Unmanned aerial vehicle flight controller

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, and discloses an unmanned aerial vehicle flight controller which comprises a flight control shell I. Two positioning holes are formed in the rear side of the flight control shell I. Two T-shaped frames are fixedly connected to the rear side of the top of the flight control shell I. Clamping blocks are slidably connected to the inner sides of the T-shaped frames. The bottom of the first flight control shell is rotatably connected with a second flight control shell, the rear side of the second flight control shell is fixedly connected with two positioning columns, the bottom of the second flight control shell is fixedly connected with two fixing columns, and the middle of each fixing column is slidably connected with a sliding rod. According to the flight control device, the clamping block is slid to cancel the clamping with the hole, and then the sliding rod is slid to cancel the clamping with the T-shaped frame, so that the flight control shell I and the flight control shell II can be unfolded, the use is convenient, the operation is simple, the storage is realized by reverse operation during storage, the space utilization rate is improved, and the carrying and the storage are convenient.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned plane technical field especially relates to a kind of unmanned plane flight control device. BACKGROUND

[0002] The origin of unmanned plane flight control device can be traced back to the early exploration of autopilot technology in aviation field, initially to meet military needs, through preset program and simple sensor to control the flight path of aircraft, this can be regarded as the prototype of unmanned plane flight control device, with the development of micro-electromechanical system technology, sensor becomes smaller and smaller, higher and higher precision and cost reduction, provides more abundant and accurate perception ability for flight control device, the appearance of gyroscope and accelerometer makes unmanned plane can perceive the attitude change of itself in real time, simultaneously the progress of computer technology, especially the continuous improvement of microprocessor performance, can process sensor data with higher speed and precision and execute complex control algorithm, provides the condition for flight control device to realize more accurate control, makes unmanned plane can steady hover, accurately controls flight trajectory, lets photographer can easily obtain the photo and video of unique perspective, promotes the development of aerial photography art.

[0003] With the rapid development of e-commerce industry, the demand of logistics distribution is increasing, flight control device makes unmanned plane can accurately deliver goods to destination according to preset route, improves distribution efficiency and reduces labor cost, in agricultural production, using flight control device to control unmanned plane to carry out pesticide spraying, farmland monitoring and other operations can improve operation efficiency and accuracy, reduce pesticide waste and pollution to environment, help to realize the modernization and intelligentization of agriculture, but in the limited storage space when using, flight control device that cannot be folded will occupy larger space, whether in the storage place of equipment box or backpack, will lead to low space utilization, cause the waste of space resources. UTILITARY MODEL CONTENT

[0004] In order to make up for the above shortcomings, the utility model provides a kind of unmanned plane flight control device, aims at improving the problem of in the limited storage space when using, flight control device that cannot be folded will occupy larger space, whether in the storage place of equipment box or backpack, will lead to low space utilization, cause the waste of space resources in prior art.

[0005] In order to achieve the above object, the utility model discloses the following technical scheme: a kind of unmanned aerial vehicle flight control device, including flight control shell one, the rear side of flight control shell one is equipped with two positioning holes, the top rear side of flight control shell one is fixedly connected with two T-shaped frames, the inner side of T-shaped frame is slidably connected with clamping block, the bottom of flight control shell one is rotatably connected with flight control shell two, the rear side of flight control shell two is fixedly connected with two positioning columns, the bottom of flight control shell two is fixedly connected with two fixed columns, the middle portion of fixed column is slidably connected with slide bar, the front side of slide bar is slidably connected with the middle portion inner wall of T-shaped frame, the top front side of slide bar is equipped with hole, the inner wall of hole is engaged with the bottom of clamping block, the front side of flight control shell one is provided with protection mechanism, and the protection mechanism is used to protect flight control device.

[0006] As further description of the above technical solution:

[0007] The protection mechanism includes two protective sleeves, the bottom of the two protective sleeves is fixedly connected at the top corner of flight control shell one, the left and right sides of flight control shell one are fixedly connected with radiating fins, the front side of flight control shell one is fixedly connected with front protection cover, the rear side of flight control shell one is fixedly connected with radiating fins, the front side of flight control shell two is fixedly connected with battery cabin protection plate, the rear side of flight control shell two is fixedly connected with waterproof and breathable membrane, and the top middle part of flight control shell two is fixedly connected with protection pad.

[0008] As further description of the above technical solution:

[0009] The top middle part of flight control shell one is fixedly connected with fixed sleeve, and the top of fixed sleeve is fixedly connected with antenna.

[0010] As further description of the above technical solution:

[0011] The top front side of flight control shell two is fixedly connected with handle, and the outer wall of handle is fixedly connected with anti-skid sleeve.

[0012] As further description of the above technical solution:

[0013] The left and right sides of flight control shell two are fixedly connected with handle, and the front side of clamping block is fixedly connected with convex sleeve.

