CN210149547U

CN210149547U - Unmanned aerial vehicle bearing structure that rises and falls

Info

Publication number: CN210149547U
Application number: CN201921178914.1U
Authority: CN
Inventors: 范帅; 闻永俊; 吴金凤; 茆先亮; 安康
Original assignee: Jiangsu Xinbo Construction Project Management Co Ltd
Current assignee: Jiangsu Xinbo Construction Project Management Co Ltd
Priority date: 2019-07-24
Filing date: 2019-07-24
Publication date: 2020-03-17
Anticipated expiration: 2029-07-24

Abstract

The utility model discloses an unmanned aerial vehicle bearing structure that rises and falls, including backup pad and unmanned aerial vehicle body, two flutings have been seted up to the bottom both sides of unmanned aerial vehicle body, and the mounting groove has all been seted up to two grooved both sides cell walls, and the equal fixed mounting in tank bottom of four mounting grooves has electric telescopic handle, and the top middle part fixed mounting of backup pad has the bottom suspension dagger, and the top of bottom suspension dagger is seted up flutedly, and the bottom fixed mounting of the cell wall of recess has two first springs, and the equal fixed mounting in top of two first springs is in the bottom of limiting plate, and the top both sides of limiting plate. The utility model relates to an unmanned aerial vehicle bearing structure that rises and falls through two sets of springs of installation between upper prop and lower prop, can effectively reduce the vibrations when unmanned aerial vehicle falls to the ground, can effectively protect the inside device of unmanned aerial vehicle, has guaranteed unmanned aerial vehicle's permanent use.

Description

Unmanned aerial vehicle bearing structure that rises and falls

Technical Field

The utility model relates to a bearing structure, in particular to unmanned aerial vehicle bearing structure that rises and falls.

Background

An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.

The existing unmanned aerial vehicle lifting support structure can only take off and land on the ground due to the fact that the bottom of the existing unmanned aerial vehicle lifting support structure is provided with the metal chassis, and the existing unmanned aerial vehicle lifting support structure cannot meet the requirements of users; the existing unmanned aerial vehicle lifting support structure has the advantages that the vibration is large when the existing unmanned aerial vehicle falls to the ground, so that the devices inside the unmanned aerial vehicle are easily damaged, and the service life of the unmanned aerial vehicle is greatly shortened.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an unmanned aerial vehicle bearing structure that rises and falls to current unmanned aerial vehicle bearing structure that rises and falls who proposes in solving above-mentioned background art, because it shakes greatly when falling to the ground, damages the inside device of unmanned aerial vehicle very easily, has reduced unmanned aerial vehicle's life's problem greatly.

In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle lifting support structure comprises a support plate and an unmanned aerial vehicle body, wherein two grooves are formed in two sides of the bottom end of the unmanned aerial vehicle body, two grooves are formed in two side groove walls of the grooves, electric telescopic rods are fixedly mounted at the bottoms of the four grooves, a lower support column is fixedly mounted in the middle of the top end of the support plate, a groove is formed in the top end of the lower support column, two first springs are fixedly mounted at the bottom end of the groove wall of the groove, the top ends of the two first springs are fixedly mounted at the bottom end of a limiting plate, second springs are respectively fixedly mounted at two sides of the top end of the limiting plate, the top ends of the two second springs are respectively fixedly connected with the two side groove walls of the top end of the groove, an upper support column is fixedly mounted at the middle of the top end of the limiting plate, clamping grooves are formed, and the two clamping blocks are fixedly arranged at one ends of the two electric telescopic rods respectively.

As a preferred technical scheme of the utility model, the equidistance fixed mounting has a plurality of lug in the bottom avris of backup pad.

As an optimal technical scheme of the utility model, a plurality of the bottom of lug is all pasted and is equipped with the slipmat.

As an optimized technical scheme of the utility model, two the fixed cover in bottom of lower support column is equipped with the gasbag.

