A crossing machine provided with a quick-release guard plate

Abstract

The application relates to the technical field of crossing machines, and provides a crossing machine provided with quick-release protective plates, which comprises a rack, an electric control assembly arranged in the rack, and quick-release protective plates arranged on the two sides of the rack to facilitate maintenance of the electric control assembly; the rack comprises upper supporting plates and lower supporting plates and a plurality of supporting columns used for parallel and spaced arrangement of the upper supporting plates and the lower supporting plates; the inner sides of the quick-release protective plates are provided with a plurality of clamping grooves; and the plurality of clamping grooves are clamped with the corresponding plurality of supporting columns. Through clamping of the clamping grooves on the quick-release protective plates and the supporting columns, the maintenance and overhaul of the electric control assembly are more convenient and fast; the quick-release protective plates can be quickly disassembled and installed without complex tools, and the maintenance efficiency is greatly improved.

Description

Technical Field

[0001] This application relates to the field of racing drone technology, and in particular to a racing drone equipped with a quick-release protective plate. Background Technology

[0002] In existing racing drone designs, protective plates are typically installed on the frame to protect the internal electronic control components from external impacts or damage during flight. However, traditional protective plate designs often present challenges in installation and removal, which complicates the maintenance and repair of the electronic control components. Utility Model Content

[0003] To address the aforementioned technical problems, this application provides a racing drone equipped with a quick-release protective plate.

[0004] This application provides a racing drone equipped with a quick-release protective plate, which adopts the following technical solution:

[0005] A trekking machine equipped with quick-release protective plates includes a frame, an electronic control component disposed within the frame, and quick-release protective plates disposed on both sides of the frame for easy maintenance of the electronic control component; the frame includes an upper support plate and a lower support plate, and a plurality of support columns arranged parallel to and spaced apart from the upper and lower support plates; the inner side of the quick-release protective plate is provided with a plurality of slots, and the plurality of slots engage with the corresponding plurality of support columns.

[0006] It also includes a pressure plate disposed above the upper support plate, and multiple cantilever arms sandwiched between the pressure plate and the upper support plate.

[0007] The frame has two parallel lens support plates at a distance from each other at its front end, and a camera is hinged between the two lens support plates.

[0008] The upper and lower ends of the two lens support plates are respectively inserted into the upper support plate and the lower support plate.

[0009] The lens support plate has positioning protrusions at both its upper and lower ends, and both the upper support plate and the lower support plate have positioning holes, with the positioning protrusions inserted into the positioning holes.

[0010] The lower end of the lens support plate is provided with a horizontal extension wall, and the end of the horizontal extension wall is provided with a positioning protrusion that cooperates with the positioning hole of the lower support plate.

[0011] The rear end of the frame is provided with a tail fin support, and the upper and lower ends of the tail fin support are respectively fastened to the upper support plate and the lower support plate.

[0012] An electrical control device is provided between the upper support plate and the lower support plate; support seats for mounting the cantilever are extended on the opposite sides of the upper support plate.

[0013] The pressure plate has extension seats on its opposite sides that correspond to the upper and lower sides of the support seat, and the root of the cantilever is sandwiched between the support seat and the extension seats.

[0014] In summary, this application includes at least one of the following beneficial technical effects:

[0015] 1. The quick-release protective plate's slots and support columns make maintenance and repair of electrical control components more convenient and efficient. The quick-release protective plate can be quickly disassembled and installed without complicated tools, greatly improving maintenance efficiency.

[0016] 2. By setting up the upper support plate, lower support plate and multiple support columns in parallel intervals, and by fastening the tail support component to the upper and lower support plates, a robust and stable frame structure is formed, which effectively improves the vibration resistance and stability of the racing aircraft during flight. Attached Figure Description

[0017] Figure 1 This is an isometric drawing of the racing drone used in this application.

[0018] Figure 2 yes Figure 1 The exploded diagram.

[0019] Figure 3 yes Figure 2 Axonometric drawing of the quick-release protective plate.

[0020] Figure 4 yes Figure 1 A magnified view of a portion of point A in the middle.

[0021] Figure 5 yes Figure 4 Axonometric view of the lens support plate.

