CN210028382U

CN210028382U - Protection mechanism for inspection unmanned aerial vehicle

Info

Publication number: CN210028382U
Application number: CN201920608396.6U
Authority: CN
Inventors: 廖彧涓
Original assignee: Sichuan Hengchuangtiandi Automation Equipment Co Ltd
Current assignee: Sichuan Hengchuangtiandi Automation Equipment Co Ltd
Priority date: 2019-04-29
Filing date: 2019-04-29
Publication date: 2020-02-07
Anticipated expiration: 2029-04-29

Abstract

The utility model discloses a protection mechanism for inspection unmanned aerial vehicle, which comprises a box body, the inside bottom of the box body is bonded with a foam cotton pad, the middle joint in the box body is provided with a baffle, the inside wall of the box body is fixedly connected with a support rod, the outside of the support rod is in threaded connection with an internal thread pipe, the end part of the internal thread pipe is connected with the side edge of the baffle through a bearing piece, the utility model discloses a baffle which is connected by the support rod matching internal thread pipe is added in the box body, a rubber mat is installed on the baffle, when the unmanned aerial vehicle is placed in the box body which is bonded with the foam cotton pad, the internal thread pipe is twisted to move along the support rod, so that the baffle which is installed with the rubber mat is matched inwards to block the unmanned aerial vehicle, the unmanned aerial vehicle is prevented from loosening, the adjustment is convenient, a sleeve rod, and the cotton pad of bubble inside the box can play certain cushioning effect, protects unmanned aerial vehicle.

Description

Protection mechanism for inspection unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is a protection machanism for patrolling and examining unmanned aerial vehicle.

Background

A drone is an unmanned aerial vehicle that is operated using a radio remote control device and a self-contained program control device. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle is applied to various industries and is really just needed; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting and the like, the use of the unmanned aerial vehicle is greatly expanded, and the development of the unmanned aerial vehicle industry is greatly promoted. The cruise unmanned aerial vehicle is the mainstream of military and most civil unmanned aerial vehicles and has the greatest characteristic of high flying speed; the unmanned helicopter is an unmanned aerial vehicle platform with the strongest flexibility and can vertically take off and hover in situ.

Current unmanned aerial vehicle that cruises need deposit unmanned aerial vehicle after using the completion for protection unmanned aerial vehicle, but the unmanned aerial vehicle majority that has now is placed in the packing carton that has the foam, and protection unmanned aerial vehicle that such structure can not be fine, and just can deposit the unmanned aerial vehicle of appointed specification, otherwise can not put into, perhaps too not hard up, can't reach the fixed action.

Therefore, the protection mechanism for the inspection unmanned aerial vehicle is provided for solving the problems in the prior art, so that the unmanned aerial vehicle is convenient to fix and protect, and is suitable for protection of various unmanned aerial vehicles with different specifications.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a protection machanism for unmanned aerial vehicle patrols and examines to solve the problem that proposes among the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a protection machanism for patrolling and examining unmanned aerial vehicle, includes the box, the inboard bottom bonds there is the cotton pad of bubble in the box, the joint has the baffle in the middle of in the box, lateral wall fixedly connected with branch in the box, the outside threaded connection of branch has the internal thread pipe, the internal thread pipe end passes through the bearing spare and connects at the baffle side, the baffle intermediate position bonds there is the cushion, cushion central point is groove structure, box upper end side has the case lid through hinge connection, the case lid other end passes through the hasp and is connected with the box, there is the sleeve pipe case inside wall through bolted connection, the cover has cup jointed the loop bar in the middle of the sleeve pipe, the loop bar lower extreme has the clamp plate through.

Preferably, the internal thread pipe lateral wall threaded connection has a handle bolt, handle bolt tip runs through the internal thread pipe lateral wall and contacts with branch.

Preferably, the lower end of the pressing plate is bonded with a foam pad with the same specification, and grooves are uniformly distributed on the end face of the foam pad.

