CN218703874U

CN218703874U - Unmanned aerial vehicle is with connecting base

Info

Publication number: CN218703874U
Application number: CN202223073580.6U
Authority: CN
Inventors: 王泽�
Original assignee: Liaoning Ruixiang Aviation Co ltd
Current assignee: Liaoning Ruixiang Aviation Co ltd
Priority date: 2022-11-18
Filing date: 2022-11-18
Publication date: 2023-03-24
Anticipated expiration: 2032-11-18

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, in particular to a connecting base for unmanned aerial vehicles, which comprises an unmanned aerial vehicle main body and a base, wherein the top of the unmanned aerial vehicle main body is provided with the base, the outer side of the base is sleeved with a protective sleeve, four groups of protective components are arranged on the outer circumferential wall of the protective sleeve, and an adjusting component and a moving frame are sequentially arranged in the base from top to bottom; the protection assembly comprises a telescopic rod, a partition plate, a first arc-shaped piece, a second arc-shaped piece and a protection pad, the protection sleeve is connected with the partition plate through the telescopic rod, the first arc-shaped piece and the second arc-shaped piece are sequentially arranged on the outer side of the telescopic rod and between the partition plate and the protection sleeve, and the protection pad is arranged on the outer side of the partition plate; the lag comprises two sets of cover casings, and is two sets of the inside of cover casing all is connected with the bolt, compares with current unmanned aerial vehicle is with being connected the base, the utility model discloses a design has improved the practicality of current unmanned aerial vehicle with being connected the base.

Description

Unmanned aerial vehicle is with connecting base

Technical Field

The utility model relates to an unmanned air vehicle technique field, concretely relates to unmanned aerial vehicle is with connecting base.

Background

Unmanned aerial vehicles, as the name implies, are unmanned aircraft. Since the birth of the 20 th century, people at that time have already proposed the idea of pilotless aircraft in consideration of the safety of piloting aircraft, and up to the 30 th century, fisher corporation in uk transformed a "queen" twin fixed wing aircraft into a drone, opening the introduction of unmanned aerial vehicles into the aviation history. With the gradual maturity of the unmanned aerial vehicle technology, the manufacturing cost and the entrance threshold are reduced, the market of consumer-grade unmanned aerial vehicles has already exploded, while the market of civil unmanned aerial vehicles is in the early night of the explosion, and in the using process of the civil unmanned aerial vehicles, the connecting base serves as an important accessory of the unmanned aerial vehicles and plays an important role in the lifting of the unmanned aerial vehicles;

after deceleration, application No.: 202220027709.0 discloses a connection base for unmanned aerial vehicle, including the unmanned aerial vehicle body, the bottom fixedly connected with of unmanned aerial vehicle body connects the bottom plate, the equal fixedly connected with horizontal backup pad in both sides of connecting the bottom plate, the outside fixedly connected with vertical plate of horizontal backup pad, the inboard below sliding connection of vertical plate has the movable plate, the top fixedly connected with pressure spring of movable plate. The utility model discloses a cooperation that sets up unmanned aerial vehicle body, connecting bottom plate, horizontal backup pad, vertical plate, movable plate, pressure spring, hollow prop, damping spring, limiting plate, shrink leg, landing leg and down tube is used, it is poor to have solved current unmanned aerial vehicle and connect the base shock attenuation effect, makes unmanned aerial vehicle receive the impact easily when contacting with ground, reduces unmanned aerial vehicle life's problem, possesses the shock attenuation effectual, avoids unmanned aerial vehicle to receive the impact when descending, improves unmanned aerial vehicle life's advantage;

with respect to the related art among the above, the inventors consider that the following drawbacks exist: the extension springs are arranged in the application, so that the supporting legs have supporting and stabilizing effects, the supporting legs can be reset more quickly when being impacted to deform, the impact force generated when the unmanned aerial vehicle lands is absorbed and attenuated, and the damping effect on the unmanned aerial vehicle body is improved;

consequently to the improvement of current unmanned aerial vehicle with connecting the base, design a novel unmanned aerial vehicle with connecting the base in order to change above-mentioned technical defect, improve the practicality of whole unmanned aerial vehicle with connecting the base.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an unmanned aerial vehicle is with connecting base 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:

