Integrated connecting piece for connecting the body of a drone to a foot stand

Abstract

The utility model relates to the field of unmanned plane connecting frame, disclose unmanned plane fuselage and foot stand are connected with integral type connecting piece, including second connecting sleeve, the upper end surface center of second connecting sleeve is provided with first connecting sleeve, the lower extreme of first connecting sleeve is through the upper end surface of second connecting sleeve and leads to inside, the upper end surface of second connecting sleeve and the two side wall junctions of first connecting sleeve are provided with first connecting buckle respectively in first connecting sleeve front and back two sides, the side wall center of second connecting sleeve is provided with third connecting sleeve, one end of third connecting sleeve is through the side wall of second connecting sleeve and the side wall of first connecting sleeve and leads to inside respectively. In the utility model, through setting up as integral moulding type structure between first connecting sleeve, second connecting sleeve and third connecting sleeve, integral type design improves production efficiency, strengthens fuselage structure strength, improves airplane stability and reliability.

Description

Technical Field

[0001] This utility model relates to the field of drone connectors, and more particularly to an integrated connector for connecting the drone fuselage and landing gear. Background Technology

[0002] With the rapid development of drone technology, drones are increasingly widely used in various fields such as aerial photography, logistics, agriculture, surveying and mapping, and rescue. The drone's fuselage and landing gear are key components that ensure stable takeoff, landing, and operation, and their connection method directly affects the drone's overall performance, stability, and service life.

[0003] Traditional drone fuselage and landing gear connections primarily employ separate connectors, where the fuselage and landing gear are fixed together using multiple independent connecting parts. While this method achieves a certain level of connectivity, it still has many shortcomings in practical applications. Separate connectors are susceptible to vibration, impact, and other external forces during use, leading to loosening or detachment. To ensure connection strength, separate connectors typically require a significant amount of metal material, increasing the overall weight of the drone and impacting its endurance and payload capacity. Therefore, those skilled in the art have provided an integrated connector for connecting the drone fuselage and landing gear to address the problems mentioned in the background section. Utility Model Content

[0004] The purpose of this utility model is to overcome the shortcomings of the existing technology and propose an integrated connector for connecting the fuselage and landing gear of a drone. By setting the first connecting sleeve, the second connecting sleeve and the third connecting sleeve as an integral molded structure, the integrated design improves production efficiency, enhances the structural strength of the fuselage, and improves the stability and reliability of the aircraft. At the same time, by using aluminum alloy or carbon fiber as the material, the weight can be reduced to the greatest extent. By reducing the overall weight, the endurance can be improved.

[0005] To achieve the above objectives, this utility model provides the following technical solution: an integrated connector for connecting the fuselage and landing gear of a drone, including a second connecting sleeve, a first connecting sleeve disposed at the center of the upper end face of the second connecting sleeve, the lower end of the first connecting sleeve penetrating through the upper end face of the second connecting sleeve and extending into the interior, first connecting buckles respectively disposed at the connection points of the upper end face of the second connecting sleeve and the side walls of the first connecting sleeve on the front and rear sides of the first connecting sleeve, and a third connecting sleeve disposed at the center of one side wall of the second connecting sleeve, one end of the third connecting sleeve penetrating through the side wall of the second connecting sleeve and the side wall of the first connecting sleeve and extending into the interior, wherein the first connecting sleeve, the second connecting sleeve and the third connecting sleeve are all made of aluminum alloy or carbon fiber;

[0006] The above technical solution, by setting the first connecting sleeve, the second connecting sleeve and the third connecting sleeve as an integral molded structure, improves production efficiency, enhances the structural strength of the fuselage, and improves the stability and reliability of the aircraft. At the same time, by setting the material as aluminum alloy or carbon fiber, the weight can be reduced to the greatest extent, thereby improving the range by reducing the overall weight.

[0007] Furthermore, through grooves are provided at the center of the front and rear side walls of the first connecting sleeve and at the center of the upper end face of the second connecting sleeve near the front and rear side edges, and second connecting buckles are provided at the upper end of the center of the front and rear side walls of the first connecting sleeve.

[0008] The above technical solution allows for adjustment of the inner diameter of the second connecting sleeve within a limited range, and it can be fixed by tightening the second connecting buckle.

