Unmanned aerial vehicle integrated with novel arrangement structure

Abstract

The utility model provides an unmanned aerial vehicle integrated with a novel arrangement structure. The unmanned aerial vehicle comprises a vehicle body and wings connected with the vehicle body, the machine plate is arranged in the machine body; the power management module is vertically arranged at the first end of the machine board, and the bottom of the power management module is connected with a plurality of first power circuits; the flight control module comprises an integrated module, a first power port is formed in the bottom of the integrated module, and the integrated module is connected with the battery through a second power circuit; a containing cavity is formed between the flight control module and the machine board, and the first power circuit and the second power circuit are contained in the containing cavity and hidden. According to the utility model, not only can a plurality of modules be arranged in a standardized manner, but also the number of wire harnesses can be reduced, and the modules are connected more intensively, so that the later maintenance is quicker, time-saving and labor-saving.

Description

Technical Field

[0001] The utility model relates to a drone with an integrated novel arrangement structure. Background Art

[0002] A drone is an aircraft that can fly without direct human control. Drones can be operated autonomously by radio remote control or by a preset flight control system. Drones have a wide range of applications in both military and civilian fields.

[0003] The existing drones have several lines arranged inside to assist the drone in connecting to a power module or other control modules. However, the inventors have found that several lines are relatively messy inside the body, and the lines may get tangled, which may cause the drone to fail to achieve the expected flight effect due to the lines. At the same time, too many messy and tangled lines will also affect the efficiency of drone maintenance. Moreover, the drone cannot maximize the use of internal space due to too many messy lines, which seriously affects the later upgrades of the drone and also causes the drone's internal electrical structure to have nowhere to install. Therefore, the research direction of the present utility model is to design a drone that integrates a new electrical structure, standardizes module arrangement, reduces the number of lines, and reduces the weight of the drone. Utility Model Content

[0004] The utility model provides a drone with an integrated novel arrangement structure, which can effectively solve the above problems.

[0005] The utility model is achieved in this way:

[0006] A drone with an integrated novel arrangement structure, comprising

[0007] a fuselage, and wings connected to the fuselage;

[0008] A machine plate, arranged inside the machine body;

[0009] A power management module is vertically arranged at the first end of the machine board, and a plurality of first power lines are connected to the bottom of the power management module;

[0010] The flight control module includes an integrated module, a first power port is provided at the bottom of the module, and the module is connected to the battery through a second power line;

[0011] A receiving cavity is formed between the flight control module and the machine board, and the first power line and the second power line are received in the receiving cavity to conceal the first power line and the second power line;

[0012] The flight control module and the board are assembled to form a mounting platform for mounting electrical components;

[0013] The mounting frame includes a power interface, which is connected to the first power line contained in the accommodating cavity for power supply, and the front end surface of the mounting frame is provided with a power board connected to the battery.

[0014] As a further improvement, a plurality of heat dissipation holes are formed at the second end of the board.

[0015] As a further improvement, the flight control module includes a first frame and a second frame, the four corners of the second frame are provided with supporting feet, and buffers are provided between the supporting feet and the four angles of the first frame.

[0016] As a further improvement, a plurality of slots are formed on the first frame to reduce the weight of the first frame.

[0017] As a further improvement, the buffer is made of rubber.

[0018] As a further improvement, an electronic speed control module is provided at the bottom of the machine board.

[0019] The beneficial effects of the utility model are:

[0020] (1) When the internal structure of the drone is actually installed, the flight control module is pre-installed on a special cover plate (not shown in the figure), the cover plate is sealed and fitted with the upper opening of the machine board, the power-on end of the second power line is connected to the power port at the bottom of the integrated module, and the connection end of the second power line is connected to the power interface on the mounting frame, the power interface is arranged on the power board, and the power board is plugged into the battery. After the connection is completed, the cover plate is connected to the machine board by screws, so that several lines can be hidden in the accommodating cavity so that the lines are not exposed. Not only can several modules be arranged in a standardized manner, but also the number of wiring harnesses can be reduced. Moreover, the connection between the modules is more centralized, which is faster in the later maintenance, saving time and effort. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] In order to more clearly illustrate the technical solution of the implementation mode of the utility model, the drawings required for use in the implementation mode will be briefly introduced below. It should be understood that the following drawings only show certain embodiments of the utility model and therefore should not be regarded as limiting the scope. For ordinary technicians in this field, other relevant drawings can be obtained based on these drawings without paying creative work.

