CN212354386U

CN212354386U - Pasture unmanned aerial vehicle support based on have buffer structure

Info

Publication number: CN212354386U
Application number: CN202021124721.0U
Authority: CN
Inventors: 马子寅; 张骋宇; 王斌; 田虎强; 韩丁; 娜茜泰
Original assignee: Inner Mongolia University
Current assignee: Inner Mongolia University
Priority date: 2020-06-17
Filing date: 2020-06-17
Publication date: 2021-01-15
Anticipated expiration: 2030-06-17

Abstract

The utility model relates to an unmanned aerial vehicle support technical field specifically is a pasturing unmanned aerial vehicle support based on have buffer structure, including support body and unmanned aerial vehicle body, the upside of support body is provided with the unmanned aerial vehicle body, both ends are articulated to have the landing leg about the support body downside, and the bottom of landing leg all is provided with the cushion, the front of landing leg all articulates there is first loop bar, and the upside of first loop bar sets up flutedly to vertical first spring that is connected with in the recess, the opening part of recess is provided with first inserted bar, and the inner of first inserted bar is connected with first spring end, the other end of first inserted bar is articulated mutually with the support body downside, the inboard of landing leg articulates there is the second inserted bar. The utility model discloses set up first inserted bar and second inserted bar, carry out fine protection to the bottom of unmanned aerial vehicle body, strengthen descending stability of in-process, through setting up swivel nut and screw rod, conveniently take out the unmanned aerial vehicle body from the device.

Description

Pasture unmanned aerial vehicle support based on have buffer structure

Technical Field

The utility model relates to an unmanned aerial vehicle support technical field specifically is a grazing unmanned aerial vehicle support based on have buffer structure.

Background

Unmanned aerial vehicle, be the unmanned aerial vehicle who utilizes radio remote control equipment and the program control device manipulation of self-contained, in-process that unmanned aerial vehicle flies need utilize the support to support unmanned aerial vehicle, but current unmanned aerial vehicle support does not carry out corresponding protection at the flight in-process, make the easy external impact of unmanned aerial vehicle bottom appear damaging, unmanned aerial vehicle's life is shorter, and stability is relatively poor when unmanned aerial vehicle descends, it is unsatisfactory to lead to the equilibrium, for this reason we have proposed a herding unmanned aerial vehicle support based on having buffer structure to solve above-mentioned problem.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a herd unmanned aerial vehicle support based on have buffer structure to the relatively poor problem of stability appears damaging and unmanned aerial vehicle descends when solving the easy external impact in the unmanned aerial vehicle bottom that provides among the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme: a pasturing unmanned aerial vehicle support based on a buffering structure comprises a support body and an unmanned aerial vehicle body, wherein the unmanned aerial vehicle body is arranged on the upper side of the support body, supporting legs are hinged to the left end and the right end of the lower side of the support body, cushion blocks are arranged at the bottom ends of the supporting legs, first sleeve rods are hinged to the front sides of the supporting legs, grooves are formed in the upper sides of the first sleeve rods, first springs are vertically connected into the grooves, first inserting rods are arranged at the openings of the grooves, the inner ends of the first inserting rods are connected with the ends of the first springs, the other ends of the first inserting rods are hinged to the lower side of the support body, second inserting rods are hinged to the inner sides of the supporting legs, one sides, close to each other, of the second inserting rods are connected through second springs, second sleeve rods are arranged on the inner sides of the supporting legs, grooves are formed in the sides, far away from, and a second insertion rod is transversely inserted into the opening of the groove, and one side of the second insertion rod, which is close to each other, is connected with the end head of the second spring.

Preferably, the inner wall fixed mounting of support body has the swivel nut, and the inside of swivel nut is inserted and is equipped with the screw rod, the opening has been seted up to the upside of support body, and the inboard of opening is provided with the connecting plate, the fixed slot with screw rod matched with has been seted up in the outside of connecting plate, the unmanned aerial vehicle body is installed to the upside of connecting plate.

Preferably, the rack body is of a circular structure, the connecting plate is of a circular structure, and the diameter of the outer side of the connecting plate is smaller than that of the inner side of the rack body.

Preferably, the screw rods are provided with four groups, the four groups of screw rods are in an annular array structure and are inserted into a fixing groove formed in the connecting plate, and one sides, far away from each other, of the screw rods are fixedly connected with rotating handles.

Preferably, the legs are arranged in an arc-shaped structure, and the convex surfaces of the legs face outwards.

Preferably, the cushion block is arranged to be a spherical structure, and a rubber pad is glued to the bottom end of the cushion block.

