CN215098272U

CN215098272U - Unmanned aerial vehicle convenient to adjust GPS

Info

Publication number: CN215098272U
Application number: CN202121706846.9U
Authority: CN
Inventors: 程启平; 李飞; 张凌威
Original assignee: Huizhou Yifei Intelligent Technology Co ltd
Current assignee: Huizhou Yifei Intelligent Technology Co ltd
Priority date: 2021-07-26
Filing date: 2021-07-26
Publication date: 2021-12-10
Anticipated expiration: 2031-07-26

Abstract

The utility model relates to an unmanned aerial vehicle convenient for adjusting GPS, which comprises a body and a plurality of arms arranged on the body, wherein the periphery of the body is coated to form a shell structure, and the shell structure comprises a lower shell, an upper shell and side shells extending towards the upper shell along the two ends of the lower shell; the novel multifunctional robot is characterized in that a mounting part is arranged on the robot body, a GPS module is arranged on the mounting part, two opposite side plates are arranged on the robot body, a corresponding mounting hole is formed in each of the two side plates, the mounting part is mounted on the two side plates through a bolt, and the GPS module is adjusted in angle through the bolt. The utility model discloses the GPS module that sets up can pass through its angle of bolt adjustment, can satisfy the flight and pass through the user demand under the different situation.

Description

Unmanned aerial vehicle convenient to adjust GPS

Technical Field

The utility model relates to an unmanned aerial vehicle field especially relates to an unmanned aerial vehicle convenient to adjust GPS.

Background

A drone is an unmanned aircraft that is operated with a radio remote control device and self-contained program control, or is operated autonomously, either completely or intermittently, by an onboard computer. When the existing unmanned aerial vehicle is manufactured, a motor and an electric controller of the unmanned aerial vehicle are generally welded, so that the unmanned aerial vehicle is inconvenient to replace and has higher welding requirements, a plurality of enterprises cannot meet the welding requirements during welding, and meanwhile, a plurality of electric controllers corresponding to the motors are required to be designed, so that the structure is unreasonable; in addition, unmanned aerial vehicle generally all need install the GPS module, but the angle generally can not be adjusted when the installation of GPS module, can't satisfy the flight and pass through the user demand under the different conditions.

SUMMERY OF THE UTILITY MODEL

Based on this, it is necessary to provide an unmanned aerial vehicle convenient to adjust GPS to the above-mentioned problem.

An unmanned aerial vehicle convenient for adjusting a GPS (global positioning system) comprises a fuselage and a plurality of arms arranged on the fuselage, wherein the periphery of the fuselage is coated to form a shell structure, and the shell structure comprises a lower shell, an upper shell and side shells extending towards the upper shell along two ends of the lower shell; the novel multifunctional robot is characterized in that a mounting part is arranged on the robot body, a GPS module is arranged on the mounting part, two opposite side plates are arranged on the robot body, a corresponding mounting hole is formed in each of the two side plates, the mounting part is mounted on the two side plates through a bolt, and the GPS module is adjusted in angle through the bolt.

In one embodiment, the GPS module is mounted at the rear end of the fuselage.

In one embodiment, the housing structure is provided with a number of plug outlets.

This application forms shell structure, and this shell structure can wrap the fuselage, especially the interior parts such as electricity of fuselage is transferred, simultaneously, is provided with the GPS module in the one end of fuselage, and its angle can be adjusted through the bolt to this GPS module, can satisfy the flight and pass through the user demand under the different situation.

Drawings

Fig. 1 is a first overall schematic diagram of the present invention.

Fig. 2 is a second overall schematic view of the present invention.

FIG. 3 is a partially enlarged view of the part A of the present invention;

fig. 4 is a schematic structural view of the connection assembly of the present invention;

fig. 5 is an exploded view of the plug, the socket, the first housing and the second housing of the present invention;

fig. 6 is an exploded view of the buckle structure of the present invention;

fig. 7 is an exploded view of the housing structure of the present invention;

fig. 8 is an exploded view of the mounting portion of the GPS module according to the present invention.

