Portable unmanned aerial vehicle circuit demonstration box

Abstract

The utility model relates to unmanned plane teaching equipment technical field especially, more particularly to a portable unmanned plane circuit demonstration box, including transparent acrylic plate assembly box body, aluminium alloy outer frame, mounting panel, rotating rod, handle, demonstration part and auxiliary part, mounting panel and transparent acrylic plate assembly box body fixed connection lie in the surface of transparent acrylic plate assembly box body, rotating rod and mounting panel dismounting connection lie in the inboard of mounting panel, handle and rotating rod rotation connection lie in one end of rotating rod, demonstration part sets up in the inside of transparent acrylic plate assembly box body, auxiliary part sets up in the outside of transparent acrylic plate assembly box body, fixed demonstration part in transparent acrylic plate assembly box body inside can directly observe its internal structure and circuit connection, through the overall setting of auxiliary part, reduce the volume and weight, carry more conveniently.

Description

Technical Field

[0001] This utility model relates to the field of drone teaching equipment technology, and in particular to a portable drone circuit demonstration box. Background Technology

[0002] With the rapid development of drone technology, drones are increasingly being used in various fields such as agricultural inspection, environmental monitoring, logistics transportation, and fire rescue. As a key component for achieving precise flight and intelligent operation, the core control circuit of drones has important research value for R&D personnel and technology learners regarding its working principle and operating status. Currently, drone-related teaching is becoming increasingly important.

[0003] The drone circuit demonstration box not only visually demonstrates the structure and workflow of drone circuits, but also provides a convenient experimental platform for teaching and research, improving the learning efficiency and promotion effect of drone-related technologies.

[0004] However, in the current technology, most mainstream teaching aids on the market are completely encapsulated with metal shells, which makes it impossible for students to directly observe the internal structure and circuit connections, thus restricting the learning effect. Moreover, most existing teaching aids are fixed structures, which are large in size and heavy in weight, making it difficult to move them between different classrooms or to conduct outdoor teaching. Utility Model Content

[0005] The purpose of this utility model is to provide a portable drone circuit demonstration box, which aims to solve the technical problems of existing mainstream teaching aids on the market, which are generally completely encapsulated with metal shells, making it impossible for students to intuitively observe the internal structure and circuit connections, thus restricting the learning effect. In addition, existing teaching aids are mostly fixed structures, which are large in size and heavy in weight, making it difficult to move between different classrooms or conduct outdoor teaching.

[0006] To achieve the above objectives, this utility model employs a portable drone circuit demonstration box, comprising a transparent acrylic panel assembly box, an aluminum alloy outer frame, and demonstration components. The aluminum alloy outer frame is detachably connected to the transparent acrylic panel assembly box and is located on the outside of the transparent acrylic panel assembly box. The demonstration assembly includes a mounting plate, a rotating rod, a handle, a demonstration component, and auxiliary components. The mounting plate is fixedly connected to the transparent acrylic panel assembly box and is located on the surface of the transparent acrylic panel assembly box. The rotating rod is detachably connected to the mounting plate and is located inside the mounting plate. The handle is rotatably connected to the rotating rod and is located at one end of the rotating rod. The demonstration component is disposed inside the transparent acrylic panel assembly box, and the auxiliary components are disposed on the outside of the transparent acrylic panel assembly box.

[0007] The demonstration components include a power distribution board, a flight control system, a GPS sensor, a signal receiver, and a fixing unit. The power distribution board is located inside the transparent acrylic panel assembly box, the flight control system is located on the surface of the power distribution board, the GPS sensor is located on the surface of the power distribution board, the signal receiver is located on the surface of the power distribution board, and the fixing unit is located inside the transparent acrylic panel assembly box.

[0008] The fixing unit includes a fixing rod, a first fixing ring, and a second fixing ring. The fixing rod is detachably connected to the power distribution board and passes through the power distribution board. The first fixing ring is fixedly connected to the fixing rod and wraps around the fixing rod. The second fixing ring is detachably connected to the fixing rod and wraps around the fixing rod. The power distribution board is located between the first fixing ring and the second fixing ring.

[0009] The auxiliary components include a locking block, a buckle, and a buffer unit. The locking block is detachably connected to the transparent acrylic panel assembly box and is located on the surface of the transparent acrylic panel assembly box. The buckle is detachably connected to the transparent acrylic panel assembly box and is located on the surface of the transparent acrylic panel assembly box. The locking block and the buckle are engaged. The buffer unit is located on one side of the transparent acrylic panel assembly box.

[0010] The buffer unit includes a telescopic rod, a spring, and a buffer plate. The telescopic rod is detachably connected to the transparent acrylic panel assembly box and is located on one side of the transparent acrylic panel assembly box. The spring is detachably connected to the transparent acrylic panel assembly box and wraps around the telescopic rod. The buffer plate is detachably connected to the telescopic rod and is located at the end of the telescopic rod away from the transparent acrylic panel assembly box. The buffer plate is also detachably connected to the end of the spring away from the transparent acrylic panel assembly box.

