Unmanned aerial vehicle landing omni-directional capturing device and honeycomb type unmanned aerial vehicle base station

Abstract

The utility model provides an unmanned aerial vehicle landing omnibearing capturing device and a honeycomb type unmanned aerial vehicle base station, the unmanned aerial vehicle landing omnibearing capturing device comprises a landing plate, an omnibearing hollow guide cover is arranged on the landing plate, and the inner side wall of the omnibearing hollow guide cover is in an inclined state that the bottom is inward and the upper part is outward. When the capturing device is used for landing capturing of the unmanned aerial vehicle, capturing direction adjustment is not needed, and landing capturing operation of the unmanned aerial vehicle is simpler and more reliable.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned plane landing capture technical field, concretely unmanned plane landing all -round capture device and honeycomb unmanned plane base station. BACKGROUND

[0002] Unmanned plane is more and more widely used in various industries, and has great potential, but in practical application, there are factors such as low intelligent level, high personnel and commuting cost, harsh outdoor working environment, and unmanned plane take-off and landing limitation, which cause the unmanned plane to be unable to realize automatic operation truly by separating from manual field control, so that the unmanned plane only becomes an auxiliary tool for industrial field inspection and patrol, and its potential has not been truly played.

[0003] The applicant applied for a vertical take-off and landing fixed-wing aircraft (authorized publication number: CN205686609U), a novel unmanned plane (authorized publication number: CN217170961U) and an innovative vertical take-off and landing fixed-wing unmanned plane (authorized publication number: CN215155592U) in the early stage, which can realize vertical take-off and landing. In a windy environment, the above aircraft and unmanned plane can land with the fuselage keeping a crosswind attitude. The crosswind landing has a small windward area, and the wind resistance landing capacity is improved. The applicant applied for an unmanned plane landing capture device (authorized publication number: CN216861307U) in the early stage, which mainly comprises a landing plate, a landing optical recognition pattern is arranged on the landing plate, and a first guide limiting rod and a second guide limiting rod are arranged on the landing plate to form a landing capture guide space between the first guide limiting rod and the second guide limiting rod. The above-mentioned unmanned plane landing capture device can realize the landing capture of the unmanned plane, and then the landing accuracy of the unmanned plane can be improved. In a windy condition, if the landing capture direction does not correspond to the crosswind landing attitude of the unmanned plane when the above-mentioned unmanned plane landing capture device is used for landing capture of the unmanned plane, the landing capture of the unmanned plane cannot be smoothly realized. If the automatic rotation of the above-mentioned landing device is to be realized, a platform capable of rotating 360 degrees needs to be added, which leads to a complex structure of the capture device and a complicated control process. At the same time, if the above-mentioned device is used to capture the unmanned plane on a moving vehicle or a ship, the driving direction of the vehicle or the ship cannot be flexibly adjusted, which leads to difficulty in realizing the landing capture of the unmanned plane. UTILITY MODEL CONTENTS

[0004] The utility model aims at providing an unmanned plane landing all -round capture device and honeycomb unmanned plane base station, which can realize the landing capture of the unmanned plane without adjusting the capture direction, so that the landing capture operation of the unmanned plane is simpler and more reliable.

[0005] The utility model solves its technical problem and adopts the technical scheme that a kind of unmanned aerial vehicle landing all-direction capture device, including landing plate, landing optical identification pattern is provided on the landing plate, a all-direction hollow guide cover is provided on the landing plate, and all-direction hollow guide cover is located the periphery of landing optical identification pattern, the inner side wall of all-direction hollow guide cover is inclined state with bottom inward upper portion outward.

[0006] Preferably, a charging interface is arranged in the middle of the landing plate.

[0007] Further, the landing plate and the all-direction hollow guide cover are fixedly connected in a detachable manner.

[0008] Further, the landing plate includes a circular plate and a plurality of first splicing plates, the first splicing plates are sequentially spliced end to end around the circumferential direction of the circular plate, and the charging interface is arranged on the circular plate.

[0009] Further, the all-direction hollow guide cover includes a plurality of second splicing plates, and the second splicing plates are fixedly connected in a detachable manner.

[0010] Further, the all-direction hollow guide cover is circular or regular polygonal.

[0011] Further, the capture device further includes a box body, the landing plate is arranged in the box body, and a box cover is arranged above the box body.

[0012] Further, the box cover is a rotating split cover or a translational split cover.

[0013] A honeycomb unmanned aerial vehicle base station includes the unmanned aerial vehicle landing all-direction capture device described above, and the honeycomb unmanned aerial vehicle base station further includes a honeycomb box body, a plurality of landing plates are sequentially and spacedly arranged in the honeycomb box body, and a switch door is arranged at the upper portion of the honeycomb box body.