Reference numbers: 1-fuselage, 11-electronic tuning, 2-horn, 21-groove, 22-mounting piece, 23-side plate, 24-bolt, 25-mounting hole, 3-flight device, 4-connecting component, 41-first plug-in piece, 42-second plug-in piece, 411-plug, 412-first wire, 413-first shell, 421-socket, 422-second wire, 423-second shell, 5-buckle structure, 51-upper buckle, 52-lower buckle, 511-side convex plate, 512-buckle hole, 521-hook part, 6-shell structure, 61-lower shell, 62-upper shell, 63-side shell and 7-GPS module.

Detailed Description

In order to make the above objects, features and advantages of the present invention more comprehensible, embodiments of the present invention are described in detail below with reference to the accompanying drawings.

The following description of at least one exemplary embodiment is merely illustrative in nature and is in no way intended to limit the invention, its application, or uses.

Techniques and apparatus known to those of ordinary skill in the relevant art may not be discussed in detail, but are intended to be considered a part of the specification where appropriate.

In all examples shown and discussed herein, any particular value should be construed as merely illustrative, and not limiting. Thus, other examples of the exemplary embodiments may have different values.

It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, further discussion thereof is not required in subsequent figures.

According to the utility model discloses, an unmanned aerial vehicle convenient to adjust GPS is provided, and this unmanned aerial vehicle can regard as carrying out the remote control to load the camera, carry out the operation of taking photo by plane.

The embodiment of the utility model provides a pair of unmanned aerial vehicle convenient to adjust GPS please refer to and refer to fig. 1, fig. 2 and fig. 3, it includes fuselage 1 and a plurality of horn 2 of setting on fuselage 1, install electricity on the fuselage 1 and adjust 11, all set up flying device 3 on every horn 2, flying device 3 includes at least one motor electricity adjust with be provided with coupling assembling 4 and buckle structure 5 between the motor, coupling assembling 4 fixes through buckle structure 5 on the horn.

Referring to fig. 1, fig. 2 and fig. 8, in the present embodiment, the mounting member 22 may be provided with a cavity and a corresponding opening, the GPS module 7 is placed into the cavity of the mounting member 22 through the opening and is fixedly mounted, wherein the mounting member 22 needs to be mounted on the body 2, therefore, two side plates 23 are provided on the body 2, for example, the front end of the body 2, for example, the rear end of the body 2, the mounting member 22 is disposed between the two side plates 23, and then, the fixing is performed by a bolt 24, and the bolt 24 may pass through the mounting member 22 and the two side plates 23 for fixing. The angle of the GPS module 7 is adjusted as required, so that the GPS module 7 can be adapted to different environments through the angle of the adjusting bolt, the angle of the GPS module 7 can be adjusted, the motor can be installed through manual adjustment, the motor can be connected with a circuit board, and the rotation of the GPS module 7 is controlled by a circuit system.

In this embodiment, a plurality of horn 2 all install on fuselage 1, and the installation of horn 2 and fuselage 1 can be: the fuselage 1 can be provided with a plurality of installation portions, and a plurality of horn 2 mechanical installation or detachable mode are installed on fuselage 1, the convenient change, or fuselage 1 and horn 2 adopt integrated into one piece's mode, for example, can be provided with a chassis on fuselage 1, and horn 2 extends outward from the chassis, forms integrative structural design with fuselage 1, and such integrative design can increase the structural strength of fuselage 1 and horn 2, can reduce when the operation, like the damage that the collision caused.

Wherein, horn 2 can be provided with four, distributes in the periphery of fuselage 1, all sets up flying device 3 on every horn 2, and then flying device 3 also has four, has better flight effect. Flight device 3 includes motor and screw structure, and the motor drives screw structure and rotates, drives unmanned aerial vehicle flight, and is preferred, and every flight device 3's screw structure can set up a plurality ofly, including main screw structure and branch screw structure, main screw structure can provide unmanned aerial vehicle flight power, divides screw structure can control unmanned aerial vehicle flight direction. Simultaneously, install on fuselage 1 and transfer 11, for example, transfer 11 and install the middle part position at fuselage 1, transfer 11 and can set up one, on every flying device 3 motor all adopted coupling assembling 5 to be connected to and transfer 11, through 11 control motor rotations of transferring electrically, and then control unmanned aerial vehicle's flight.