[0011] This utility model discloses a portable drone circuit demonstration box. The circuit board is fixed inside the transparent acrylic panel assembly box by the fixing unit, so that the internal structure and circuit connection of the transparent acrylic panel assembly box can be easily observed from the outside. The buckle and the locking block can easily open the transparent acrylic panel assembly box, so as to facilitate the installation or removal of the demonstration components inside. This reduces the overall size and weight of the drone teaching equipment, making it more convenient to carry. Attached Figure Description

[0012] To more clearly illustrate the technical solutions in the embodiments of this utility model 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 only some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0013] Figure 1 This is a schematic diagram of the portable drone circuit demonstration box of this utility model.

[0014] Figure 2 This is a front view of the portable drone circuit demonstration box of this utility model.

[0015] Figure 3 This is a side view of the portable drone circuit demonstration box of this utility model.

[0016] Figure 4 This is a top view of the portable drone circuit demonstration box of this utility model.

[0017] Figure 5 This is the utility model Figure 2 A cross-sectional view of the AA line structure.

[0018] Figure 6 This is the utility model Figure 3 BB line structural cross-sectional view.

[0019] 101-Transparent acrylic sheet assembly box, 102-Aluminum alloy outer frame, 103-Mounting plate, 104-Rotating rod, 105-Handle, 106-Power distribution board, 107-Flight control system, 108-GPS sensor, 109-Signal receiver, 110-Fixing rod, 111-First fixing ring, 112-Second fixing ring, 113-Clamping block, 114-Snap fastener, 115-Telescopic rod, 116-Spring, 117-Buffer plate. Detailed Implementation

[0020] The embodiments of this utility model are described in detail below. Examples of these embodiments are shown in the accompanying drawings, wherein the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The embodiments described below with reference to the accompanying drawings are exemplary and intended to explain this utility model, and should not be construed as limiting this utility model.

[0021] Please see Figures 1-6 ,in Figure 1 This is a schematic diagram of the portable drone circuit demonstration box of this utility model. Figure 2 This is a front view of the portable drone circuit demonstration box of this utility model. Figure 3This is a side view of the portable drone circuit demonstration box of this utility model. Figure 4 This is a top view of the portable drone circuit demonstration box of this utility model. Figure 5 This is the utility model Figure 2 AA-line structural cross-sectional view, Figure 6 This is the utility model Figure 3 BB line structural cross-sectional view.

[0022] This utility model provides a portable drone circuit demonstration box, including a transparent acrylic plate assembly box 101, an aluminum alloy outer frame 102, and demonstration components. The aluminum alloy outer frame 102 is detachably connected to the transparent acrylic plate assembly box 101 and is located on the outside of the transparent acrylic plate assembly box 101. The demonstration assembly includes a mounting plate 103, a rotating rod 104, a handle 105, a demonstration component, and auxiliary components. The mounting plate 103 is fixedly connected to the transparent acrylic sheet assembly box 101 and is located on the surface of the transparent acrylic sheet assembly box 101. The rotating rod 104 is detachably connected to the mounting plate 103 and is located inside the mounting plate 103. The handle 105 is rotatably connected to the rotating rod 104 and is located at one end of the rotating rod 104. The demonstration component is disposed inside the transparent acrylic sheet assembly box 101, and the auxiliary components are disposed on the outside of the transparent acrylic sheet assembly box 101.

[0023] In this embodiment, the power distribution board 106 is fixed inside the transparent acrylic panel assembly box 101 by the fixing unit, so that the internal structure and circuit connection of the transparent acrylic panel assembly box 101 can be easily observed from the outside. The buckle 114 and the latch 113 can easily open the transparent acrylic panel assembly box 101, thereby facilitating the installation or removal of the demonstration components inside, thereby reducing the overall size and weight of the UAV teaching equipment and making it more convenient to carry.

[0024] Furthermore, the demonstration component includes a power distribution board 106, a flight control system 107, a GPS sensor 108, a signal receiver 109, and a fixing unit. The power distribution board 106 is disposed inside the transparent acrylic panel assembly box 101, the flight control system 107 is disposed on the surface of the power distribution board 106, the GPS sensor 108 is disposed on the surface of the power distribution board 106, the signal receiver 109 is disposed on the surface of the power distribution board 106, and the fixing unit is disposed inside the transparent acrylic panel assembly box 101.

[0025] In this embodiment, the fixing unit fixes the power distribution board 106 inside the transparent acrylic assembly box 101, thereby facilitating the observation of the circuit connection between the flight control system 107, the GPS sensor 108 and the signal receiver 109, which is convenient for display.

[0026] Furthermore, the fixing unit includes a fixing rod 110, a first fixing ring 111, and a second fixing ring 112. The fixing rod 110 is detachably connected to the power distribution board 106 and passes through the power distribution board 106. The first fixing ring 111 is fixedly connected to the fixing rod 110 and wraps around the fixing rod 110. The second fixing ring 112 is detachably connected to the fixing rod 110 and wraps around the fixing rod 110. The power distribution board 106 is located between the first fixing ring 111 and the second fixing ring 112.

