CN221090400U

CN221090400U - Amphibious cleaning robot

Info

Publication number: CN221090400U
Application number: CN202322518125.0U
Authority: CN
Inventors: 刘兴超
Original assignee: Chongqing Wuzu Bird Robot Co ltd
Current assignee: Chongqing Wuzu Bird Robot Co ltd
Priority date: 2023-09-17
Filing date: 2023-09-17
Publication date: 2024-06-07
Anticipated expiration: 2033-09-17

Abstract

The utility model relates to the technical field of cleaning, in particular to a land-air amphibious cleaning robot. Including arrange in proper order in length direction, and the identical first folding fuselage of appearance structure, unmanned aerial vehicle fuselage and second fold the fuselage, first folding fuselage with the second fold the fuselage all with link to each other through the pin joint structure between the unmanned aerial vehicle fuselage, so that first folding fuselage and second fold the fuselage rotatable extremely the upper end of unmanned aerial vehicle fuselage, just be provided with clean structure on first folding fuselage and the second folding fuselage, be provided with on the unmanned aerial vehicle fuselage and be used for providing the rotor part of flight power and be used for providing the walking part that the land march the power, through adopting folding fuselage, pin joint structure and the identical appearance structural design, realized carrying out the function of clean task in ground and sky.

Description

Amphibious cleaning robot

Technical Field

The utility model relates to the technical field of cleaning, in particular to a land-air amphibious cleaning robot.

Background

In modern society, with rapid development of technology and acceleration of life rhythm, demands for cleaning work are increasing, and manual cleaning is undoubtedly a time-consuming and labor-intensive task. Due to the high-efficiency, lasting and intelligent characteristics of the automatic cleaning robot, the robot gradually goes into the life of people, and helps us solve various cleaning problems. Although many cleaning robots can perform cleaning operations on the floor, their ability appears to catch the fly for cleaning operations in the air or at high altitudes.

Most of the cleaning robots in the current market are in a single mode, either roll on the ground or fly for cleaning, and the design cannot meet the cleaning requirement of amphibious air-ground. Moreover, these robots tend to be bulky, inconvenient to carry and store, and prone to user confusion. In addition, the design of fixed structure leads to uneven gravity center distribution and poor stability during flight

Therefore, the existing cleaning robots lack the capability of amphibious air-ground and cannot efficiently cope with complex and changeable cleaning requirements.

Disclosure of Invention

First, the technical problem to be solved

The utility model mainly aims at the problems and provides a land-air amphibious cleaning robot, which aims at solving the technical problems that the existing cleaning robot lacks the capability of land-air amphibious and cannot efficiently cope with complex and changeable cleaning requirements.

(II) technical scheme

In order to achieve the above purpose, the utility model provides an amphibious cleaning robot for land and air, which comprises a first folding body, an unmanned aerial vehicle body and a second folding body which are sequentially arranged in the length direction and have the same appearance structure, wherein the first folding body and the second folding body are connected with the unmanned aerial vehicle body through a pin joint structure, so that the first folding body and the second folding body can rotate to the upper end of the unmanned aerial vehicle body, cleaning structures are arranged on the first folding body and the second folding body, and a rotor wing part for providing flight power and a walking part for providing land travelling power are arranged on the unmanned aerial vehicle body.

Further, the pin joint structure includes first pivot portion, two first bellying and first pivot, first pivot portion and two first bellying set up one side of first folding fuselage, first pivot hole has been seted up on the first pivot portion, first end hole has been seted up on the first bellying, first pivot wears to establish the first pivot hole of this first pivot portion, the first end hole back fixed connection of two first bellying first folding fuselage.

Further, the pin joint structure includes second pivot portion, two second bellying and second pivot, second pivot portion and two second bellying set up one side of second folding fuselage, second pivot hole has been seted up on the second pivot portion, second end hole has been seted up on the second bellying, the second pivot is worn to establish the second pivot hole of this second pivot portion, the second end hole back fixed connection of two second bellying the second folding fuselage.

Further, the first pivot portion includes shell, steering wheel and gear train set up in the shell, the steering wheel with the gear train is in link to each other in the shell, is constructed the steering wheel drive the gear train rotates, first pivot outer wall is provided with the rotation tooth, the rotation tooth with the gear train meshing.

