CN218858701U - Unmanned aerial vehicle field take-off and landing platform - Google Patents

Unmanned aerial vehicle field take-off and landing platform Download PDF

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Publication number
CN218858701U
CN218858701U CN202222301314.8U CN202222301314U CN218858701U CN 218858701 U CN218858701 U CN 218858701U CN 202222301314 U CN202222301314 U CN 202222301314U CN 218858701 U CN218858701 U CN 218858701U
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China
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platform
sub
supporting
aerial vehicle
unmanned aerial
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Active
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CN202222301314.8U
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Chinese (zh)
Inventor
程纪
王朝军
方炯
韩冲
陈绍令
聂堃
赵志伟
蒋安荔
余俊
郭承涛
彭静
朱志强
谢本孝
关奉
康泉
李晴
张玉琳
王佳
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National Pipeline Network Group Sichuan to East Natural Gas Pipeline Co Ltd
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National Pipeline Network Group Sichuan to East Natural Gas Pipeline Co Ltd
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Priority to CN202222301314.8U priority Critical patent/CN218858701U/en
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/60Other road transportation technologies with climate change mitigation effect
    • Y02T10/70Energy storage systems for electromobility, e.g. batteries

Abstract

The utility model discloses an open-air platform that takes off and land of unmanned aerial vehicle, including brace table and support piece, support piece arranges subaerial in, the brace table is installed support piece's upper end, support piece is used for supporting the brace table is right the brace table leveling, the upper end of brace table is used for supplying unmanned aerial vehicle to descend, and so accessible support piece comes to support the brace table and the leveling to it is good to make the levelness of brace table upper end, and supply unmanned aerial vehicle that like this can be safe takes off and land.

