Unmanned aerial vehicle frame with reinforcing side plates

Abstract

The utility model relates to an unmanned aerial vehicle frame with reinforced side plates, which comprises a vehicle body, a first vehicle arm, a second vehicle arm, a third vehicle arm and a fourth vehicle arm, and the vehicle body comprises a vehicle body top plate, a vehicle body middle plate and a vehicle body bottom plate. The unmanned aerial vehicle further comprises a first reinforcing side plate, a second reinforcing side plate, a first fixed type XT90 power interface, a second fixed type XT90 power interface and a two-in-one antenna pedestal, one end of the first reinforcing side plate is fixedly connected with the first vehicle arm, the other end of the first reinforcing side plate is fixedly connected with the second vehicle arm, the first fixed type XT90 power interface is installed at one end of the vehicle body top plate, and the second fixed type XT90 power interface is installed at the other end of the vehicle body top plate. The second fixed type XT90 power interface is installed at the other end of the top plate of the machine body. The two-in-one antenna pedestal is installed on the side, close to the second fixed type XT90 power interface, of the machine body. Through reasonable arrangement, the rigidity and performance of the unmanned aerial vehicle frame are greatly improved, and the unmanned aerial vehicle frame is simple in structure, convenient to operate and capable of meeting use requirements.

Description

Technical Field

[0001] This utility model relates to the field of drone frames, and in particular to a drone frame with reinforced side plates. Background Technology

[0002] Unmanned aerial vehicles, or "drones" for short, are unmanned aircraft controlled by radio remote control equipment and their own program control devices, or operated autonomously by an onboard computer, either completely or intermittently. With the development of technology, drones are being used more and more widely. For drones, the drone frame is one of the most important components.

[0003] Currently, most drones suffer severe damage after a collision. The main problem is that the drone frame is not sturdy and the materials are poor. There is an urgent need to invent a drone frame with high rigidity and structural stability. Utility Model Content

[0004] Therefore, it is necessary to provide a drone frame with reinforced side plates to address the above problems.

[0005] A drone frame with reinforced side plates includes a fuselage, a first arm, a second arm, a third arm, and a fourth arm. The fuselage includes a top plate, a middle plate, and a bottom plate. The first, second, third, and fourth arms are all mounted between the middle plate and the bottom plate using press-fit nuts and are located at the four corners of the fuselage. The frame also includes a first reinforced side plate, a second reinforced side plate, a first fixed XT90 power interface, a second fixed XT90 power interface, and a 2-in-1 antenna mount. One end of the first reinforced side plate is fixedly connected to the first arm, and the other end is fixedly connected to the second arm. One end of the second reinforced side plate is fixedly connected to the third arm, and the other end is fixedly connected to the fourth arm. The first fixed XT90 power interface is installed at one end of the top plate, and the second fixed XT90 power interface is installed at the other end of the top plate.

[0006] The two-in-one antenna mount is installed on the side of the chassis near the second fixed XT90 power interface.

[0007] In one embodiment, the middle plate of the fuselage is provided with a plurality of aluminum pillars, and the top plate of the fuselage is connected and fixed to the middle plate of the fuselage through the plurality of aluminum pillars, and an equipment installation area is formed between the top plate of the fuselage and the middle plate of the fuselage.

[0008] In one embodiment, the fuselage plate is provided with multiple device mounting slots.

[0009] In one embodiment, the device mounting area is provided with a lens mounting base near the first fixed XT90 power interface, and the lens mounting base further includes a first lens side plate and a second lens side plate.

[0010] In one embodiment, both the first lens side plate and the second lens side plate are provided with camera fixing blocks.

[0011] In one embodiment, the first arm, the second arm, the third arm and the fourth arm are each provided with a motor mounting slot.

[0012] In one embodiment, the middle plate of the fuselage and the bottom plate of the fuselage are fixed together by a plurality of screws, and a clamping plate is provided between the middle plate of the fuselage and the bottom plate of the fuselage.

[0013] In one embodiment, the drone frame is made of carbon fiber.

[0014] The aforementioned drone frame with reinforced side plates, by setting a first reinforced side plate and a second reinforced side plate, makes the overall structural deformation control of the drone smaller during flight and improves the overall rigidity. The setting of the two-in-one antenna mount ensures the communication quality of electronic devices structurally, and the setting of the first fixed XT90 power interface and the second fixed XT90 power interface can better fix the power cord; thus meeting production needs. Attached Figure Description

[0015] Figure 1 This is a schematic diagram of the overall structure of this utility model;

[0016] Figure 2 This is a schematic diagram of the fuselage structure of this utility model;

[0017] Figure 3 This is a schematic diagram of the lens mounting bracket structure of this utility model.