[0014] Further, the high honeycomb unmanned aerial vehicle base station further includes a motor vehicle, and the honeycomb box body is arranged on the motor vehicle.

[0015] The utility model discloses beneficial effect is: the utility model simple structure, processing and manufacturing are convenient, the inclined inner side wall of all -round hollow guide cover is in the 360 degree closed distribution of landing board, in the process that unmanned plane is about to land to landing board, under the condition that not landing board capture azimuth adjustment is carried out, no matter unmanned plane's belly is oriented to which direction, utilizes the inclined inner side wall and can realize the landing guide of unmanned plane, then makes the vertical landing operation of unmanned plane more simple and reliable, landing board adopts splicing mode assembly, all -round hollow guide cover adopts splicing mode assembly and landing board and all -round hollow guide cover adopt splicing mode assembly, can be convenient for realizing the manufacturing processing of landing board and all -round hollow guide cover, simultaneously, it is convenient for the flexible transportation and application of the utility model, when unmanned plane does not carry out flight task, unmanned plane can be placed in the box in the device, thereby realizing the storage of unmanned plane, when unmanned plane needs charging, utilizes the charging interface on landing board to be convenient for realizing the charging of unmanned plane, when utilizing the honeycomb unmanned plane base station to carry out flight task, can carry out intermittent flight control to multiple unmanned planes, satisfies the execution of long -time continuous flight task in the field. BRIEF DESCRIPTION OF DRAWINGS

[0016] In order to more clearly illustrate the technical scheme in the embodiment of the utility model or prior art, below will to the embodiment or prior art description needed to use the drawing briefly introduce, obviously, below description in the drawing is part preferred embodiment of the utility model, for the ordinary skilled person in the art comes, under the premise of not paying the creative labor, can also obtain other drawings according to these drawings.

[0017] Figure 1 It is the structure schematic diagram of the first embodiment of the utility model;

[0018] Figure 2 It is the front view of the optical landing identification pattern first specific embodiment distribution on landing board;

[0019] Figure 3 It is the structure schematic diagram of the second embodiment of the utility model;

[0020] Figure 4 It is the structure schematic diagram of the third embodiment of the utility model;

[0021] Figure 5 It is the structure schematic diagram of the second embodiment of landing board;

[0022] Figure 6 It is the state schematic diagram of the vertical take -off and landing unmanned plane landing on the first embodiment of the utility model;

[0023] Figure 7 It is the state schematic diagram of the vertical take -off and landing unmanned plane landing on the second embodiment of the utility model;

[0024] Figure 8 A schematic diagram of the state of the vertical take-off and landing unmanned aerial vehicle landing on the first embodiment of the box;

[0025] Figure 9 A schematic diagram of the state of the vertical take-off and landing unmanned aerial vehicle landing on the second embodiment of the box;

[0026] Figure 10 A schematic diagram of the structure of a specific embodiment of the honeycomb box placed on a motor vehicle;

[0027] In the figure: 1 landing plate, 11 optical landing identification pattern, 12 circular plate, 13 fan-shaped plate, 2 omnidirectional hollow guide cover, 3 charging interface, 31 negative charging pole, 32 positive charging pole, 4 unmanned aerial vehicle, 5 box, 51 sliding door, 52 rotating door, 53 straight reciprocating motion execution assembly, 54 damping support rod, 6 honeycomb box, 7 motor vehicle. DETAILED DESCRIPTION

[0028] The specific embodiments will be described below with reference to the accompanying drawings. Figures 1-9 The technical solutions in the embodiments of the present application are clearly and completely described. Obviously, the described embodiments are only a part of the preferred embodiments of the present application, not all embodiments. Those skilled in the art can make similar modifications without departing from the connotation of the present application, so the present application is not limited by the specific embodiments disclosed below.