As a preferred technical scheme of the utility model, the battery jar has been seted up to unmanned aerial vehicle body shell's bottom, the inside fixed mounting of battery jar has the battery, one side fixed surface of unmanned aerial vehicle body shell installs electric telescopic handle control switch, four electric telescopic handle all passes through electric telescopic handle control switch and battery electric connection.

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

1. the anti-slip pad is attached to the bottom end of the bump, so that the friction force between the bump and the ground can be increased, and the vibration sense of the unmanned aerial vehicle when descending to contact the ground can be effectively reduced;

2. the unmanned aerial vehicle provided with the support structure can take off and land on the water surface through the air bag arranged at the bottom of the outer side of the lower support column, so that the practicability of the unmanned aerial vehicle is greatly improved;

3. through two sets of springs of installing between last pillar and lower pillar, vibrations when can effectively reducing unmanned aerial vehicle and falling to the ground can effectively protect the inside device of unmanned aerial vehicle, have guaranteed unmanned aerial vehicle's permanent use.

Drawings

FIG. 1 is a schematic structural view of the present invention;

FIG. 2 is a schematic view of a partial structure of the present invention;

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

In the figure: 1. a support plate; 2. a lower support pillar; 3. an upper support column; 4. an air bag; 5. an unmanned aerial vehicle body; 6. a bump; 7. a groove; 8. a first spring; 9. a limiting plate; 10. a second spring; 11. a card slot; 12. grooving; 13. mounting grooves; 14. an electric telescopic rod; 15. and (7) clamping blocks.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Referring to fig. 1-3, the utility model provides an unmanned aerial vehicle lifting support structure, which comprises a support plate 1 and an unmanned aerial vehicle body 5, two slots 12 are provided on both sides of the bottom end of the unmanned aerial vehicle body 5, mounting grooves 13 are provided on both side walls of the two slots 12, electric telescopic rods 14 are fixedly mounted on the bottoms of the four mounting grooves 13, a lower support post 2 is fixedly mounted on the middle portion of the top end of the support plate 1, a groove 7 is provided on the top end of the lower support post 2, two first springs 8 are fixedly mounted on the bottom end of the groove wall of the groove 7, the top ends of the two first springs 8 are fixedly mounted on the bottom end of a limit plate 9, second springs 10 are respectively fixedly mounted on both sides of the top end of the limit plate 9, the top ends of the two second springs 10 are respectively fixedly connected with both side walls of the top end of the groove 7, an upper support post, the inside of two draw-in grooves 11 all blocks and is connected with fixture block 15, and two fixture blocks 15 are fixed mounting respectively in the one end of two electric telescopic handle 14.

Preferably, the equal equidistance fixed mounting in bottom avris of backup pad 1 has a plurality of lug 6, and a plurality of lug 6 can make unmanned aerial vehicle more stable when ground is placed.

Preferably, the bottom of a plurality of lug 6 is all pasted and is equipped with the slipmat, can increase the frictional force on lug 6 and ground, and the sense of vibration when can also effectively reduce unmanned aerial vehicle decline contact ground.

Preferably, the fixed cover in bottom of two lower support columns 2 is equipped with gasbag 4, can make the unmanned aerial vehicle of this bearing structure of installation take off and land on the surface of water.

Preferably, the battery jar has been seted up to the bottom of 5 casings of unmanned aerial vehicle body, and the inside fixed mounting of battery jar has the battery, and one side fixed surface of 5 casings of unmanned aerial vehicle body installs electric telescopic handle control switch, and four electric telescopic handle 14 are all through electric telescopic handle control switch and battery electric connection.