[0014] As further description of the above technical solution:

[0015] The front side top of front protection cover is fixedly connected with nameplate, and the front middle part of front protection cover is fixedly connected with switch.

[0016] As further description of the above technical solution:

[0017] The front side left end top of the front protective cover is fixedly connected with two breathing lamps, and the front side of the front protective cover is fixedly connected with two operation buttons.

[0018] As a further description of the above technical solution:

[0019] The rear side of the flight control shell two is fixedly connected with a display screen, and the rear side middle part of the flight control shell two is fixedly connected with a transparent plate.

[0020] The utility model has the advantages of the following beneficial effects:

[0021] 1、 in the utility model, when needing to use, the clamping with the hole can be cancelled through the sliding clamp, and then the clamping with the T-shaped frame is cancelled through the sliding of the slide rod, the flight control shell one and the flight control shell two are unfolded, convenient to use, simple operation, without complicated tools and tedious steps, can quickly enter the use state, when storage, the positioning column is aligned with the positioning hole through the rotation of the flight control shell two, and then the storage is realized through the reverse operation, the space occupied during storage is effectively reduced, storage is facilitated, the space utilization is improved, and carrying and storage are facilitated.

[0022] 2、 in the utility model, the protective sleeve at the top of the flight control shell one can play a buffering role when the flight control device is accidentally collided and dropped, and the impact on the top of the flight control device is reduced, the heat sink can quickly conduct heat to the outside air, the performance of the flight control device is prevented from being reduced due to overheating, the front protective cover can protect the sensitive components and interfaces on the front side of the flight control device, and the rear side heat dissipation fin can guide the air flow and form a good air flow channel, and the heat dissipation performance is improved. BRIEF DESCRIPTION OF DRAWINGS

[0023] Figure 1 A front side perspective view of the flight control shell one of the unmanned aerial vehicle flight control device is provided for the utility model;

[0024] Figure 2 A heat dissipation fin display view of the unmanned aerial vehicle flight control device is provided for the utility model;

[0025] Figure 3 A slide rod disassembly view of the unmanned aerial vehicle flight control device is provided for the utility model;

[0026] Figure 4 A transparent plate disassembly view of the unmanned aerial vehicle flight control device is provided for the utility model;

[0027] Figure 5 A flight control shell two schematic view of the unmanned aerial vehicle flight control device is provided for the utility model;

[0028] Figure 6 A heat dissipation fin disassembly view of the unmanned aerial vehicle flight control device is provided for the utility model.

[0029] Legend:

[0030] 1, flight control shell one; 2, protection mechanism; 201, protective sleeve; 202, fin; 203, front protective cover; 204, heat dissipation fin; 205, waterproof and breathable membrane; 206, battery compartment protection plate; 207, protective pad; 3, positioning hole; 4, T-shaped frame; 5, clamping block; 6, flight control shell two; 7, positioning column; 8, fixed column; 9, sliding rod; 10, hole; 11, fixed sleeve; 12, antenna; 13, handle; 14, anti-skid sleeve; 15, handle; 16, convex sleeve; 17, nameplate; 18, switch; 19, breathing lamp; 20, operation button; 21, display screen; 22, transparent plate. DETAILED DESCRIPTION

[0031] The technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the drawings in the embodiments of the present application. Obviously, the described embodiments are only part of the embodiments of the present application, rather than all the embodiments. Based on the embodiments in the present application, all other embodiments obtained by those skilled in the art without creative labor fall within the scope of protection of the present application.

[0032] Please refer to the drawings Figure 1 , the drawings Figure 2 and the drawings Figure 3 , an embodiment provided by the present application: a kind of unmanned aerial vehicle flight control device, including flight control shell one 1, the rear side of flight control shell one 1 is equipped with two positioning holes 3, the top rear side of flight control shell one 1 is fixedly connected with two T-shaped frames 4, the inner side of T-shaped frame 4 is slidably connected with clamping block 5, the bottom of flight control shell one 1 is rotatably connected with flight control shell two 6, the rear side of flight control shell two 6 is fixedly connected with two positioning columns 7, the bottom of flight control shell two 6 is fixedly connected with two fixed columns 8, the middle part of fixed column 8 is slidably connected with sliding rod 9, the front side of sliding rod 9 is slidably connected with the middle part inner wall of T-shaped frame 4, the top front side of sliding rod 9 is equipped with hole 10, the inner wall of hole 10 is clamped with the bottom of clamping block 5, the front side of flight control shell one 1 is provided with protection mechanism 2, protection mechanism 2 is used for the protection of flight control device;

[0033] Specifically, the flight control shell 1 is the core component of the entire flight control system, two positioning holes 3 are arranged on the back side of the flight control shell 1, which ensures that the flight control device can be connected with other components, the T-shaped frame 4 is slidably connected with the clamping block 5 on the inner side, which provides additional stability and flexibility for the flight control device, the flight control shell 2 6 is used to adapt to different flight conditions, and the positioning column 7 ensures the correct position of the flight control shell during storage, the middle part of the fixing column 8 is slidably connected with the slide rod 9, which allows the position to be adjusted within a certain range to adapt to different installation requirements, the front side of the slide rod 9 is slidably connected with the middle inner wall of the T-shaped frame 4, and the inner wall of the hole 10 is clamped with the bottom of the clamping block 5, which ensures the stability of the flight control device during storage.