Preferably, the spring is sleeved inside the sleeve, the end part of the spring is connected with the loop bar through a bolt, and the outer diameter of the spring is smaller than the diameter of the loop bar.

Preferably, the side wall of the end part of the pressing plate is a chamfered edge, and the thickness of the pressing plate is the same as that of the partition plate.

Preferably, the inner side wall of the box body is provided with sliding grooves matched with the partition plates, and the partition plate structures are symmetrically arranged in two groups.

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

the utility model discloses at the inside baffle that is increased by branch cooperation internal thread union coupling of box, install the cushion on the baffle, place unmanned aerial vehicle when pasting the box inside that has the cotton pad of bubble, twist and move the internal thread pipe and remove along branch, make the baffle inside cooperation of installing the cushion block unmanned aerial vehicle, it is not hard up to avoid unmanned aerial vehicle, and it is convenient to adjust, connect the loop bar through the sleeve pipe on the case lid, loop bar tip installation clamp plate, be used for preventing that unmanned aerial vehicle from rocking from top to bottom, maintain unmanned aerial vehicle at the inside stability of box, and the cotton pad of the inside bubble of box can play certain cushioning effect, protect unmanned aerial vehicle.

Drawings

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

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

fig. 3 is a schematic structural view of the bushing assembly of the present invention.

In the figure: the box body 1, the cotton pad of 2 bubbles, 3 baffle, 4 spinal branchs pole, 5 internal thread pipes, 6 cushions, 7 case lids, 8 sleeve pipes, 9 loop bars, 10 clamp plates, 11 handle bolts, 12 springs.

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 present invention provides a technical solution: a protection mechanism for an inspection unmanned aerial vehicle comprises a box body 1, a foam cotton pad 2 is bonded at the bottom of the inner side of the box body 1, a partition plate 3 is clamped in the middle of the inner side of the box body 1, a supporting rod 4 is fixedly connected to the inner side wall of the box body 1, an inner threaded pipe 5 is connected to the outer side of the supporting rod 4 in a threaded manner, the end part of the inner threaded pipe 5 is connected to the side edge of the partition plate 3 through a bearing piece, a rubber pad 6 is bonded at the middle position of the partition plate 3, the center position of the rubber pad 6 is of a groove structure, the side edge of the upper end of the box body 1 is connected with a box cover 7 through a hinge, the other end of the box cover 7 is connected with the box body 1 through a lock catch, a sleeve 8 is connected to the inner side wall of the box cover 7 through a bolt, a sleeve rod 9 is sleeved in the middle of, install cushion 6 on baffle 3, place unmanned aerial vehicle when pasting 1 inside of box that has the cotton pad of bubble 2, twist and move internal thread pipe 5 and remove along branch 4, make baffle 3 of installing cushion 6 to the fit-in block unmanned aerial vehicle, avoid unmanned aerial vehicle not hard up, and it is convenient to adjust, connect sleeve rod 9 through sleeve pipe 8 on the

case lid

7, 9 tip installation clamp plates of sleeve rod 10, be used for preventing unmanned aerial vehicle from rocking from top to bottom, maintain unmanned aerial vehicle at 1 inside stability of box, and 1 inside bubble cotton pad 2 of box can play certain cushioning effect, protect unmanned aerial vehicle.

Specifically, the 5 lateral walls threaded connection of internal thread pipe has handle bolt 11, the 11 tip of handle bolt runs through 5 lateral walls of internal thread pipe and contacts with branch 4, and handle bolt 11 is used for further fixing internal thread pipe 5 on branch 4, maintains the stability of 5 positions of internal thread pipe.

Specifically, the lower end of the pressing plate 10 is bonded with a foam pad 2 with the same specification, and grooves are uniformly distributed on the end face of the foam pad 2.

Specifically, 8 inside springs 12 that have cup jointed of sleeve pipe, 12 tip of spring passes through the bolt and is connected with loop bar 9, just 12 external diameters of spring are less than the diameter of loop bar 9, and springs 12 are used for cooperating 8 connection loop bars 9 of sleeve pipe, maintain the elasticity that loop bar 9 popped out downwards, guarantee that clamp plate 10 that 9 lower extremes of loop bar are connected can stabilize the pressfitting on unmanned aerial vehicle.

