Racing unmanned aerial vehicle capable of quickly disassembling side plates

Abstract

The utility model provides a racing unmanned aerial vehicle capable of quickly disassembling side plates, which comprises an unmanned aerial vehicle body and unmanned aerial vehicle side plates, and the unmanned aerial vehicle side plates are detachably arranged on the unmanned aerial vehicle body; the unmanned aerial vehicle body comprises a mounting cavity, an unmanned aerial vehicle side opening is formed in the mounting cavity, one side of the unmanned aerial vehicle side plate is rotationally arranged on the side wall of the mounting cavity, the other side of the unmanned aerial vehicle side plate is clamped to the side wall of the mounting cavity, and the unmanned aerial vehicle side plate opens or closes the unmanned aerial vehicle side opening. According to the racing unmanned aerial vehicle, structures such as a control circuit in the mounting cavity can be quickly mounted, maintained and replaced, particularly, components such as circuit components and batteries in the racing unmanned aerial vehicle can be quickly replaced and maintained in the racing process, and the time consumed for replacement or maintenance is short; and influence on competition results and even loss of competition qualification due to too much time delay in the competition are avoided.

Description

TECHNICAL FIELD

[0001] The patent relates to the technical field of aerial devices, in particular to a racing unmanned aerial vehicle with quickly detachable side plates. BACKGROUND

[0002] The racing unmanned aerial vehicle is a kind of racing unmanned aerial vehicle, and the racing unmanned aerial vehicle needs to frequently replace and maintain internal circuit components, batteries and other components. Sometimes, the internal circuit components, batteries and other components need to be replaced and maintained during the racing unmanned aerial vehicle event. However, the side plates of the current racing unmanned aerial vehicle are assembled with the main body of the racing unmanned aerial vehicle through screws. When the circuit components, batteries and other components are replaced or maintained, the screws need to be removed, and the side plates of the racing unmanned aerial vehicle need to be taken off. Then, the internal circuit components, batteries and other components are replaced or maintained. The replacement or maintenance takes a long time, which is most obvious in the event. If too much time is wasted in the event, the competition result can be affected, and even the competition qualification can be lost. CONTENT OF THE UTILITY MODEL

[0003] To solve the above technical problems, the technical solution of the patent is: a racing unmanned aerial vehicle with quickly detachable side plates, comprising a unmanned aerial vehicle body and a unmanned aerial vehicle side plate, the unmanned aerial vehicle side plate is detachably arranged on the unmanned aerial vehicle body; the unmanned aerial vehicle body comprises a mounting chamber, the mounting chamber is provided with a unmanned aerial vehicle side opening, one side of the unmanned aerial vehicle side plate is rotatably arranged on the side wall of the mounting chamber, the other side of the unmanned aerial vehicle side plate is clamped on the side wall of the mounting chamber, and the unmanned aerial vehicle side plate opens or closes the unmanned aerial vehicle side opening.

[0004] Further, one of the side wall of the mounting chamber and the unmanned aerial vehicle side plate is provided with a rotating mounting portion, and the other one is provided with a mounting shaft, and the mounting shaft is rotatably arranged in the rotating mounting portion.

[0005] Further, the mounting shaft is provided with a blocking portion, the blocking portion is arranged at one end of the mounting shaft away from the unmanned aerial vehicle side plate, and the blocking portion blocks the mounting shaft from being separated from the rotating mounting portion.

[0006] Further, the blocking portion comprises a plurality of spherical blocking blocks, each of the blocking blocks is arranged at one end of the mounting shaft away from the unmanned aerial vehicle side plate, and the adjacent blocking blocks are arranged at intervals.

[0007] Further, the rotating mounting portion comprises a plug-in ring and a connecting rod, the plug-in ring is mounted in the inner side of the side wall of the mounting chamber through the connecting rod, and the mounting shaft is plug-in mounted in the plug-in ring.

[0008] Further, the unmanned aerial vehicle side plate is provided with a clamping block, the side wall of the mounting chamber is provided with a clamping table, the clamping block is matched with the clamping table, and the clamping block is detachably clamped on the clamping table.

[0009] Further, the card block is a soft glue structure.

[0010] Further, the unmanned aerial vehicle side plate is further provided with a hand buckle position, which is arranged on the unmanned aerial vehicle side plate close to the card block.

[0011] Further, the racing unmanned aerial vehicle with the quickly detachable side plate further comprises a circuit structure, the circuit structure comprises a first circuit board, a second circuit board and a third circuit board, and the first circuit board, the second circuit board and the third circuit board are sequentially stacked in the mounting cavity.