Description

Unmanned aerial vehicle field take-off and landing platform
Technical Field
The utility model belongs to unmanned aerial vehicle equipment field especially relates to an open-air platform of taking off and land of unmanned aerial vehicle.
Background
At present, the small-size multi-propeller unmanned aerial vehicle of a large amount of configurations has been arranged in patrolling of long-distance pipeline of natural gas, but in hilly land, because the earth's surface is unsmooth, so unmanned aerial vehicle's take off and land is more difficult usually, especially can the automated inspection ground condition when present unmanned aerial vehicle descends, and the screw and aircraft itself can be damaged in the forced landing.
SUMMERY OF THE UTILITY MODEL
In order to solve the technical problem, the utility model aims to provide a simple structure, and can supply the platform of taking off and land of the open-air take off and land of unmanned aerial vehicle.
In order to realize the purpose, the technical scheme of the utility model is as follows: the utility model provides an unmanned aerial vehicle field platform of taking off and land, includes brace table and support piece, support piece arranges subaerial in, the brace table is installed support piece's upper end, support piece is used for supporting the brace table is right it is right to prop up the brace table leveling, the upper end of brace table is used for supplying unmanned aerial vehicle to descend.
The beneficial effects of the above technical scheme are that: so accessible support piece comes to support and the leveling to the brace table to make the levelness of brace table upper end good, supply unmanned aerial vehicle take off and land that like this can be safe.
In the technical scheme, the supporting platform is detachably connected with the supporting piece.
The beneficial effects of the above technical scheme are that: thus, the support table and the support member can be detached for carrying.
In the technical scheme, the supporting platform comprises two sub-platform bodies, one side of each sub-platform body is connected in a rotating mode, and the two sub-platform bodies can rotate to be unfolded and located on the same plane or rotate to be overlapped with each other to be stored.
The beneficial effects of the above technical scheme are that: through forming the supporting table by two sub-table bodies, and two sub-table bodies are connected in a rotating mode, the supporting table can be folded and stored, and therefore the occupied space of the supporting table is smaller.
In the technical scheme, the two sub-tables are in a groove shape, one side of the notch of each sub-table is rotatably connected, and when the two sub-tables are rotatably unfolded, the notches of the two sub-tables face downwards, the bottom walls of the two sub-tables are located in the same plane, or the two sub-tables are rotated to be stored, the notches of the two sub-tables are close to each other and enclose to form an inner hollow cavity.
The beneficial effects of the above technical scheme are that: through setting up the sub-stage body into the trough bodily form, make two brace tables be similar to the structure of case like this, supply to store the article in the cavity that forms is enclosed to two sub-stage bodies when it accomodates, the drawing support piece can all can be accommodated in the cavity with the receiver that holds unmanned aerial vehicle to make whole unmanned aerial vehicle field take off and land the platform and conveniently carry more.
In the technical scheme, the upper end of at least one of the sub-table bodies is embedded with a horizontal bubble.
The beneficial effects of the above technical scheme are that: therefore, the levelness of the two sub-tables can be conveniently observed when the two sub-tables are unfolded and installed on the supporting piece.
In the technical scheme, the sub-table bodies are rectangular grooves, the length of the long side of each sub-table body is twice that of the wide side of the sub-table body, and the long side of the groove of each sub-table body is connected in a rotating mode.
The beneficial effects of the above technical scheme are that: so make two sub-stage bodies expand the shape that the diapire of back two makes up into square, the unmanned aerial vehicle take off and land of being convenient for like this more.
In the technical scheme, the supporting piece comprises four supporting legs with adjustable lengths, each supporting leg comprises a sub-table body and is far away from the other sub-table body, two corners of the sub-table body are respectively provided with an installation hole with internal threads, each supporting leg is provided with external threads matched with the installation holes, and when the sub-table body is unfolded, the upper ends of the supporting legs correspond to the installation holes in a threaded connection mode.
The beneficial effects of the above technical scheme are that: the novel support leg is simple in structure, convenient to disassemble and assemble, and the length of the support leg is adjustable, so that the levelness of the support table can be flexibly adjusted.
In the technical scheme, the supporting leg comprises a rod body and a sleeve, the upper end of the rod body is provided with external threads matched with the mounting hole, the lower end of the rod body passes through the upper end of the sleeve and extends into the sleeve, and the lower end of the rod body extends into the sleeve and the length of the supporting leg is adjustable and can be adjusted.
The beneficial effects of the above technical scheme are that: therefore, the length of each supporting leg can be conveniently adjusted according to needs.
In the technical scheme, the upper end of the sleeve is also provided with a locking piece, and the locking piece locks the rod body on the sleeve.
The beneficial effects of the above technical scheme are that: so the body of rod locking that accessible retaining member will correspond on the sleeve, avoids when unmanned aerial vehicle takes off and land, because of unexpected condition leads to the body of rod to slide for the sleeve and influence the levelness of propping up supporting bench.
Among the above-mentioned technical scheme the retaining member is the bolt, be provided with on the lateral wall of sleeve upper end and run through the inside screw of sleeve, the retaining member with screw threaded connection screws up or unscrews the retaining member is in order to incite somebody to action the body of rod with sleeve locking or unclamp.
The beneficial effects of the above technical scheme are that: the structure is simple, and the locking is convenient.
Drawings