[0022] Figure 1 It is the front view of the utility model.

[0023] Figure 2 It is an exploded view of the utility model.

[0024] Figure 3It is a schematic diagram of a machine plate of the utility model.

[0025] Figure 4 It is a schematic diagram of the flight control module of the utility model.

[0026] Figure 5 It is an internal schematic diagram of the body of the utility model.

[0027] Figure 6 It is an enlarged view of B of the present utility model.

[0028] Description of Figure Numbers:

[0029] 1. Body; 2. Wing; 3. Mounting slot; 4. Board; 40. Heat dissipation hole;

[0030] 5. flight control module; 50. first frame; 51. slot; 52. mounting portion; 54. second frame; 55. support leg; 57. integrated module; 58. buffer;

[0031] 6. Power management module; 7. Power board; 8. Electronic speed control module; 9. Mounting bracket; 10. Power interface. DETAILED DESCRIPTION

[0032] In order to make the purpose, technical scheme and advantages of the embodiments of the utility model clearer, the technical scheme in the embodiments of the utility model will be clearly and completely described below in conjunction with the drawings in the embodiments of the utility model. Obviously, the described embodiments are part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without making creative work belong to the scope of protection of the utility model. Therefore, the following detailed description of the embodiments of the utility model provided in the drawings is not intended to limit the scope of the utility model for which protection is sought, but merely represents the selected embodiments of the utility model. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without making creative work belong to the scope of protection of the utility model.

[0033] In the description of the present invention, the terms "first" and "second" are used for descriptive purposes only and cannot be understood as indicating or implying relative importance or implicitly indicating the number of the indicated technical features. Therefore, the features defined as "first" and "second" may explicitly or implicitly include one or more of the features. In the description of the present invention, the meaning of "plurality" is two or more, unless otherwise clearly and specifically defined.

[0034] Reference Figure 1-6 As shown, a drone with an integrated novel arrangement structure includes

[0035] A fuselage 1 and a wing 2 connected to the fuselage 1.

[0036] The machine board 4 is arranged inside the machine body 1 ; an electronic speed regulating module 8 is arranged at the bottom of the machine board 4 .

[0037] The power management module 6 is vertically arranged at the first end of the machine board 4. The top of the vertically arranged power management module 6 is also provided with a connection port connected to other modules. The bottom of the power management module 6 is connected with a plurality of first power lines; the flight control module 5 includes an integrated module 57, the bottom of which is provided with a first power port, and is connected to the battery through a second power line; a receiving cavity is formed between the flight control module 5 and the machine board 4, and the first power line and the second power line are accommodated in the receiving cavity, and the first power line and the second power line are concealed. The flight control module 5 and the machine board 4 are assembled to form a mounting platform for installing electrical components. The mounting platform has a flat surface and is connected to the machine board 4 by screws, and a plurality of first power lines and second power lines can be placed in the receiving cavity, so that the first power lines and the second power lines do not need to be exposed outside, or placed on the mounting platform. When the first power lines and the second power lines are concealed, the power management module 6 is installed on the upper shell of the mounting platform to maximize the use of the internal space of the drone, and if the drone needs to be modified and upgraded, other modules (such as sensing modules, etc.) can also be placed on the mounting platform.

