CN212099386U

CN212099386U - Unmanned aerial vehicle's descending platform

Info

Publication number: CN212099386U
Application number: CN202020647238.4U
Authority: CN
Inventors: 郑碧霞
Original assignee: Individual
Current assignee: Individual
Priority date: 2020-04-24
Filing date: 2020-04-24
Publication date: 2020-12-08
Anticipated expiration: 2030-04-24

Abstract

The utility model discloses an unmanned aerial vehicle's descending platform, including box, spring post, cavity board, apron, electro-magnet, iron plate, lamp strip, locator, electric liquid push rod, fretwork hole, stabilizer blade, pattern instruction district and handle. The utility model discloses contain ejection mechanism, unmanned aerial vehicle is when launching, under the effect of the electro-hydraulic push rod of ejection mechanism and electro-magnet, can make the shrink of spring post, after the spring post shrinks to the maximum, the switch of electro-magnet is closed this moment, electro-magnet and iron plate separation this moment, the spring of spring post resets, upwards produces elasticity, and then can bounce unmanned aerial vehicle, be favorable to reducing the consumption when unmanned aerial vehicle launches, be favorable to unmanned aerial vehicle's transmission; the utility model discloses an install locator and lamp strip in the cavity inboard, the locator is favorable to returning to the launching position that unmanned aerial vehicle is accurate, and the lamp strip is favorable to illuminating the pattern instruction area on the apron, the accurate discernment descending position of unmanned aerial vehicle at night of being convenient for, and device simple structure, use are comparatively convenient.

Description

Unmanned aerial vehicle's descending platform

Technical Field

The utility model relates to an unmanned aerial vehicle's descending platform specifically is an unmanned aerial vehicle's descending platform, belongs to unmanned aerial vehicle auxiliary assembly application technical field.

Background

An unmanned plane, called unmanned plane for short, is an unmanned plane operated by a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by a vehicle-mounted computer, and is widely applied to the fields of aerial photography, agriculture, plant protection, miniature self-shooting, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, electric inspection, disaster relief, film and television shooting, romantic manufacturing and the like.

The landing platform of the existing unmanned aerial vehicle is mostly a simple cushion or a block of board, and mainly aims to avoid collision of the unmanned aerial vehicle with the roof when landing, so that the function is single, the unmanned aerial vehicle cannot be easily identified when used at night, the unmanned aerial vehicle cannot be subjected to auxiliary launching, the power consumption is high when the unmanned aerial vehicle launches, and certain defects exist. Therefore, provide a landing platform of unmanned aerial vehicle to above-mentioned problem.

SUMMERY OF THE UTILITY MODEL

The utility model aims at providing an unmanned aerial vehicle's descending platform just in order to solve above-mentioned problem.

The utility model discloses a technical scheme realizes above-mentioned purpose, an unmanned aerial vehicle's landing platform, including box, spring post, cavity board, apron, lamp strip, locator and ejection mechanism, the central department of box roof top surface opens there is the fretwork hole, four corners of box roof top surface are vertically installed the spring post, and four the top of spring post is installed in four corners of cavity board bottom surface, the apron is installed at the top of cavity board, the central department of apron top surface is equipped with the pattern instruction district, the top surface of cavity board bottom plate is installed lamp strip and locator in proper order, the ejection mechanism is installed on box and cavity board;

the ejection mechanism comprises an electromagnet, an iron block and an electro-hydraulic push rod, the electro-hydraulic push rod is vertically installed at the center of the top surface of the bottom plate of the box body, the electromagnet is installed at the top end of the electro-hydraulic push rod, and the iron block is fixedly installed at the center of the bottom surface of the cavity plate.

Preferably, the outer walls of the two side plates corresponding to each other of the box body are fixedly connected with handles, and the outer walls of the handles are wrapped with anti-skidding sleeves.

Preferably, the top surface of the pattern indication area of the cover plate is painted with an H-shaped character.

Preferably, the four corners of the bottom surface of the box bottom plate are provided with support legs, and the bottom surfaces of the support legs are attached with wear-resistant anti-slip pads.

Preferably, the spring post comprises a barrel, a post body and a spring, the bottom end of the post body is sleeved in the barrel, the spring is installed in the barrel, and two ends of the spring are respectively connected with the bottom end of the post body and a bottom plate of the barrel.

Preferably, the box body is an aluminum alloy box body, and a plurality of hollowed-out drain holes are formed in a bottom plate of the box body.

