Six-rotor unmanned aerial vehicle supporting mounting of multiple types of loads

Abstract

The utility model discloses a six-rotor unmanned aerial vehicle supporting mounting of multiple types of loads, and relates to the technical field of six-rotor unmanned aerial vehicles, the six-rotor unmanned aerial vehicle comprises a six-rotor unmanned aerial vehicle body, a mounting shell, a mounting bolt, a fixing bolt, a landing foot stool, a connecting bolt, a mounting box and a limiting mechanism; wherein the top side of the six-rotor unmanned aerial vehicle body is fixedly connected with a mounting shell through mounting bolts, the bottom side of the six-rotor unmanned aerial vehicle body is fixedly connected with a landing foot stand through connecting bolts, the bottom side of the six-rotor unmanned aerial vehicle body is fixedly connected with a limiting mechanism through fixing bolts, and a mounting box is mounted in the limiting mechanism; the limiting mechanism comprises a fixing rod, a fixing bolt, a fixing plate and a fixing nut, the fixing plate and the bottom side connecting end of the six-rotor unmanned aerial vehicle body are fixed through the fixing bolt, the fixing rod penetrates through the bottom end of the fixing plate, and the surface of the fixing rod is sleeved with the fixing nut in a threaded mode. The six-rotor unmanned aerial vehicle supporting mounting of multiple types of loads is novel in design and simple in structure.

Description

Technical Field

[0001] The present application relates to the technical field of six-rotor UAVs, and in particular to a six-rotor UAV that supports mounting of multiple types of payloads. Background Art

[0002] The 6-rotor UAV is a scientific instrument used in the fields of natural science-related engineering and technology, and surveying and mapping science and technology. It was put into use on June 1, 2016. The optical payloads used by the UAV are mainly Canon and Haselblad. In addition to conventional photogrammetry, it is more suitable for high-precision, large-scale photogrammetry. Since the gimbal has a load-bearing capacity of more than 5kg, it can also carry payloads such as infrared and laser radar to achieve multi-source data acquisition.

[0003] At present, in the process of using drones, some existing drones are mostly fixed, which is not convenient for disassembling and assembling the drone structure according to needs, reducing the efficiency of subsequent disassembly, maintenance and replacement of drones. At the same time, some drone mounting boxes are inconvenient to install, which is not convenient for fixed installation of drone mounting boxes. Therefore, in order to solve the above problems, a six-rotor drone that supports multiple types of load mounting is proposed. Utility Model Content

[0004] In this embodiment, a six-rotor UAV that supports multiple types of payload mounting is provided to solve the problem that some existing UAVs are mostly fixed in the use of UAVs, which makes it inconvenient to disassemble and assemble the UAV structure according to needs, reducing the efficiency of subsequent disassembly, maintenance and replacement of the UAV, and at the same time, some UAV mounting boxes are inconvenient to install and inconvenient to fix the UAV mounting boxes.

[0005] According to one aspect of the present application, there is provided a six-rotor drone supporting multiple types of load mounting, comprising a six-rotor drone body, a mounting shell, mounting bolts, fixing bolts, a landing tripod, connecting bolts, a mounting box, and a limiting mechanism; wherein the top side of the six-rotor drone body is fixedly connected to the mounting shell by means of mounting bolts, the bottom side of the six-rotor drone body is fixedly connected to the landing tripod by means of connecting bolts, the bottom side of the six-rotor drone body is fixedly connected to the limiting mechanism by means of fixing bolts, and the mounting box is installed in the limiting mechanism;

[0006] The limiting mechanism includes a fixing rod, a fixing bolt, a fixing plate and a fixing nut. The fixing plate is fixed to the bottom connecting end of the six-rotor drone body by a fixing bolt. A fixing rod passes through the bottom end of the fixing plate, and a fixing nut is threadedly sleeved on the surface of the fixing rod.

[0007] Furthermore, mounting bolts are threadedly penetrated at four corner positions of the bottom surface of the mounting shell, and the ends of the mounting bolts are threadedly connected to the top side surface of the hexacopter drone body.

[0008] Furthermore, there are two fixing rods, which are placed in parallel, and fixing nuts threadedly connected to the surfaces of the fixing rods fit with the side surface of the bottom end of the fixing plate.

[0009] Furthermore, the number of the fixing plates is four, and the four fixing plates are symmetrically arranged on opposite sides of the mounting box.

[0010] Furthermore, there are two landing legs, which are symmetrically arranged at the bottom of the hexacopter drone body, and the top of the landing legs is threadedly connected to the bottom side surface of the hexacopter drone body through connecting bolts.