[0029] The present application provides a kind of unmanned aerial vehicle landing omnidirectional capture device (as shown in Figure 1 , 3 , 4, 8 and 9), including landing plate 1, it is provided with one omnidirectional hollow guide cover 2 on the landing plate 1, the inner side wall of the omnidirectional hollow guide cover 2 is in the inclined state of bottom inward upper part outward. The omnidirectional hollow guide cover 2 is used to realize the vertical landing capture of unmanned aerial vehicle 4, in actual application, when unmanned aerial vehicle 4 performs a flight task and is positioned to a certain height above the omnidirectional hollow guide cover 2, then unmanned aerial vehicle 4 starts vertical landing, with the continuous descent of unmanned aerial vehicle above the landing plate 1, when the bottom of unmanned aerial vehicle 4 corresponds with the inclined side wall of the omnidirectional hollow guide cover 2 and contacts, with the continuous landing of unmanned aerial vehicle 4, the unmanned aerial vehicle 4 can be moved to the central region of the landing plate 1 under the guidance of the inclined side wall, and then finally the precise landing of the unmanned aerial vehicle 4 on the landing plate 1 can be realized. The inclined inner side wall of the omnidirectional hollow guide cover 2 is distributed in 360 degrees on the landing plate 1 in a closed manner, in the process of landing the unmanned aerial vehicle 4 to the landing plate 1, without adjusting the capture direction of the landing plate 1, no matter which direction the belly of the unmanned aerial vehicle 4 faces, the inclined inner side wall can realize the landing guidance of the unmanned aerial vehicle 4, and then the vertical landing operation of the unmanned aerial vehicle 4 is more simple.

[0030] The initial positioning of the UAV 4 above the landing plate 1 can be achieved by using the existing GPS method. After the UAV 4 completes the initial positioning, the final precise landing of the UAV 4 on the landing plate 1 can be achieved by using the existing infrared visual recognition positioning method or image recognition positioning technology. In this specific embodiment, the UAV 4 uses image recognition positioning technology to assist in achieving precise landing on the landing plate 1. Specifically, the landing optical recognition pattern 11 is arranged on the landing plate 1, and the omnidirectional hollow guide cover 2 is located at the periphery of the landing optical recognition pattern 11. The guidance of the landing optical recognition pattern 11 makes the UAV 4 more accurately land above the omnidirectional hollow guide cover 2 during the further landing process. During the landing process of the UAV 4 above the landing plate 1, the UAV recognizes the landing optical recognition pattern 11, analyzes the pattern, and adjusts the flight attitude according to the analysis result. Through the continuous positioning and navigation of the landing optical recognition pattern 11, the UAV can finally achieve precise navigation and landing. In actual application, the landing optical recognition pattern 11 can be composed of different color patterns or different two-dimensional code patterns. When different color patterns are used to compose the landing optical recognition pattern 11, the areas of different color patterns are also different. The landing optical recognition pattern 11 uses different color patterns and the sizes of the color pattern areas to achieve precise navigation. When different two-dimensional code patterns are used to compose the landing optical recognition pattern 11, the areas of different two-dimensional code patterns are also different. The landing optical recognition pattern 11 uses different sizes of two-dimensional code patterns to achieve precise navigation.

[0031] To facilitate the implementation of the endurance charging of the UAV 4, a charging interface 3 can be arranged in the middle of the landing plate 1. The charging interface 3 is divided into a charging negative pole 31 and a charging positive pole 32. The charging negative pole 31 is assembled by a plurality of spring pins and arranged in a ring shape. The charging positive pole 32 is assembled by a plurality of spring pins and arranged in a circular shape. On the landing plate 1, the circular charging positive pole 32 is arranged in the middle area of the landing plate 1, and the ring-shaped charging negative pole 31 is arranged at the periphery of the charging positive pole 21.

[0032] To facilitate the processing, assembly and disassembly of the landing plate 1 and the omnidirectional hollow guide cover 2, the landing plate 1 and the omnidirectional hollow guide cover 2 are fixedly connected in a detachable manner. For example, the landing plate 1 and the omnidirectional hollow guide cover 2 are connected in a plug-in manner. Specifically, a plurality of insertion holes are arranged on the landing plate 1, and a plurality of insertion rods corresponding to the insertion holes are arranged at the bottom of the omnidirectional hollow guide cover 2. The insertion rods are stably inserted into the corresponding insertion holes, thereby achieving the quick installation and fixation of the omnidirectional hollow guide cover 2 on the landing plate 1.

[0033] To further improve the processing and portability of the landing plate 1, the landing plate 1 can be circular, and is composed of a circular plate and a plurality of first splicing plates. Specifically, the landing plate 1 is composed of a circular plate 12 and four sector plates 13. Adjacent two sector plates 13 are fixedly connected by clamping. The circular plate 12 and the sector plates 13 are also fixedly connected by clamping. The charging interface 3 is arranged on the circular plate 12.

