom end walls of the two positioning mounting plates 18. A plurality of limiting screw grooves 21 are respectively opened on the bottom end walls of the counterweight cross plate 20. The plurality of limiting screw grooves 21 are adapted to the plurality of limiting screw grooves 19, and the counterweight cross plate 20 fits the positioning mounting plate 18.

[0040] The working principle of the present invention is as follows: when it is needed, through the cooperation between the adjustment support block 11 and the counterweight pillar 13 and the positioning support plate 14 and the fixed support block 15 and the counterweight support block 17, the drone equipment body 10 can freely adjust its own counterweight and can quickly disassemble the counterweight.

[0041] When it is needed, the device can be quickly disassembled and assembled and the counterweight can be adjusted through the cooperation between the positioning mounting plate 18 and the limiting screw groove 19 and the counterweight cross plate 20 and the limiting screw groove 21.

[0042] The present application also proposes a drone, which includes the center of gravity adjustment component of the above-mentioned drone. The specific structure of the center of gravity adjustment component of the drone refers to the above-mentioned embodiment. Since this drone adopts all the technical solutions of all the above-mentioned embodiments, it also has all the beneficial effects brought by the technical solutions of the above-mentioned embodiments, which will not be repeated here.

[0043] The above shows and describes the basic principles and main features of the present invention and the advantages of the present invention. It should be understood by those skilled in the art that the present invention is not limited to the above embodiments. The above embodiments and descriptions are merely illustrative of the principles of the present invention. Various changes and improvements may be made to the present invention without departing from the spirit and scope of the present invention, and such changes and improvements shall fall within the scope of the present invention as claimed.

Claims

1. A center of gravity adjustment component for a drone, comprising a drone device body (10), characterized in that: The outer walls of the left and right ends of the drone equipment body (10) are respectively provided with adjustment mechanisms, the adjustment mechanisms including an adjustment support block (11) and a counterweight pillar (13) and a fixed support block (15) and a counterweight support block (17). The bottom end of the drone equipment body (10) is provided with a deployment mechanism, the deployment mechanism including a positioning mounting plate (18) and a counterweight transverse plate (20).

2. The center of gravity adjustment assembly of a drone according to claim 1, characterized in that: There are two adjusting support blocks (11) in total, and the two adjusting support blocks (11) are respectively fixedly mounted on the outer walls of the left and right ends of the drone equipment body (10) that are away from each other.

3. The center of gravity adjustment assembly for a drone according to claim 1, characterized in that: A plurality of adjustment installation slots (12) are respectively provided on the top end walls of the two adjustment support blocks (11), and a plurality of counterweight pillars (13) are provided. The plurality of counterweight pillars (13) are movably installed in the plurality of adjustment installation slots (12).

4. The center of gravity adjustment assembly for a drone according to claim 1, characterized in that: Positioning support plates (14) are fixedly mounted on the top walls of the plurality of counterweight pillars (13), and there are a plurality of fixed support blocks (15). The plurality of fixed support blocks (15) are fixedly mounted on the outer walls of the left and right ends of the two adjustment support blocks (11) that are away from each other.

5. The center of gravity adjustment assembly of a drone according to claim 1, characterized in that: The top walls of the plurality of fixed support blocks (15) are respectively provided with counterweight installation grooves (16). There are a plurality of counterweight support blocks (17), and the plurality of counterweight support blocks (17) are movably installed in the plurality of fixed support blocks (15).

6. The center of gravity adjustment assembly for a drone according to claim 1, characterized in that: There are two positioning mounting plates (18) in total. The two positioning mounting plates (18) are respectively fixedly mounted on the bottom end wall of the drone equipment body (10). The bottom end walls of the two positioning mounting plates (18) are respectively provided with a plurality of limiting screw grooves (19).

7. The center of gravity adjustment assembly of a drone according to claim 1, characterized in that: The bottom end wall of the counterweight transverse plate (20) is respectively provided with a plurality of limiting screw grooves 2 (21), the plurality of limiting screw grooves 2 (21) are adapted to the plurality of limiting screw grooves 1 (19), and the counterweight transverse plate (20) is fitted with the positioning mounting plate (18).

8. A drone, characterized in that: A center of gravity adjustment component for a drone comprising any one of claims 1-7.

Images