[0011] Through the above-mentioned embodiments of the present application, a six-rotor drone body, a mounting shell, mounting bolts, fixing bolts, a landing gear, connecting bolts, a mounting box and a limiting mechanism are adopted to solve the problem that during the current use of drones, some existing drones have fixed settings, which makes it inconvenient to disassemble and assemble the drone structure according to needs, reducing the efficiency of subsequent disassembly, maintenance and replacement of the drone, and at the same time, some drone mounting boxes are inconvenient to install and inconvenient to fix the drone mounting boxes. BRIEF DESCRIPTION OF THE DRAWINGS

[0012] In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings required for use in the embodiments or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the present application.

[0013] Figure 1 This is a schematic diagram of the overall three-dimensional structure of an embodiment of the present application;

[0014] Figure 2 It is a schematic diagram of the overall three-dimensional structure of an embodiment of the present application in another direction.

[0015] In the figure: 1. Hexacopter body; 2. Mounting shell; 3. Mounting bolts; 4. Fixing bolts; 5. Fixing rod; 6. Mounting box; 7. Fixing nut; 8. Landing tripod; 9. Connecting bolts; 10. Fixing plate. DETAILED DESCRIPTION

[0016] In order to enable those skilled in the art to better understand the present application, the technical solutions in the embodiments of the present application will be clearly and completely described below in conjunction with the drawings in the embodiments of the present application. Obviously, the described embodiments are only part of the embodiments of the present application, not all of the embodiments. Based on the embodiments in the present application, all other embodiments obtained by ordinary technicians in this field without creative work should fall within the scope of protection of this application.

[0017] It should be noted that the terms "first", "second", etc. in the specification and claims of the present application and the above-mentioned drawings are used to distinguish similar objects, and are not necessarily used to describe a specific order or sequential order. It should be understood that the data used in this way can be interchanged where appropriate, so that the embodiments of the present application described here. In addition, the terms "including" and "having" and any of their variations are intended to cover non-exclusive inclusions, for example, a process, method, system, product or device comprising a series of steps or units is not necessarily limited to those steps or units clearly listed, but may include other steps or units that are not clearly listed or inherent to these processes, methods, products or devices.

[0018] In the present application, the terms "upper", "lower", "left", "right", "front", "back", "top", "bottom", "inner", "outer", "middle", "vertical", "horizontal", "lateral", "longitudinal" and the like indicate positions or positional relationships based on the positions or positional relationships shown in the drawings. These terms are mainly used to better describe the present application and its embodiments, and are not used to limit the indicated devices, elements or components to have a specific orientation, or to be constructed and operated in a specific orientation.

[0019] In addition, some of the above terms may be used to express other meanings in addition to indicating orientation or positional relationship. For example, the term "on" may also be used to express a certain dependency or connection relationship in some cases. For those of ordinary skill in the art, the specific meanings of these terms in this application can be understood according to specific circumstances.

[0020] In addition, the terms "installed", "set", "provided with", "connected", "connected", and "socketed" should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integral structure; it can be a mechanical connection, or an electrical connection; it can be a direct connection, or an indirect connection through an intermediate medium, or it can be an internal connection between two devices, elements, or components. For those of ordinary skill in the art, the specific meanings of the above terms in this application can be understood according to specific circumstances.

[0021] It should be noted that, in the absence of conflict, the embodiments and features in the embodiments of the present application may be combined with each other.

[0022] The following is an introduction to the six-rotor drone of an embodiment of the present application.

[0023] See also Figure 1-2As shown, a six-rotor drone supporting multiple types of load mounting includes a six-rotor drone body 1, a mounting shell 2, mounting bolts 3, fixing bolts 4, a landing leg 8, connecting bolts 9, a mounting box 6, and a limiting mechanism; wherein the top side of the six-rotor drone body 1 is fixedly connected to the mounting shell 2 by the mounting bolts 3, the bottom side of the six-rotor drone body 1 is fixedly connected to the landing leg 8 by the connecting bolts 9, the bottom side of the six-rotor drone body 1 is fixedly connected to the limiting mechanism by the fixing bolts 4, the mounting box 6 is installed in the limiting mechanism, and the disassembly and assembly of the landing leg 8 is facilitated by disassembly of the connecting bolts 9;

[0024] The limiting mechanism includes a fixing rod 5, a fixing bolt 4, a fixing plate 10 and a fixing nut 7. The fixing plate 10 is fixed to the bottom connecting end of the six-rotor unmanned aerial vehicle body 1 by the fixing bolt 4. The fixing rod 5 passes through the bottom end of the fixing plate 10. The fixing nut 7 is threadedly sleeved on the surface of the fixing rod 5. The fixing plate 10 is fixed to the bottom surface of the six-rotor unmanned aerial vehicle body 1 by the fixing bolt 4. The fixing rod 5 passes through the bottom side surface of the fixing plate 10. By rotating the fixing nut 7, the fixing nut 7 fixes the fixing rod 5 to the bottom surface of the fixing plate 10, thereby improving the fixing stability of the fixing rod 5. Then, the mounting box 6 is placed on the top of the fixing rod 5 to meet the use of the mounting box 6.