[0012] Further, the mounting cavity is provided with a positioning column, a separation ring and a fixing nut, the separation ring and the fixing nut are both sleeved on the positioning column; the first circuit board, the second circuit board and the third circuit board are all arranged on the positioning column in a penetrating manner, the first circuit board and the second circuit board and the second circuit board and the third circuit board are both separated and limited by the separation ring, and the third circuit board is fixed on the positioning column by the fixing nut.

[0013] The beneficial effects realized by the patent include that the unmanned aerial vehicle side plate is detachably arranged on the shell of the unmanned aerial vehicle body, so that the unmanned aerial vehicle side plate can be detached from the shell of the unmanned aerial vehicle body to maintain or replace the control circuit and other structures in the shell. One side of the unmanned aerial vehicle side plate is rotatably arranged on the side wall of the mounting cavity, so that the unmanned aerial vehicle side plate can be opened by rotation to fully open the unmanned aerial vehicle side opening, facilitating the installation, maintenance and replacement of the control circuit and other structures in the mounting cavity. The other side of the unmanned aerial vehicle side plate is clamped on the side wall of the mounting cavity, and the unmanned aerial vehicle side plate is installed on the side wall of the mounting cavity by clamping, facilitating the quick opening and closing of the unmanned aerial vehicle side opening, so that the control circuit and other structures in the mounting cavity can be quickly installed, maintained and replaced. In particular, it is convenient to quickly replace and maintain the internal circuit components, batteries and other components during the racing unmanned aerial vehicle competition, the replacement or maintenance time is short, and the time lost during the competition is avoided to affect the competition results or even lose the competition qualification. BRIEF DESCRIPTION OF DRAWINGS

[0014] Figure 1 It is a structural schematic view of the racing unmanned aerial vehicle with the quickly detachable side plate from one angle in the patent specification embodiment.

[0015] Figure 2 It is a structural schematic view of the racing unmanned aerial vehicle with the quickly detachable side plate from another angle in the patent specification embodiment.

[0016] Figure 3 It is a structural schematic view of the racing unmanned aerial vehicle with the quickly detachable side plate in the patent specification embodiment.

[0017] Figure 4Structure diagram of the structure of installing the side plate of the unmanned aerial vehicle in the installation cavity of the embodiment of the patent specification;

[0018] Figure 5 Structure diagram of the structure of removing the side plate of the unmanned aerial vehicle in the installation cavity of the embodiment of the patent specification;

[0019] Figure 6 Structure diagram of the structure of installing the circuit structure on the bottom wall of the installation cavity of the embodiment of the patent specification;

[0020] Figure 7 Structure diagram of the structure of the side plate of the unmanned aerial vehicle at one angle of the embodiment of the patent specification;

[0021] Figure 8 Structure diagram of the structure of the side plate of the unmanned aerial vehicle at another angle of the embodiment of the patent specification.

[0022] The accompanying drawings are only used for illustrative description, and cannot be understood as a limitation of the patent; in order to better illustrate the embodiment, some components in the drawings may be omitted, enlarged or reduced, and do not represent the actual product size; for those skilled in the art, it is understandable that some well-known structures and their descriptions in the drawings may be omitted; the same or similar reference numerals correspond to the same or similar components; the use of language to describe the positional relationship in the drawings is only used for illustrative description, and cannot be understood as a limitation of the patent. DETAILED DESCRIPTION

[0023] In order to facilitate understanding of those skilled in the art, the following will be described in words and drawings to illustrate multiple embodiments of the patent. For the purpose of clear description, many practical details will be described in the following description. However, it should be understood that these practical details should not be used to limit the patent. That is, in some embodiments of the patent, these practical details are unnecessary. In addition, for the convenience of understanding, some conventional structures and components will be drawn in a simple schematic manner in the drawings.

[0024] In the description of the patent, it should be understood that the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer" and the like indicate the orientation or positional relationship shown in the drawings, which is only for the convenience of describing the patent and simplifying the description, and does not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore cannot be understood as a limitation of the patent.

[0025] In addition, the terms "first", "second", etc. are used only for the purpose of description, and should not be understood as indicating or implying relative importance or implying the number of the technical features indicated. Therefore, the features defined as "first", "second" can explicitly or implicitly include one or more of the features. In the description of the patent, the meaning of "a plurality of" is two or more, unless otherwise explicitly specified and limited.

[0026] In this patent, unless otherwise explicitly specified and limited, the terms "mounting", "connecting", "connecting", "fixing" and other terms should be understood broadly, for example, it can be fixedly connected, or it can be detachably connected, or it can be integrated; it can be mechanically connected, or it can be electrically connected; it can be directly connected, or it can be indirectly connected through an intermediate medium; it can be the internal communication of two elements or the interaction relationship between two elements. For those skilled in the art, the specific meaning of the above terms in this patent can be understood according to the specific circumstances.