When in specific use, the utility model relates to an unmanned aerial vehicle lifting support structure, when the unmanned aerial vehicle lifting support structure is used, firstly, the unmanned aerial vehicle support structure is arranged at the bottom end of the unmanned aerial vehicle, firstly, the top part of the upper support column 3 of the support structure is placed in the groove 12 at the bottom end of the unmanned aerial vehicle body 5, then the electric telescopic rod 14 is started through the electric telescopic rod control switch, then the electric telescopic rod 14 extends out to drive the clamping block 15, then the clamping block 15 is clamped and connected with the clamping groove 11 on the upper supporting column 3, then the electric telescopic rod 14 is closed through the electric telescopic rod control switch, after the unmanned aerial vehicle supporting structure is completed, the unmanned aerial vehicle is supported and descended, when the unmanned aerial vehicle descends, firstly, the convex block 6 contacts the ground, the non-slip mat arranged at the bottom end of the convex block 6 can reduce part of vibration, then the vibration is transmitted to the lower support column 2, and most of vibration can be effectively eliminated through the first spring 8 and the second spring 10; when taking off this unmanned aerial vehicle on the surface of water, directly place unmanned aerial vehicle on the surface of water, 4 buoyancy of utilizing water of gasbag can hold up whole unmanned aerial vehicle, and unmanned aerial vehicle descends at the surface of water after that, and gasbag 4 also can hold up unmanned aerial vehicle on the surface of water.

In the description of the present invention, it should be understood that the indicated orientation or positional relationship is based on the orientation or positional relationship shown in the drawings, and is only for convenience of description and simplification of description, and does not indicate or imply that the indicated device or element must have a particular orientation, be constructed and operated in a particular orientation, and thus should not be construed as limiting the present invention.

In the present invention, unless otherwise explicitly specified or limited, for example, it may be fixedly connected, detachably connected, or integrated; can be mechanically or electrically connected; they may be directly connected or indirectly connected through an intermediate medium, and may be connected through the inside of two elements or in an interaction relationship between two elements, unless otherwise specifically defined, and the specific meaning of the above terms in the present invention will be understood by those skilled in the art according to specific situations.

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

Claims

1. An unmanned aerial vehicle lifting support structure comprises a support plate (1) and an unmanned aerial vehicle body (5), and is characterized in that two grooves (12) are formed in two sides of the bottom end of the unmanned aerial vehicle body (5), mounting grooves (13) are formed in two side groove walls of the two grooves (12), electric telescopic rods (14) are fixedly mounted at bottoms of the four mounting grooves (13), a lower support column (2) is fixedly mounted in the middle of the top end of the support plate (1), a groove (7) is formed in the top end of the lower support column (2), two first springs (8) are fixedly mounted at the bottom end of the groove wall of the groove (7), the top ends of the two first springs (8) are fixedly mounted at the bottom end of a limiting plate (9), second springs (10) are fixedly mounted at two sides of the top end of the limiting plate (9) respectively, and the top ends of the two second springs (10) are fixedly connected with two side groove walls of the, middle part fixed mounting on limiting plate (9) top has last support column (3), draw-in groove (11), two have all been seted up to the both sides at last support column (3) top the equal block in inside of draw-in groove (11) is connected with fixture block (15), two fixture block (15) fixed mounting is in the one end of two electric telescopic handle (14) respectively.

2. An unmanned aerial vehicle landing and landing support structure according to claim 1, wherein: the equal equidistance fixed mounting of bottom avris of backup pad (1) has a plurality of lug (6).

3. An unmanned aerial vehicle landing and landing support structure according to claim 2, wherein: the bottom ends of the plurality of lugs (6) are all provided with anti-slip pads in an attached mode.

4. An unmanned aerial vehicle landing and landing support structure according to claim 1, wherein: and the bottom of the two lower supporting columns (2) is fixedly sleeved with an air bag (4).

5. An unmanned aerial vehicle landing and landing support structure according to claim 1, wherein: the battery jar has been seted up to the bottom of unmanned aerial vehicle body (5) casing, the inside fixed mounting of battery jar has the battery, one side fixed surface of unmanned aerial vehicle body (5) casing installs electric telescopic handle control switch, four electric telescopic handle (14) are all through electric telescopic handle control switch and battery electric connection.