[0034] Please refer to the attached Figure 2 , attached Figure 5 and attached Figure 6 , the protection mechanism 2 includes two protective sleeves 201, the bottom of the two protective sleeves 201 is fixedly connected to the top corner of the flight control shell 1, the left and right sides of the flight control shell 1 are fixedly connected with the heat dissipation fins 202, the front side of the flight control shell 1 is fixedly connected with the front protective cover 203, the rear side of the flight control shell 1 is fixedly connected with the heat dissipation fins 204, the front side of the flight control shell 2 6 is fixedly connected with the battery compartment protection plate 206, the rear side of the flight control shell 2 6 is fixedly connected with the waterproof and breathable membrane 205, and the top middle part of the flight control shell 2 6 is fixedly connected with the protection pad 207.

[0035] Specifically, the protective sleeve 201 is connected to the top corner of the flight control shell 1 to achieve the protection effect, the heat dissipation fins 202 ensure that the equipment can effectively dissipate heat during operation, the front protective cover 203 provides additional protection in front of the equipment, the heat dissipation fins 204 help to improve the heat dissipation efficiency, the battery compartment protection plate 206 can protect the battery compartment from external impact and environmental factors, the waterproof and breathable membrane 205 ensures the waterproof performance of the equipment and allows air circulation, thereby avoiding the generation of internal condensed water, and the protection pad 207 can reduce friction and impact when the equipment is placed and moved.

[0036] Please refer to the attached Figure 1 , attached Figure 3 and attached Figure 4 , the top front side of the flight control shell 2 6 is fixedly connected with the handle 13, the outer wall of the handle 13 is fixedly connected with the anti-skid sleeve 14, the rear side of the flight control shell 2 6 is fixedly connected with the display screen 21, the rear middle part of the flight control shell 2 6 is fixedly connected with the transparent plate 22, the top of the left and right sides of the flight control shell 2 6 is fixedly connected with the handle 15, and the front side of the clamping block 5 is fixedly connected with the convex sleeve 16.

[0037] Specifically, the handle 13 facilitates the taking and placing of the flight controller, the outer wall of the handle 13 is fixedly connected with the anti-skid sleeve 14 to ensure better grip and stability during operation, the display screen 21 provides intuitive flight information and control interface for the operator, in the middle of the rear side of the flight control shell two 6, a transparent plate 22 is fixedly connected, which can be used to protect the display screen 21 while providing visual information, the handle 15 enables comfortable holding of the device from different angles, and the convex sleeve 16 facilitates the adjustment of the position of the clamping block 5 to ensure the convenience of adjustment.

[0038] Please refer to the attached Figure 1 , attached Figure 3 and attached Figure 4 , the front side of the front protective cover 203 is fixedly connected with the nameplate 17, the front side of the front protective cover 203 is fixedly connected with the switch 18, the top end of the flight control shell one 1 is fixedly connected with the fixed sleeve 11, the top of the fixed sleeve 11 is fixedly connected with the antenna 12, the front side of the front protective cover 203 is fixedly connected with two breathing lights 19, and the front side of the front protective cover 203 is fixedly connected with two operation buttons 20.

[0039] Specifically, the nameplate 17 is used to identify the relevant information of the device, the switch 18 is a key component for controlling the power on and off of the flight control device, the fixed sleeve 11 provides a stable mounting position for the antenna 12, ensuring that the antenna 12 can be stably erected at the top end of the device, the breathing light 19 emits soft light when the device is working, indicating the state of the device, and the operation button 20 is an important interface for interacting with the flight control device, which can facilitate various operations.

