Unmanned aerial vehicle hanging frame

Abstract

The utility model discloses an unmanned aerial vehicle hanging rack, which relates to the technical field of unmanned aerial vehicles, and comprises a main hanging rack and two auxiliary hanging racks symmetrically arranged on the two sides of the main hanging rack, the main hanging rack comprises a main framework, the top of the main framework is fixedly connected with a hanging rod fixedly connected with an unmanned aerial vehicle, the bottom of the main framework is provided with a hanging groove, and the hanging rod is fixedly connected with the hanging groove. The main hanging frame comprises a main framework, a hanging groove is formed in the main framework, a movable first hanging buckle is installed at the hanging groove, a lock catch assembly is arranged on one side of the main framework, the auxiliary hanging frame comprises an auxiliary framework, and second hanging grooves are formed in the upper side and the lower side of the auxiliary framework. The main hanging frame is fixed below the unmanned aerial vehicle through the hanging rod, the hanging buckle can be locked, opened and closed through the lock catch assembly, hanging use is convenient, the lock catch assembly and the hanging buckle are convenient to open and close, use is convenient and fast, the object dismounting and mounting efficiency is high, the main hanging frame and the auxiliary hanging frame of the device are used in cooperation, and the use effect is good. The device can be high in suspension stability and higher in practicability.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, specifically an unmanned aerial vehicle mounting bracket. Background Art

[0002] Weapon equipment such as a cartridge canister can be installed at the bottom of an unmanned aerial vehicle platform. The cartridge canisters are mostly directly fixed to the bottom of the airframe in a side-by-side arrangement. Since the connection positions between the cartridge canisters and the bottom of the unmanned aerial vehicle airframe are few, the stability of the cartridge canister installation is affected, making it difficult to ensure the accuracy of shell firing and the safety of operators. Therefore, an unmanned aerial vehicle mounting bracket is proposed here. Summary of the Utility Model

[0003] Technical Problems to be Solved

[0004] The purpose of the utility model is to make up for the deficiencies of the prior art and provide an unmanned aerial vehicle mounting bracket.

[0005] Technical Solution

[0006] To achieve the above object, the utility model provides the following technical solution: an unmanned aerial vehicle mounting bracket, including a main mounting bracket and two auxiliary mounting brackets symmetrically arranged on both sides of the main mounting bracket;

[0007] The main mounting bracket includes a main frame. A hanging rod fixedly connected to the unmanned aerial vehicle is fixedly connected to the top of the main frame. A hanging groove is arranged at the bottom of the main frame. A movable first hanging buckle is installed at the hanging groove. A locking component is arranged on one side of the main frame. The main mounting bracket is fixed under the unmanned aerial vehicle through the hanging rod. The hanging buckle can be locked and opened through the locking component, which is convenient for hanging use. Moreover, the opening and closing between the locking component and the hanging buckle in this application are convenient, and it is convenient and fast to use, with high efficiency in disassembling and assembling objects;

[0008] The auxiliary mounting bracket includes an auxiliary frame. Second hanging grooves are respectively arranged on the upper and lower sides of the auxiliary frame. A rotatable second hanging buckle is installed at the second hanging grooves. A locking component is arranged on one side of the auxiliary frame. The main mounting bracket and the auxiliary mounting bracket of this device are used in cooperation, which can make the suspension stability of this device high and the practicability stronger.

[0009] Preferably, the locking component includes a fixed frame fixed on the main frame. A locking frame is movably connected inside the fixed frame through a pin shaft structure.

[0010] Preferably, a locking rod is threadedly connected inside the locking frame. A locking block is also fixedly connected inside the fixed frame.

[0011] Preferably, one end of the locking rod is in a hook shape, and this hook-shaped end can be detachably buckled on the first hanging buckle or the second hanging buckle. A connecting thread is arranged at the other end of the locking rod.

[0012] Preferably, a fixed shaft is fixedly connected inside the buckle frame, a threaded hole for installing the buckle rod is opened inside the fixed shaft, and one end of the connecting thread of the buckle rod is threadedly connected inside the threaded hole.