Fig. 1 is a schematic structural diagram of an unmanned aerial vehicle field take-off and landing platform according to embodiment 1 of the present invention;
fig. 2 is a state diagram of the supporting table according to embodiment 1 of the present invention when it is unfolded;
fig. 3 is a plan view of the support platform of embodiment 1 of the present invention when it is deployed;
fig. 4 is a state diagram of the supporting platform of embodiment 1 of the present invention when it is stored;
fig. 5 is a state diagram of the supporting table according to embodiment 2 of the present invention when the supporting table is unfolded;
fig. 6 is a state diagram of the supporting table according to embodiment 2 of the present invention when stored;
fig. 7 is a schematic view of the sub-platform body of the embodiment 2 of the present invention, which is provided with a handle.
In the figure: 1 support platform, 11 sub-platforms, 111 mounting holes, 12 hasps, 13 handles, 2 supports, 21 support legs, 211 rod bodies, 212 sleeves, 213 locking parts and 3 horizontal bubbles.
Detailed Description
The principles and features of the present invention are described below in conjunction with the following drawings, the examples given are only intended to illustrate the present invention and are not intended to limit the scope of the present invention. The invention is described in more detail in the following paragraphs by way of example with reference to the accompanying drawings. The advantages and features of the present invention will become more fully apparent from the following description and appended claims. It should be noted that the drawings are in simplified form and are not to precise scale, and are provided for convenience and clarity in order to facilitate the description of the embodiments of the present invention.
Example 1
As shown in fig. 1-4, this embodiment provides an unmanned aerial vehicle field take-off and landing platform, including brace table 1 and support piece 2, support piece 2 arranges in subaerial, brace table 1 installs support piece 2's upper end, support piece 2 is used for supporting brace table 1 and right brace table 1 leveling, brace table 1's upper end is used for supplying unmanned aerial vehicle to descend, and accessible support piece comes to support the brace table and the leveling like this to make the levelness of brace table upper end good, supply unmanned aerial vehicle take-off and landing that like this can be safe.
In the above technical solution, the supporting platform 1 and the supporting member 2 are detachably connected, so that the supporting platform and the supporting member can be detached to facilitate carrying.
Among the above-mentioned technical scheme support bench 1 includes two sub-stage bodies 11, two one side of sub-stage body 11 is rotated and is connected, two sub-stage body 11 can rotate to expand and be in the coplanar, or rotate to coincide each other in order to accomodate, constitute through propping up a supporting bench by two sub-stage bodies, and two sub-stage bodies rotate and connect, can make the brace table fold like this and accomodate to it is littleer to make its occupation space.
Among the above-mentioned technical scheme support piece 2 includes four length-adjustable supporting legs 21, and every another is kept away from to sub-stage body 11 two corners of sub-stage body 11 all are equipped with mounting hole 111 of taking internal screw thread, every the upper end of supporting leg 21 be equipped with mounting hole 111 matched with external screw thread is two when sub-stage body 11 expandes, the upper end of supporting leg 21 with correspond mounting hole 111 threaded connection, its simple structure, and easy dismounting, and the length of supporting leg is adjustable to the levelness of regulation brace table that can be nimble.
Among the above-mentioned technical scheme the supporting leg 21 includes the body of rod 211 and sleeve 212, the upper end of the body of rod 211 be equipped with mounting hole 111 matched with external screw thread, the lower extreme warp of the body of rod 211 the upper end of sleeve 212 stretches into in the sleeve 212, the lower extreme of the body of rod 211 stretches into length adjustable in the sleeve 212 is in order to adjust the length of supporting leg 21, so can be convenient adjust every as required the length of supporting leg.
In the above-mentioned technical scheme the upper end of sleeve 212 still is equipped with retaining member 213, retaining member 213 is in order to incite somebody to action the body of rod 211 locking is in on the sleeve 212, so accessible retaining member will correspond the body of rod locking on the sleeve, avoid when unmanned aerial vehicle takes off and land, lead to the body of rod to slide for the sleeve and influence the levelness of propping up the platform because of unexpected circumstances.
Among the above-mentioned technical scheme retaining member 213 is the bolt (can adopt butterfly bolt or plum blossom handle bolt, and its locking principle is similar to the last tightening bolt of slide caliper), be provided with on the lateral wall of sleeve 212 upper end and run through the inside screw of sleeve 212, retaining member 213 with screw threaded connection screws up or unscrews retaining member 213 is in order to incite somebody to action the body of rod 211 with sleeve 212 locking or loosening, its simple structure, and locking is convenient.
The length of the sub-stage body may be 1m, and the width thereof may be 0.5m.
At least one among the above-mentioned technical scheme the upper end of the sub-stage body 11 is inlayed and is equipped with a spirit bubble 3, the levelness of two sub-stage bodies of observation when so can be convenient expandes and install on support piece, because unmanned aerial vehicle is not very high to the levelness requirement of the platform of taking off and land (not required absolute level, it can to be close to the level), after the completion is built to the open-air platform of taking off and land of whole unmanned aerial vehicle, the levelness of propping up the platform through the visual observation accords with unmanned aerial vehicle's the take off and land can (certainly for the insurance sake, can adjust the length of supporting leg so that the levelness of propping up the platform improves with the help of the spirit bubble).
In this embodiment the open-air platform of taking off and land of unmanned aerial vehicle can adopt a handbag to accomodate when accomodating (be similar to the portable computer package of a large-size to can accomodate four supporting legs and accomodate the brace table of hand and be good).
The unmanned aerial vehicle field take-off and landing platform is suitable for take-off and landing (and similar types) of a Dajiang imperial mi i type unmanned aerial vehicle.