a connecting base for an unmanned aerial vehicle comprises an unmanned aerial vehicle main body and a base, wherein the top of the unmanned aerial vehicle main body is provided with the base, a protective sleeve is sleeved on the outer side of the base, four groups of protective assemblies are arranged on the outer circumferential wall of the protective sleeve, and an adjusting assembly and a moving frame are sequentially arranged in the base from top to bottom;

the protection assembly comprises a telescopic rod, a partition plate, a first arc-shaped piece, a second arc-shaped piece and a protection pad, the protection sleeve is connected with the partition plate through the telescopic rod, the first arc-shaped piece and the second arc-shaped piece are sequentially arranged on the outer side of the telescopic rod and between the partition plate and the protection sleeve, and the protection pad is arranged on the outer side of the partition plate;

the lag comprises two sets of cover shells, and is two sets of the inside of cover shell all is connected with the bolt, the outside that one end of bolt extended to the cover shell is provided with the knob.

As the utility model discloses preferred scheme, the protection pad forms for the preparation of rubber material, first arc piece and second arc piece are the preparation of elastic steel sheet material and form.

As the utility model discloses preferred scheme, the bolt is integral type structural design with the knob, the corresponding position department of base and two sets of bolts all sets up threaded hole, the bolt is threaded connection with the connected mode of cover shell and screw hole, and is two sets of the one end of cover shell is the hinge and connects, just the lag is open-close type structural design.

As the utility model discloses preferred scheme, adjusting part includes lead screw, first bevel gear and second bevel gear, it is connected with the base through the lead screw to remove the frame, the lead screw is connected with second bevel gear through first bevel gear, second bevel gear is connected with the motor through the drive shaft.

As the utility model discloses preferred scheme, the connected mode that removes frame and base is sliding connection, four corners that remove the frame bottom all are provided with removes the seat, four groups the inside of removing the seat all rotates and is connected with the gyro wheel.

As the utility model discloses preferred scheme, unmanned aerial vehicle main part and base formula structural design as an organic whole, the lag is detachable structural design with the base.

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

1. in the utility model, through the design of the protective sleeve, the bolt and the protective component; utilize the bolt convenience to install lag and base fixedly, the protection component of being convenient for carries out the anticollision protection to the base, avoids base and external object direct bump, causes the friction damage to the life of base has been prolonged.

2. The utility model discloses in, through adjusting part and the design that removes the frame, utilize motor drive adjusting part to rotate, make through adjusting part to remove the frame and can carry out altitude mixture control to be convenient for stretch out the use or stretch into from the base is inside with it and accomodate, improved the practicality of using.

Drawings

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

FIG. 2 is a schematic view of the base and the protective cover of the present invention;

FIG. 3 is a schematic view of the bottom structure of the base of the present invention;

FIG. 4 is a schematic view of the structure of the protective cover and the protective assembly of the present invention;

fig. 5 is an enlarged view of the present application a.

In the figure: 1. an unmanned aerial vehicle main body; 2. a base; 3. a protective sleeve; 301. a housing; 302. a bolt; 303. a knob; 4. a guard assembly; 401. a telescopic rod; 402. a partition plate; 403. a first arcuate segment; 404. a second arc piece; 405. a protective pad; 5. an adjustment assembly; 501. a screw rod; 502. a first bevel gear; 503. a second taper tooth; 6. a movable frame; 601. and a movable seat.

Detailed Description

The technical solution in the embodiments of the present invention will be clearly and completely described below in conjunction with the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, rather than all embodiments, and all other embodiments obtained by a person of ordinary skill in the art without creative work belong to the scope of the present invention based on the embodiments of the present invention.

In order to facilitate understanding of the invention, a number of embodiments of the invention will be described more fully hereinafter with reference to the accompanying drawings, in which, however, the invention may be embodied in many different forms and is not limited to the embodiments described herein, but rather these embodiments are provided so as to render the disclosure more thorough and complete.

It will be understood that 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, that 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, and that the terms "vertical", "horizontal", "left", "right" and the like are used herein for descriptive purposes only.