Further, a notch accommodating the first pivot portion is formed in the side wall of the unmanned aerial vehicle body.

Further, the rotor component comprises a horn mounted on the unmanned aerial vehicle body and a power component arranged on the horn, and a propeller is arranged on the power component.

Further, the walking component comprises a frame, a walking motor, a driving wheel, a driven wheel and a track, wherein the walking motor, the driving wheel and the driven wheel are arranged on the frame, an output shaft of the walking motor is connected with the driving wheel, and the track is installed around the driving wheel and the driven wheel.

Further, the rotor members are four groups arranged on the peripheral side of the unmanned aerial vehicle body.

Further, the walking parts are arranged at two groups at the lower end of the unmanned aerial vehicle body.

(III) beneficial effects

Compared with the prior art, the amphibious cleaning robot provided by the utility model has the advantages that the functions of executing cleaning tasks on the ground and in the air are realized by adopting the folding machine body, the pivoting structure and the same appearance structural design. The robot has the arrangement mode of the first folding body, the unmanned aerial vehicle body and the second folding body, so that when in a folding mode, the weight can be effectively concentrated by the same design of the appearance structure, the flight stability is improved, the size requirement on an unmanned aerial vehicle automatic airport can be reduced in a folding state, and more flexible and efficient cleaning operation is realized.

Drawings

Fig. 1 is a schematic view showing an unfolding structure of a amphibious cleaning robot according to the present application.

FIG. 2 is a schematic view of a cleaning structure according to the present disclosure.

Fig. 3 is a schematic diagram of an assembled structure of a hinge structure according to the present disclosure.

Fig. 4 is an exploded view of a hinge structure according to the present disclosure.

Fig. 5 is a schematic view illustrating an internal structure of a first pivot portion according to the present disclosure.

Fig. 6 is a schematic perspective view of a walking member according to the present disclosure.

Reference numerals shown in the drawings:

1. A first folded body; 2. an unmanned aerial vehicle body; 3. a second folded body; 4. a pin joint structure; 5. a cleaning structure; 6. a rotor component; 7. a walking member;

40. A first pivot portion; 41. a first boss; 42. a first pivot; 401. a first pivot hole; 410. a first end hole;

40a, a housing; 40b, steering engine; 40c, a gear set; 42a, rotating teeth;

60. a horn; 61. a power component; 62. a propeller;

70. a frame; 71. a walking motor; 72. a driving wheel; 73. driven wheel; 74. a track.

Detailed Description

The following detailed description of the present utility model, taken in conjunction with the accompanying drawings, will clearly and fully describe the technical solutions of the embodiments of the present utility model, it being evident that the described embodiments are only some, but not all, embodiments of the present utility model. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.

It will be understood that when an element is referred to as being "fixed to" another element, it can be directly on the other element or intervening elements may also be present. When a component is considered to be "connected" to another component, it can be directly connected to the other component or intervening components may also be present. When an element is referred to as being "disposed on" another element, it can be directly on the other element or intervening elements may also be present. The terms "vertical," "horizontal," "left," "right," and the like are used herein for illustrative purposes only.

Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this utility model belongs. The terminology used herein in the description of the utility model is for the purpose of describing particular embodiments only and is not intended to be limiting of the utility model. The term "and/or" as used herein includes any and all combinations of one or more of the associated listed items.

Referring to fig. 1-6, a schematic structural diagram of a amphibious cleaning robot according to a preferred embodiment of the application is shown. In the embodiment shown in fig. 1-6, the amphibious cleaning robot comprises a first folding body 1, an unmanned aerial vehicle body 2 and a second folding body 3 which are sequentially arranged in the length direction and have the same appearance structure, wherein the first folding body 1 and the second folding body 3 are connected with the unmanned aerial vehicle body 2 through a pin joint structure 4, so that the first folding body 1 and the second folding body 3 can rotate to the upper end position of the unmanned aerial vehicle body 2, the design with the same appearance structure can effectively concentrate weight in the folding mode, the flight stability is improved, the size requirements on the unmanned aerial vehicle automatic field can be reduced in the folding state, the cleaning structures 5 are arranged on the first folding body 1 and the second folding body 3 and are used for executing cleaning tasks, a rotor wing part 6 for providing flight power and a walking part 7 for providing land traveling power are arranged on the unmanned aerial vehicle body 2, and the robot can execute tasks on the land and also can execute traveling and cleaning operations on the land.