[0009] Furthermore, a T-groove is provided at the center of the upper end face of the third connecting sleeve near one side edge. The lower end of the T-groove penetrates the upper end face of the third connecting sleeve and extends into the interior. Third connecting buckles are fixedly connected to the upper end faces of the third connecting sleeve on both sides of the T-groove.

[0010] With the above technical solution, the two third connecting buckles can be tightened by screws during installation and use, and the T-slot can accommodate connectors of different sizes within a limited range.

[0011] Furthermore, the diameters of the first connecting sleeve, the second connecting sleeve, and the third connecting sleeve are all the same;

[0012] The above technical solution facilitates assembly and connection during use.

[0013] Furthermore, the first connecting sleeve, the second connecting sleeve, and the third connecting sleeve are integrally molded.

[0014] The above technical solutions result in a high-strength, one-piece molded structure, and the integrated design improves production efficiency.

[0015] Furthermore, the angle between the lower end of the first connecting sleeve and the upper end face of the second connecting sleeve is 65 degrees;

[0016] The above technical solution can effectively adjust the center of gravity of the drone, making it closer to the geometric center, thereby improving flight stability.

[0017] This utility model has the following beneficial effects:

[0018] 1. In this utility model, by setting the first connecting sleeve, the second connecting sleeve and the third connecting sleeve as an integral molding structure, the integral design improves production efficiency, enhances the structural strength of the fuselage, and improves the stability and reliability of the aircraft.

[0019] 2. In this utility model, by setting the material to aluminum alloy or carbon fiber, the weight can be reduced to the greatest extent, thereby improving the battery life by reducing the overall weight. Attached Figure Description

[0020] Figure 1 This is an isometric view of the integrated connector for connecting the fuselage and landing gear of the UAV proposed in this utility model;

[0021] Figure 2 This is an isometric view from another perspective of the integrated connector for connecting the fuselage and landing gear of the UAV proposed in this utility model.

[0022] Figure 3 This is an isometric view of the lower side of the integrated connector for connecting the fuselage and landing gear of the UAV proposed in this utility model.

[0023] Figure 4 This is a side view of the integrated connector for connecting the fuselage and landing gear of the UAV proposed in this utility model.

[0024] Legend:

[0025] 1. First connecting sleeve; 2. Second connecting sleeve; 3. First connecting buckle; 4. Second connecting buckle; 5. Third connecting buckle; 6. Third connecting sleeve; 7. Through groove; 8. T-groove. Detailed Implementation

[0026] 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.

[0027] Reference Figure 1-4This utility model provides an embodiment of an integrated connector for connecting the fuselage and landing gear of a drone, including a second connecting sleeve 2. A first connecting sleeve 1 is provided at the center of the upper end face of the second connecting sleeve 2. The lower end of the first connecting sleeve 1 passes through the upper end face of the second connecting sleeve 2 and leads to the interior. First connecting buckles 3 are respectively provided at the connection points of the upper end face of the second connecting sleeve 2 and the side walls of the first connecting sleeve 1 on the front and rear sides of the first connecting sleeve 1. A third connecting sleeve 6 is provided at the center of one side wall of the second connecting sleeve 2. One end of the third connecting sleeve 6 passes through the side wall of the second connecting sleeve 2 and the side wall of the first connecting sleeve 1 and leads to the interior. The first connecting sleeve 1, the second connecting sleeve 2, and the third connecting sleeve 6 are all made of aluminum alloy or carbon fiber, which can achieve maximum weight reduction. By reducing the overall weight, the endurance is improved. At the same time, the integrated molding structure has higher strength, is more stable during use, and can improve production efficiency, enhance the structural strength of the fuselage, and improve the stability and reliability of the aircraft.

[0028] Through grooves 7 are provided at the center of the front and rear side walls of the first connecting sleeve 1 and at the center of the upper end face of the second connecting sleeve 2 near the front and rear side edges, respectively. Second connecting buckles 4 are provided at the upper end of the center of the front and rear side walls of the first connecting sleeve 1, which can adjust the inner diameter of the second connecting sleeve 2 when connected within a limited range. The second connecting buckles 4 can be tightened to fix it.