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 invention belongs, and the terms used herein in the specification of the present invention are for the purpose of describing particular embodiments only and are not intended to limit the present invention, and the term "and/or" as used herein includes any and all combinations of one or more of the associated listed items.

Examples

Referring to fig. 1-5, the present invention provides a technical solution:

a connecting base 2 for an unmanned aerial vehicle comprises an unmanned aerial vehicle main body 1 and a base 2, wherein the base 2 is arranged at the top of the unmanned aerial vehicle main body 1, a protective sleeve 3 is sleeved outside the base 2, four groups of protective components 4 are arranged on the outer circumferential wall of the protective sleeve 3, and an adjusting component 5 and a moving frame 6 are sequentially arranged inside the base 2 from top to bottom;

referring to fig. 1, fig. 2 and fig. 4, in the present embodiment, the specific structure of the protecting jacket 3 is as follows:

the protective sleeve 3 consists of two groups of sleeves 301, bolts 302 are connected inside the two groups of sleeves 301, and one ends of the bolts 302 extend to the outer sides of the sleeves 301 and are provided with knobs 303;

the bolt 302 and the knob 303 are designed to be in an integrated structure, threaded holes are formed in the positions, corresponding to the two groups of bolts 302, of the base 2, the bolt 302 is in threaded connection with the casing 301 and the threaded holes, one ends of the two groups of casings 301 are in hinged connection, and the protective sleeve 3 is designed to be in an open-close structure;

the open-close type protecting sleeve 3 is convenient to open or close, the protecting sleeve 3 is correspondingly sleeved on the outer side of the base 2, and then the two groups of bolts 302 are correspondingly screwed into the threaded holes, so that the protecting sleeve 3 and the base 2 are fixed.

Next, referring to fig. 1, fig. 2 and fig. 4, in the present embodiment, the specific structure of the protection component 4 is as follows:

the protection assembly 4 comprises a telescopic rod 401, a partition plate 402, a first arc-shaped sheet 403, a second arc-shaped sheet 404 and a protection pad 405, the protection sleeve 3 is connected with the partition plate 402 through the telescopic rod 401, the first arc-shaped sheet 403 and the second arc-shaped sheet 404 are sequentially arranged on the outer side of the telescopic rod 401 and between the partition plate 402 and the protection sleeve 3, and the protection pad 405 is arranged on the outer side of the partition plate 402;

the protective pad 405 is made of rubber, and the first arc-shaped sheet 403 and the second arc-shaped sheet 404 are both made of elastic steel sheets;

after lag 3 equipment is accomplished, can prevent collision protection to base 2 through protective component 4, when protective component 4 protects base 2, baffle 402 receives the striking and carries out the elasticity extrusion to first arc piece 403 and second arc piece 404 simultaneously, and simultaneously, telescopic link 401 stretches out and draws back, butt through first arc piece 403 and second arc piece 404, cushion the weakening to the impact force, make the striking dynamics that transmits base 2 reduce, thereby prevent collision protection to base 2, prolong base 2's life.

Further, referring to fig. 3 and fig. 5, in the present embodiment, the specific structure of the adjusting assembly 5 is as follows:

the adjusting assembly 5 comprises a screw rod 501, a first bevel gear 502 and a second bevel gear 503, the movable frame 6 is connected with the base 2 through the screw rod 501, the screw rod 501 is connected with the second bevel gear 503 through the first bevel gear 502, the second bevel gear 503 is connected with the motor through a driving shaft, the screw rod 501 is rotatably connected with the base 2, the screw rod 501 is in threaded connection with the movable frame 6, the first bevel gear 502 is in meshed connection with the second bevel gear 503, and the screw rod 501 and the first bevel gear 502 are in an integrated structural design;

utilize adjusting part 5 to be convenient for carry out height control to removing seat 601, be convenient for stretch out and income operation from base 2 inside with removing seat 601, rotate just in reverse through controlling motor drive axle and second bevel gear 503 and carry out synchronous, drive lead screw 501 through first bevel gear 502 and rotate just in reverse when second bevel gear 503 rotates to make removal frame 6 carry out lift adjustment, thereby be convenient for stretch out and income operation from base 2 inside with removing seat 601.