Example 2
As shown in fig. 5 and fig. 6, the difference from embodiment 1 is that in the above technical solution, two of the sub-tables 11 are both in a trough shape, one side of the notches of the two sub-tables 11 is rotatably connected, when the two sub-tables 11 are rotatably unfolded, the notches of the two sub-tables 11 face downward, and the bottom walls of the two sub-tables are in the same plane, or when the two sub-tables 11 are rotated to be stored, the notches of the two sub-tables 11 are close to each other and enclose a hollow cavity inside, and by setting the sub-tables to be in a trough shape, the two support tables are similar to a box structure, when the two sub-tables are stored, objects are stored in the cavity enclosed by the two sub-tables, and the storage box of the support member, which can contain the unmanned aerial vehicle, can be contained in the cavity, so that the whole unmanned aerial vehicle lifting platform is more convenient to carry.
Among the above-mentioned technical scheme the secondary platform body 11 is the rectangular groove, and the length on its long limit is two times of its broadside length, two the long avris of 11 slots of secondary platform body department rotates to be connected, so makes the shape that two diapire after two secondary platform body expandes make up into square, the unmanned aerial vehicle take off and land of being convenient for more like this.
As shown in fig. 7, two buckles 12 may be disposed on a side of the sub-platform body away from the rotational connection between the sub-platform body and the base body, and two sub-platform bodies may be disposed on two male buckle elements and two female buckle elements, respectively, so that the two sub-platform bodies may be connected by the male buckle elements and the female buckle elements (which belong to a conventional technical means of a person skilled in the art, and are not described herein in detail), so that the two sub-platform bodies are locked on a side away from the rotational connection between the two sub-platform bodies, and a handle 13 (which may be a rotationally mounted n-shaped handle, and is known in the general knowledge of a person skilled in the art, and is not described herein in detail) may be further added on a side of any one of the sub-platform bodies away from the rotational connection between the sub-platform bodies, so that the two sub-platform bodies may be used as a suitcase while being stored, and the support legs may be placed in the suitcase after being detached, and in order to reduce the weight of the unmanned aerial vehicle landing platform, the sub-platform and the support legs may be made of the unmanned aerial vehicle.
Wherein, the groove depth of each sub-table body can be 2-10cm (the groove depth is preferably at least capable of satisfying that four supporting legs are accommodated in the suitcase after the sub-table bodies are accommodated).
It should be noted that the above detailed description is exemplary and is intended to provide further explanation of the disclosure. 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 application belongs.
It is noted that the terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of exemplary embodiments according to the present application. As used herein, the singular forms "a", "an", and "the" are intended to include the plural forms as well, and it should be understood that when the terms "comprises" and/or "comprising" are used in this specification, they specify the presence of stated features, steps, operations, devices, components, and/or combinations thereof, unless the context clearly indicates otherwise.
It should be noted that the terms "first," "second," and the like in the description and claims of this application and in the drawings described above are used for distinguishing between similar elements and not necessarily for describing a particular sequential or chronological order. It is to be understood that the terms so used are interchangeable under appropriate circumstances such that the embodiments of the application described herein are, for example, capable of operation in sequences other than those illustrated or otherwise described herein.
Also, when an element is referred to as being "secured to" another element, it can be directly on the other element or intervening elements may also be present. When an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present. The terms "vertical," "horizontal," "left," "right," and the like as used herein are for illustrative purposes only and do not represent the only embodiments.
Moreover, the terms "comprises," "comprising," and "having," and any variations thereof, are intended to cover a non-exclusive inclusion, such that a process, method, system, article, or apparatus that comprises a list of steps or elements is not necessarily limited to those steps or elements expressly listed, but may include other steps or elements not expressly listed or inherent to such process, method, article, or apparatus.
For ease of description, spatially relative terms, such as "on," "over," "on top of," "above," and the like, may be used herein to describe one device or feature's spatial relationship to another device or feature as illustrated in the figures. It will be understood that the spatially relative terms are intended to encompass different orientations of the device in use or operation in addition to the orientation depicted in the figures.
For example, if a device in the figures is turned over, devices described as "above" or "on" other devices or configurations would then be oriented "below" or "under" the other devices or configurations. Thus, the exemplary term "above" may include both an orientation of "above" and "below". The device may be otherwise variously oriented (rotated 90 degrees or at other orientations) and the spatially relative descriptors used herein interpreted accordingly.
The above description is only a preferred embodiment of the present invention, and is not intended to limit the present invention in any way; the present invention can be smoothly implemented by those skilled in the art according to the drawings and the above description; however, those skilled in the art should understand that the equivalent embodiments of the present invention are equivalent embodiments of the present invention, and that the changes, modifications and evolutions made by the above-disclosed technical contents are not departed from the technical scope of the present invention; meanwhile, any changes, modifications, evolutions, etc. of the above embodiments, which are equivalent to the actual techniques of the present invention, still belong to the protection scope of the technical solution of the present invention.