[0027] In this embodiment, when fixing the power distribution plate 106, the fixing rod 110 can be passed through the power distribution plate 106, and the second fixing ring 112 can be fixed on the fixing rod 110. The power distribution plate 106 is clamped and fixed by the first fixing ring 111 and the second fixing ring 112.

[0028] Furthermore, the auxiliary components include a locking block 113, a buckle 114, and a buffer unit. The locking block 113 is detachably connected to the transparent acrylic panel assembly box 101 and is located on the surface of the transparent acrylic panel assembly box 101. The buckle 114 is detachably connected to the transparent acrylic panel assembly box 101 and is located on the surface of the transparent acrylic panel assembly box 101. The locking block 113 is engaged with the buckle 114. The buffer unit is disposed on one side of the transparent acrylic panel assembly box 101.

[0029] In this embodiment, the buckle 114 and the latch 113 can easily open the transparent acrylic panel assembly box 101, thereby facilitating the installation or removal of the demonstration components inside.

[0030] Furthermore, the buffer unit includes a telescopic rod 115, a spring 116, and a buffer plate 117. The telescopic rod 115 is detachably connected to the transparent acrylic panel assembly box 101 and is located on one side of the transparent acrylic panel assembly box 101. The spring 116 is detachably connected to the transparent acrylic panel assembly box 101 and wraps around the telescopic rod 115. The buffer plate 117 is detachably connected to the telescopic rod 115 and is located at the end of the telescopic rod 115 away from the transparent acrylic panel assembly box 101. The buffer plate 117 is also detachably connected to the end of the spring 116 away from the transparent acrylic panel assembly box 101.

[0031] In this embodiment, when the transparent acrylic panel assembly box 101 is opened, the buffer plate 117 is placed on the ground, and the telescopic rod 115 and the spring 116 cooperate to play a buffering role.

[0032] The above-disclosed embodiments are merely preferred embodiments of the present utility model and should not be construed as limiting the scope of the present utility model. Those skilled in the art can understand that implementing all or part of the above-described embodiments and making equivalent changes in accordance with the claims of the present utility model are still within the scope of the utility model.

Claims

1. A portable drone circuit demonstration box, comprising a transparent acrylic panel assembly box and an aluminum alloy outer frame, wherein the aluminum alloy outer frame is detachably connected to the transparent acrylic panel assembly box and is located on the outside of the transparent acrylic panel assembly box, characterized in that, It also includes a demo component; The demonstration assembly includes a mounting plate, a rotating rod, a handle, a demonstration component, and auxiliary components. The mounting plate is fixedly connected to the transparent acrylic panel assembly box and is located on the surface of the transparent acrylic panel assembly box. The rotating rod is detachably connected to the mounting plate and is located inside the mounting plate. The handle is rotatably connected to the rotating rod and is located at one end of the rotating rod. The demonstration component is disposed inside the transparent acrylic panel assembly box, and the auxiliary components are disposed on the outside of the transparent acrylic panel assembly box.

2. The portable drone circuit demonstration box as described in claim 1, characterized in that, The demonstration components include a power distribution board, a flight control system, a GPS sensor, a signal receiver, and a fixing unit. The power distribution board is located inside the transparent acrylic panel assembly box, the flight control system is located on the surface of the power distribution board, the GPS sensor is located on the surface of the power distribution board, the signal receiver is located on the surface of the power distribution board, and the fixing unit is located inside the transparent acrylic panel assembly box.

3. The portable drone circuit demonstration box as described in claim 2, characterized in that, The fixing unit includes a fixing rod, a first fixing ring, and a second fixing ring. The fixing rod is detachably connected to the power distribution board and passes through the power distribution board. The first fixing ring is fixedly connected to the fixing rod and wraps around the fixing rod. The second fixing ring is detachably connected to the fixing rod and wraps around the fixing rod. The power distribution board is located between the first fixing ring and the second fixing ring.

4. The portable drone circuit demonstration box as described in claim 1, characterized in that, The auxiliary components include a locking block, a buckle, and a buffer unit. The locking block is detachably connected to the transparent acrylic panel assembly box and is located on the surface of the transparent acrylic panel assembly box. The buckle is detachably connected to the transparent acrylic panel assembly box and is located on the surface of the transparent acrylic panel assembly box. The locking block and the buckle are engaged. The buffer unit is located on one side of the transparent acrylic panel assembly box.

5. The portable drone circuit demonstration box as described in claim 4, characterized in that, The buffer unit includes a telescopic rod, a spring, and a buffer plate. The telescopic rod is detachably connected to the transparent acrylic panel assembly box and is located on one side of the transparent acrylic panel assembly box. The spring is detachably connected to the transparent acrylic panel assembly box and wraps around the telescopic rod. The buffer plate is detachably connected to the telescopic rod and is located at the end of the telescopic rod away from the transparent acrylic panel assembly box. The buffer plate is also detachably connected to the end of the spring away from the transparent acrylic panel assembly box.

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