CN210212781U

CN210212781U - Multifunctional aircraft with automatic charging function

Info

Publication number: CN210212781U
Application number: CN201921214847.4U
Authority: CN
Inventors: Zhiyong Liang; 梁智勇; Yufa Liang; 梁余发; Xin Yang; 杨昕; Jun Chen; 陈俊; Qiwei Ying; 应启围; Yi Man; 满毅; Yunhui Liu; 刘云辉; Ming Ke; 柯明; Zhidong Liang; 梁智东; Lishuai Zhang; 张立帅
Original assignee: Guangxi Jiutian Intelligent Control Technology Co Ltd
Current assignee: Guangxi Jiutian Intelligent Control Technology Co Ltd
Priority date: 2019-07-30
Filing date: 2019-07-30
Publication date: 2020-03-31
Anticipated expiration: 2029-07-30

Abstract

The utility model discloses a multifunctional aircraft with automatic function of charging belongs to unmanned aerial vehicle application. The automatic charging device comprises an unmanned aerial vehicle, a modeling model, an automatic charging device and a positioning module; the modeling model is arranged on the upper end face of the unmanned aerial vehicle; the automatic charging device comprises an airborne module and a ground module, wherein a positioning recess is formed in the lower end face of the airborne module, a first positive contact is arranged at the top in the positioning recess, and a first negative contact is arranged on the side wall of the positioning recess; the upper end face of the ground module is provided with a positioning protrusion matched with the positioning recess, the upper end of the positioning protrusion is provided with a second positive contact, the side wall of the positioning protrusion is provided with a second negative contact, and the second positive contact and the second negative contact are respectively connected with the power adapter through leads; the positioning module is used for positioning the position of the unmanned aerial vehicle. The problem of unmanned aerial vehicle's performance molding presentation form be abundant inadequately, load the figurative unmanned aerial vehicle of performance and rise and fall difficult and can not realize fixed point and descend and the automatic function of charging is solved.

Description

Multifunctional aircraft with automatic charging function

Technical Field

The utility model relates to an unmanned aerial vehicle application especially relates to a multifunctional aircraft with automatic function of charging.

Background

The unmanned aerial vehicle is an unmanned aerial vehicle operated by utilizing a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by an onboard computer, compared with a manned aircraft, the unmanned aerial vehicle is more suitable for tasks too 'fool, dirty or dangerous', the unmanned aerial vehicle can be divided into military use and civil use according to the application field, the unmanned aerial vehicle is divided into a reconnaissance aircraft and a target aircraft, and the unmanned aerial vehicle is matched with industrial application in the civil use and is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, and the application of the unmanned aerial vehicle is greatly expanded. Although the unmanned aerial vehicle technology is mature, the existing application and artistic performance is only mounting lamplight, characters or figures are demonstrated by a plurality of unmanned aerial vehicle formations and the combination of lamplight effects, and the artistic performance is not vivid enough. The existing unmanned aerial vehicle can not carry the model with artistic modeling for aerial display. An unmanned aerial vehicle-based air dance line drawing puppet with application number of CN201520186003.9 comprises a pull rope, a puppet and an unmanned aerial vehicle body, wherein a line drawing mechanism is arranged on the unmanned aerial vehicle body, one end of the pull rope is connected to the movable part of the puppet, the other end of the pull rope is connected with the line drawing mechanism, and the line drawing mechanism is used for controlling the pull rope to be drawn and drawn; be provided with the decoration umbrella on the unmanned aerial vehicle body, the umbrella top of decorating the umbrella is the fretwork, should decorate the umbrella and both can shelter from the unmanned aerial vehicle body, and the reinforcing performance effect does not influence the flight again. Should combine act as go-between puppet and unmanned aerial vehicle technique, make the puppet freely perform in the air, the place can be changed at any time moreover, has changed the traditional manual performance form of the puppet of acting as go-between, has higher sight and interest. Because this patent is based on unmanned aerial vehicle flight platform's suspension line puppet, the puppet is in the below of aircraft, and there is the suspension line puppet aircraft below, and the aircraft is difficult to descend. And the device has no automatic charging device, has limited cruising ability, and can not realize fixed-point landing and automatic charging functions.

SUMMERY OF THE UTILITY MODEL

The utility model discloses an invention purpose is, to above-mentioned problem, provides a multi-functional aircraft with automatic function of charging, solves unmanned aerial vehicle's performance molding presentation form abundant inadequately, load performance molding's unmanned aerial vehicle and play and fall difficult and can not realize the problem of fixed point landing and automatic function of charging.