Specifically, the side wall of the end of the pressing plate 10 is a chamfered edge, and the thickness of the pressing plate 10 is the same as that of the partition plate 3.

Specifically, the inside wall of the box body 1 is provided with a sliding groove matched with the partition board 3, and the partition board 3 is symmetrically arranged in two groups.

The structure principle is as follows: the unmanned aerial vehicle is characterized in that a partition plate 3 connected by a support rod 4 in a matched mode with an internal thread pipe 5 is additionally arranged inside a box body 1, a rubber mat 6 is installed on the partition plate 3, when the unmanned aerial vehicle is placed inside the box body 1 pasted with a foam cotton mat 2, the internal thread pipe 5 is screwed to move along the support rod 4, the partition plate 3 provided with the rubber mat 6 is matched inwards to clamp the unmanned aerial vehicle, looseness of the unmanned aerial vehicle is avoided, the box cover 7 is connected with a sleeve rod 9 through a sleeve 8, a pressing plate 10 is installed at the end part of the sleeve rod 9 and used for preventing the unmanned aerial vehicle from shaking up and down and maintaining the stability of the unmanned aerial vehicle inside the box body 1, the foam cotton mat 2 inside the box body 1 can play a certain damping role and protect the unmanned aerial vehicle, a handle bolt 11 is used for further fixing the internal thread pipe 5 on the support rod 4 and maintaining the position stability of the internal thread pipe 5, guarantee that the clamp plate 10 that the lower extreme of loop bar 9 is connected can stabilize the pressfitting on unmanned aerial vehicle.

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. The utility model provides a protection machanism for patrolling and examining unmanned aerial vehicle, includes box (1), its characterized in that: the foam cotton pad (2) is bonded at the bottom of the inner side of the box body (1), a partition plate (3) is clamped in the middle of the box body (1), a supporting rod (4) is fixedly connected to the inner side wall of the box body (1), an internal thread pipe (5) is connected to the outer side of the supporting rod (4) in a threaded manner, the end of the internal thread pipe (5) is connected to the side edge of the partition plate (3) through a bearing piece, a rubber pad (6) is bonded to the middle position of the partition plate (3), the center position of the rubber pad (6) is of a groove structure, a box cover (7) is connected to the side edge of the upper end of the box body (1) through a hinge, the other end of the box cover (7) is connected with the box body (1) through a lock catch, a sleeve (8) is connected to the inner side wall of the box cover, the pressing plates (10) are positioned between the partition plates (3).

2. The protection mechanism for the inspection unmanned aerial vehicle according to claim 1, wherein: the utility model discloses a handle bolt, including internal thread pipe (5), branch (4) and handle bolt (11), internal thread pipe (5) lateral wall threaded connection has handle bolt (11), handle bolt (11) tip runs through internal thread pipe (5) lateral wall and contacts.

3. The protection mechanism for the inspection unmanned aerial vehicle according to claim 1, wherein: the lower end of the pressing plate (10) is bonded with a foam pad (2) with the same specification, and grooves are uniformly distributed on the end face of the foam pad (2).

4. The protection mechanism for the inspection unmanned aerial vehicle according to claim 1, wherein: the spring (12) is sleeved inside the sleeve (8), the end part of the spring (12) is connected with the loop bar (9) through a bolt, and the outer diameter of the spring (12) is smaller than the diameter of the loop bar (9).

5. The protection mechanism for the inspection unmanned aerial vehicle according to claim 1, wherein: the side wall of the end part of the pressing plate (10) is a chamfered edge, and the thickness of the pressing plate (10) is the same as that of the partition plate (3).

6. The protection mechanism for the inspection unmanned aerial vehicle according to claim 1, wherein: the inner side wall of the box body (1) is provided with sliding grooves matched with the partition boards (3), and the partition boards (3) are symmetrically arranged.