[0022] Explanation of reference numerals in the attached figures:

[0023] 1. Frame; 11. Upper support plate; 111. Positioning hole; 112. Support base; 12. Lower support plate; 13. Support column; 14. Lens support plate; 141. Positioning protrusion; 142. Horizontal extension wall; 15. Tail wing support; 2. Quick-release protective plate; 21. Slot; 3. Pressure plate; 31. Extension base; 4. Cantilever; 5. Camera. Detailed Implementation

[0024] The present application will be further described in detail below with reference to the accompanying drawings.

[0025] In the description of the embodiments of this application, it should be noted that, unless otherwise explicitly specified and limited, the terms "installation" and "connection" should be interpreted broadly. For example, "connection" can be a detachable connection or a non-detachable connection; it can be a direct connection or an indirect connection through an intermediate medium. "Multiple" refers to at least two.

[0026] The directional terms used in the embodiments of this application, such as "upper," "lower," "inner," "outer," "top," "bottom," and "side," are only for reference to the directions in the accompanying drawings. Therefore, the directional terms used are for better and clearer explanation and understanding of this application.

[0027] The embodiments described herein are not intended to indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be construed as limiting the embodiments of this application.

[0028] In the embodiments of this application, the relative positional relationships mentioned, such as parallel, perpendicular, and aligned, are defined in relation to the current technological level, rather than being absolutely strict. Slight deviations are permissible; approximations of parallelism, perpendicularity, or alignment are all acceptable. For example, "A and B are parallel" means that A and B are parallel or approximately parallel, and the angle between A and B can be between 0 and 10 degrees. Similarly, "A and B are perpendicular" means that A and B are perpendicular or approximately perpendicular, and the angle between A and B can be between 80 and 100 degrees.

[0029] In the embodiments of this application, the terms "first," "second," "third," and "fourth" are used for descriptive purposes only and should not be construed as indicating or implying relative importance or implicitly specifying the number of indicated technical features. Thus, a feature defined with "first," "second," "third," and "fourth" may explicitly or implicitly include one or more of that feature.

[0030] Combination Figure 1 As shown in the figure, this application discloses a racing drone equipped with quick-release protective plates. The racing drone includes a frame 1, an electronic control component disposed within the frame 1, and quick-release protective plates 2 disposed on both sides of the frame 1 for convenient maintenance of the electronic control component. The quick-release protective plates 2 not only provide shielding and protection for the electronic control component disposed within the frame 1, effectively protecting the electronic control component from external collisions and damage, and improving the service life of the racing drone, but also make the maintenance of the electronic control component more convenient and quick. The quick-release protective plates can be quickly disassembled and installed without complicated tools, thus improving maintenance efficiency.

[0031] Combination Figure 2 and Figure 3As shown, preferably, the frame 1 includes an upper support plate 11 and a lower support plate 12, and a plurality of support columns 13 arranged parallel to and spaced apart from the upper support plate 11 and the lower support plate 12. In order to facilitate the quick disassembly and assembly of the quick-release protective plates 2 on both sides of the frame 1, a plurality of slots 21 are provided on the inner sidewalls of the two quick-release protective plates 2 to engage with the corresponding support columns 13. The slots 21 are C-shaped and can be integrally formed with the quick-release protective plates 2. The inner diameter of the slot 21 opening is slightly smaller than the outer diameter of the support column 13 and has a certain degree of elasticity. This ensures both the stability after engaging with the support column 13 and the ease of disassembly.

[0032] Furthermore, combining Figure 2 and Figure 4 As shown, in order to facilitate the installation of the camera, two lens support plates 14 are vertically spaced between the upper support plate 11 and the lower support plate 12 at the front end of the frame 1. During installation, the camera 5 can be hinged between the two lens support plates 14, and then the upper support plate 11 and the lower support plate 12 are pressed onto the upper and lower ends of the two lens support plates 14.

[0033] To further simplify the installation process, improve assembly efficiency, and increase post-assembly stability, combined with Figure 4 and Figure 5 As shown, both the upper and lower ends of the lens support plate 14 have positioning protrusions 141 extending outwards. The upper support plate 11 and the lower support plate 12 are respectively provided with positioning holes 111 that cooperate with the positioning protrusions 141. During installation, the positioning protrusions 141 can be inserted into the corresponding positioning holes 111 respectively, and then the upper support plate 11 and the lower support plate 12 are locked with the support column 13, thereby clamping the two lens support plates 14 together. This can save a lot of trouble caused by fixing the lens support plate 14 with screws.

