Collision protection structure of unmanned aerial vehicle

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, and discloses an unmanned aerial vehicle collision protection structure which comprises an unmanned aerial vehicle body, a supporting leg rod is fixed to the unmanned aerial vehicle body, and screw joints are arranged at the two ends of the supporting leg rod; the unmanned aerial vehicle further comprises a buffering mechanism, a screw joint sleeve is connected to the screw joint in a screwed mode, the buffering mechanism is installed on the screw joint sleeve and used for buffering and damping the unmanned aerial vehicle body, and the buffering mechanism comprises an inserting rod connected to the screw joint sleeve in a sleeving mode. By arranging a screw joint sleeve and a screw joint, mounting and dismounting of the buffer mechanism can be facilitated, assembly of the unmanned aerial vehicle is facilitated, by arranging a fixing block, a fixing column and a nut, after long-term use, the buffer spring can be independently replaced when the buffer spring is damaged, traditional whole replacement is avoided, the replacement cost is reduced, mounting and dismounting are convenient, and the unmanned aerial vehicle is convenient to use. And by arranging an inserting rod and an inserting groove, the mounting stability of the buffering anti-collision mechanism is further improved, and the practicability is improved.

Description

Technical Field

[0001] This application relates to the technical field of unmanned aerial vehicles, and in particular to a collision protection structure for an unmanned aerial vehicle. Background Art

[0002] An unmanned aerial vehicle, abbreviated as "UAV" and with the English abbreviation "UAV", is an unpiloted aircraft controlled by a radio remote control device and a self - contained program control device, or is operated completely or intermittently autonomously by an on - vehicle computer. Currently, UAV technology has been widely applied, and UAVs can replace humans in performing some tasks that are difficult or dangerous for humans.

[0003] To avoid damage to the UAV when it collides with a location during recovery, some existing UAVs are equipped with spring buffer components on their support legs. However, after long - term use, the springs will rust due to aging, reducing their original elasticity. When replacing them, the staff needs to replace the support legs together, increasing the replacement cost and making it inconvenient for normal use. Utility Model Content

[0004] To solve the problem, this application provides a collision protection structure for an unmanned aerial vehicle.

[0005] A collision protection structure for an unmanned aerial vehicle provided by this application adopts the following technical solutions:

[0006] A collision protection structure for an unmanned aerial vehicle includes a UAV body, on which a support leg rod is fixed, and screw joints are provided at both ends of the support leg rod; it also includes a buffer mechanism. A screw sleeve is screwed onto the screw joint, and the buffer mechanism is installed on the screw sleeve for buffering and damping the UAV body.

[0007] Preferably, the buffer mechanism includes an insertion rod sleeved on the screw sleeve. The insertion rod is slidably connected to the screw sleeve. A fixed block is fixed at the extending end of the insertion rod, and a fixed column is sleeved on the fixed block. The fixed column is slidably connected to the fixed block.

[0008] Preferably, a screw joint is also provided at the top of the fixed column, and a nut is screwed onto the screw joint.

[0009] Preferably, a support foot pad is fixed at the bottom end of the fixed column. It also includes a buffer spring, which is sleeved outside the fixed column and is connected to the fixed block and the support foot pad respectively.

[0010] Preferably, an insertion slot is formed on the end face of the support leg rod, and the insertion rod is adapted to the insertion slot.

[0011] Preferably, a positioning piece is fixed on the insertion rod, and the positioning piece can be connected to the support leg rod.

[0012] Preferably, a chamfer is provided at the notch of the insertion groove.

