CN212766721U

CN212766721U - High-performance unmanned aerial vehicle for cruising

Info

Publication number: CN212766721U
Application number: CN202021567392.7U
Authority: CN
Inventors: 任永伟; 任永鹏
Original assignee: Hebei Qidun Technology Co ltd
Current assignee: Hebei Qidun Technology Co ltd
Priority date: 2020-08-01
Filing date: 2020-08-01
Publication date: 2021-03-23
Anticipated expiration: 2030-08-01

Abstract

The utility model discloses a high-performance unmanned aerial vehicle for cruising, which comprises a body, wherein a pair of openings are respectively arranged at two sides of the body, foot rests are respectively arranged at the bottom ends of the four openings, two foot plates are arranged at the bottom ends of the four foot rests, two rotating rods are arranged at the top ends of the four foot rests, one side of each rotating rod is fixedly connected with two corresponding foot rests, a connecting box is arranged at the top ends of the two rotating rods, racks are respectively arranged at two sides of the connecting box, the two racks are meshed with corresponding gears and are connected, a telescopic rod is inserted and connected at the top end of the connecting box, a universal camera is fixedly arranged at the bottom end of the connecting box, the rotating rods are controlled to rotate through the gears and the racks, so that the foot rests stretch out of the body downwards when the universal camera extends out of the body, the influence on a lens picture is avoided, the universal camera is retracted into the body when the, the safety during unmanned aerial vehicle's functionality and operation has effectively been improved.

Description

High-performance unmanned aerial vehicle for cruising

Technical Field

The utility model relates to an unmanned aerial vehicle application apparatus field, in particular to a high performance unmanned aerial vehicle for cruise.

Background

Unmanned aerial vehicle technique and product are by industrial and commercial usage such as wide application in aerial photography, remote sensing survey and drawing, forest fire prevention, electric power inspection line, search and rescue, movie & TV advertisement, and cruise is one of them common function of unmanned aerial vehicle, and the general duration of this type of unmanned aerial vehicle is stronger, carries out the region of operation diversified.

A but, unmanned aerial vehicle for cruising generally adopts adjustable multi-direction camera, and the existence of foot rest may cause the lens picture to shelter from when adjusting some directions, or influence picture luminance, and when some special areas operation, ground environment is difficult to predict, and the foot rest can not be fine adaptation topography, and the camera is arranged in the organism outside and may receive the fish tail, causes the loss.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a high performance unmanned aerial vehicle for cruise to the foot rest that proposes in solving above-mentioned background shelters from the camera lens, can not adapt to the topography of falling to the ground and the problem of fragile damage camera when falling to the ground.

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a high performance unmanned aerial vehicle for cruise, includes the organism, the top fixed mounting wing of organism, the one end fixed mounting fin of organism, a pair of opening is all seted up to the both sides of organism, four the open-ended bottom all is equipped with the foot rest, four the foot rest bottom is equipped with two footboards, the inside of organism is equipped with built-in power supply.

As an optimal technical scheme of the utility model, four the top of foot rest is equipped with two bull sticks, two one side of bull stick all corresponds foot rest fixed connection with two of them, two the both ends of bull stick are all rotated and are connected bearing, four the bearing all with the inner wall fixed connection of organism.

As a preferred technical scheme of the utility model, two the middle part of bull stick all is equipped with the gear, two the top of bull stick is equipped with the connecting box, the both sides of connecting box all are equipped with the rack, two the rack is connected with corresponding gear engagement.

As a preferred technical scheme of the utility model, the telescopic link is connected in the interlude on the top of connecting box, the top and the inside top fixed connection of organism of telescopic link, telescopic link and built-in power supply electric connection.

As a preferred technical scheme of the utility model, the universal camera of bottom fixed mounting of connecting box, universal camera and built-in power supply electric connection.

As an optimal technical scheme of the utility model, four the first engaging lug of the equal fixed connection in bottom of foot rest, two the equal two pairs of second engaging lugs of fixed connection in top of sole, four first engaging lug all rotates with a pair of second engaging lug that corresponds to be connected.

As an optimized technical scheme of the utility model, two the bottom fixed connection slipmat of sole.

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

1. the utility model discloses set up the bull stick, rotated through gear and rack control bull stick for when universal camera stretches out the organism downwards, the foot rest opens, thereby has avoided the influence to the lens picture, has effectively promoted unmanned aerial vehicle's the function of cruising, and the sole that the foot of foot rest bottom rotation connection can be according to the angle automatically regulated of foot rest, makes unmanned aerial vehicle can adapt to more descending topography.

2. The utility model discloses set up the connecting box, through the cooperation of gear on rack and the bull stick on the connecting box for when unmanned aerial vehicle adjusts the foot rest angle and carries out descending, in advancing the organism with universal camera shrink, prevent that the camera from receiving the damage, the security performance of machine when effectively having improved the unmanned aerial vehicle operation.

Drawings

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

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

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

in the figure: 1. a body; 2. an airfoil; 3. a tail wing; 4. an opening; 5. a foot rest; 6. a foot plate; 7. a rotating rod; 8. a bearing; 9. a gear; 10. a connection box; 11. a rack; 12. a telescopic rod; 13. a universal camera; 14. a first connecting lug; 15. a second engaging lug; 16. a non-slip mat.