[0018] 1. Body, 11. Top plate of body, 111. First fixed XT90 power interface, 112. Second fixed XT90 power interface, 113. Two-in-one antenna mount, 114. Aluminum column, 115. Equipment installation area, 1151. Equipment installation slot, 12. Middle plate of body, 13. Bottom plate of body, 2. First arm, 3. Second arm, 4. Third arm, 5. Fourth arm, 6. First reinforcing side plate, 7. Second reinforcing side plate, 8. Lens mount, 81. First side plate, 82. Second side plate, 83. Camera mounting block, 9. Motor mounting slot, 10. Clamping plate. Detailed Implementation

[0019] To make the above-mentioned objects, features, and advantages of this utility model more apparent and understandable, the specific embodiments of this utility model will be described in detail below with reference to the accompanying drawings. Many specific details are set forth in the following description to provide a full understanding of this utility model. However, this utility model can be implemented in many other ways different from those described herein, and those skilled in the art can make similar modifications without departing from the spirit of this utility model. Therefore, this utility model is not limited to the specific embodiments disclosed below.

[0020] It should be noted that when an element is said to be "fixed to" another element, it can be directly on the other element or there may be an intervening element. When an element is said to be "connected to" another element, it can be directly connected to the other element or there may be an intervening element. Conversely, when an element is said to be "directly on" another element, there is no intervening element. The terms "vertical," "horizontal," "left," "right," and similar expressions used in this document are for illustrative purposes only.

[0021] Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention pertains. The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. The term "and / or" as used herein includes any and all combinations of one or more of the associated listed items.

[0022] A drone frame with reinforced side plates includes a fuselage 1, a first arm 2, a second arm 3, a third arm 4, and a fourth arm 5. The fuselage 1 includes a top fuselage plate 11, a middle fuselage plate 12, and a middle fuselage plate 13. The first arm 2, the second arm 3, the third arm 4, and the fourth arm 5 are all installed between the middle fuselage plate 12 and the middle fuselage plate 13 by press-fit nuts and are respectively located at the four corners of the fuselage 1. The frame also includes a first reinforced side plate 6, a second reinforced side plate 7, and a first fixed XT90 power interface 111. The system includes a second fixed XT90 power interface 112 and a two-in-one antenna mount 113. One end of the first reinforcing side plate 6 is fixedly connected to the first arm 2, and the other end is fixedly connected to the second arm 3. One end of the second reinforcing side plate 7 is fixedly connected to the third arm 4, and the other end is fixedly connected to the fourth arm 5. The first fixed XT90 power interface 111 is installed at one end of the top plate 11 of the fuselage, and the second fixed XT90 power interface 112 is installed at the other end of the top plate 11 of the fuselage.

[0023] The dual-mode antenna mount 113 is installed on the side of the fuselage 1 near the second fixed XT90 power interface 112; by setting the first reinforcing side plate 6 and the second reinforcing side plate 7, the drone frame is made more robust and more stable; by setting the dual-mode antenna mount 113, the problem of drone signal interference is solved; and the setting of the first fixed XT90 power interface 111 and the second fixed XT90 power interface 112 avoids the problem of the drone cutting or damaging the power cable during flight.

[0024] Furthermore, the middle plate 12 of the fuselage is provided with a plurality of aluminum pillars 114, and the top plate 11 of the fuselage is connected and fixed to the middle plate 12 of the fuselage through the plurality of aluminum pillars 114, and an equipment installation area 115 is formed between the top plate 11 of the fuselage and the middle plate 12 of the fuselage; the aluminum pillars 114 can be used to connect the top plate 11 of the fuselage and the middle plate 12 of the fuselage, reserving space for internal equipment installation.

[0025] Furthermore, the fuselage plate 12 is provided with a plurality of device mounting slots 1151; by providing a plurality of device mounting slots 1151, electronic equipment required for the drone can be installed on the device mounting slots 1151.

[0026] Furthermore, the device mounting area 115 is provided with a lens mounting base 8 near the first fixed XT90 power interface 111, and the lens mounting base 8 also includes a first lens side plate 81 and a second lens side plate 82.

[0027] Furthermore, both the first lens side plate 81 and the second lens side plate 82 are provided with camera fixing blocks 83; by setting the first lens side plate 81, the second lens side plate 82 and the camera mounting slot, a first-person drone camera is installed.

[0028] Furthermore, motor mounting slots 9 are provided on the first arm 2, the second arm 3, the third arm 4, and the fourth arm 5; by providing motor mounting slots 9 on the first arm 2, the second arm 3, the third arm 4, and the fourth arm 5, it is beneficial to install the motor of the UAV.

[0029] Furthermore, the fuselage middle plate 12 and the fuselage middle plate 13 are fixed by multiple screw threads, and a clamping plate 10 is provided between the fuselage middle plate 12 and the fuselage middle plate 13.

[0030] Furthermore, the drone frame is made of carbon fiber; the lightweight properties of carbon fiber improve the drone's flight efficiency, its high strength and rigidity ensure structural stability, and its corrosion resistance and heat resistance enable it to operate stably in harsh environments.

