Anti-shaking support for unmanned aerial vehicle transportation

Abstract

The utility model relates to the technical field of transportation supports, in particular to an anti-shaking support for unmanned aerial vehicle transportation, which comprises a first limiting seat and a second limiting seat which are horizontally opposite, and the two sides of the width of the first limiting seat and the two sides of the width of the second limiting seat are fixedly connected through connecting rods. A first supporting step is arranged at the bottom of the end, close to the second limiting seat, of the first limiting seat, limiting protruding blocks are arranged on the two sides of the bottom of the end, close to the first limiting seat, of the second limiting seat in the width direction of the second limiting seat, and the bottom ends of the first limiting seat, the second limiting seat, the first supporting step and the limiting protruding blocks are flush. After the unmanned aerial vehicle is placed between the first limiting base and the second limiting base, the two connecting rods clamp and limit the unmanned aerial vehicle in the width direction, the first supporting step and the limiting protruding block abut against the two sides of the bottom end of the unmanned aerial vehicle in the length direction correspondingly, then the unmanned aerial vehicle can be prevented from shaking in the transportation process, and the structure is simple and practical.

Description

Technical Field

[0001] The utility model relates to the technical field of transportation brackets, in particular to an anti-shake bracket for transporting unmanned aerial vehicles (UAVs). Background Technique

[0002] An unmanned aerial vehicle, abbreviated as "UAV", is an unpiloted aircraft controlled by a radio remote control device and a self-contained program control device.

[0003] During the transportation of existing UAVs, shaking is likely to occur, and when colliding with other objects, it may cause damage to the equipment. Therefore, an anti-shake bracket is needed. Summary of the Invention

[0004] The purpose of the utility model is to provide an anti-shake bracket for transporting UAVs to solve the problems raised in the above background technique.

[0005] To achieve the above purpose, the utility model provides the following technical solution: An anti-shake bracket for transporting UAVs, including horizontally opposite first limit seats and second limit seats, and both sides of the widths of the first limit seats and the second limit seats are fixedly connected through connecting rods. A first support step is arranged at the bottom of one end of the first limit seat close to the second limit seat. Limit bumps are arranged on both sides along the width direction of the bottom of one end of the second limit seat close to the first limit seat. The bottoms of the first limit seat, the second limit seat, the first support step and the limit bumps are flush.

[0006] Further, both ends of the connecting rod are fixedly connected to the side walls of the first limit seat and the second limit seat respectively.

[0007] Further, both the first limit seat and the second limit seat are of hollow structures, and liquid injection ports can be opened and closed on both the first limit seat and the second limit seat.

[0008] Further, telescopic rods for adjusting the distance between the two connecting rods are arranged at both ends of the first limit seat and the second limit seat away from each other. The telescopic rod includes a second outer tube arranged along the width direction of the first limit seat and the second limit seat, two second inner rods movably inserted into both ends of the length of the second outer tube, and a fastening component for fixing the second inner rods.

[0009] Further, the fastening component includes a limit rod fixed on the second inner rod. A strip-shaped hole is arranged along the length direction of the second outer tube at one end of the second outer tube close to the limit rod, and the limit rod passes through the strip-shaped hole and extends to the outside of the limit rod and is threadedly connected with a fastening knob.

[0010] Further, the connecting rod includes a first outer tube and two first inner rods respectively threadedly connected to both ends of the first outer tube. The threads of the two first inner rods are opposite, and the two first inner rods are respectively installed and positioned with the first limit seat and the second limit seat.

[0011] Compared with the prior art, the beneficial effects of the present utility model are as follows:

[0012] By providing the first limit seat, the second limit seat and the connecting rod, after placing the drone between the first limit seat and the second limit seat, the two connecting rods clamp and limit the width direction of the drone. At the bottom ends of the opposite sides of the first limit seat and the second limit seat, a first support step and a limit convex block are respectively provided. The first support step and the limit convex block respectively abut against both sides of the bottom length of the drone, thereby avoiding the shaking of the drone during transportation. The structure is simple and practical.

[0013] By setting the first limit seat and the second limit seat as hollow structures, and the top ends of the first limit seat and the second limit seat are provided with liquid injection ports that can be opened and closed. During transportation, water can be filled into the first limit seat and the second limit seat to increase the weight of the bracket, reduce the overall shaking and improve the stability.

[0014] By setting the connecting rod as an adjustable structure of the first inner rod and the first outer tube, telescopic rods are provided at both ends of the two connecting rods, and the distance between the first limit seat and the second limit seat and the distance between the two connecting rods can be adjusted according to the size of the drone to meet different usage requirements. BRIEF DESCRIPTION OF THE DRAWINGS

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

[0016] Figure 2 is a front structural schematic diagram of the present utility model in the transportation state;

[0017] Figure 3 is a three-dimensional structural schematic diagram of Embodiment 3 of the present utility model;

[0018] Figure 4 is an exploded schematic diagram of Embodiment 3 of the present utility model.