Referring to fig. 1, fig. 2, fig. 4 and fig. 5, in this embodiment, the connection assembly 4 includes a first plug 41 and a second plug 42, the first plug 41 includes a plug 411 and at least one first conductive wire 412, one end of the first conductive wire 412 is connected to the plug 411, the other end of the first conductive wire 412 is connected to the electronic module 11 along the wire of the horn 2, the second plug 42 includes a socket 421 and at least one second conductive wire 422, one end of the second conductive wire 422 is connected to the socket 421, and the other end of the second conductive wire 422 is connected to the motor along the wire of the horn 2; the plug 411 and the socket 421 are coupled to each other by insertion and removal.

It is understood that the connection assembly 4 is an electrical connection component between the electronic tilt 11 and the motor, and the plug 411 and the socket 421 are matched to be connected in a plug-in manner, that is, the first plug-in 41 and the second plug-in 42 can be matched in a plug-in manner. First wire 412 may be provided with a plurality of wires, each having one end connected to electronic module 11 and the other end connected to plug 411, and running along horn 2. Meanwhile, the second wire 422 may be provided with a plurality of wires, each having one end connected to the motor and the other end connected to the socket 421, and running the wire along the horn 2. The first wire 412 and the second wire 422 may be routed along the upper end surface of the horn 2, along the lower end surface of the horn 2, or along the side end surface of the horn 2. It should be noted that the first conducting wire 412 and the second conducting wire 422 may be electric wires commonly used in daily life, and when the electric power is turned on, the electric power regulator 11 and the motor are turned on. For example, interfaces may be formed at both ends of the first conductive line 412 and the second conductive line 422, and corresponding interfaces may be provided at the plug 411, the socket 421, the electronic module 11, and the motor, so that the plug connection and the pull connection may be performed more conveniently. In addition, the plug 411 and the socket 421 may be connected at any position of the arm 2, for example, at the middle of the arm. Set up like this, the motor can need not adopt welded operation with being connected of electricity accent, when appearing damaging, more conveniently changes, reduces replacement cost and reduce time. Preferably, the lengths of the first wire 412 and the second wire 422 are not too long, and after the first wire 412 and the second wire 422 are respectively conducted with the electronic device 11 and the motor, the sum of the lengths is slightly greater than the length of the horn 2, so as to prevent the first wire 412 and the second wire 422 from being thrown away due to too long lengths.

In this embodiment, the plug device further comprises a first housing 413 and a second housing 423, wherein the first housing 413 surrounds at least one end of the plug 411, and the second housing 423 surrounds at least one end of the socket 421. One end of the plug 411 is provided with a plurality of first metal ends, the first shell 413 is provided with a plurality of first isolation holes, and the first metal ends are correspondingly inserted into the first isolation holes; one end of the socket 421 is provided with a plurality of second metal ends, the second housing 423 is provided with a plurality of second isolation holes, and the second metal ends are correspondingly inserted into the second isolation holes.

It can be understood that the first shell 413 and the second shell 423 both play an insulating role, one end of the plug 411 is connected with one end of the socket 421 in a plugging manner, and then the other end of the plug 411 has a plurality of first metal ends to leak out, and a plurality of first isolation holes are arranged on the first shell 413 corresponding to the first metal ends to prevent short circuit between the plurality of first metal ends leaking out of the plug 411. Similarly, a plurality of second metal ends of the other end of the socket 421 are exposed, and a plurality of second isolation holes are formed in the second housing 423 corresponding to the second metal ends to prevent the second metal ends exposed from the socket 421 from being short-circuited. In this way, a plurality of wires arranged on the plug or the socket are also isolated and cannot be short-circuited.

Referring to fig. 1, 2 and 6, in the present embodiment, a fastening structure 5 is used to fix a connecting component 4, the fastening structure 5 includes an upper fastening member 51 and a lower fastening member 52, and the upper fastening member 51 and the lower fastening member 52 form a cavity when assembled, and the cavity fastens the connecting component 4 and the horn 2. Set up like this, coupling assembling 4 can stabilize on horn 2, and unmanned aerial vehicle rocks when the flight can not influence coupling assembling 4's stability.