[0013] In summary, the present application includes the following beneficial technical effects:

[0014] By providing a screwed sleeve and a screwed joint, the installation and disassembly of the buffer mechanism can be facilitated, which is helpful for the assembly of the drone. By providing a fixing block, a fixing column and a nut, after long-term use, when the buffer spring is damaged, it can be replaced individually, so as to avoid replacing the whole as in the traditional method, reduce the replacement cost, and the installation and disassembly are relatively convenient. Moreover, by providing an insertion rod and an insertion groove, the installation stability of the buffer and anti-collision mechanism is further improved, and the practicability is enhanced. Description of the Drawings

[0015] Figure 1 is a three-dimensional structural schematic diagram of the present utility model;

[0016] Figure 2 is a partial explosion and sectional structural schematic diagram of the present utility model;

[0017] Figure 3 is Figure 2 an enlarged structural schematic diagram of part A in

[0018] Description of the reference numerals: 1, drone body; 2, support leg rod; 3, support foot pad; 4, fixing block; 5, screwed sleeve; 6, screwed joint; 7, insertion groove; 8, insertion rod; 9, positioning piece; 10, fixing column; 11, nut; 12, buffer spring. Detailed Description of the Embodiment

[0019] The following further describes the present application in detail with reference to the Figures 1 - 3 drawings.

[0020] The embodiment of the present application discloses a collision protection structure for a drone. Refer to Figures 1 - 3, a collision protection structure for a drone, comprising a drone body 1, on which a support leg rod 2 is fixed, and screw joints 6 are arranged at both ends of the support leg rod 2; further comprising a buffer mechanism, a screw sleeve 5 is screwed onto the screw joint 6, and the buffer mechanism is installed on the screw sleeve 5 for buffering and shock-absorbing the drone body 1. The buffer mechanism includes an insertion rod 8 sleeved on the screw sleeve 5, the insertion rod 8 is slidably connected to the screw sleeve 5, a fixed block 4 is fixed at the protruding end of the insertion rod 8, a fixed column 10 is sleeved on the fixed block 4, and the fixed column 10 is slidably connected to the fixed block 4. The insertion rod 8 and the screw sleeve 5 are slidably connected. Therefore, the screw sleeve 5 can rotate freely on the insertion rod 8. During installation, only by aligning and screwing the screw sleeve 5 clockwise can the buffer mechanism be installed on the support leg rod 2, which is convenient for operation. Through the design of the screw sleeve 5, it is also unnecessary to use tools during the installation process, and the staff can operate with their hands, improving the practicality and facilitating subsequent maintenance.

[0021] In this embodiment, as Figure 3 shown, a support foot pad 3 is fixed at the bottom end of the fixed column 10. Further comprising a buffer spring 12, the buffer spring 12 is sleeved outside the fixed column 10 and is respectively connected to the fixed block 4 and the support foot pad 3. When the drone body 1 lands, first, the support foot pad 3 contacts the ground, and the collision force will be transmitted to the fixed column 10, causing the fixed column 10 to move upward. At this time, the support foot pad 3 squeezes the buffer spring 12, and part of the collision force will be transmitted to the buffer spring 12, so as to slow down the force through the characteristics of the buffer spring 12 itself, thereby realizing the function of buffering and anti-collision.

[0022] In this embodiment, as Figure 3 shown, a screw joint 6 is also arranged at the top end of the fixed column 10, and a nut 11 is screwed onto the screw joint 6. When the buffer spring 12 is damaged or cannot play a normal buffering role, unscrew and remove the nut 11, and pull out the fixed column 10 to replace it, reducing the cumbersome steps of traditional overall replacement and lowering the replacement cost.

[0023] In this embodiment, as Figure 3 shown, an insertion slot 7 is opened on the end face of the support leg rod 2, and the insertion rod 8 is adapted to the insertion slot 7. This setting further improves the installation stability of the buffer anti-collision mechanism and improves the practicality.

[0024] In this embodiment, as Figure 3 shown, a positioning piece 9 is fixed on the insertion rod 8, and the positioning piece 9 can be connected to the support leg rod 2. When the insertion rod 8 is inserted into the insertion slot 7, the positioning piece 9 fits against the end face of the support leg rod 2, playing a limiting role.

[0025] In this embodiment, as Figure 3As shown, a chamfer is provided at the notch of the insertion slot 7. The chamfer enables the insertion rod 8 to be inserted into the insertion slot 7 more smoothly, facilitating the installation operation and having practicality.