[0040] Working principle: when needed, the clamping between the clamping block 5 and the hole 10 can be cancelled by sliding, and the clamping between the slide rod 9 and the T-shaped frame 4 can be cancelled by sliding, the flight control shell one 1 and the flight control shell two 6 are unfolded, the bottom of the flight control shell one 1 is clamped and fixed with the top of the flight control shell two 6 after unfolding, which is convenient to use and simple to operate, without the need for complex tools and cumbersome steps, and can quickly enter the use state, facilitating various operations on the flight controller, when storing, rotate the flight control shell two 6 to make the positioning column 7 align with the positioning hole 3, and then reverse the operation to realize storage, effectively reducing the space occupied during storage, facilitating the storage of the flight controller in a smaller space, improving the space utilization, and facilitating carrying and storage;

[0041] The protective sleeve 201 on the top of the flight control shell 1 can play a buffering role when the flight controller is accidentally collided and dropped, reducing the impact on the top of the flight controller and protecting the internal electronic components from damage. The heat dissipation fins 202 on the left and right sides of the flight control shell 1 can quickly conduct heat to the outside air, preventing the flight controller from overheating, performance degradation, shortened life, or even failure. The front protective cover 203 on the front side of the flight control shell 1 can protect the sensitive components and interfaces on the front side of the flight controller. The rear heat dissipation fins 204 can guide air flow and form a good air flow channel, allowing air to flow more smoothly over the surface of the flight controller and carry away more heat, improving heat dissipation performance. The waterproof and breathable membrane 205 on the rear side of the flight control shell 2 6 allows the internal environment of the flight controller to exchange gas with the external environment, balancing the internal and external air pressure. The battery compartment protection plate 206 on the front side of the flight control shell 2 6 can protect the battery from external collisions and extrusion damage, preventing the battery case from being damaged or deformed and ensuring the safety performance and normal operation of the battery. The protective pad 207 on the top of the flight control shell 2 6 can act as a shock absorber, reducing the impact force on the top of the flight controller and ensuring the normal operation and installation precision of the flight controller.

[0042] Finally, it should be noted that the above-described preferred embodiments of the present application are not intended to limit the present application, and although the present application has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent replacements to some technical features, and any modifications, equivalent replacements, improvements, etc. made within the spirit and principles of the present application shall be included within the scope of protection of the present application.

Claims

1. A drone flight controller comprising a flight controller housing one (1), characterized by: The rear side of the flight control shell one (1) is provided with two positioning holes (3), the top rear side of the flight control shell one (1) is fixedly connected with two T-shaped frames (4), the inner sides of the T-shaped frames (4) are slidably connected with clamping blocks (5), the bottom of the flight control shell one (1) is rotatably connected with a flight control shell two (6), the rear side of the flight control shell two (6) is fixedly connected with two positioning columns (7), the bottom of the flight control shell two (6) is fixedly connected with two fixed columns (8), the middle parts of the fixed columns (8) are slidably connected with slide rods (9), the front sides of the slide rods (9) are slidably connected with the middle inner walls of the T-shaped frames (4), the top front sides of the slide rods (9) are provided with holes (10), the inner walls of the holes (10) are clamped with the bottoms of the clamping blocks (5), and the front side of the flight control shell one (1) is provided with a protection mechanism (2) for protecting the flight control device.

2. The unmanned aerial vehicle flight controller of claim 1, wherein: The protection mechanism (2) comprises two protective sleeves (201), the bottoms of the two protective sleeves (201) are fixedly connected at the top corners of the flight control shell one (1), the left and right sides of the flight control shell one (1) are fixedly connected with heat dissipation fins (202), the front side of the flight control shell one (1) is fixedly connected with a front protective cover (203), the rear side of the flight control shell one (1) is fixedly connected with heat dissipation fins (204), the front side of the flight control shell two (6) is fixedly connected with a battery compartment protection plate (206), the rear side of the flight control shell two (6) is fixedly connected with a waterproof and breathable film (205), and the top middle part of the flight control shell two (6) is fixedly connected with a protection pad (207).

3. The unmanned aerial vehicle flight controller of claim 1, wherein: The top middle part of the flight control shell one (1) is fixedly connected with a fixed sleeve (11), and the top of the fixed sleeve (11) is fixedly connected with an antenna (12).

4. The unmanned aerial vehicle flight controller of claim 1, wherein: The top front side of the flight control shell two (6) is fixedly connected with a handle (13), and the outer wall of the handle (13) is fixedly connected with an anti-skid sleeve (14).

5. The unmanned aerial vehicle flight controller of claim 1, wherein: The left and right sides of the flight control shell two (6) are fixedly connected with handles (15), and the front sides of the clamping blocks (5) are fixedly connected with convex sleeves (16).

6. The unmanned aerial vehicle flight controller of claim 2, wherein: The front side of the front protective cover (203) is fixedly connected with a nameplate (17), and the front middle part of the front protective cover (203) is fixedly connected with a switch (18).

7. The unmanned aerial vehicle flight controller of claim 2, wherein: The front side of the front protective cover (203) is fixedly connected with two breathing lights (19), and the front side of the front protective cover (203) is fixedly connected with two operation buttons (20).

8. The unmanned aerial vehicle flight controller of claim 2, wherein: The rear side of the flight control shell two (6) is fixedly connected with a display screen (21), and the rear middle part of the flight control shell two (6) is fixedly connected with a transparent plate (22).

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