[0027] In addition, the technical solutions of each embodiment can be combined with each other, but it must be based on the fact that those skilled in the art can realize it, when the combination of technical solutions appears contradictory or cannot be realized, it should be considered that the combination of technical solutions does not exist, nor is it within the protection scope of this patent.

[0028] Reference Figures 1-8The application discloses a racing unmanned plane with detachable side plates, which comprises an unmanned plane body 1 and unmanned plane side plates 2. The unmanned plane body 1 is the main structure of the racing unmanned plane and comprises a shell and structures arranged on the shell, such as a control circuit, a motor, a fan blade and a battery. The unmanned plane side plates 2 are detachably arranged on the shell of the unmanned plane body 1, so that the unmanned plane side plates 2 can be detached from the shell of the unmanned plane body 1 for maintenance or replacement of the control circuit and other structures in the shell. The unmanned plane body 1 comprises a mounting chamber 11, which is a mounting structure of the control circuit and other structures. The mounting structure of the control circuit and other structures is arranged inside the mounting chamber 11, and the control circuit and other structures can be protected by the closed mounting chamber 11. The mounting chamber 11 can be formed by one-piece molding or by splicing of multiple side plates. An unmanned plane side opening 12 is arranged on the mounting chamber 11, so as to facilitate installation, replacement and maintenance of the control circuit and other structures in the mounting chamber 11. The unmanned plane side plates 2 are rotatably arranged on the side wall of the mounting chamber 11, so that the unmanned plane side plates 2 can be rotated to open the unmanned plane side opening 12, thereby facilitating installation, maintenance and replacement of the control circuit and other structures in the mounting chamber 11. Preferably, the rotating shaft of the unmanned plane side plates 2 on the mounting chamber 11 is perpendicular to the side wall where the unmanned plane side opening 12 is located, so that the unmanned plane side plates 2 can be completely opened outside the unmanned plane side opening 12 by rotation, so as to completely open the unmanned plane side opening 12. The other side of the unmanned plane side plates 2 is clamped on the side wall of the mounting chamber 11. The unmanned plane side plates 2 are clamped on the side wall of the mounting chamber 11, so as to facilitate quick opening or closing of the unmanned plane side opening 12, thereby facilitating quick replacement and maintenance of internal circuit components, batteries and other components during the racing unmanned plane competition, and shortening the time for replacement or maintenance, thereby avoiding too much time loss in the competition and even losing the competition qualification.

[0029] Referring to Figure 4 、 5 , 7 and 8, one of the side wall of the mounting chamber 11 and the unmanned plane side plates 2 is provided with a rotating mounting part 13, and the other one is provided with a mounting shaft 21. The mounting shaft 21 is rotatably arranged in the mounting shaft 21, so that the unmanned plane side plates 2 can be rotatably mounted on the side wall of the mounting chamber 11. In the embodiment, the rotating mounting part 13 is arranged on the side wall of the mounting chamber 11, and the mounting shaft 21 is arranged on the unmanned plane side plates 2.

[0030] Referring to Figure 4 、 5, 7 and 8, in order to avoid the UAV side plate 2 from the side wall of the installation chamber 11, the mounting shaft 21 is provided with a blocking part 22, the blocking part 22 is provided on the mounting shaft 21 away from the UAV side plate 2 one end, the blocking part 22 blocks the mounting shaft 21 from the rotating mounting part 13, thus the mounting shaft 21 of the UAV side plate 2 is installed on the side wall of the installation chamber 11, can be blocked by the blocking part 22 on the mounting shaft 21, avoid the UAV side plate 2 from the side wall of the installation chamber 11, further save the time of the mounting shaft 21 from the rotating mounting part 13 after falling again. The blocking part 22 can adopt the common blocking structure, the blocking part 22 adopts the following structure in the embodiment: including a plurality of spherical surface structure blocking block 221, each blocking block 221 is provided on the mounting shaft 21 away from the UAV side plate 2 one end, the adjacent blocking block 221 is arranged at intervals, so that each blocking block 221 can be inserted into the rotating mounting part 13 by pinching, the mounting shaft 21 is inserted into the rotating mounting part 13, each blocking block 221 can be expanded outward to block the mounting shaft 21 from the rotating mounting part 13. The blocking part 22 adopts the mode of a plurality of spherical surface structure blocking block 221, which can facilitate the installation and disassembly of the mounting shaft 21 and the rotating mounting part 13, and improve the production and assembly efficiency of the racing UAV with quick disassembly side plate. The mounting shaft 21, the blocking part 22 and the UAV side plate 2 can adopt an integral injection molding structure, or a stamping metal structure.