[0031] It should be noted that the first arm 2, the second arm 3, the third arm 4, and the fourth arm 5 are used to install motors, connect to the fuselage 1, and apply lift to the overall structure; the fuselage top plate 11 is used as a battery mounting platform or to fix other equipment; the fuselage middle plate 13 is used to strengthen the overall structure of the fuselage 1 and fix the arms; the fuselage middle plate 12 is used to strengthen the overall structure of the fuselage 1 and to install equipment; due to the setting of the aluminum column 114, an equipment installation area 115 is formed between the fuselage top plate 11 and the fuselage middle plate 12. During the installation process, the electronic equipment required for assembling the drone is installed in the equipment installation area 115; by setting the first reinforcing side plate 6 and the second reinforcing side plate 7, the overall structural deformation of the drone can be controlled to be smaller during flight, greatly improving the overall rigidity of the drone frame, while also suppressing resonance generated during high-speed flight, making the power system more efficient. The drone can perform large maneuvers with ease during flight; the design of the two-in-one antenna mount 113 efficiently utilizes the plastic structure, integrating two different frequencies without sacrificing overall strength and usability. It also avoids signal interference caused by cluttered antenna placement during flight, structurally ensuring the communication quality of electronic devices. Regarding antenna installation, since the drone's main power cable extends outside the fuselage 1 and is exposed, it is difficult to secure. This not only poses a risk of the power cable being cut off during high-speed rotation of the motor-driven propellers but also complicates battery installation during flight preparation. The first fixed XT90 power interface 111 and the second fixed XT90 power interface 112 provide a clean and tidy main power connection method, solving the problem of the difficulty in securing the conventional main power cable extending outside the fuselage 1. This fixed power interface provides a convenient way to install and connect batteries, avoids the risk of cutting the power cable, and makes drone flight safer.

[0032] The aforementioned drone frame with reinforced side plates, by setting the first reinforced side plate 6 and the second reinforced side plate 7, makes the overall structural deformation control of the drone smaller during flight and improves the overall rigidity. The setting of the two-in-one antenna mount 113 ensures the structural quality of electronic device communication, and the setting of the first fixed XT90 power interface 111 and the second fixed XT90 power interface 112 can better fix the power cord; thus meeting production needs.

[0033] The technical features of the above embodiments can be combined in any way. For the sake of brevity, not all possible combinations of the technical features in the above embodiments are described. However, as long as there is no contradiction in the combination of these technical features, they should be considered to be within the scope of this specification.

[0034] The embodiments described above are merely illustrative of several implementations of this utility model, and while the descriptions are relatively specific and detailed, they should not be construed as limiting the scope of the utility model patent. It should be noted that those skilled in the art can make various modifications and improvements without departing from the concept of this utility model, and these all fall within the protection scope of this utility model. Therefore, the protection scope of this utility model patent should be determined by the appended claims.

Claims

1. A drone frame with reinforced side panels, comprising a fuselage, a first arm, a second arm, a third arm, and a fourth arm, wherein the fuselage includes a top fuselage plate, a middle fuselage plate, and a bottom fuselage plate, and the first, second, third, and fourth arms are all mounted between the middle fuselage plate and the bottom fuselage plate by press-fit nuts, and are respectively located at the four corners of the fuselage, characterized in that, It also includes a first reinforcing side plate, a second reinforcing side plate, a first fixed XT90 power interface, a second fixed XT90 power interface, and a two-in-one antenna mount. One end of the first reinforcing side plate is fixedly connected to the first arm, and the other end is fixedly connected to the second arm. One end of the second reinforcing side plate is fixedly connected to the third arm, and the other end is fixedly connected to the fourth arm. The first fixed XT90 power interface is installed at one end of the top panel of the fuselage, and the second fixed XT90 power interface is installed at the other end of the top panel of the fuselage. The two-in-one antenna mount is installed on the side of the chassis near the second fixed XT90 power interface.

2. The UAV frame with reinforced side plates according to claim 1, characterized in that, The middle plate of the fuselage is provided with multiple aluminum pillars, and the top plate of the fuselage is connected and fixed to the middle plate of the fuselage through multiple aluminum pillars, and the equipment installation area is formed between the top plate of the fuselage and the middle plate of the fuselage.

3. A UAV frame with reinforced side plates according to claim 2, characterized in that, The fuselage plate has multiple equipment mounting slots.

4. A UAV frame with reinforced side plates according to claim 3, characterized in that, The device mounting area is provided with a lens mounting base near the first fixed XT90 power interface, and the lens mounting base also includes a first lens side plate and a second lens side plate.

5. A UAV frame with reinforced side plates according to claim 4, characterized in that, Both the first lens side plate and the second lens side plate are equipped with camera fixing blocks.

6. A UAV frame with reinforced side plates according to claim 1, characterized in that, The first, second, third, and fourth arms are all equipped with motor mounting slots.

7. A UAV frame with reinforced side plates according to claim 1, characterized in that, The middle plate of the fuselage and the bottom plate of the fuselage are fixed together by multiple screws, and a clamping plate is provided between the middle plate of the fuselage and the bottom plate of the fuselage.

8. A UAV frame with reinforced side plates according to any one of claims 1-7, characterized in that, The drone's frame is made of carbon fiber.

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