Compared with the prior art, the beneficial effects of the utility model are that: the utility model discloses a set up first inserted bar and second inserted bar, be convenient for carry out fine protection to the bottom of unmanned aerial vehicle body at the unmanned aerial vehicle body in flight process, reduce the loss that the striking brought, cushion impact force, reduce part dislocation and wearing and tearing vibration to increase of service life, when bringing convenience for people's use, reduce the maintenance to the unmanned aerial vehicle body, reinforcing economic benefits, can play the shock attenuation effect in the in-process of descending simultaneously, reinforcing the stability in the descending process;

through setting up swivel nut and screw rod, the person of facilitating the use realizes dismantling and installing the connecting plate through rotating the commentaries on classics handle that the screw rod outside is connected, conveniently takes out the unmanned aerial vehicle body from the device, and then has reduced the area of this device, and it is accomodate after the person of facilitating the use flight is accomplished.

Description of the drawings:

in order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings 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 these drawings without creative efforts.

FIG. 1 is a schematic sectional view of the front view of the structure of the present invention;

fig. 2 is a partially enlarged schematic view of a in fig. 1 according to the present invention;

fig. 3 is a partially enlarged schematic view of B in fig. 1 according to the present invention;

fig. 4 is a schematic top view of the structure of the present invention.

In the figure: 1. a frame body; 2. a threaded sleeve; 3. a screw; 4. a connecting plate; 5. an unmanned aerial vehicle body; 6. a support leg; 7. cushion blocks; 8. a first loop bar; 9. a first spring; 10. a first plunger; 11. a second plunger; 12. a second spring; 13. a second loop bar.

The specific implementation mode is as follows:

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. 1-4, the present invention provides an embodiment: a grazing unmanned aerial vehicle support based on a buffering structure comprises a support body 1 and an unmanned aerial vehicle body 5, wherein the unmanned aerial vehicle body 5 is arranged on the upper side of the support body 1, supporting legs 6 are hinged to the left end and the right end of the lower side of the support body 1, cushion blocks 7 are arranged at the bottom ends of the supporting legs 6, first loop bars 8 are hinged to the front sides of the supporting legs 6, grooves are formed in the upper sides of the first loop bars 8, first springs 9 are vertically connected into the grooves, first inserting bars 10 are arranged at the openings of the grooves, the inner ends of the first inserting bars 10 are connected with the ends of the first springs 9, the other ends of the first inserting bars 10 are hinged to the lower side of the support body 1, second inserting bars 11 are hinged to the inner sides of the supporting legs 6, one side, close to each other, of the second inserting bars 11 is connected through second springs 12, second loop bars 13 are arranged on the inner sides of the supporting legs 6, one side, far away from, a second insertion rod 11 is transversely inserted into the opening of the slot, and one side, close to each other, of the second insertion rod 11 is connected with the end head of a second spring 12;

further, as shown in fig. 1, fig. 2 and fig. 4, a threaded sleeve 2 is fixedly installed on the inner wall of the frame body 1, a screw rod 3 is inserted into the threaded sleeve 2, an opening is formed in the upper side of the frame body 1, a connecting plate 4 is arranged on the inner side of the opening, a fixing groove matched with the screw rod 3 is formed in the outer side of the connecting plate 4, an unmanned aerial vehicle body 5 is installed on the upper side of the connecting plate 4, a user can rotate a rotating handle connected to the outer side of the screw rod 3 conveniently, the connecting plate 4 can be detached and installed, and the unmanned aerial vehicle is simple;

further, as shown in fig. 1, fig. 2 and fig. 4, the frame body 1 is set to be a circular structure, the connecting plate 4 is set to be a circular structure, the outside diameter of the connecting plate 4 is smaller than the inside diameter of the frame body 1, when in use, the frame body 1 and the connecting plate 4 which are circularly arranged are convenient for a user to place the connecting plate 4 inside the frame body 1, so that the connecting plate 4 extends into a through opening formed inside the frame body 1, and convenience is brought to the user in the use process;

furthermore, as shown in fig. 1, fig. 2 and fig. 4, four groups of screws 3 are arranged, the four groups of screws 3 are inserted into a fixing groove formed in the connecting plate 4 in an annular array structure, a rotating handle is fixedly connected to one side, away from each other, of each screw 3, the screws 3 inserted into the screw sleeve 2 are stressed by rotating the rotating handle connected to the outer end of each screw 3, the two groups of screws are in threaded fit, the screws 3 are stretched, the rotating handle can be continuously rotated until the screws 3 extend into the fixing groove formed in the outer side of the connecting plate 4, the connecting plate 4 is installed, and the stability in the installation process is enhanced by the arrangement of the four groups of screws 3;

further, as shown in fig. 1, the supporting leg 6 is of an arc structure, the convex surface of the supporting leg 6 faces outwards, the supporting leg 6 of the arc structure enables the reaction force applied when the supporting leg is in contact with the ground to be small, the conduction of the reaction force is dispersed, and the use is safe;