The utility model has the advantages that:

1. the utility model discloses contain ejection mechanism, unmanned aerial vehicle is when launching, under the effect of the electro-hydraulic push rod of ejection mechanism and electro-magnet, can make the shrink of spring post, after the spring post shrinks to the maximum, the switch of electro-magnet is closed this moment, electro-magnet and iron plate separation this moment, the spring of spring post resets, upwards produces elasticity, and then can bounce unmanned aerial vehicle, be favorable to reducing the consumption when unmanned aerial vehicle launches, be favorable to unmanned aerial vehicle's transmission;

2. the utility model discloses an install locator and lamp strip in the cavity inboard, the locator is favorable to returning to the launching position that unmanned aerial vehicle is accurate, and the lamp strip is favorable to illuminating the pattern instruction area on the apron, the accurate discernment descending position of unmanned aerial vehicle at night of being convenient for, and during unmanned aerial vehicle descended, the spring of spring post was slightly compressed, was favorable to cushioning the impact force that unmanned aerial vehicle descending produced, and the unmanned aerial vehicle's of being convenient for descending, device simple structure, it is comparatively convenient to use.

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings needed to be used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without inventive exercise.

FIG. 1 is a perspective view of the present invention;

FIG. 2 is a front view of the present invention;

fig. 3 is a schematic view of the internal structure of the present invention.

In the figure: 1. the box, 2, spring post, 3, cavity board, 4, apron, 5, electro-magnet, 6, iron plate, 7, lamp strip, 8, locator, 9, electric liquid push rod, 10, fretwork hole, 11, stabilizer blade, 12, pattern indication area, 13, handle.

Detailed Description

In order to make the objects, features and advantages of the present invention more obvious and understandable, the drawings in the embodiments of the present invention are combined below to clearly and completely describe the technical solutions in the embodiments of the present invention, and obviously, the embodiments described below are only some embodiments of the present invention, but not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts belong to the protection scope of the present invention.

The technical solution of the present invention is further explained by the following embodiments with reference to the accompanying drawings.

In the description of the present invention, it is to be understood that the terms "upper", "lower", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description and simplicity of description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore should not be construed as limiting the present invention.

Referring to fig. 1-3, an unmanned aerial vehicle landing platform comprises a box body 1, spring columns 2, a cavity plate 3, a cover plate 4, a light bar 7, a positioner 8 and an ejection mechanism, wherein a hollow hole 10 is formed in the center of the top surface of a top plate of the box body 1, the spring columns 2 are vertically installed at four corners of the top surface of the top plate of the box body 1, the top ends of the four spring columns 2 are installed at four corners of the bottom surface of the cavity plate 3, the cover plate 4 is installed at the top of the cavity plate 3, a pattern indication area 12 is arranged at the center of the top surface of the cover plate 4, the light bar 7 and the positioner 8 are sequentially installed on the top surface of a bottom plate of the cavity plate 3, and the ejection mechanism is installed on the box body 1;

the ejection mechanism comprises an electromagnet 5, an iron block 6 and an electro-hydraulic push rod 9, wherein the electro-hydraulic push rod 9 is vertically installed at the center of the top surface of the bottom plate of the box body 1, the electromagnet 5 is installed at the top end of the electro-hydraulic push rod 9, and the iron block 6 is fixedly installed at the center of the bottom surface of the cavity plate 3.

The outer walls of the two corresponding side plates of the box body 1 are fixedly connected with handles 13, and the outer walls of the handles 13 are wrapped with anti-skidding sleeves; the top surface of the pattern indication area 12 of the cover plate 4 is coated with an H-shaped pattern, and the cover plate 4 coated with the H-shaped pattern is made of transparent materials, so that the light bar 7 can conveniently illuminate the pattern indication area 12 at night; supporting legs 11 are arranged at four corners of the bottom surface of the bottom plate of the box body 1, and wear-resistant anti-slip pads are attached to the bottom surfaces of the supporting legs 11; the spring column 2 is composed of a cylinder body, a cylinder body and a spring, the bottom end of the cylinder body is sleeved in the cylinder body, the spring is installed in the cylinder body, and two ends of the spring are respectively connected with the bottom end of the cylinder body and a bottom plate of the cylinder body; the box body 1 is an aluminum alloy box body, and a plurality of hollowed-out drain holes are formed in a bottom plate of the box body 1.

