CN219097018U

CN219097018U - Intelligent unmanned aerial vehicle capable of landing and buffering

Info

Publication number: CN219097018U
Application number: CN202320068742.2U
Authority: CN
Inventors: 赵飞; 南恒春; 张秋丽
Original assignee: Xi'an Yiketong Uav System Co ltd
Current assignee: Xi'an Yiketong Uav System Co ltd
Priority date: 2023-01-10
Filing date: 2023-01-10
Publication date: 2023-05-30
Anticipated expiration: 2033-01-10

Abstract

The utility model relates to the technical field of intelligent unmanned aerial vehicles, in particular to an intelligent unmanned aerial vehicle capable of landing and buffering, which comprises a support frame body and a control main bin, wherein the control main bin is fixedly connected to the top end position of the support frame body, bent pipes are fixedly screwed to the left lower position and the right lower position of the support frame body, an arc bar is fixedly connected to one side position of each bent pipe, a side clamping plate is fixedly connected to the inclined lower position of each arc bar, and when the support frame of the intelligent unmanned aerial vehicle is connected with the intelligent unmanned aerial vehicle to roll over due to collision, the support frame body with one side end lifted returns to the original horizontal placement state along the arc track of the arc bar, so that the intelligent unmanned aerial vehicle capable of landing and buffering is prevented from rolling over due to the occurrence of the rolling over of the direct side, and damage to the unmanned aerial vehicle body or other important accessories due to the collision is effectively avoided.

Description

Intelligent unmanned aerial vehicle capable of landing and buffering

Technical Field

The utility model relates to the technical field of intelligent unmanned aerial vehicles, in particular to an intelligent unmanned aerial vehicle capable of landing and buffering.

Background

The intelligent unmanned aerial vehicle capable of landing and buffering refers to an intelligent unmanned aerial vehicle which completes aerial photographing operation in high altitude through a high-definition camera and can realize stable landing, and the intelligent unmanned aerial vehicle is protected by buffering when landing so as to ensure that the intelligent unmanned aerial vehicle can be landed, and a special buffer pad of the unmanned aerial vehicle is installed on a supporting frame arranged at the bottom of the intelligent unmanned aerial vehicle when the intelligent unmanned aerial vehicle is assembled;

in-process that actual intelligent unmanned aerial vehicle that can land buffering was taking photo by plane the operation is accomplished, needs to stably land on horizontal mesa because the intelligent unmanned aerial vehicle that is in the landing state opportunity appears turning on one's side when receiving external force collision, and this phenomenon of turning on one's side can influence intelligent unmanned aerial vehicle and realize stably landing, and the intelligent unmanned aerial vehicle that can land buffering is whole can be because of the focus skew that takes place when turning on one's side, appears the phenomenon that inclines.

Disclosure of Invention

The utility model aims to provide an intelligent unmanned aerial vehicle capable of landing and buffering, which solves the problems that the intelligent unmanned aerial vehicle capable of landing and buffering is provided in the background art, aerial photographing operation is completed, and when a rollover phenomenon occurs due to external force collision, the phenomenon of side dumping occurs due to gravity center deviation during rollover.

In order to achieve the above purpose, the present utility model provides the following technical solutions:

the utility model provides an intelligent unmanned aerial vehicle that can land buffering, includes support frame body and control main bin, the top position fixedly connected with control main bin of support frame body, and the equal screw fixation in left side below and right side below of support frame body has the return bend, one side position fixedly connected with arc strip of return bend, the oblique below position fixedly connected with side cardboard of arc strip, and the rear position rotation of side cardboard is connected with the runner.

Preferably, the middle part position of the bottom end of the control main bin is fixedly connected with a mounting seat, one side position of the mounting seat is fixedly provided with a camera body, and the wiring terminal of the camera body is connected with the wiring terminal of a microprocessor arranged in the control main bin.

Preferably, both sides position in the control main storehouse is all fixedly connected with side branch, and the top position in the control main storehouse is fixed with sun-proof top cap, side branch keeps away from the one side position fixedly connected with auxiliary cutting ferrule in the control main storehouse, and auxiliary cutting ferrule's inboard is equipped with micro-motor, micro-motor's output is connected with spiral She Benti, and micro-motor's wiring end is connected with the wiring end of the microprocessor that is equipped with in the control main storehouse inside.

Preferably, the appearance of support frame body is that the vertical end is "U" structural distribution setting that the slope form structural distribution set up, and the blotter body has all been cup jointed to the horizontal end both sides position of support frame body.

Preferably, the arc strip is symmetrically arranged along the vertical central axis of the support frame body, the arc strip and the bent pipe are connected to form an included angle inclined by 41 degrees, and the arc strip is connected with the rotating wheel through the side clamping plate.