[0026] The implementation principle of a drone collision protection structure according to an embodiment of the present application is as follows: During installation, only need to align the insertion rod 8 and insert it into the insertion slot 7. At this time, the screwed sleeve 5 is sleeved on the support leg rod 2, and by clockwise screwing the screwed sleeve 5, the buffer mechanism can be installed on the support leg rod 2. The operation is convenient. Through the design of the screwed sleeve 5, it is also unnecessary to use tools during the installation process, and the staff can operate with their hands, improving the practicality and facilitating subsequent maintenance. When the buffer spring 12 is damaged or cannot play a normal buffering role, unscrew and remove the nut 11, and pull out the fixed column 10 to replace it, reducing the cumbersome steps of traditional overall replacement and reducing the replacement cost. By providing the screwed sleeve 5 and the screwed joint 6, it is convenient for the installation and disassembly of the buffer mechanism, which helps the assembly of the drone. By providing the fixed block 4, the fixed column 10 and the nut 11, after long-term use, when the buffer spring 12 is damaged, it can be replaced separately, avoiding traditional overall replacement, reducing the replacement cost, and the installation and disassembly are both relatively convenient. Moreover, by providing the insertion rod 8 and the insertion slot 7, the installation stability of the buffer and anti-collision mechanism is further improved, and the practicality is enhanced.

[0027] Finally, several points should be noted: First, in the description of the present application, it should be noted that unless otherwise specified and limited, the terms "installation", "connection", and "coupling" should be understood in a broad sense, which can be mechanical connection or electrical connection, or the internal communication of two components, and can be directly connected. "Up", "down", "left", "right", etc. are only used to represent the relative position relationship. When the absolute position of the described object changes, the relative position relationship may change;

[0028] Second: In the attached drawings of the disclosed embodiments of the present utility model, only the structures related to the disclosed embodiments are involved. Other structures can refer to the usual designs. Without conflict, the same embodiment and different embodiments of the present utility model can be combined with each other;

[0029] Finally: The above are only the preferred embodiments of the present utility model and are not used to limit the present utility model. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present utility model shall be included in the protection scope of the present utility model.

[0030] The above are all the preferred embodiments of the present application, and do not limit the protection scope of the present application accordingly. Therefore, all equivalent changes made according to the structure, shape, and principle of the present application shall be covered by the protection scope of the present application.

Claims

1. A collision protection structure for a drone, comprising a drone body (1), characterized in that: A support leg rod (2) is fixed on the UAV body (1), and screw joints (6) are arranged at both ends of the support leg rod (2); It further includes a buffer mechanism. A screw sleeve (5) is screwed on the screw joint (6), and the buffer mechanism is installed on the screw sleeve (5) for buffering and shock-absorbing the UAV body (1).

2. The collision protection structure of an unmanned aerial vehicle according to claim 1, characterized in that: The buffer mechanism includes an insertion rod (8) sleeved on the screw sleeve (5). The insertion rod (8) is slidably connected to the screw sleeve (5). A fixed block (4) is fixed at the protruding end of the insertion rod (8). A fixed column (10) is sleeved on the fixed block (4), and the fixed column (10) is slidably connected to the fixed block (4).

3. The drone collision protection structure according to claim 2, wherein: A screw joint (6) is also arranged at the top end of the fixed column (10), and a nut (11) is screwed on the screw joint (6).

4. The drone collision protection structure according to claim 2, characterized in that: A support foot pad (3) is fixed at the bottom end of the fixed column (10). It further includes a buffer spring (12). The buffer spring (12) is sleeved outside the fixed column (10) and is respectively connected to the fixed block (4) and the support foot pad (3).

5. The drone collision protection structure according to claim 2, wherein: An insertion slot (7) is formed in the end face of the support leg rod (2), and the insertion rod (8) is adapted to the insertion slot (7).

6. The drone collision protection structure according to claim 2, wherein: A positioning piece (9) is fixed on the insertion rod (8), and the positioning piece (9) can be connected to the support leg rod (2).

7. The collision protection structure of an unmanned aerial vehicle according to claim 5, characterized in that: A chamfer is arranged at the notch of the insertion slot (7).

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