[0038] Furthermore, the integrated module 57 is further optimized, so that the original need for several lines to connect to the integrated module 57 is optimized to only require a second power line connection, thereby reducing the number of wiring harnesses and reducing the weight of the drone. Moreover, a TF Card (memory card) is also provided on the side of the integrated module 57 for storing data. Compared with the original integrated module 57, some data interfaces are omitted. While omitting some interfaces, the number of wiring harnesses is further reduced, thereby reducing the weight.

[0039] The mounting frame 9 includes a power interface 10, which is connected to a first power line contained in the accommodating cavity for power supply, and a power board 7 connected to a battery is disposed on the front end surface of the mounting frame 9.

[0040] It is worth noting that when actually installing the internal structure of the drone, the flight control module 5 is pre-installed on a special cover plate, the cover plate is sealed and fitted with the upper opening of the machine board 4, the first power line on the power management module 6 is connected to the bottom power port of the integrated module 57 in the flight control module 5, and the second power line is connected to the power interface 10 on the mounting frame 9, the power interface 10 is arranged on the power board 7, and the power board 7 is plugged into the battery. After the connection is completed, the cover plate is connected to the machine board 4 by screws, so that several lines can be hidden in the accommodating cavity so that the lines will not be exposed. Not only can several modules be arranged in a standardized manner, but also the number of wiring harnesses can be reduced. Moreover, the connection between each module is more centralized, which is faster in the later maintenance, saving time and effort.

[0041] A plurality of heat dissipation holes 40 are formed at the second end of the base plate 4 .

[0042] The flight control module 5 includes a first frame 50 and a second frame 54. The four corners of the second frame 54 are provided with support legs 55, and buffer members 58 are provided between the support legs 55 and the four angles of the first frame 50. A plurality of slots 51 are formed on the first frame 50 to reduce the weight of the first frame 50. The buffer members 58 are made of rubber.

[0043] The first frame 50 and the second frame 54 are connected via a buffer 58. When the drone is vibrated, the buffer 58 made of rubber can reduce the vibration of the integrated module 57 installed on the second frame 54, so that it will not shake violently.

[0044] The above description is only the preferred implementation of the utility model, and is not intended to limit the utility model. For those skilled in the art, the utility model can have various modifications and changes. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the utility model shall be included in the protection scope of the utility model.

Claims

1. A drone with an integrated novel arrangement structure, characterized in that: include A body (1), and a wing (2) connected to the body (1); A machine plate (4) is arranged inside the machine body (1); A power management module (6) is vertically arranged at the first end of the machine board (4), and a plurality of first power lines are connected to the bottom of the power management module (6); The flight control module (5) comprises an integrated module (57), the bottom of which is provided with a first power port and is connected to a battery via a second power line; A receiving cavity is formed between the flight control module (5) and the machine board (4), and the first power line and the second power line are received in the receiving cavity, so that the first power line and the second power line are concealed; The flight control module (5) and the machine board (4) are assembled to form a mounting platform for mounting electrical components; The mounting frame (9) includes a power interface (10), the power interface (10) being connected to the first power line contained in the accommodating cavity for power supply, and a power board (7) connected to a battery is provided on the front end surface of the mounting frame (9).

2. The drone with integrated novel arrangement structure according to claim 1, characterized in that: A plurality of heat dissipation holes (40) are formed at the second end of the machine plate (4).

3. The drone with integrated novel arrangement structure according to claim 1, characterized in that: The flight control module (5) comprises a first frame (50) and a second frame (54), wherein four corners of the second frame (54) are provided with supporting feet (55), and buffer components (58) are provided between the supporting feet (55) and four angles between the first frame (50).

4. The drone with integrated novel arrangement structure according to claim 3, characterized in that: A plurality of slots (51) are formed on the first frame (50) for reducing the weight of the first frame (50).

5. The drone with integrated novel arrangement structure according to claim 3, characterized in that: The buffer member (58) is made of rubber.

6. The drone with integrated novel arrangement structure according to claim 1, characterized in that: An electronic speed regulation module (8) is arranged at the bottom of the machine board (4).

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