[0034] In order to further improve the processing and convenient carrying of the omnibearing hollow guide cover 2, the omnibearing hollow guide cover 2 can be composed of a plurality of second splicing plates, the plurality of second splicing plates are fixedly connected in a detachable manner, the omnibearing hollow guide cover 2 can be processed into a circular ring shape, when the omnibearing hollow guide cover 2 is processed into a circular ring shape, the omnibearing hollow guide cover 2 can be sequentially spliced by a plurality of arc-shaped plates, adjacent arc-shaped plates are fixedly connected in a plug-in connection manner, and meanwhile, the lower part of the arc-shaped plate can also be fixedly connected with the landing plate 1 in a plug-in connection manner; when the hollow guide cover 2 is assembled by using the plurality of arc-shaped plates, the outer edges of the plurality of arc-shaped plates which are sequentially butted on the inner side of the bottom form a circular limiting boundary, in order to ensure that the unmanned aerial vehicle 4 can finally land on the landing plate 1, the diameter of the circular limiting boundary needs to be slightly larger than the distance between the two outermost sides of the wings of the unmanned aerial vehicle 4; in the landing process of the unmanned aerial vehicle 4, the outermost sides of the wings are guided by the inner side walls of the arc-shaped plates, and finally the unmanned aerial vehicle 4 is positioned and landed within the circular limiting boundary; because the inner side wall of the arc-shaped plate is a smooth arc surface, in the process that the outermost sides of the wings slide downward along the arc surface of the arc-shaped plate, the arc surface of the arc-shaped plate cannot accurately realize the rotation limiting of the outermost sides of the wings in the horizontal plane; in the process that the unmanned aerial vehicle 4 is guided to descend by the arc-shaped plate, if the wings rotate to a certain extent, although the unmanned aerial vehicle 4 can successfully land on the landing plate 1, there is a possibility that the charging socket of the unmanned aerial vehicle 4 cannot be accurately butted with the charging interface 3 on the landing plate 1 due to the rotation of the unmanned aerial vehicle 3, and then the subsequent automatic charging function of the unmanned aerial vehicle 4 cannot be realized; in order to overcome the problem that the omnibearing hollow guide cover 2 has low landing capturing and guiding accuracy, the omnibearing hollow guide cover 2 is processed into a hollow regular polygonal deformation, the omnibearing hollow guide cover 2 is sequentially spliced by a plurality of plates, adjacent plates are fixedly connected in a plug-in connection manner, meanwhile, the lower part of the plate also realizes fixed connection with the landing plate 1 in a plug-in connection manner, and the inner side of the lower part of the plurality of plates forms a regular polygonal limiting boundary after the boundaries of the plurality of plates are sequentially butted at the tail; the diagonal length of the regular polygonal limiting boundary is equal to or slightly larger than the distance between the outer sides of the two wings of the unmanned aerial vehicle 4; when the unmanned aerial vehicle 4 is guided to land by the hollow guide cover 2 of the regular polygon, the unmanned aerial vehicle 4 adjusts its crosswind vertical landing attitude according to the guiding information of the landing optical recognition pattern 11 on the landing plate 1, so that the distribution direction of the two wings of the unmanned aerial vehicle 4 is vertically coincident with the diagonal direction of the closest polygonal limiting boundary, and then slow landing can be performed; when the outermost sides of the wings land at the butting boundary of two adjacent plates, the two adjacent plates of the outermost sides of the wings have a rotation limiting function for the wings, and then the unmanned aerial vehicle 4 can only slide downward along the butting boundary of the two plates during the landing of the wings.During the process of sliding down, the unmanned aerial vehicle 4 is limited to rotate, so as to improve the landing positioning accuracy of the unmanned aerial vehicle 4, and the improved landing positioning accuracy of the unmanned aerial vehicle 4 is beneficial to realize the precise butt joint of the charging port of the unmanned aerial vehicle 4 and the charging interface 3 on the landing plate 1. In actual application, the omnibearing hollow guide cover 2 can be processed into a hollow hexagonal shape or a hollow octagonal shape.