[0019] In the figure: 1, first limit seat; 101, first support step; 2, second limit seat; 201, limit convex block; 3, connecting rod; 301, first inner rod; 302, first outer tube; 4, liquid injection port; 5, telescopic rod; 501, second outer tube; 502, second inner rod; 503, fastening assembly; 5031, limit rod; 5032, fastening knob; 5033, strip hole. DETAILED DESCRIPTION OF THE EMBODIMENTS

[0020] The following will clearly and completely describe the technical solutions in the embodiments of the present utility model in conjunction with the accompanying drawings in the embodiments of the present utility model. In the description of the present utility model, it should be noted that the descriptions of terms such as "first" and "second" are only for descriptive purposes, and do not particularly refer to the order or sequence, nor are they used to limit the present utility model. They are only used to distinguish components or operations described with the same technical terms, and cannot be understood as indicating or implying their relative importance or implicitly indicating the quantity of the indicated technical features. Thus, the features defined with "first" and "second" may explicitly or implicitly include at least one of such features. For the terms "including" and any variations thereof in the description, claims and above-mentioned drawings of the present utility model, the intention is to cover non-exclusive inclusion.

[0021] In the description of the present utility model, it should be noted that unless otherwise clearly specified and limited, the terms "installed", "connected", "connected", and "set" should be understood in a broad sense. For example, it can be a fixed connection or a detachable connection; it can be a mechanical connection or an electrical connection; it can be directly connected or indirectly connected through an intermediate medium, and it can be the communication inside two elements. For those of ordinary skill in the art, the specific meanings of the above terms in the present utility model can be understood according to specific situations. In addition, in the description of the present utility model, it should be understood that the orientation or positional relationship indicated by terms such as "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", etc. is based on the orientation or positional relationship shown in the accompanying drawings, and is only for the convenience of describing the present utility model and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation to the present utility model.

[0022] Please refer to Figure 1-2 , an embodiment provided by the present utility model: an anti-shake bracket for drone transportation, including a first limiting seat 1 and a second limiting seat 2 that are horizontally opposite, and both sides of the widths of the first limiting seat 1 and the second limiting seat 2 are connected and fixed through connecting rods 3. In this embodiment, the first limiting seat 1 and the second limiting seat 2 have the same width, the length of the connecting rod 3 is fixed, and its two ends are respectively fixedly connected to the side walls of the first limiting seat 1 and the second limiting seat 2. Referring to the attached Figure 2 , the first limiting seat 1, the second limiting seat 2 and the two connecting rods 3 form an open receiving cavity. When the drone is placed between the two connecting rods 3, the two sides of the width of the drone fuselage can be clamped and limited. Further, rubber pads can be provided on the opposite sides of the two connecting rods 3, which are flexibly connected to the drone to reduce scratching.

[0023] A first support step 101 is provided at the bottom of one end of the first limit seat 1 close to the second limit seat 2. Limit bumps 201 are provided on both sides along the width direction of the bottom of one end of the second limit seat 2 close to the first limit seat 1. The bottoms of the first limit seat 1, the second limit seat 2, the first support step 101 and the limit bumps 201 are flush. Refer to the appendix Figure 2 The gimbal camera of the drone abuts against the top of the first support step 101. The first support step 101 and the limit bumps 201 respectively abut against both sides of the bottom end of the drone, which can limit both sides in the length direction of the drone and prevent it from shaking during transportation.

[0024] Working principle: During transportation, the drone is directly placed between the first limit seat 1 and the second limit seat 2 from top to bottom. The wings are located above the first limit seat 1 and the second limit seat 2. The two connecting rods 3 are clamped on both sides of the width of the drone fuselage. The gimbal camera on one side of the bottom end of the drone is lapped above the first support step 101. The first support step 101 and the limit bumps 201 respectively abut against both sides of the length of the drone base, which can prevent the drone from shaking back and forth, left and right during transportation.

[0025] Embodiment 2: On the basis of Embodiment 1, the first limit seat 1 and the second limit seat 2 are set as hollow structures, and liquid injection ports 4 are provided at the tops of the first limit seat 1 and the second limit seat 2. Sealing caps are threadedly provided at the tops of the liquid injection ports 4. When transporting, filling the inside of the first limit seat 1 and the second limit seat 2 with water can increase the weight of the bracket, thereby improving its stability. When not transporting, the water can be poured out for convenient storage.

[0026] Embodiment 3: Please refer to Figure 3-4 On the basis of Embodiment 2, telescopic rods 5 for adjusting the distance between the two connecting rods 3 are provided at both ends of the first limit seat 1 and the second limit seat 2 away from each other. The telescopic rod 5 includes a second outer tube 501 arranged along the width direction of the first limit seat 1 and the second limit seat 2, two second inner rods 502 movably inserted at both ends of the length of the second outer tube 501, and a fastening assembly 503 for fixing the second inner rod 502. In this embodiment, the fastening assembly 503 includes a limit rod 5031 fixed on the second inner rod 502. A strip hole 5033 is provided along the length direction of one end of the second outer tube 501 close to the limit rod 5031. The limit rod 5031 passes through the strip hole 5033 and extends to the outside of the limit rod 5031 and is threadedly connected with a fastening knob 5032. By loosening the fastening knob 5032, the positions of the two second inner rods 502 inside the second outer tube 501 can be adjusted, and then drones with different widths can be transported. At the same time, the sliding of the limit rod 5031 inside the strip hole 5033 can play a role in limiting to prevent the second inner rod 502 from separating from the second outer tube 501.