[0031] Referring to Figure 5 , the rotating mounting part 13 includes a plug-in ring 131 and a connecting rod 132, the plug-in ring 131 is installed inside the side wall of the installation chamber 11 through the connecting rod 132, and the mounting shaft 21 is inserted into the plug-in ring 131. The plug-in ring 131 is installed inside the side wall of the installation chamber 11 through the connecting rod 132, and the UAV side plate 2 can block the plug-in ring 131 and the connecting rod 132 after being installed on the installation chamber 11, so as to avoid the plug-in ring 131 and the connecting rod 132 exposed to affect the flight and appearance integrity of the racing UAV. The plug-in ring 131 and the connecting rod 132 can be integrally formed with the side wall of the installation chamber 11, such as integrally injection molding, integrally stamping.

[0032] Referring to Figure 4 , 5The UAV side plate 2 is provided with a clamping block 23, the side wall of the mounting chamber 11 is provided with a clamping table 14, the clamping block 23 is matched with the clamping table 14, that is, the position, size and shape of the clamping block 23 are matched with the position, size and shape of the clamping table 14, so that the clamping block 23 can be detachably clamped on the clamping table 14. The clamping block 23 is preferably made of soft glue, for example, a rubber block, so that when the UAV side plate 2 is pushed, the UAV side plate 2 can be clamped on the UAV side opening 12 of the mounting chamber 11, and when the UAV side plate 2 is pulled, the UAV side plate 2 can be opened from the UAV side opening 12 of the mounting chamber 11. The UAV side plate 2 is also provided with a buckle hand position 24, which is arranged on the UAV side plate 2 close to the clamping block 23, so as to facilitate opening the UAV side plate 2 from the UAV side opening 12 of the mounting chamber 11 by pulling through the buckle hand position 24.

[0033] Referring to Figures 1-6 The control circuit of the quick-dismounting side plate racing UAV includes a circuit structure 3, the circuit structure 3 includes a first circuit board 31, a second circuit board 32 and a third circuit board 33, the first circuit board 31, the second circuit board 32 and the third circuit board 33 are sequentially stacked in the mounting chamber 11, and the first circuit board 31, the second circuit board 32 and the third circuit board 33 are arranged in the mounting chamber 11 by stacking, which can reduce the space occupation, thereby reducing the volume and weight of the racing UAV and improving the flight speed and time of the racing UAV.

[0034] Referring to Figure 6In order to stably install the first circuit board 31, the second circuit board 32 and the third circuit board 33 in the installation cavity 11, positioning columns 41, separation rings 42 and fixing nuts 43 are arranged in the installation cavity 11, the separation rings 42 and the fixing nuts 43 are sleeved on the positioning columns 41; the first circuit board 31, the second circuit board 32 and the third circuit board 33 are arranged on the positioning columns 41, the first circuit board 31 and the second circuit board 32 and the second circuit board 32 and the third circuit board 33 are separated and limited by the separation rings 42, and the third circuit board 33 is fixed on the positioning column 41 by the fixing nut 43. When the first circuit board 31, the second circuit board 32 and the third circuit board 33 are installed in the installation cavity 11, first, each positioning column 41 is fixed on the bottom wall of the installation cavity 11, then a separation ring 42 is sleeved on each positioning column 41, the first circuit board 31 is installed on each positioning column 41, a separation ring 42 is sleeved on the positioning column 41 above the first circuit board 31, then the second circuit board 32 is installed on the first circuit board 31, a separation ring 42 is sleeved on the positioning column 41 above the second circuit board 32, finally the third circuit board 33 is installed on the first circuit board 31, and the third circuit board 33 is fixed on the positioning column 41 by the fixing nut 43, the first circuit board 31 and the second circuit board 32 are also fixed on the positioning column 41 by the third circuit board 33. The first circuit board 31, the second circuit board 32 and the third circuit board 33 can be stably fixed in the installation cavity 11 by the positioning columns 41, the separation rings 42 and the fixing nuts 43, and the first circuit board 31, the second circuit board 32 and the third circuit board 33 are electrically separated, and the first circuit board 31, the second circuit board 32 and the third circuit board 33 have heat dissipation space, which is beneficial to heat dissipation of components on the circuit board.

