Unmanned aerial vehicle with detachable load radar device

Abstract

The utility model relates to an unmanned aerial vehicle with a detachable load radar device. The unmanned aerial vehicle mainly solves the technical problems that a traditional radar installation mode is low in disassembly and assembly efficiency, poor in equipment adaptability and lack of buffer protection. Four mounting blocks are arranged at the top of a rack of the unmanned aerial vehicle, rapid clamping connection with the load radar device is achieved through limiting holes in mounting battens, and bare-handed disassembly and assembly operation is supported. The load radar device is of a hollow frame structure, additional holes are formed in the upper portion to expand auxiliary equipment, a mounting plate with multiple distributed holes is arranged on the lower portion, and the load radar device is compatible with various radar models by selecting different mounting holes. And a buffer spring mechanism is arranged in the mounting block, when the unmanned aerial vehicle abnormally lands, a spring absorbs impact energy through the lifting plate, and the radar equipment is prevented from being damaged. According to the structure, the disassembly and assembly efficiency is remarkably improved, the equipment universality is enhanced, and the damage risk caused by landing impact is effectively reduced.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) technology, specifically a UAV with a detachable radar device. Background Technology

[0002] The application of drone technology in surveying, disaster monitoring, and other fields is becoming increasingly widespread, and radar, as a critical payload device, often needs to be mounted on drone platforms. Currently, the industry generally uses bolts or straps to secure radar devices to the drone body, forming a rigid connection structure. This traditional method has revealed a series of technical defects in practical applications: First, the disassembly and assembly process relies on specialized tools and requires the removal of a large number of fasteners, resulting in excessively long maintenance or replacement times for the radar; second, the mounting holes of the mounting brackets are only compatible with specific radar models, requiring custom-made brackets when switching to different sized devices, lacking flexibility; more importantly, the rigid connection cannot buffer the impact force during abnormal drone landings, and the impact energy is directly transmitted to the delicate radar equipment, significantly increasing the risk of damage.

[0003] To address the aforementioned issues, there is an urgent need to develop a new type of load-bearing structure. Its core objectives are to enable rapid assembly and disassembly of radar devices to improve maintenance efficiency, provide multi-size compatible mounting interfaces to accommodate different equipment models, and integrate a buffer protection mechanism to reduce the risk of damage from landing impacts. Summary of the Invention

[0004] The purpose of this invention is to provide a modular load-bearing UAV structure that enables manual assembly and disassembly of the radar device through a quick-connect mechanism between the mounting block and the limiting hole. It utilizes a multi-hole mounting plate to be compatible with different radar models and uses a buffer spring to absorb landing impact, thereby comprehensively solving the three major technical defects of traditional UAV radar installation: cumbersome assembly and disassembly, poor compatibility, and lack of protective buffer.

[0005] To solve the above-mentioned technical problems, the technical solution proposed in this application is as follows:

[0006] A drone with a detachable radar payload includes:

[0007] The frame has a flight controller fixedly installed inside, a propeller on the side, a camera at the front, and landing gear at the bottom.

[0008] Four fixed mounting blocks are installed on the top of the frame;

[0009] The detachable load radar device includes a hollow frame, additional holes in the upper part of the frame, a mounting plate in the lower part of the frame, multiple mounting holes on the mounting plate, and mounting strips.

[0010] The load radar device is fixedly connected to the mounting block through the first limiting hole on the mounting plate.

[0011] Furthermore, it also includes:

[0012] A detachable protective frame is provided on the upper part of the load radar device;

[0013] Connecting rods;

[0014] The detachable protective frame is connected by connecting rods passing through the second limiting hole of the mounting strip.

[0015] Furthermore, the mounting block includes:

[0016] Two mounting rods are provided on the mounting block;

[0017] The lifting platform is located above the mounting rod.

[0018] The connecting rod extends through the upper part of the mounting block;

[0019] A buffer spring is located below the lifting plate;

[0020] The mounting rod passes through the third limiting hole;

[0021] The connecting rod is fixedly connected to the lifting plate;

[0022] The buffer spring connects the lifting plate and the mounting block.

[0023] Furthermore:

[0024] The mounting holes are arranged in multiple rows and columns on the mounting plate.

[0025] Compared with the prior art, the present invention achieves the following beneficial technical effects:

[0026] This application achieves rapid manual assembly and disassembly of the radar device through a limiting hole snap-fit ​​mechanism, significantly improving maintenance efficiency; the multi-hole distributed mounting plate flexibly adapts to different specifications of radar equipment, enhancing system compatibility; and the buffer spring mechanism effectively absorbs landing impact energy, preventing damage to the precision radar due to abnormal landing. The overall structure represents a substantial advancement in simplifying operating procedures, expanding the applicability of the equipment, and improving safety protection. Attached Figure Description

[0027] To more clearly illustrate the technical solutions in the embodiments of the present invention or the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are some embodiments of the present invention. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0028] Figure 1 This application presents an overall structural schematic diagram of a UAV with a detachable load radar device.

[0029] Figure 2 This application provides a schematic diagram of the structure of a load radar device for a UAV with a detachable load radar device.

[0030] Figure 3 This application presents a schematic diagram of the mounting block for a UAV with a detachable load radar device.