Claims (7)

1. The field take-off and landing platform of the unmanned aerial vehicle is characterized by comprising a supporting platform (1) and a supporting piece (2), wherein the supporting piece (2) is arranged on the ground, the supporting platform (1) is installed at the upper end of the supporting piece (2), the supporting piece (2) is used for supporting the supporting platform (1) and leveling the supporting platform (1), and the upper end of the supporting platform (1) is used for landing the unmanned aerial vehicle; the supporting platform (1) is detachably connected with the supporting piece (2); the supporting table (1) comprises two sub-table bodies (11), one sides of the two sub-table bodies (11) are rotatably connected, and the two sub-table bodies (11) can be rotated to be unfolded and positioned on the same plane or rotated to be mutually overlapped for storage; support piece (2) include four length adjustable supporting legs (21), and every other is kept away from in the stage body (11) two corners of the stage body (11) all are equipped with mounting hole (111) of taking the internal screw thread, every the upper end of supporting leg (21) be equipped with mounting hole (111) matched with external screw thread, two when the stage body (11) expand, the upper end of supporting leg (21) with correspond mounting hole (111) threaded connection.
2. The unmanned aerial vehicle field lifting platform of claim 1, wherein the two sub-platform bodies (11) are both trough-shaped, one side of the notches of the two sub-platform bodies (11) is rotatably connected, when the two sub-platform bodies (11) are rotatably unfolded, the notches of the two sub-platform bodies (11) are both downward, and the bottom walls of the two sub-platform bodies are in the same plane, or when the two sub-platform bodies (11) are rotated to be stored, the notches of the two sub-platform bodies (11) are close to each other and enclose to form a hollow cavity.
3. The unmanned aerial vehicle field lifting platform of claim 2, wherein the upper end of at least one of the sub-platform bodies (11) is embedded with a horizontal bubble (3).
4. The unmanned aerial vehicle field lifting platform of claim 2, wherein the sub-platform body (11) is a rectangular slot, the length of the long side of the sub-platform body is twice that of the wide side of the sub-platform body, and the long sides of the slot openings of the two sub-platform bodies (11) are rotatably connected.
5. The unmanned aerial vehicle field lifting platform of any one of claims 1-4, wherein the support leg (21) comprises a rod body (211) and a sleeve (212), the upper end of the rod body (211) is provided with an external thread matched with the mounting hole (111), the lower end of the rod body (211) extends into the sleeve (212) through the upper end of the sleeve (212), and the length of the lower end of the rod body (211) extending into the sleeve (212) is adjustable so as to adjust the length of the support leg (21).
6. The unmanned aerial vehicle field landing stage of claim 5, wherein the upper end of the sleeve (212) is further provided with a retaining member (213), and the retaining member (213) is used for locking the rod body (211) on the sleeve (212).
7. The unmanned aerial vehicle field lifting platform of claim 6, characterized in that retaining member (213) is the bolt, be provided with on the lateral wall of sleeve (212) upper end and run through the inside screw of sleeve (212), retaining member (213) with screw threaded connection screws up or unscrews retaining member (213) with body of rod (211) with sleeve (212) locking or unclamp.
CN202222301314.8U 2022-08-31 2022-08-31 Unmanned aerial vehicle field take-off and landing platform Active CN218858701U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202222301314.8U CN218858701U (en) 2022-08-31 2022-08-31 Unmanned aerial vehicle field take-off and landing platform

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202222301314.8U CN218858701U (en) 2022-08-31 2022-08-31 Unmanned aerial vehicle field take-off and landing platform

Publications (1)

Publication Number Publication Date
CN218858701U true CN218858701U (en) 2023-04-14

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