[0013] Preferably, installation holes for installing hanging buckles are opened inside both the main skeleton and the sub-skeleton, and installation shafts adapted to the installation holes are fixed on the first hanging buckle and the second hanging buckle.

[0014] Beneficial effects:

[0015] Compared with the prior art, the drone hanger has the following beneficial effects:

[0016] When the present utility model is in use, the main hanger is fixed under the drone through the hanging rod, and the hanging buckle can be locked and opened through the buckle assembly, which is convenient for hanging use. Moreover, the opening and closing between the buckle assembly and the hanging buckle in this application is convenient, and it is convenient and fast to use, with high efficiency in disassembling and assembling objects. In addition, the main hanger and the sub-hanger of this device are used in cooperation, which can make the hanging stability of this device high and the practicability stronger. Description of the drawings

[0017] In order to more clearly illustrate the technical solutions in the embodiments of the present utility model or the prior art, the following will briefly introduce the drawings required for use in the description of the embodiments or the prior art. Obviously, the following drawings are only some embodiments of the present utility model. For those of ordinary skill in the art, other drawings can be obtained based on these drawings without creative efforts.

[0018] Figure 1 It is a structural schematic diagram of the present utility model;

[0019] Figure 2 It is a structural schematic diagram of the main hanger and the sub-hanger of the present utility model;

[0020] Figure 3 For the present utility model Figure 2 The enlarged structural schematic diagram of part A;

[0021] Figure 4 It is a structural schematic diagram of the buckle rod of the present utility model;

[0022] Figure 5 It is a side view structural schematic diagram of the main hanger of the present utility model;

[0023] Figure 6 For the present utility model Figure 5 The enlarged structural schematic diagram of part A.

[0024] In the figure:

[0025] 1. Main hanging rack; 101. Main skeleton; 102. Hanging rod; 103. Hanging groove; 104. First hanging buckle; 2. Sub-hanging rack; 201. Sub-skeleton; 202. Second hanging groove; 203. Second hanging buckle; 3. Locking component; 301. Fixed rack; 302. Locking rack; 303. Locking rod; 304. Locking block; 3031. In the shape of a hook; 3032. Connecting thread; 3021. Fixed shaft; 3022. Threaded hole; 4. Mounting hole; 5. Mounting shaft; 6. Suspended object. Detailed implementation manner

[0026] The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present invention without creative efforts shall fall within the protection scope of the present invention.

[0027] Please refer to Figures 1 to 6 As shown, the present invention provides a technical solution: a drone hanging rack, including a main hanging rack 1 and two sub-hanging racks 2 symmetrically arranged on both sides of the main hanging rack 1. As Figure 1 shown, the suspended object 6 is installed on the main hanging rack 1 and the sub-hanging rack 2. The main hanging rack 1 includes a main skeleton 101. The top of the main skeleton 101 is fixedly connected with a hanging rod 102 fixedly connected to the drone. The bottom of the main skeleton 101 is provided with a hanging groove 103. A movable first hanging buckle 104 is installed at the hanging groove 103. A locking component 3 is arranged on one side of the main skeleton 101. The sub-hanging rack 2 includes a sub-skeleton 201. Second hanging grooves 202 are opened on both the upper and lower sides of the sub-skeleton 201. A rotatable second hanging buckle 203 is installed at the second hanging grooves 202. A locking component 3 is arranged on one side of the sub-skeleton 201. Mounting holes 4 for installing hanging buckles are opened inside both the main skeleton 101 and the sub-skeleton 201. Mounting shafts 5 adapted to the mounting holes 4 are fixed on the first hanging buckle 104 and the second hanging buckle 203. The main hanging rack 1 is fixed under the drone through the hanging rod 102. The locking component 3 can lock and open the hanging buckle, which is convenient for hanging use. Moreover, the opening and closing between the locking component 3 and the hanging buckle in this application are convenient, easy and fast to use, the disassembly and assembly efficiency of objects is high, and the main hanging rack 1 and the sub-hanging rack 2 of this device are used in cooperation.