further, as shown in fig. 1, the cushion block 7 is arranged in a spherical structure, and a rubber pad is glued to the bottom end of the cushion block 7, so that the cushion block 7 in a spherical design is in full contact with the ground in the falling process of the device, and the friction coefficient between the cushion block 7 and the ground is increased through the glued rubber pad;

the working principle is as follows: during the use, can place connecting plate 4 inside support body 1, make connecting plate 4 extend to the opening of 1 inside setups of support body, the accessible this moment rotates the commentaries on classics handle of 3 outer ends connections of screw rod, make insert and establish the screw rod 3 atress of 2 insides of swivel nut, two sets of screw-thread fit that carry on, realize the flexible of screw rod 3, sustainable rotation is changeed to the screw rod 3 and is extended to the fixed slot that the 4 outsides of connecting plate were seted up, the realization is to the installation of connecting plate 4, can install the upside at support body 1 with the unmanned aerial vehicle body 5 of 4 upside connections of connecting plate, convenient to use person is to the dismouting of first.

When the bottom end of the unmanned aerial vehicle body 5 is subjected to external force in the flying process, the supporting legs 6 hinged with the bottom end of the frame body 1 are subjected to angle change, meanwhile, the first loop bar 8 hinged on the front surface of the supporting leg 6 is stressed to extrude a first spring 9 connected inside the first loop bar 8, the first inserted link 10 is made to extend and retract inside the first sleeve 8 through the first spring 9, and part of the impact force is buffered by using the self elastic characteristic of the first spring 9, meanwhile, the second inserted bar 11 hinged at the inner side of the supporting leg 6 is stressed to press the second spring 12 connected with the second inserted bar 11, so that the second inserted bar 11 slides in the second sleeve rod 13, so that the second spring 12 is elastically deformed under stress and buffers the impact force again, thereby realizing the protection of the bottom end of the unmanned aerial vehicle body 5, simultaneously can play the buffering effect at the in-process that descends, prolong unmanned aerial vehicle body 5's life, do above the utility model discloses a whole theory of operation.

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.

Claims

1. The utility model provides a grazing unmanned aerial vehicle support based on have buffer structure, includes support body (1) and unmanned aerial vehicle body (5), its characterized in that: an unmanned aerial vehicle body (5) is arranged on the upper side of the frame body (1), supporting legs (6) are hinged to the left end and the right end of the lower side of the frame body (1), cushion blocks (7) are arranged at the bottom ends of the supporting legs (6), first loop bars (8) are hinged to the front sides of the supporting legs (6), grooves are formed in the upper sides of the first loop bars (8), first springs (9) are vertically connected into the grooves, first inserting rods (10) are arranged at openings of the grooves, the inner ends of the first inserting rods (10) are connected with the ends of the first springs (9), the other ends of the first inserting rods (10) are hinged to the lower side of the frame body (1), second inserting rods (11) are hinged to the inner sides of the supporting legs (6), one sides of the second inserting rods (11) close to each other are connected through second springs (12), second loop bars (13) are arranged on the inner sides of the supporting legs (6), and one side of the second loop bar (13) which is far away from each other is provided with a groove, a second spring (12) is arranged in the groove, a second inserting bar (11) is transversely inserted into the opening of the groove, and one side of the second inserting bar (11) which is close to each other is connected with the end of the second spring (12).

2. The support of claim 1, wherein the support is based on a grazing unmanned aerial vehicle with a buffer structure, and comprises: the utility model discloses an unmanned aerial vehicle, including support body (1), inner wall fixed mounting of support body (1) has swivel nut (2), and the inside of swivel nut (2) is inserted and is equipped with screw rod (3), the opening has been seted up to the upside of support body (1), and the inboard of opening is provided with connecting plate (4), the fixed slot with screw rod (3) matched with has been seted up in the outside of connecting plate (4), unmanned aerial vehicle body (5) are installed to the upside of connecting plate (4).

3. The support of claim 2, wherein the support is based on a grazing unmanned aerial vehicle with a buffer structure, and comprises: the support body (1) is of a circular structure, the connecting plate (4) is of a circular structure, and the diameter of the outer side of the connecting plate (4) is smaller than that of the inner side of the support body (1).

4. The support of claim 2, wherein the support is based on a grazing unmanned aerial vehicle with a buffer structure, and comprises: the screw rods (3) are provided with four groups in total, the four groups of screw rods (3) are arranged in a ring array structure and inserted into a fixing groove formed in the connecting plate (4), and a rotating handle is fixedly connected to one side, far away from each other, of each screw rod (3).

5. The support of claim 1, wherein the support is based on a grazing unmanned aerial vehicle with a buffer structure, and comprises: the supporting legs (6) are arranged to be arc-shaped structures, and convex surfaces of the supporting legs (6) face outwards.

6. The support of claim 1, wherein the support is based on a grazing unmanned aerial vehicle with a buffer structure, and comprises: the cushion block (7) is of a spherical structure, and a rubber pad is glued at the bottom end of the cushion block (7).