In order to achieve the above purpose, the utility model adopts the technical proposal that: a multifunctional aircraft with an automatic charging function comprises an unmanned aerial vehicle, a modeling model, an automatic charging device and a positioning module; the unmanned aerial vehicle comprises a machine body, a flight control device, a power supply device, two landing gears, a plurality of machine arms, a plurality of motors and a plurality of propellers, wherein the flight control device and the power supply device are arranged in the machine body, and the landing gears are arranged on two sides of the lower end surface of the machine body; the machine arms are rod-shaped, one ends of the machine arms are connected with the machine body, the other ends of the machine arms horizontally extend out, and the machine arms are uniformly distributed around the machine body in a radiation mode; the motor is arranged at the end part of the extending end of each horn, each motor is respectively connected with the flight control device and the power supply device, each propeller is respectively connected with an output shaft of one motor, and the propeller is positioned below the horn; the modeling model is arranged on the upper end surface of the machine body; the automatic charging device comprises an airborne module and a ground module, wherein the airborne module is arranged at the lower end of the machine body and is positioned between the two undercarriage; a positioning recess is formed in the lower end of the airborne module, a first positive contact is arranged at the top in the positioning recess, and a first negative contact is arranged on the side wall of the positioning recess; the first positive contact is connected with the positive electrode of the power supply device through a lead, and the first negative contact is connected with the negative electrode of the power supply device through a lead; the ground module is arranged on the ground, a positioning protrusion matched with the positioning recess is arranged on the upper end face of the ground module, a second positive contact is arranged at the upper end of the positioning protrusion, a second negative contact is arranged on the side wall of the positioning protrusion, the first positive contact corresponds to the second positive contact in position, the first negative contact corresponds to the second negative contact in position, and the second positive contact and the second negative contact are respectively connected with a power adapter through wires; the positioning module is used for positioning the position of the unmanned aerial vehicle.

Furthermore, the positioning module comprises a Beidou navigation positioning module and an infrared sensing positioning module, and the Beidou navigation positioning module is arranged on any one of the machine arms; the infrared induction positioning module comprises an infrared transmitter and an infrared receiver, the infrared transmitter is arranged on the lower end face of the machine body, and the infrared receiver is arranged on the upper end face of the ground module.

Furthermore, the quantity of infrared ray emitter and infrared receiver of infrared ray induction positioning module is a plurality of, and a plurality of infrared ray emitter encircles automatic charging device, a plurality of infrared receiver with infrared emitter one-to-one.

Further, the positioning protrusion is a trapezoidal frustum or a conical frustum.

Furthermore, the number of the first negative electrode contacts and the number of the second negative electrode contacts are both a plurality, the first negative electrode contacts surround the first positive electrode contacts, and the second negative electrode contacts surround the second positive electrode contacts.

Further, the modeling model is an inflatable model

Due to the adoption of the technical scheme, the beneficial effects of the utility model are that:

1. the utility model discloses during the use, be provided with the face of placing of molding through the up end at the organism, through being provided with the screw of underneath type, guarantee that the screw can not get into and place the face top, can place molding on unmanned aerial vehicle's upper portion, it is aerial with molding through unmanned aerial vehicle, make molding in the show aloft, its expression form is novel, give other people and use different perception feelings, unmanned aerial vehicle performance form has been richened more, be different from traditional unmanned aerial vehicle performance form, higher sight and interest have. Because the model of modelling is located unmanned aerial vehicle's top, the model of modelling can not influence taking off and descending of unmanned aerial vehicle, makes the utility model discloses it is safer reasonable. The utility model discloses a be provided with automatic charging device, unmanned aerial vehicle passes through descending after the orientation module location, after falling, through first positive pole contact and the connection of second positive pole contact, first negative pole contact and the connection of second negative pole contact for the electricity adapter can charge for power supply unit, realizes unmanned aerial vehicle's automatic charging, real unmanned aerial vehicle's multi-functional usage.

2. The utility model discloses a be provided with a plurality of infrared receiver and a plurality of infrared emitter for first positive contact is located the second positive contact directly over, ensures the accuracy of location.

3. The utility model discloses a set the model of modelling to inflatable structure, can be in order to alleviate model of modelling weight, make unmanned aerial vehicle obtain longer duration, the model of modelling gassing can be folded model of modelling again, is convenient for accomodate the transportation.