[0028] Please refer particularly to Figure 2 , Figure 3 and Figure 4 , the locking component 3 includes a fixed rack 301 fixed on the main skeleton 101. The inside of the fixed rack 301 is movably connected with a locking rack 302 through a pin shaft structure. A locking rod 303 is threadedly connected inside the locking rack 302. A locking block 304 is also fixedly connected inside the fixed rack 301.

[0029] Please refer specifically to Figure 4 , one end of the latch rod 303 is in the shape of a hook 3031, and this hooked end can be detachably buckled on the first buckle 104 or the second buckle 203. The other end of the latch rod 303 is provided with a connecting thread 3032. Inside the latch bracket 302, a fixed shaft 3021 is fixedly connected. Inside the fixed shaft 3021, a threaded hole 3022 for installing the latch rod 303 is opened. One end of the connecting thread 3032 of the latch rod 303 is threadedly connected inside this threaded hole 3022.

[0030] Working principle: The main hanger 1 is fixed under the unmanned aerial vehicle through the hanging rod 102. The buckle can be locked, opened and closed through the buckle assembly 3, which is convenient for hanging use. The opening and closing between the buckle assembly 3 and the buckle is convenient, and it is convenient and fast to use. The main hanger 1 and the auxiliary hanger 2 of this device are used in cooperation, which can make the hanging stability of this device high.

[0031] It should be noted that in this article, relational terms such as first and second are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Moreover, the terms "include", "comprise" or any other variant thereof are intended to cover non-exclusive inclusion, so that a process, method, article or device including a series of elements not only includes those elements, but also includes other elements not expressly listed, or also includes elements inherent to this process, method, article or device.

[0032] Although the embodiments of the present invention have been shown and described, for those of ordinary skill in the art, it can be understood that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principle and spirit of the present invention. The scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. An unmanned aerial vehicle pylon, comprising a main pylon (1) and two auxiliary pylons (2) symmetrically arranged on both sides of the main pylon (1), characterized in that: The main pylon (1) comprises a main frame (101), the top of the main frame (101) is fixedly connected to a hanging rod (102) fixedly connected to the drone, the bottom of the main frame (101) is provided with a hanging groove (103), a movable first hanging buckle (104) is installed at the hanging groove (103), and a locking buckle assembly (3) is provided on one side of the main frame (101); The secondary hanging frame (2) comprises a secondary frame (201), the secondary frame (201) is provided with second hanging grooves (202) on both upper and lower sides, a rotatable second hanging buckle (203) is installed at the second hanging groove (202), and a locking buckle assembly (3) is provided on one side of the secondary frame (201).

2. The drone rack according to claim 1, characterized in that: The locking assembly (3) comprises a fixing frame (301) fixed on the main frame (101), and the interior of the fixing frame (301) is movably connected to a locking frame (302) via a pin structure.

3. The UAV rack according to claim 2, characterized in that: The locking frame (302) is internally threadedly connected to a locking rod (303), and the fixing frame (301) is also internally fixedly connected to a locking block (304).

4. The UAV rack according to claim 3, characterized in that: One end of the locking rod (303) is in the shape of a hook (3031), and the hook-shaped end can be buckled on the first hook (104) or the second hook (203), and the other end of the locking rod (303) is provided with a connecting thread (3032).

5. The drone rack according to claim 4, characterized in that: A fixed shaft (3021) is fixedly connected to the interior of the locking frame (302), a threaded hole (3022) for mounting a locking rod (303) is provided inside the fixed shaft (3021), and one end of a connecting thread (3032) of the locking rod (303) is threadedly connected to the interior of the threaded hole (3022).

6. The UAV rack according to claim 1, characterized in that: The main frame (101) and the auxiliary frame (201) are both provided with mounting holes (4) for mounting hooks, and the first hook (104) and the second hook (203) are fixed with mounting shafts (5) adapted to the mounting holes (4).

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