When the utility model is used, the electric elements appearing in the application are externally connected with a power supply and a control switch when in use, when the device is used, the device is placed on the roof, the device comprises an ejection mechanism, when the unmanned aerial vehicle is launched, the electro-hydraulic push rod 9 is extended through the control switch until the electromagnet 5 at the top end of the electro-hydraulic push rod 9 is contacted with the iron block 6 at the bottom surface of the cavity plate 3, then the electromagnet 5 works, at the moment, the electromagnet 5 generates magnetic force to be adsorbed with the iron block 6, then the electro-hydraulic push rod 9 is contracted, the spring post 2 is contracted when the electro-hydraulic push rod 9 is contracted, after the spring post 2 is contracted to the maximum degree, the switch of the electromagnet 5 is closed, at the moment, the magnetic force of the electromagnet 5 disappears, the electromagnet 5 is separated from the iron block 6, after the electromagnet 5 is separated from the iron block 6, the spring of the spring post 2 is reset, the consumption when being favorable to reducing unmanned aerial vehicle transmission, be favorable to unmanned aerial vehicle's transmission, install locator 8 and lamp strip 7 in the cavity board 3 of device, locator 8 is favorable to returning to the transmission position that unmanned aerial vehicle is accurate, lamp strip 7 is favorable to illuminating pattern instruction district 12 on the apron 4, the accurate discernment descending position of unmanned aerial vehicle at night of being convenient for, when unmanned aerial vehicle descends, the spring of spring post 2 is slightly compressed, be favorable to cushioning the impact force that unmanned aerial vehicle descended and produce, unmanned aerial vehicle's descending of being convenient for, device simple structure, it is comparatively convenient to use.

It is well within the skill of those in the art to implement, without undue experimentation, the present invention does not relate to software and process improvements, as related to circuits and electronic components and modules.

It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention 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.

The above embodiments are only used to illustrate the technical solution of the present invention, and not to limit the same; although the present invention has been described in detail with reference to the foregoing embodiments, it should be understood by those skilled in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some technical features may be equivalently replaced; such modifications and substitutions do not depart from the spirit and scope of the present invention in its corresponding aspects.

Claims

1. The utility model provides an unmanned aerial vehicle's descending platform which characterized in that: the ejection device comprises a box body (1), spring columns (2), a cavity plate (3), a cover plate (4), a lamp strip (7), a positioner (8) and an ejection mechanism, wherein hollow holes (10) are formed in the center of the top surface of a top plate of the box body (1), the spring columns (2) are vertically installed at four corners of the top surface of the top plate of the box body (1), the top ends of the four spring columns (2) are installed at the four corners of the bottom surface of the cavity plate (3), the cover plate (4) is installed at the top of the cavity plate (3), a pattern indication area (12) is arranged at the center of the top surface of the cover plate (4), the lamp strip (7) and the positioner (8) are sequentially installed on the top surface of a bottom plate of the cavity plate (3), and the ejection mechanism is installed on the box body (1;

the ejection mechanism comprises an electromagnet (5), an iron block (6) and an electro-hydraulic push rod (9), wherein the electro-hydraulic push rod (9) is vertically installed at the center of the top surface of the bottom plate of the box body (1), the electromagnet (5) is installed at the top end of the electro-hydraulic push rod (9), and the iron block (6) is fixedly installed at the center of the bottom surface of the cavity plate (3).

2. A landing platform for unmanned aerial vehicles according to claim 1, wherein: the outer walls of the two side plates corresponding to each other of the box body (1) are fixedly connected with handles (13), and the outer walls of the handles (13) are coated with anti-skidding sleeves.

3. A landing platform for unmanned aerial vehicles according to claim 1, wherein: the top surface of the pattern indication area (12) of the cover plate (4) is brushed with H-shaped characters.

4. A landing platform for unmanned aerial vehicles according to claim 1, wherein: supporting legs (11) are installed at four corners of the bottom surface of the bottom plate of the box body (1), and wear-resistant anti-slip pads are attached to the bottom surfaces of the supporting legs (11).

5. A landing platform for unmanned aerial vehicles according to claim 1, wherein: the spring column (2) is composed of a cylinder body, a cylinder body and a spring, the bottom end of the cylinder body is sleeved in the cylinder body, the spring is installed in the cylinder body, and the two ends of the spring are respectively connected with the bottom end of the cylinder body and the bottom plate of the cylinder body.

6. A landing platform for unmanned aerial vehicles according to claim 1, wherein: the box body (1) is an aluminum alloy box body, and a plurality of hollowed-out drain holes are formed in a bottom plate of the box body (1).