Drawings

FIG. 1 is a three-dimensional structure diagram of the present invention;

fig. 2 is the internal structure diagram of the machine body and the automatic charging device of the present invention.

In the attached drawing, 1-an unmanned aerial vehicle, 2-a modeling model, 3-an automatic charging device, 4-a positioning module, 11-a machine body, 12-an undercarriage, 13-a machine arm, 14-a motor, 15-a propeller, 16-a flight control device, 17-a power supply device, 31-an airborne module, 32-a ground module, 41-a Beidou navigation positioning module, 42-an infrared emitter, 43-an infrared receiver, 311-a first positive contact, 312-a first negative contact, 321-a positioning protrusion, 322-a second positive contact, 323-a second negative contact and 324-a power adapter.

Detailed Description

The following describes the embodiments of the present invention with reference to the accompanying drawings.

In the description of the present invention, it is to be understood that the terms "center", "length", "width", "up", "down", "vertical", "horizontal", "top", "bottom", "inner", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience in describing the present invention and simplifying the description, but do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention.

In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," and "fixed" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally formed; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.

In the present disclosure, unless expressly stated or limited otherwise, the first feature "on" or "under" the second feature may comprise direct contact between the first and second features, or may comprise contact between the first and second features not directly. Also, the first feature being "on," "above" and "over" the second feature includes the first feature being directly on and obliquely above the second feature, or merely indicating that the first feature is at a higher level than the second feature. A first feature being "under," "below," and "beneath" a second feature includes the first feature being directly under and obliquely below the second feature, or simply meaning that the first feature is at a lesser elevation than the second feature.

As shown in fig. 1, a multifunctional aircraft with an automatic charging function comprises an unmanned aerial vehicle 1, a modeling model 2, an automatic charging device 3 and a positioning module 4; wherein:

the unmanned aerial vehicle 1 comprises a body 11, two undercarriages 12, a plurality of horn 13, a plurality of motors 14, a plurality of propellers 15, a flight control device 16 and a power supply device 17, wherein the flight control device 16 and the power supply device 17 are arranged in the body 11, and the undercarriages 12 are arranged on the lower end surface of the body 11; the machine arm 13 is rod-shaped, one end of the machine arm 13 is connected with the machine body 11, the other end of the machine arm 13 horizontally extends out, and the plurality of machine arms 13 are uniformly distributed around the machine body 11 in a radiation mode; a motor 14 is arranged at the end part of the extending end of each machine arm 13, each motor 14 is respectively connected with a flight control device 16 and a power supply device 17, each propeller 15 is respectively connected with an output shaft of each motor 14, and the propeller 15 is positioned below the machine arm 13; the modeling model 2 is arranged on the upper end face of the machine body 11, and the modeling model 2 is an inflatable model. It should be noted that it is a mature prior art that the power supply device 17 supplies power to the flight control device 16 and the motor 14, and the flight control device 16 controls the motor 14 to make the unmanned aerial vehicle 1 start and stop, which is not a research range of the present application, and is not described in detail in the present application.

As shown in fig. 2, the automatic charging device 3 includes an onboard module 31 and a ground module 32, the onboard module 31 is mounted on the lower end surface of the machine body 11 and is located in the undercarriage 12; a positioning recess is formed in the lower end face of the airborne module 31, a first positive contact 311 is arranged at the top in the positioning recess, and a first negative contact 312 is arranged on the side wall of the positioning recess; the first positive contact 311 is connected with the positive electrode of the power supply device 17 through a lead, and the first negative contact 312 is connected with the negative electrode of the power supply device 17 through a lead; the ground module 32 is installed on the ground, a positioning protrusion 321 matched with the positioning recess is arranged on the upper end surface of the ground module 32, a second positive contact 322 is arranged at the upper end of the positioning protrusion 321, a second negative contact 323 is arranged on the side wall of the positioning protrusion 321, the first positive contact 311 corresponds to the second positive contact 322 in position, the first negative contact 212 corresponds to the second negative contact 323 in position, and the second positive contact 322 and the second negative contact 323 are respectively connected through a wire power adapter 324; the number of the first negative contacts 312 and the number of the second negative contacts 323 are several, the first negative contacts 312 surround the first positive contacts 311, and the second negative contacts 323 surround the second positive contacts 322. The positioning protrusion 321 is a trapezoidal or conical frustum. In the present embodiment, the number of the first negative contacts 312 is four, and the first negative contacts are respectively disposed on four sidewalls of the positioning recess, and the number of the second negative contacts 323 is four, and the second negative contacts are respectively disposed on four sidewalls of the positioning protrusion 321.