Compared with the prior art, the utility model has the beneficial effects that:

1. according to the intelligent unmanned aerial vehicle landing system, through the rotating wheel, the supporting frame body, the arc bars, the bent pipe and the side clamping plates, when the intelligent unmanned aerial vehicle is connected and the supporting frame is in rollover due to collision, the supporting frame body with the one side end lifted can quickly return to original horizontal arrangement along the arc track of the arc bars, the phenomenon that the intelligent unmanned aerial vehicle capable of landing and buffering is in rollover due to direct side dumping is avoided, and the situation that the intelligent unmanned aerial vehicle capable of landing and buffering is in rollover dumping due to collision in the landing process is effectively avoided, so that the unmanned aerial vehicle body or other important accessories are damaged due to collision;

2. according to the utility model, through the arranged cushion pad body and the support frame body, when the intelligent unmanned aerial vehicle capable of landing and buffering stably lands on the horizontal table surface under the influence of collision of external force, the cushion pad body which is an opening of the intelligent unmanned aerial vehicle and is free of installation is contacted with the ground, and the cushion pad body can support the intelligent unmanned aerial vehicle capable of landing and buffering, and simultaneously can utilize the rebound effect which is made of rubber material, so that the impact force generated when the intelligent unmanned aerial vehicle lands on the horizontal table surface can be effectively buffered, and the intelligent unmanned aerial vehicle can be ensured to stably land.

Drawings

FIG. 1 is a schematic diagram of the overall structure of the present utility model;

FIG. 2 is a schematic view of a side-turning structure of a support frame body according to the present utility model;

FIG. 3 is a schematic view of the structure of the elbow of the present utility model.

In the figure: 1-control main bin, 2-support frame body, 3-return bend, 4-blotter body, 5-arc strip, 6-side cardboard, 7-runner, 8-mount pad, 9-camera body, 10-sun-proof top cap, 11-side branch, 12-auxiliary cutting ferrule, 13-spiral leaf body, 14-micromotor.

Description of the embodiments

The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. 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.

Referring to fig. 1-3, the present utility model provides a technical solution:

the utility model provides an intelligent unmanned aerial vehicle that can land buffering, includes support frame body 2 and control main storehouse 1, the top position fixedly connected with control main storehouse 1 of support frame body 2, and the equal screw fixation in the left side below and the right side below of support frame body 2 has return bend 3, and the one side position fixedly connected with arc strip 5 of return bend 3, the oblique below position fixedly connected with side cardboard 6 of arc strip 5, and the rear position rotation of side cardboard 6 is connected with runner 7.

As shown in fig. 1 and 2, the middle position of the bottom end of the control main cabin 1 is fixedly connected with a mounting seat 8, one side position of the mounting seat 8 is fixedly provided with a camera body 9, the wiring end of the camera body 9 is connected with the wiring end of a microprocessor arranged in the control main cabin 1, and when the intelligent unmanned aerial vehicle capable of landing and buffering is assembled, the camera body 9 can be connected with the mounting seat 8 in a multi-bolt fixing manner in advance, so that the camera after being fixedly installed can be stably arranged at the position below the bottom end of the intelligent unmanned aerial vehicle capable of landing and buffering; the intelligent unmanned aerial vehicle comprises a control main cabin 1, a sun-proof top cover 10, an auxiliary cutting sleeve 12, a micro motor 14, a screw She Benti, a wiring terminal of the micro motor 14 and a wiring terminal of a microprocessor arranged in the control main cabin 1, wherein the two side positions of the control main cabin 1 are fixedly connected with the side supporting rods 11, the top end position of the control main cabin 1 is fixedly provided with the sun-proof top cover 10, the side position of the side supporting rods 11 away from the control main cabin 1 is fixedly connected with the auxiliary cutting sleeve 12, the micro motor 14 is arranged on the inner side of the auxiliary cutting sleeve 12, the output end of the micro motor 14 is connected with the screw She Benti, the wiring terminal of the micro motor 14 is connected with the wiring terminal of the microprocessor arranged in the control main cabin 1, and when the intelligent unmanned aerial vehicle capable of landing and buffering is in a high-altitude running state, a plurality of micro motors 14 started simultaneously can carry a plurality of groups of spiral blade bodies 13 to realize high-speed rotation, so that the intelligent unmanned aerial vehicle capable of landing and buffering can realize stable flight in high altitude by means of upward thrust generated in the rotation process; the appearance of support frame body 2 is the setting of "U" type structural distribution that the vertical end was slope form structural distribution setting, and the blotter body 4 has all been cup jointed to the horizontal end both sides position of support frame body 2, and when installing a set of blotter body 4, the opening of a set of blotter body 4 adoption exempts from the dress design, when making things convenient for the mode that a set of blotter can cup joint, when quick connect support frame body 2, later stage operator only need outwards break the mode of opening off with the fingers and thumb, can pull down the blotter fast.