[0027] In this embodiment, the connecting rod 3 is specifically a telescopic structure, including a first outer tube 302 and two first inner rods 301 respectively threadedly connected to both ends of the first outer tube 302. The threads of the two first inner rods 301 are opposite, and the two first inner rods 301 are respectively installed and positioned with the first limit seat 1 and the second limit seat 2. Specifically, the first inner rods 301 on both sides are respectively fixedly connected to the second inner rods 502 outside the second outer tube 501. By rotating the first outer tube 302, the two first inner rods 301 on both sides can be driven to move simultaneously to both sides or to the middle, so as to limit unmanned aerial vehicles (UAVs) of different lengths, and the adjustment is convenient. Further, the connecting rod 3 can also be set as an outer tube and an inner rod movably inserted inside the outer tube, and the two are fixed by bolts. The ends of the outer tube and the inner rod away from each other are respectively connected to the telescopic rods 5 on both sides.

[0028] Working principle: When it is necessary to transport UAVs of different sizes, first loosen the fastening knob 5032, slide the limit rod 5031 inside the strip hole 5033, and then adjust the distance between the two connecting rods 3 through the second inner rod 502. After the adjustment is completed, tighten the fastening knob 5032 to fix the second inner rod 502. Rotate the first outer tube 302 to drive the two first inner rods 301 to move in the opposite direction inside the first outer tube 302, and the distance between the first limit seat 1 and the second limit seat 2 can be adjusted to be applicable to UAVs of different sizes.

[0029] For those skilled in the art, it is obvious that the present utility model is not limited to the details of the above exemplary embodiments, and without departing from the spirit or basic characteristics of the present utility model, the present utility model can be implemented in other specific forms. Therefore, from any point of view, the embodiments should be regarded as exemplary and non-restrictive. The scope of the present utility model is defined by the appended claims rather than the above description. Therefore, it is intended to include all changes falling within the meaning and scope of the equivalent elements of the claims in the present utility model. Any reference signs in the claims should not be regarded as limiting the claims involved.

Claims

1. Anti-shake bracket for drone transportation, characterized in that: It includes horizontally opposite first limiting seats (1) and second limiting seats (2), and both sides of the widths of the first limiting seats (1) and the second limiting seats (2) are connected and fixed by connecting rods (3). A first support step (101) is provided at the bottom of one end of the first limiting seat (1) close to the second limiting seat (2). Limiting bumps (201) are provided on both sides along the width direction of the bottom of one end of the second limiting seat (2) close to the first limiting seat (1). The bottoms of the first limiting seat (1), the second limiting seat (2), the first support step (101) and the limiting bumps (201) are flush.

2. The anti-shake bracket for drone transportation according to claim 1, characterized in that: Both ends of the connecting rod (3) are fixedly connected to the side walls of the first limiting seat (1) and the second limiting seat (2) respectively.

3. The anti-shake bracket for drone transportation according to claim 1, characterized in that: Both the first limiting seat (1) and the second limiting seat (2) are of hollow structures, and liquid injection ports (4) can be opened and closed on the first limiting seat (1) and the second limiting seat (2).

4. The anti-shake bracket for drone transportation according to claim 1, characterized in that: Both ends of the first limiting seat (1) and the second limiting seat (2) far away from each other are provided with telescopic rods (5) for adjusting the distance between the two connecting rods (3). The telescopic rod (5) includes a second outer tube (501) arranged along the width direction of the first limiting seat (1) and the second limiting seat (2), two second inner rods (502) movably inserted at both ends of the length of the second outer tube (501), and a fastening assembly (503) for fixing the second inner rod (502).

5. The anti-shake bracket for drone transportation according to claim 4, characterized in that: The fastening assembly (503) includes a limiting rod (5031) fixed on the second inner rod (502). A strip-shaped hole (5033) is penetrated along the length direction of the second outer tube (501) at one end of the second outer tube (501) close to the limiting rod (5031), and the limiting rod (5031) passes through the strip-shaped hole (5033) and extends to the outside of the limiting rod (5031) and is threadedly connected with a fastening knob (5032).

6. The anti-shake bracket for drone transportation according to claim 1, wherein: The connecting rod (3) includes a first outer tube (302) and two first inner rods (301) respectively threadedly connected to both ends of the first outer tube (302). The threads of the two first inner rods (301) are opposite, and the two first inner rods (301) are respectively installed and positioned with the first limiting seat (1) and the second limiting seat (2).

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