[0031] The components include: frame 1, propeller 2, camera 3, landing gear 4, mounting block 5, load radar device 6, additional hole 7, mounting plate 8, first limiting hole 9, mounting hole 10, connecting rod 11, second limiting hole 12, protective frame 13, mounting strip 14, connecting rod 15, lifting plate 16, mounting rod 17, buffer spring 18, and third limiting hole 19. Detailed Implementation

[0032] To make the objectives, technical solutions, and advantages of the embodiments of the present invention clearer, the technical solutions of the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of the present invention.

[0033] like Figure 1-3 As shown in this application, a drone with a detachable radar payload is provided, comprising:

[0034] The frame 1 has a flight controller fixedly installed inside, a propeller 2 on the side, a camera 3 at the front, and landing gear 4 connected to the bottom.

[0035] Four fixed mounting blocks 5 are installed on the top of the frame 1;

[0036] The detachable load radar device 6 includes a hollow frame, an additional hole 7 opened in the upper part of the frame, a mounting plate 8 located in the lower part of the frame, a plurality of mounting holes 10 provided on the mounting plate 8, and a mounting strip 14.

[0037] The load radar device 6 is fixedly connected to the mounting block 5 through the first limiting hole 9 on the mounting strip 14.

[0038] Furthermore, it also includes:

[0039] A detachable protective frame 13 is provided on the upper part of the load radar device 6;

[0040] Connecting rod 11;

[0041] The detachable protective frame 13 is connected by a connecting rod 11 passing through the second limiting hole 12 of the mounting plate 14.

[0042] Furthermore, mounting block 5 includes:

[0043] Two vertical mounting rods 17 are provided on the body of the mounting block 5;

[0044] The lifting plate 16 is located above the mounting rod 17;

[0045] Connecting rod 15 passes through the upper part of mounting block 5;

[0046] A buffer spring 18 is located below the lifting plate 16;

[0047] The mounting rod 17 passes through the third limiting hole 19;

[0048] The connecting rod 15 is fixedly connected to the lifting plate 16;

[0049] The buffer spring 18 connects the lifting plate 16 and the mounting block 5.

[0050] Furthermore, the mounting holes 10 are distributed in multiple rows and columns on the mounting plate 8.

[0051] As described above, the top of the UAV frame 1 of this utility model is fixedly equipped with four mounting blocks 5, and the load radar device 6 is detachably connected to the mounting blocks 5 through the first limiting hole 9 on its mounting plate 14. The load radar device 6 adopts a hollow frame structure, with additional holes 7 opened on the upper connecting rod of the frame for expanding auxiliary equipment, and a mounting plate 8 provided at the lower part of the frame. The mounting plate 8 has multiple rows and columns of mounting holes 10, which can be adapted to various radar devices by selecting different positions of the mounting holes 10. A detachable protective frame 13 is configured on the upper part of the load device. The protective frame 13 is fixed by connecting rods 11 passing through the second limiting hole 12 of the mounting plate 14, forming a protective structure that wraps around the radar body.

[0052] Two mounting rods 17 are installed inside the mounting block 5. The mounting rods 17 pass through the third limiting hole 19 and are connected to the lifting plate 16 above. The lifting plate 16 is linked by a connecting rod 15 passing through the upper part of the mounting block 5. A buffer spring 18 is provided below the lifting plate 16, and the two ends of the buffer spring 18 are connected to the lifting plate 16 and the main body of the mounting block 5, respectively. When the UAV lands, the impact force drives the lifting plate 16 to press down, pushing the connecting rod 15 to compress the buffer spring 18 to absorb energy. After the impact, the buffer spring 18 returns to its original position to prevent structural deformation.

[0053] The above description is merely a specific embodiment of this utility model, but the protection scope of this utility model is not limited thereto. Any variations or substitutions that can be easily conceived by those skilled in the art within the technical scope disclosed in this utility model should be included within the protection scope of this utility model. Therefore, the protection scope of this utility model should be determined by the scope of the claims.

Claims

1. A drone having a detachable payload radar device, characterized in that, include: The frame (1) has a flight controller fixedly installed inside, a propeller (2) on the side, a camera (3) at the front, and landing gear (4) connected to the bottom. Four fixed mounting blocks (5) are set on the top of the frame (1); The detachable load radar device (6) includes a hollow frame, an additional hole (7) opened on the upper part of the frame, a mounting plate (8) located on the lower part of the frame, a plurality of mounting holes (10) provided on the mounting plate (8), and a mounting strip (14). The load radar device (6) is fixedly connected to the mounting block (5) through the first limiting hole (9) on the mounting strip (14).

2. The drone of claim 1, wherein, Also includes: A detachable protective frame (13) is provided on the upper part of the load radar device (6); Connecting rod (11); The detachable protective frame (13) is connected by a connecting rod (11) passing through the second limiting hole (12) of the mounting plate (14).

3. The drone of claim 1, wherein, Mounting block (5) includes: Two mounting rods (17) are provided on the mounting block (5); The lifting plate (16) is located above the mounting rod (17); The connecting rod (15) passes through the upper part of the mounting block (5); A buffer spring (18) is located below the lifting plate (16); The mounting rod (17) passes through the third limiting hole (19); The connecting rod (15) is fixedly connected to the lifting plate (16); The buffer spring (18) connects the lifting plate (16) and the mounting block (5).

4. The UAV according to claim 1, characterized in that: The mounting holes (10) are distributed in multiple rows and columns on the mounting plate (8).

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