[0034] Furthermore, to further improve the stability and reliability of the lens support plate 14 after installation, such as... Figure 5 As shown, the lower end of the lens support plate 14 has a horizontal extension wall 142, and the end of the horizontal extension wall 142 is also provided with the aforementioned positioning protrusion 141. In this way, the contact area between the lens support plate 14 and the lower support plate 12 is increased by the horizontal extension wall 142, thereby improving the installation stability of the lens support plate 14 and avoiding problems such as unclear shooting images caused by the instability of the lens support plate 14 during the flight of the whole aircraft.

[0035] In addition, a tail fin support 15 is provided at the rear end of the frame 1. The upper and lower ends of the tail fin support 15 are respectively fastened to the upper support plate 11 and the lower support plate 12. The tail fin support 15 not only enhances the strength of the tail structure of the racing aircraft and improves the balance and stability of flight, but also, through the fastening connection between the tail fin support 15 and the upper support plate 11 and the lower support plate 12, makes the structure of the entire frame 1 more integrated and reduces vibration during flight.

[0036] Furthermore, the aforementioned electronic control device is installed between the upper support plate 11 and the lower support plate 12. Support seats 112 extend outward from the opposite sides of the upper support plate 11, and cantilever arms 4 extend outward from the support seats 112. A motor is installed at the end of the cantilever arm 4 and is electrically connected to the electronic control components to provide power for the traverse machine. In order to further increase the stability and reliability of the cantilever arm 4, a pressure plate 3 is also pressed at the root of the cantilever arm 4. Extension seats 31 corresponding to the support seats 112 extend outward from the opposite sides of the pressure plate 3. In this way, the root of the cantilever arm 4 is clamped by the support seats 112 and the extension seats 31 and provides certain support to the root of the cantilever arm 4, so that the cantilever arm 4 can be stably and reliably connected to the frame 1, thereby effectively improving the structural strength of the whole machine.

[0037] The above are all preferred embodiments of this application, and are not intended to limit the scope of protection of this application. Therefore, all equivalent changes made in accordance with the structure, shape and principle of this application should be covered within the scope of protection of this application.

Claims

1. A racing drone equipped with a quick-release protective plate, characterized in that, The device includes a frame, an electrical control component disposed within the frame, and quick-release protective plates disposed on both sides of the frame for easy maintenance of the electrical control component. The frame includes an upper support plate and a lower support plate, and a plurality of support columns arranged parallel to and spaced apart from the upper and lower support plates. The inner side of the quick-release protective plate is provided with a plurality of slots, which engage with the corresponding plurality of support columns.

2. A stunt drone equipped with a quick-release protective plate according to claim 1, characterized in that, It also includes a pressure plate disposed above the upper support plate, and a plurality of cantilever arms sandwiched between the pressure plate and the upper support plate.

3. A safari vehicle equipped with a quick-release protective plate according to claim 1, characterized in that, Two lens support plates are arranged parallel to each other at the front end of the frame, and a camera is hinged between the two lens support plates.

4. A stunt drone equipped with a quick-release protective plate according to claim 3, characterized in that, The upper and lower ends of the two lens support plates are respectively inserted into the upper support plate and the lower support plate.

5. A stunt drone equipped with a quick-release protective plate according to claim 4, characterized in that, The lens support plate has positioning protrusions at both the upper and lower ends, and both the upper support plate and the lower support plate have positioning holes, with the positioning protrusions inserted into the positioning holes.

6. A stunt drone equipped with a quick-release protective plate according to claim 5, characterized in that, The lower end of the lens support plate is provided with a horizontal extension wall, and the end of the horizontal extension wall is provided with a positioning protrusion that cooperates with the positioning hole of the lower support plate.

7. A stunt drone equipped with a quick-release protective plate according to claim 1, characterized in that, The rear end of the frame is provided with a tail fin support, and the upper and lower ends of the tail fin support are respectively fastened to the upper support plate and the lower support plate.

8. A stunt drone equipped with a quick-release protective plate according to claim 2, characterized in that, An electrical control device is provided between the upper support plate and the lower support plate; support seats for mounting the cantilever are extended on the opposite sides of the upper support plate.

9. A stunt drone equipped with a quick-release protective plate according to claim 8, characterized in that, The pressure plate has extension seats on its opposite sides that correspond to the upper and lower sides of the support seat, and the root of the cantilever is sandwiched between the support seat and the extension seats.

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