[0025] Mounting bolts 3 are threadedly penetrated at the four corner positions of the bottom surface of the mounting shell 2, and the ends of the mounting bolts 3 are threadedly connected to the top side surface of the six-rotor drone body 1, which is convenient for disassembly and assembly of the mounting shell 2. There are two fixing rods 5, and the two fixing rods 5 are placed in parallel. The fixing nuts 7 threadedly connected to the surfaces of the fixing rods 5 are fitted with the bottom side surface of the fixing plates 10. There are four fixing plates 10, and the four fixing plates 10 are symmetrically arranged on the opposite sides of the mounting box 6. There are two landing legs 8, and the two landing legs 8 are symmetrically arranged at the bottom of the six-rotor drone body 1. The tops of the landing legs 8 are threadedly connected to the bottom side surface of the six-rotor drone body 1 through connecting bolts 9, which is convenient for disassembly and assembly of the landing gear.

[0026] When the utility model is in use, the electrical components appearing in the present application are all externally connected to the power supply and the control switch, the fixing plate 10 is fixed to the bottom surface of the six-rotor drone body 1 by the fixing bolts 4, the fixing rod 5 penetrates the bottom side surface of the fixing plate 10, and the fixing nut 7 is rotated to fix the fixing nut 7 to fix the fixing rod 5 to the bottom surface of the fixing plate 10, thereby improving the fixing stability of the fixing rod 5, and then the mounting box 6 is placed on the top of the fixing rod 5 to meet the use of the mounting box 6, and the disassembly and assembly of the landing frame 8 is facilitated by disassembly of the connecting bolts 9.

[0027] The benefits of this application are:

[0028] 1. This six-rotor drone that supports multiple types of load mounting has a novel design and a simple structure. The fixing plate is fixed to the bottom surface of the six-rotor drone body by fixing bolts, and the fixing rod penetrates the bottom side surface of the fixing plate. The fixing nut is rotated to fix the fixing rod to the bottom surface of the fixing plate, thereby improving the fixing stability of the fixing rod. Then, the mounting box is placed on the top of the fixing rod to meet the use of the mounting box. The disassembly of the connecting bolts facilitates the disassembly and assembly of the landing tripod.

[0029] The circuits, electronic components and modules involved are all prior art and can be fully implemented by those skilled in the art. Needless to say, the content protected by this application does not involve improvements to software and methods.

[0030] The above description is only the preferred embodiment of the present application and is not intended to limit the present application. For those skilled in the art, the present application may have various modifications and variations. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present application shall be included in the protection scope of the present application.

Claims

1. A six-rotor drone supporting multiple types of payload mounting, characterized in that: The invention comprises a six-rotor unmanned aerial vehicle body (1), a mounting shell (2), mounting bolts (3), fixing bolts (4), a landing footrest (8), connecting bolts (9), a mounting box (6) and a limiting mechanism; wherein the top side of the six-rotor unmanned aerial vehicle body (1) is fixedly connected to the mounting shell (2) via the mounting bolts (3), the bottom side of the six-rotor unmanned aerial vehicle body (1) is fixedly connected to the landing footrest (8) via the connecting bolts (9), the bottom side of the six-rotor unmanned aerial vehicle body (1) is fixedly connected to the limiting mechanism via the fixing bolts (4), and the mounting box (6) is installed in the limiting mechanism; The limiting mechanism comprises a fixing rod (5), a fixing bolt (4), a fixing plate (10) and a fixing nut (7); the fixing plate (10) is fixed to the bottom connecting end of the hexacopter drone body (1) via the fixing bolt (4); the fixing rod (5) passes through the bottom end of the fixing plate (10); and the fixing nut (7) is threadedly sleeved on the surface of the fixing rod (5).

2. The six-rotor drone supporting multiple types of payload mounting according to claim 1, characterized in that: Mounting bolts (3) are threadedly penetrated at four corner positions of the bottom surface of the mounting shell (2), and the ends of the mounting bolts (3) are threadedly connected to the top side surface of the hexacopter drone body (1).

3. The six-rotor drone supporting multiple types of payload mounting according to claim 1, characterized in that: There are two fixing rods (5), which are placed in parallel. The fixing nuts (7) threadedly connected to the surfaces of the fixing rods (5) fit the bottom side surface of the fixing plate (10).

4. The six-rotor drone supporting multiple types of payload mounting according to claim 1, characterized in that: The number of the fixing plates (10) is four, and the four fixing plates (10) are symmetrically arranged on opposite sides of the mounting box (6).

5. The six-rotor drone supporting multiple types of payload mounting according to claim 1, characterized in that: The number of the landing legs (8) is two, and the two landing legs (8) are symmetrically arranged at the bottom of the hexacopter drone body (1), and the top ends of the landing legs (8) are threadedly connected to the bottom surface of the hexacopter drone body (1) via connecting bolts (9).

Images