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 a technical scheme for high performance unmanned aerial vehicle who cruises:

according to the drawings of fig. 1, fig. 2 and fig. 3, the wind power generation device comprises a machine body 1, a wing 2 is fixedly installed at the top end of the machine body 1, a tail wing 3 is fixedly installed at one end of the machine body 1, a pair of openings 4 are respectively formed in two sides of the machine body 1, foot rests 5 are respectively arranged at the bottom ends of the four openings 4, two foot plates 6 are arranged at the bottom ends of the four foot rests 5, a built-in power supply is arranged in the machine body 1, two rotating rods 7 are arranged at the top ends of the four foot rests 5, one sides of the two rotating rods 7 are respectively and fixedly connected with the two corresponding foot rests 5, bearings 8 are respectively and rotatably connected with two ends of the two rotating rods 7, the four bearings 8 are respectively and fixedly connected with the inner wall of the machine body 1, gears 9 are respectively arranged in the middle parts of the two rotating rods 7, a connecting box 10 is arranged at the top ends of the two rotating rods 7, racks 11 are respectively meshed with the, the telescopic rod 12 is electrically connected with the built-in power supply, the bottom end of the connecting box 10 is fixedly provided with the universal camera 13, the universal camera 13 is electrically connected with the built-in power supply, the bottom ends of four foot rests 5 are fixedly connected with the first connecting lugs 14, the top ends of two foot plates 6 are fixedly connected with two pairs of second connecting lugs 15, the four first connecting lugs 14 are rotatably connected with the corresponding pair of second connecting lugs 15, the bottom ends of the two foot plates 6 are fixedly connected with the anti-skid pads 16, the rotating rod 7 is controlled to rotate through the gear 9 and the rack 11, so that the foot rests 5 are opened when the universal camera 13 extends downwards out of the machine body 1, the influence on the picture of the lens is avoided, the cruising function of the unmanned aerial vehicle is effectively improved, the foot plates 6 rotatably connected with the bottom ends of the foot rests 5 can be automatically adjusted according to the angles of the foot rests 5, the unmanned aerial vehicle can adapt to more landforms, through the matching of, make when 5 angles of foot rest are adjusted at unmanned aerial vehicle and descend, in contracting into organism 1 with universal camera 13, prevent that the camera from receiving the damage, the security performance of machine when effectively having improved unmanned aerial vehicle operation.

When the unmanned aerial vehicle is used, the utility model relates to a high-performance unmanned aerial vehicle for cruising, after the unmanned aerial vehicle takes off, the extension of the telescopic link 12 is adjusted, the connecting box 10 is pushed downwards, so that the universal camera 13 extends out of the machine body 1 downwards, meanwhile, the rotating rod 7 is controlled to rotate through the rack 11 on the connecting box 10 and the gear 9 on the rotating rod 7, the foot rest 5 is opened towards two sides, the picture of the universal camera 13 is prevented from being shielded, then the universal camera 13 is adjusted to cruise, after the cruise task is finished, the telescopic link 12 is adjusted to contract when the unmanned aerial vehicle falls, through the matching of the rack 11 on the connecting box 10 and the gear 9 on the rotating rod 7, the universal camera 13 is contracted into the machine body 1 when the unmanned aerial vehicle adjusts the angle to fall, so as to protect the universal camera 13, the foot plate 6 rotatably connected with the bottom end of the foot rest 5 can be automatically adjusted according to the angle, make unmanned aerial vehicle can adapt to descending topography, stably descend.

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. A high performance unmanned aerial vehicle for cruise, includes organism (1), its characterized in that: the aircraft engine is characterized in that wings (2) are fixedly mounted at the top end of the engine body (1), empennages (3) are fixedly mounted at one end of the engine body (1), a pair of openings (4) are formed in the two sides of the engine body (1), four foot frames (5) are arranged at the bottom ends of the openings (4), four foot frames (5) are arranged at the bottom ends of the foot frames (5), and a built-in power supply is arranged inside the engine body (1).

2. A high-performance drone for cruising according to claim 1, characterised in that: four the top of foot rest (5) is equipped with two bull sticks (7), two one side of bull stick (7) all corresponds foot rest (5) fixed connection with two of them, two the both ends of bull stick (7) are all rotated and are connected bearing (8), four bearing (8) all with the inner wall fixed connection of organism (1).

3. A high-performance drone for cruising according to claim 2, characterised in that: the middle part of two bull stick (7) all is equipped with gear (9), two the top of bull stick (7) is equipped with connecting box (10), the both sides of connecting box (10) all are equipped with rack (11), two rack (11) are connected with corresponding gear (9) meshing.

4. A high-performance drone for cruising according to claim 3, characterised in that: the top end of the connecting box (10) is connected with a telescopic rod (12) in an inserting mode, the top end of the telescopic rod (12) is fixedly connected with the top end inside the machine body (1), and the telescopic rod (12) is electrically connected with a built-in power supply.

5. A high-performance drone for cruising according to claim 3, characterised in that: the bottom end of the connecting box (10) is fixedly provided with a universal camera (13), and the universal camera (13) is electrically connected with the built-in power supply.

6. A high-performance drone for cruising according to claim 1, characterised in that: four the equal fixed connection first engaging lug (14) in bottom of foot rest (5), two the equal fixed connection two pairs of second engaging lugs (15) in top of sole (6), four first engaging lug (14) all rotate with a pair of second engaging lug (15) that correspond and are connected.

7. A high-performance drone for cruising according to claim 1, characterised in that: the bottom ends of the two foot plates (6) are fixedly connected with anti-skid pads (16).