[0035] When the unmanned aerial vehicle 4 does not perform a flight task, in order to facilitate the storage of the unmanned aerial vehicle, the device further comprises a box body 5, the landing plate 1 is arranged inside the box body 5, and a box cover is arranged above the box body 5. The box cover can be a rotary split cover or a translational split cover. When the box cover is a rotary split cover, two rotary doors 52 are arranged, the outer sides of the two rotary doors 52 are hingedly connected to the upper outer side of the box body 5, the rotary door 52 is realized by a linear reciprocating motion execution assembly 53 and a damping support rod 54, and the rotary door 52 is hingedly connected to one end of the linear reciprocating motion execution assembly 53 and the side wall of the box body 5. The other end of the linear reciprocating motion execution assembly 53 is hingedly connected to the side wall of the box body 5. The other end of the damping support rod 54 is hingedly connected to the rotary door 52. The other end of the damping support rod 54 is hingedly connected to the side wall of the box body 5. The synchronous extension and contraction of the two electric push rods realizes the rotary split or closure of the two rotary doors 52. When the box cover is a translational split cover, two translational doors 51 are arranged, the two translational doors 51 are symmetrically arranged on the upper part of the box body 5, and each translational door 51 can be driven by an electric push rod or a synchronous belt to realize translation. The relative moving away of the two translational doors 51 realizes the opening of the upper part of the box body 5, and the relative moving close of the two translational doors 51 realizes the closing of the upper part of the box body 5. When the unmanned aerial vehicle 4 needs to perform a flight task, first, the box cover is opened, then the unmanned aerial vehicle 4 flies, and after the unmanned aerial vehicle 4 is recovered and landed in the box body 5, the box cover is closed, and then the unmanned aerial vehicle 4 recovery operation can be completed. When the unmanned aerial vehicle 4 is stored in the box body 5, in order to realize the on-duty charging function of the unmanned aerial vehicle 4, an automatic charging device can be arranged in the box body 5, the automatic charging device is connected to the charging interface 3 on the landing plate 1, and when the unmanned aerial vehicle 4 is automatically landed on the landing plate 1, the charging port on the unmanned aerial vehicle is connected to the charging interface 3 on the landing plate 1. When the unmanned aerial vehicle needs to be charged, the automatic charging device automatically charges the unmanned aerial vehicle 4.

[0036] When the unmanned aerial vehicle 4 is used for field investigation, in order to meet the long-time continuous flight task in the field, the utility model provides a honeycomb type unmanned aerial vehicle base station, the base station comprises at least one set of the unmanned aerial vehicle landing omnibearing capturing device, the honeycomb type unmanned aerial vehicle base station further comprises a honeycomb type box body 6, a plurality of landing plates 1 are sequentially and spacedly arranged in the honeycomb type box body 6, and a switch door is arranged on the upper part of the honeycomb type box body 6. Through the intermittent and continuous work of a plurality of unmanned aerial vehicles, the long-time continuous flight task in the field is realized.

[0037] In order to further improve the application maneuverability of the unmanned aerial vehicle, and to quickly reach the designated flight area, the honeycomb box 6 is arranged on a motor vehicle 7, and the motor vehicle 7 is used to transport the unmanned aerial vehicle to the designated flight area.

[0038] In the utility model, "upper", "lower", "front", "rear", "left" and "right" are relative positions for the convenience of describing the positional relationship, and therefore cannot be understood as absolute positions for limiting the protection scope.

[0039] In addition to the technical features described in the specification, they are known to those skilled in the art.

[0040] The preferred embodiments and examples of the utility model are described in detail above in combination with the drawings, but the utility model is not limited to the above-mentioned embodiments and examples, and those of ordinary skill in the art can make several improvements and modifications without departing from the concept of the utility model, and these improvements and modifications should also be regarded as the protection scope of the utility model.

Claims

1. A drone landing omnidirectional capture device, comprising a landing plate, characterized in that, The landing plate is provided with a full-direction hollow guide cover, and the inner side wall of the full-direction hollow guide cover is in an inclined state with the bottom inward and the upper part outward.

2. The all-directional capturing device for drone landing according to claim 1, characterized in that, A charging interface is arranged in the middle of the landing plate.

3. The all-directional capturing device for drone landing according to claim 2, characterized in that, The landing plate and the full-direction hollow guide cover are fixedly connected in a detachable manner.

4. The all-directional capturing device for drone landing according to claim 3, characterized in that, The landing plate comprises a circular plate and a plurality of first splicing plates, the first splicing plates are sequentially and end-to-end spliced around the circumferential direction of the circular plate, and the charging interface is arranged on the circular plate.

5. The all-directional capturing device for drone landing according to claim 3 or 4, characterized in that, The full-direction hollow guide cover comprises a plurality of second splicing plates, and the second splicing plates are fixedly connected in a detachable manner.

6. The all-directional capturing device for drone landing according to claim 5, characterized in that, The full-direction hollow guide cover is in a circular shape or a regular even polygon.

7. The all-directional capturing device for drone landing according to claim 6, characterized in that, The capturing device further comprises a box body, the landing plate is arranged in the box body, and a box cover is arranged above the box body.

8. The all-directional capturing device for drone landing according to claim 7, characterized in that, The box cover is a rotating split cover or a translating split cover.

9. A cellular drone base station, characterized by, The honeycomb unmanned aerial vehicle base station further comprises a honeycomb box body, and a plurality of landing plates are sequentially and spacedly arranged in the honeycomb box body.

10. The cellular drone base station of claim 9, wherein, The honeycomb box body is arranged on the motor vehicle. The motor vehicle is further provided with the honeycomb box body.

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