In this embodiment, the outer side of the upper fastener 51 extends to form a side protruding plate 511, the side protruding plate 511 is formed with a fastening hole 512, the lower fastener 52 is provided with a hooking portion 521 corresponding to the side protruding plate 511, the hooking portion 521 is connected with the side protruding plate 511 of the upper fastener 51, and the hooking portion 521 passes through the fastening hole 512 and is connected with the fastening hole 512 in a matching manner, so as to fasten the upper fastener 51 and the lower fastener 52. So, motor or electricity are transferred and are damaged in the use, when needing to be changed, only need will open buckle structure 5, just can be very convenient change, also can not damage unmanned aerial vehicle's inner structure.

Simultaneously, preferentially, in installation buckle structure 5's horn 2 position department, horn 2 both sides contract inwards and are formed with recess 21, and recess 21 is equivalent to the installation position, has the effect of conveniently fixing a position buckle structure 5, makes things convenient for buckle structure 5's installation. Preferably, after the snap structure 5 is mounted on the horn 2 through the groove 21, the side wall thereof does not protrude outwards from the side wall of the horn.

Referring to fig. 1, 2 and 7, in the present application, the outer periphery of the fuselage 1 is wrapped to form a shell structure 6, and the shell structure 6 includes a lower shell 61, an upper shell 62 and side shells 63 extending along two ends of the lower shell 61 toward the upper shell 62. It can be understood that the housing structure 6 may have an upper housing 62, a lower housing 61 and two side housings 63, the housing structure 6 may protect the internal components of the body for cladding protection, and at the same time, an outlet is left at the place where the connector is needed to form a plurality of plug outlets, while effectively protecting the internal components of the body, the other components can be connected in and out.

Referring to fig. 1, in the present application, the vehicle body further includes a GPS module 7, a mounting member 22 is disposed at a front end or a rear end of the vehicle body 2, the GPS module 7 is mounted on the mounting member 22, the vehicle body 2 is provided with two opposite side plates 23, each of the two side plates 23 is provided with a corresponding mounting hole 25, and the two side plates 23 are mounted on the two side plates 23 by passing through the mounting member 22 through a bolt 24, and the GPS module 7 adjusts an angle through the bolt 24.

The robot arm comprises a robot body and a plurality of robot arms, wherein each robot arm is provided with a motor, an electric controller is arranged on the robot body, one electric controller can control the motor on each robot arm, a connecting assembly is adopted to connect the electric controller and the motor in a mode of routing along the robot arms, and the connecting assembly is fixed on the robot arms by a buckling mechanism; coupling assembling includes first plug-in components and second plug-in components, and the form through socket and plug is connected first plug-in components and second plug-in components plug to connect through first wire electricity and transfer, the motor is connected to the second wire, effectively solves traditional electricity and transfers and adopt welded connection's mode with the motor, need not to weld and can connect the motor and transfer with electricity, reduces the manufacturing degree of difficulty, and electricity is transferred or the motor is when appearing damaging, more conveniently changes. Meanwhile, the shell structure is arranged to protect the aircraft body, and the angle of the GPS module can be adjusted by adopting a bolt structure, so that different software parameters and different use requirements are met, and the flying requirement of crossing under different conditions is met.

The above-mentioned embodiments only represent some embodiments of the present invention, and the description thereof is specific and detailed, but not to be construed as limiting the scope of the present invention. It should be noted that, for those skilled in the art, without departing from the spirit of the present invention, several variations and modifications can be made, which are within the scope of the present invention. Therefore, the protection scope of the present invention should be subject to the appended claims.

Claims

1. An unmanned aerial vehicle convenient for adjusting a GPS (global positioning system) is characterized by comprising a fuselage (1) and a plurality of arms (2) arranged on the fuselage, wherein the periphery of the fuselage is wrapped to form a shell structure (6), and the shell structure comprises a lower shell (61), an upper shell (62) and side shells (63) extending towards the upper shell along two ends of the lower shell; the novel GPS module is characterized in that a mounting part (22) is arranged on the machine body, a GPS module (7) is arranged on the mounting part, two opposite side plates (23) are arranged on the machine body, a corresponding mounting hole (25) is formed in each of the two side plates, a bolt (24) penetrates through the mounting part and is mounted on the two side plates, and the GPS module is further adjusted in angle through the bolt.

2. Unmanned aerial vehicle convenient to adjust GPS according to claim 1, characterized in that the GPS module is installed at the rear end of the fuselage.

3. Unmanned aerial vehicle convenient to adjust GPS according to claim 1, characterized in that the housing structure (6) is provided with several plug outlets.