The composition and connection relationship of the above components will be specifically described below.

As shown in fig. 3 and 4, the pivot structure 4 of the robot includes a first pivot structure and a second pivot structure according to an example of the present disclosure. The first pivoting structure is composed of a first pivot portion 40, two first protrusions 41 and a first pivot 42 for connecting the first folded body 1. Similarly, the second pivot structure is composed of a second pivot part, two second protruding parts and a second pivot shaft and is used for connecting the second folded machine body. Wherein:

The first pivot portion 40 and the two first protruding portions 41 are disposed on one side of the first folding body 1, the first pivot portion 40 is provided with a first pivot hole 401, the first protruding portion 41 is provided with a first end hole 410, and the first pivot 42 is fixedly connected with the first folding body 1 after penetrating through the first pivot hole 401 of the first pivot portion 40 and the first end holes 410 of the two first protruding portions 41.

Similarly, the second pivot part and the two second protruding parts are arranged on the other side of the second folding machine body, the second pivot part is provided with a second pivot hole, the second protruding part is provided with a second end hole, and the second pivot is fixedly connected with the second folding machine body 3 after penetrating through the second pivot hole of the second pivot part and the second end holes of the two second protruding parts.

The design of this pivoting structure 4 enables the first folded fuselage 1 and the second folded fuselage 3 to be connected to the unmanned aerial vehicle fuselage 2 by rotation. By the implementation of such a pivoting structure 4, the robot can be operated flexibly in different environments. When an aerial mission is required, the rotor member 6 provides flight power, and the first folded fuselage 1 and the second folded fuselage 3 can be manually rotated to the upper end of the unmanned plane fuselage 2 before flight. When it is required to perform a land mission, the first and second folded bodies 1 and 3 may be unfolded and land traveling power is provided using the traveling member 7. The design enables the robot to have the functions of cleaning the air and the land at the same time, and improves the capability and the working efficiency of adapting to different scenes.

As shown in fig. 5, the pivot structure 4 adopts an automatic rotation manner, wherein the first pivot portion 40 includes a housing 40a, a steering engine 40b and a gear set 40c. The steering engine 40b and the gear set 40c are located in the housing 40a, and the gear set 40c is driven to rotate by the steering engine 40b connected in the housing 40 a. The outer wall of the first pivot 42 is provided with rotating teeth 42a which engage the gear set 40c. Thus, the gear set 40c is driven to rotate by the steering engine 40b, and the rotating teeth 42a and the first pivot 42 rotate accordingly, thereby realizing the rotation of the first folding body 1. Similarly, the second folded body is also completed in the same manner. This solution allows an automatic rotation of the first folded body 1 and the second folded body 3. The rotation of the first and second folded bodies can be easily controlled by driving the rotation of the gear set 42b through the steering gear 40 b. The design of automatic rotation enables the robot to be capable of rapidly adapting to different task demands, and has higher flexibility and operation efficiency.

Further, the side wall of the unmanned aerial vehicle body 2 is provided with a notch for accommodating the installation of the first pivot part 40, so that the first pivot part 40 is fixedly connected with the unmanned aerial vehicle body 2 through a connecting structure such as a bolt, a screw and the like.

Specifically, the rotor member 6 in the pivotal structure 4 includes a horn 60 and a power member 61 mounted on the horn 60, and a propeller 62 is provided on the power member 61. As shown in fig. 6, the walking member 7 is composed of a frame 70, a walking motor 71, a driving wheel 72, a driven wheel 73 and a track 74, wherein the walking motor 71, the driving wheel 72 and the driven wheel 73 are all installed on the frame 70, an output shaft of the walking motor 71 is connected with the driving wheel 72, and the track 74 is wound between the driving wheel 72 and the driven wheel 73. Thereby realizing the multifunctional operation of the robot. Through the pivot structure 4 of the swivelling joint unmanned aerial vehicle fuselage 2, the robot can utilize rotor components 6 to realize the aerial flight ability, uses walking components 7 to realize the land ability of marcing simultaneously. The propeller 62 provides stable lift and propulsion, enabling the robot to fly freely in the air. The design of the walking members 7 enables smooth movement of the robot on land and increases the adaptability to different terrains by means of the tracks 74.