[0029] A T-groove 8 is provided at the center of the upper end face of the third connecting sleeve 6 near one side edge. The lower end of the T-groove 8 passes through the upper end face of the third connecting sleeve 6 and leads to the interior. Third connecting buckles 5 are fixedly connected to the upper end faces of the third connecting sleeve 6 on both sides of the T-groove 8. During installation and use, the two third connecting buckles 5 can be tightened by using screws. The T-groove 8 can accommodate connectors of different sizes within a limited range.

[0030] The diameters of the first connecting sleeve 1, the second connecting sleeve 2, and the third connecting sleeve 6 are all the same, which facilitates assembly and connection during use. The first connecting sleeve 1, the second connecting sleeve 2, and the third connecting sleeve 6 are integrally molded, which has high structural strength and improves production efficiency. The angle between the lower end of the first connecting sleeve 1 and the upper end face of the second connecting sleeve 2 is 65 degrees. The angle can effectively adjust the center of gravity of the UAV, making it closer to the geometric center, thereby improving flight stability.

[0031] Working principle: This utility model is an integrated connector for connecting the fuselage and landing gear of a drone. By setting the first connecting sleeve 1, the second connecting sleeve 2 and the third connecting sleeve 6 as an integral molded structure, the integrated design improves production efficiency, enhances the structural strength of the fuselage, and improves the stability and reliability of the aircraft. At the same time, by setting the material as aluminum alloy or carbon fiber, the weight can be reduced to the greatest extent. By reducing the overall weight, the endurance can be improved.

[0032] Finally, it should be noted that the above description is only a preferred embodiment of the present utility model and is not intended to limit the present utility model. Although the present utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions for some of the technical features. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present utility model should be included within the protection scope of the present utility model.

Claims

1. An integrated connector for connecting the fuselage and landing gear of a drone, including a second connecting sleeve (2), characterized in that: A first connecting sleeve (1) is provided at the center of the upper end face of the second connecting sleeve (2). The lower end of the first connecting sleeve (1) passes through the upper end face of the second connecting sleeve (2) and leads to the interior. A first connecting buckle (3) is provided at the connection between the upper end face of the second connecting sleeve (2) and the two side walls of the first connecting sleeve (1) on the front and rear sides of the first connecting sleeve (1). A third connecting sleeve (6) is provided at the center of one side wall of the second connecting sleeve (2). One end of the third connecting sleeve (6) passes through the side wall of the second connecting sleeve (2) and the side wall of the first connecting sleeve (1) and leads to the interior. The first connecting sleeve (1), the second connecting sleeve (2) and the third connecting sleeve (6) are all made of aluminum alloy or carbon fiber.

2. The integrated connector for connecting the fuselage and landing gear of a drone according to claim 1, characterized in that: A through groove (7) is provided at the center of the front and rear side walls of the first connecting sleeve (1) and at the center of the upper end face of the second connecting sleeve (2) near the front and rear side edges, and a second connecting buckle (4) is provided at the upper end of the center of the front and rear side walls of the first connecting sleeve (1).

3. The integrated connector for connecting the fuselage and landing gear of a drone according to claim 1, characterized in that: A T-groove (8) is provided at the center of the upper end face of the third connecting sleeve (6) near one side edge. The lower end of the T-groove (8) passes through the upper end face of the third connecting sleeve (6) and leads to the interior. Third connecting buckles (5) are fixedly connected to the upper end faces of the third connecting sleeve (6) on both sides of the T-groove (8).

4. The integrated connector for connecting the fuselage and landing gear of a drone according to claim 1, characterized in that: The diameters of the first connecting sleeve (1), the second connecting sleeve (2), and the third connecting sleeve (6) are all the same.

5. The integrated connector for connecting the fuselage and landing gear of a drone according to claim 1, characterized in that: The first connecting sleeve (1), the second connecting sleeve (2) and the third connecting sleeve (6) are integrally molded.

6. The integrated connector for connecting the fuselage and landing gear of a drone according to claim 1, characterized in that: The angle between the lower end of the first connecting sleeve (1) and the upper end face of the second connecting sleeve (2) is 65 degrees.

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