[0035] Referring to Figures 1-8When the racing drone of the embodiment needs to replace components such as the first circuit board 31, the second circuit board 32 and the third circuit board 33, the side plate 2 of the drone is pulled by the buckle hand position 24 to separate the clamping block 23 from the clamping table 14, so that the mounting shaft 21 of the side plate 2 of the drone can rotate to open the side opening 12 of the drone in the rotating mounting part 13 of the mounting chamber 11, and then the components such as the first circuit board 31, the second circuit board 32 and the third circuit board 33 in the mounting chamber 11 can be replaced, maintained and maintained; after completion, the mounting shaft 21 of the side plate 2 of the drone is rotated to close the side opening 12 of the drone in the rotating mounting part 13 of the mounting chamber 11, and the clamping block 23 is clamped to the clamping table 14 by pressing the side plate 2 of the drone, which realizes the quick replacement, maintenance and maintenance of the components such as the first circuit board 31, the second circuit board 32 and the third circuit board 33 in the mounting chamber 11, facilitates the quick replacement and maintenance of the internal circuit components, battery and other components during the racing drone competition, and the replacement or maintenance time is shorter, which avoids too much time delay in the competition and affects the competition results or even loses the competition qualification.

[0036] Obviously, the above-mentioned embodiments of the patent are only examples for clearly illustrating the patent, and are not limited to the embodiments of the patent. Based on the above description, other different forms of changes or variations can be made by those skilled in the art. Here, all the embodiments are not required to be exhausted. Any modification, equivalent replacement and improvement within the spirit and principle of the patent should be included in the protection scope of the patent claims.

Claims

1. A racing drone with quick detachable side plates, characterized in that: The unmanned aerial vehicle includes a body (1) and a side plate (2) which is detachably arranged on the body (1); the body (1) includes a mounting chamber (11) provided with an unmanned aerial vehicle side opening (12), one side of the side plate (2) is rotatably arranged on the side wall of the mounting chamber (11), and the other side of the side plate (2) is clamped on the side wall of the mounting chamber (11), and the side plate (2) opens or closes the unmanned aerial vehicle side opening (12).

2. The racing drone with quick detachable side plates of claim 1, wherein: One of the side wall of the mounting chamber (11) and the side plate (2) is provided with a rotating mounting portion (13), and the other is provided with a mounting shaft (21), and the mounting shaft (21) is rotatably arranged in the mounting shaft (21).

3. The racing drone of claim 2, wherein: The mounting shaft (21) is provided with a blocking portion (22) arranged at one end of the mounting shaft (21) away from the side plate (2), and the blocking portion (22) blocks the mounting shaft (21) from being separated from the rotating mounting portion (13).

4. The racing drone of claim 3, wherein: The blocking portion (22) includes a plurality of spherical blocking blocks (221), each of which is arranged at one end of the mounting shaft (21) away from the side plate (2), and the adjacent blocking blocks (221) are arranged at intervals.

5. The racing drone of claim 2, wherein: The rotating mounting portion (13) includes a plug-in ring (131) and a connecting rod (132), the plug-in ring (131) is mounted on the inner side of the side wall of the mounting chamber (11) through the connecting rod (132), and the mounting shaft (21) is inserted into the plug-in ring (131).

6. The racing drone of claim 1, wherein: The side plate (2) is provided with a clamping block (23), and the side wall of the mounting chamber (11) is provided with a clamping table (14), the clamping block (23) is matched with the clamping table (14), and the clamping block (23) is detachably clamped on the clamping table (14).

7. The racing drone of claim 6, wherein: The clamping block (23) is a soft rubber structure.

8. The racing drone of claim 6, wherein: The side plate (2) is further provided with a hand buckle position (24) arranged near the clamping block (23) on the side plate (2).

9. The racing drone of any one of claims 1-8, wherein: The racing unmanned aerial vehicle with the detachable side plate further includes a circuit structure (3), the circuit structure (3) includes a first circuit board (31), a second circuit board (32) and a third circuit board (33), and the first circuit board (31), the second circuit board (32) and the third circuit board (33) are sequentially stacked in the mounting chamber (11).

10. The racing drone of claim 9, wherein: Positioning columns (41), separation rings (42) and fixing nuts (43) are arranged in the mounting chamber (11), the separation rings (42) and the fixing nuts (43) are sleeved on the positioning columns (41); the first circuit board (31), the second circuit board (32) and the third circuit board (33) are all arranged on the positioning columns (41) in a penetrating mode, the first circuit board (31) and the second circuit board (32) and the second circuit board (32) and the third circuit board (33) are all separated and limited by the separation rings (42), and the third circuit board (33) is fixed on the positioning columns (41) by the fixing nuts (43).

Images