The positioning module 4 is used for positioning the unmanned aerial vehicle. Orientation module 4 includes big dipper navigation orientation module 41 and infrared ray induction orientation module, and big dipper navigation orientation module 41 is installed on arbitrary horn 13, and infrared ray induction orientation module includes infrared emitter 42 and infrared receiver 43, and infrared emitter 42 is installed at the lower terminal surface of organism 11, and infrared receiver 43 is installed at the up end of ground module 32. The number of the infrared emitters 42 and the infrared receivers 43 of the infrared sensing and positioning module is a plurality, the infrared emitters 42 surround the automatic charging device 3, and the infrared receivers 43 correspond to the infrared emitters 42 one by one. In the present case, the number of the infrared emitters 42 and the infrared receivers 43 is four. It should be explained that the Beidou navigation positioning technology and the infrared induction accurate positioning technology are mature prior art, and the realization that the Beidou navigation positioning technology and the infrared induction accurate positioning technology are used for assisting the automatic charging function in the present case is not repeated in the present case.

The above description is for the detailed description of the preferred possible embodiments of the present invention, but the embodiments are not intended to limit the scope of the present invention, and all equivalent changes or modifications accomplished under the technical spirit suggested by the present invention should fall within the scope of the present invention.

Claims

1. The utility model provides a multi-functional aircraft with automatic function of charging which characterized in that: the automatic charging device comprises an unmanned aerial vehicle, a modeling model, an automatic charging device and a positioning module; the unmanned aerial vehicle comprises a machine body, a flight control device, a power supply device, two landing gears, a plurality of machine arms, a plurality of motors and a plurality of propellers, wherein the flight control device and the power supply device are arranged in the machine body, and the landing gears are arranged on two sides of the lower end surface of the machine body; the machine arms are rod-shaped, one ends of the machine arms are connected with the machine body, the other ends of the machine arms horizontally extend out, and the machine arms are uniformly distributed around the machine body in a radiation mode; the motor is arranged at the end part of the extending end of each horn, each motor is respectively connected with the flight control device and the power supply device, each propeller is respectively connected with an output shaft of one motor, and the propeller is positioned below the horn; the modeling model is arranged on the upper end surface of the machine body; the automatic charging device comprises an airborne module and a ground module, wherein the airborne module is arranged at the lower end of the machine body and is positioned between the two undercarriage; a positioning recess is formed in the lower end of the airborne module, a first positive contact is arranged at the top in the positioning recess, and a first negative contact is arranged on the side wall of the positioning recess; the first positive contact is connected with the positive electrode of the power supply device through a lead, and the first negative contact is connected with the negative electrode of the power supply device through a lead; the ground module is arranged on the ground, a positioning protrusion matched with the positioning recess is arranged on the upper end face of the ground module, a second positive contact is arranged at the upper end of the positioning protrusion, a second negative contact is arranged on the side wall of the positioning protrusion, the first positive contact corresponds to the second positive contact in position, the first negative contact corresponds to the second negative contact in position, and the second positive contact and the second negative contact are respectively connected with a power adapter through wires; the positioning module is used for positioning the position of the unmanned aerial vehicle.

2. The multifunctional aircraft with the automatic charging function according to claim 1, wherein: the positioning module comprises a Beidou navigation positioning module and an infrared sensing positioning module, and the Beidou navigation positioning module is arranged on any one of the machine arms; the infrared induction positioning module comprises an infrared transmitter and an infrared receiver, the infrared transmitter is arranged on the lower end face of the machine body, and the infrared receiver is arranged on the upper end face of the ground module.

3. The multifunctional aircraft with the automatic charging function according to claim 2, characterized in that: the quantity of infrared ray emitter and infrared receiver of infra red ray induction orientation module is a plurality of, and a plurality of infrared ray emitter encircles automatic charging device, a plurality of infrared receiver with infrared emitter one-to-one.

4. The multifunctional aircraft with the automatic charging function according to claim 1, wherein: the positioning protrusion is a trapezoidal table or a conical table.

5. The multifunctional aircraft with the automatic charging function according to claim 1, wherein: the number of the first negative electrode contacts and the number of the second negative electrode contacts are both a plurality, the first negative electrode contacts surround the first positive electrode contacts, and the second negative electrode contacts surround the second positive electrode contacts.

6. The multifunctional aircraft with the automatic charging function according to claim 1, wherein: the modeling model is an inflatable model.