In addition, referring to fig. 3, in the present embodiment, the movable frame 6 is connected to the base 2 in a sliding manner, the movable seats 601 are disposed at four corners of the bottom of the movable frame 6, and the four groups of movable seats 601 are rotatably connected to rollers;

the unmanned aerial vehicle main body 1 and the base 2 are designed into an integrated structure, and the protective sleeve 3 and the base 2 are designed into a detachable structure;

the utility model discloses work flow: when the user is using this unmanned aerial vehicle to connect base 2 when, at first through cup jointing lag 3 in the outside of base 2, then utilize two sets of bolts 302 to assemble lag 3 and base 2 fixedly, increase the stability of quick-witted lag 3 installation, through unmanned aerial vehicle main part 1 during flight its base 2 with the external world when bumping, cushion the protection to base 2 through the buffering subassembly, it weakens to cushion the impact force, make the striking dynamics that transmits base 2 reduce, thereby anticollision protection is carried out to base 2, prolong the life of base 2, drive the drive shaft through driving motor simultaneously and rotate, carry out altitude mixture control to removal frame 6 and removal seat 601 through adjusting part 5, removal seat 601 after flexible is convenient for carry out unmanned aerial vehicle main part 1 and descends and support the use, and with its income to base 2 inside convenient storage protection, whole operation flow is simple convenient, compare with current unmanned aerial vehicle with connecting base 2, the utility model discloses a design has improved the practicality of current unmanned aerial vehicle with connecting base 2.

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 an unmanned aerial vehicle is with connecting base, includes unmanned aerial vehicle main part (1) and base (2), its characterized in that: the unmanned aerial vehicle is characterized in that a base (2) is arranged at the top of the unmanned aerial vehicle main body (1), a protective sleeve (3) is sleeved on the outer side of the base (2), four groups of protective assemblies (4) are arranged on the outer circumferential wall of the protective sleeve (3), and an adjusting assembly (5) and a moving frame (6) are sequentially arranged in the base (2) from top to bottom;

the protection assembly (4) comprises a telescopic rod (401), a partition plate (402), a first arc-shaped piece (403), a second arc-shaped piece (404) and a protection pad (405), the protection sleeve (3) is connected with the partition plate (402) through the telescopic rod (401), the first arc-shaped piece (403) and the second arc-shaped piece (404) are sequentially arranged on the outer side of the telescopic rod (401) and between the partition plate (402) and the protection sleeve (3), and the protection pad (405) is arranged on the outer side of the partition plate (402);

the protective sleeve (3) is composed of two sets of sleeves (301), bolts (302) are connected to the insides of the sleeves (301), and knobs (303) are arranged on the outer sides, extending to the sleeves (301), of one ends of the bolts (302).

2. The connection base for the unmanned aerial vehicle according to claim 1, wherein: the protection pad (405) is made of rubber, and the first arc-shaped piece (403) and the second arc-shaped piece (404) are made of elastic steel sheets.

3. The connection base for the unmanned aerial vehicle according to claim 1, wherein: bolt (302) are integral type structural design with knob (303), the corresponding position department of base (2) and two sets of bolt (302) all sets up threaded hole, bolt (302) are threaded connection with the connected mode of cover shell (301) and threaded hole, and are two sets of the one end of cover shell (301) is for the hinge connection, just lag (3) are for open-close type structural design.

4. The connection base for the unmanned aerial vehicle according to claim 1, wherein: the adjusting assembly (5) comprises a screw rod (501), a first bevel gear (502) and a second bevel gear (503), the moving frame (6) is connected with the base (2) through the screw rod (501), the screw rod (501) is connected with the second bevel gear (503) through the first bevel gear (502), and the second bevel gear (503) is connected with a motor through a driving shaft.

5. The connection base for the unmanned aerial vehicle according to claim 1, wherein: the connection mode that removes frame (6) and base (2) is sliding connection, four corners of removing frame (6) bottom all are provided with removes seat (601), four groups the inside of removing seat (601) all rotates all to be connected with the gyro wheel.

6. The connection base for the unmanned aerial vehicle according to claim 1, wherein: unmanned aerial vehicle main part (1) and base (2) formula structural design as an organic whole, lag (3) are detachable structural design with base (2).