As shown in fig. 1, fig. 2 and fig. 3, the arc strip 5 is symmetrical along the vertical axis of the support frame body 2, and the arc strip 5 and the connection of the elbow 3 form an inclined included angle of 41 degrees, the arc strip 5 is connected with the rotating wheel 7 through the side clamping plate 6, combine before installing the operation as the support frame of this intelligent unmanned aerial vehicle bottom support component, a set of elbow 3 can be in the same place with support frame body 2 screw fixed connection, a set of arc strip 5 and a set of rotating wheel 7 both can stably install the both sides position of support frame body 2, the support frame that is equipped with in the bottom position of this intelligent unmanned aerial vehicle that can land the buffering is in the process of landing contact ground, when the contact is realized to the rotating wheel 7 that makes support frame both sides position be equipped with and ground, as shown in fig. 2, under the auxiliary connection cooperation of elbow 3 and side clamping plate 6, the rotating wheel 7 that contacts with ground is providing certain auxiliary support effect to this intelligent unmanned aerial vehicle that can land the phenomenon of rolling over, according to the lever principle can, under the state that can increase potential energy, along with the control the support frame that the main storehouse 1 is by the side end is by the arc strip is placed down, the intelligent unmanned aerial vehicle can avoid the phenomenon that the side of rolling over is placed down along with the side of the support frame that the main storehouse 1 to roll over down the side of the intelligent unmanned aerial vehicle, the intelligent unmanned aerial vehicle is avoided to roll down the side of the situation to roll down.

The working flow is as follows: when the intelligent unmanned aerial vehicle capable of landing and buffering is in operation, under the auxiliary connection cooperation of the auxiliary clamping sleeve 12 and the side supporting rods 11, the started micro motor 14 can realize stable rising while carrying the spiral blade body 13, so that the intelligent unmanned aerial vehicle capable of landing and buffering can fly to the high altitude, and the camera body 9 after being electrified can be used for carrying out corresponding aerial photographing operation from the high altitude position.

Although embodiments of the present utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made therein without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides an intelligent unmanned aerial vehicle that can land buffering, includes support frame body (2) and control main storehouse (1), its characterized in that: the novel automatic control device is characterized in that a control main bin (1) is fixedly connected to the top end position of the support frame body (2), an elbow (3) is fixedly arranged at the left lower side and the right lower side of the support frame body (2) through screws, an arc strip (5) is fixedly connected to one side position of the elbow (3), a side clamping plate (6) is fixedly connected to the inclined lower side of the arc strip (5), and a rotating wheel (7) is rotatably connected to the rear side of the side clamping plate (6).

2. The intelligent unmanned aerial vehicle capable of landing and buffering as claimed in claim 1, wherein: the intelligent control device is characterized in that an installation seat (8) is fixedly connected to the middle of the bottom end of the control main bin (1), a camera body (9) is fixedly installed at one side of the installation seat (8), and a wiring terminal of the camera body (9) is connected with a wiring terminal of a microprocessor arranged in the control main bin (1).

3. The intelligent unmanned aerial vehicle capable of landing and buffering as claimed in claim 1, wherein: the control main bin (1) is characterized in that side struts (11) are fixedly connected to the two side positions of the control main bin (1), a sun-proof top cover (10) is fixedly installed at the top end position of the control main bin (1), an auxiliary clamping sleeve (12) is fixedly connected to one side position of the side struts (11) away from the control main bin (1), a micro motor (14) is arranged on the inner side of the auxiliary clamping sleeve (12), a spiral She Benti (13) is connected to the output end of the micro motor (14), and a wiring end of the micro motor (14) is connected with a wiring end of a microprocessor arranged in the control main bin (1).

4. The intelligent unmanned aerial vehicle capable of landing and buffering as claimed in claim 1, wherein: the appearance of support frame body (2) is that the vertical end is "U" type structure distribution setting that the slope form structure distributes and sets up, and the horizontal end both sides position of support frame body (2) has all cup jointed blotter body (4).

5. The intelligent unmanned aerial vehicle capable of landing and buffering as claimed in claim 1, wherein: the arc strip (5) is symmetrically arranged along the vertical central axis of the support frame body (2) and is connected with the bent pipe (3) to form an included angle inclined by 41 degrees, and the arc strip (5) is connected with the rotating wheel (7) through the side clamping plate (6).