Still further, the rotor members 6 are four groups arranged on the peripheral side of the unmanned aerial vehicle body 2.

Further, the traveling members 7 are two groups arranged at the lower end of the unmanned aerial vehicle body 2.

It will be evident to those skilled in the art that the application is not limited to the details of the foregoing illustrative embodiments, and that the present application may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The present embodiments are, therefore, to be considered in all respects as illustrative and not restrictive, the scope of the application being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned. Furthermore, it is evident that the word "comprising" does not exclude other elements or steps, and that the singular does not exclude a plurality. Several of the units or means recited in the apparatus claims may also be embodied by one and the same unit or means, either in software or hardware. The terms first, second, etc. are used to denote a name, but not any particular order.

The above embodiments are only for illustrating the technical solution of the present application and not for limiting the same, and although the present application has been described in detail with reference to the preferred embodiments, it should be understood by those skilled in the art that modifications and equivalents may be made thereto without departing from the spirit and scope of the technical solution of the present application.

Claims

1. The utility model provides an amphibious cleaning robot of land and air, its characterized in that, include arrange in proper order in length direction, and the identical first folding fuselage of appearance structure, unmanned aerial vehicle fuselage and second fold the fuselage, first folding fuselage with the second fold the fuselage all with link to each other through the pin joint structure between the unmanned aerial vehicle fuselage, so that first folding fuselage and second fold the fuselage rotatable extremely the upper end of unmanned aerial vehicle fuselage, just be provided with cleaning structure on first folding fuselage and the second folding fuselage, be provided with the rotor part that is used for providing flight power and the walking part that is used for providing land and advances power on the unmanned aerial vehicle fuselage.

2. The amphibious cleaning robot according to claim 1, wherein the pivoting structure comprises a first pivot part, two first protruding parts and a first pivot, the first pivot part and the two first protruding parts are arranged on one side of the first folding body, a first pivot hole is formed in the first pivot part, a first end hole is formed in the first protruding part, and the first pivot is fixedly connected with the first folding body after penetrating through the first pivot hole of the first pivot part and the first end holes of the two first protruding parts.

3. The amphibious cleaning robot according to claim 1, wherein the pivoting structure comprises a second pivot part, two second protruding parts and a second pivot, the second pivot part and the two second protruding parts are arranged on one side of the second folding body, a second pivot hole is formed in the second pivot part, a second end hole is formed in the second protruding part, and the second pivot is fixedly connected with the second folding body after penetrating through the second pivot hole of the second pivot part and the second end holes of the two second protruding parts.

4. The amphibious cleaning robot according to claim 2, wherein the first pivot portion comprises a housing, a steering engine and a gear set, the steering engine and the gear set are arranged in the housing, the steering engine is connected with the gear set in the housing and is configured to drive the gear set to rotate, and rotating teeth are arranged on the outer wall of the first pivot and meshed with the gear set.

5. The amphibious cleaning robot according to claim 4, wherein a notch for accommodating the first pivot portion is formed in a side wall of the unmanned aerial vehicle body.

6. The amphibious cleaning robot according to claim 1, wherein the rotor component comprises a horn mounted on the unmanned aerial vehicle body and a power component provided on the horn, and the power component is provided with a propeller.

7. The amphibious cleaning robot according to claim 1, wherein the traveling component comprises a frame, a traveling motor, a driving wheel, a driven wheel and a crawler belt, the traveling motor, the driving wheel and the driven wheel are all arranged on the frame, an output shaft of the traveling motor is connected with the driving wheel, and the crawler belt is installed around the driving wheel and the driven wheel.

8. The amphibious cleaning robot according to claim 6, wherein the rotor members are four groups arranged on the periphery of the unmanned aerial vehicle.

9. The amphibious cleaning robot according to claim 7, wherein the traveling parts are two groups arranged at a lower end of the unmanned aerial vehicle body.