CN214296426U

CN214296426U - Portable many rotor unmanned aerial vehicle

Info

Publication number: CN214296426U
Application number: CN202120415524.2U
Authority: CN
Inventors: 罗波; 周慧玲; 黄琼
Original assignee: Wuhan Tianbo Technology Co ltd
Current assignee: Wuhan Tianbo Technology Co ltd
Priority date: 2021-02-25
Filing date: 2021-02-25
Publication date: 2021-09-28
Anticipated expiration: 2031-02-25

Abstract

The utility model discloses a portable many rotor unmanned aerial vehicle relates to the unmanned aerial vehicle field. This portable many rotor unmanned aerial vehicle, including the fuselage, four first draw-in grooves have been seted up to the fuselage upper surface, first spout has been seted up to the inner wall of first draw-in groove, the first elastic component of inside wall fixedly connected with of first spout, the one end fixedly connected with of first elastic component presses the piece, and the one end that the draw-in groove was kept away from to first dwang rotates and is connected with first rotor, the second draw-in groove has all been seted up to the both sides of fuselage, and the inner wall of second draw-in groove all rotates and is connected with two second dwangs, the upper surface of second dwang is provided with spacing subassembly, and the one end that the second draw-in groove was kept away from to the second dwang rotates and is connected with the turning block, the upper surface of turning block rotates and is connected with the second rotor, and one side of second dwang is provided with sliding assembly. This portable many rotor unmanned aerial vehicle can fold the rotor, need not dismantle convenient to carry.

Description

Portable many rotor unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is a portable many rotor unmanned aerial vehicle.

Background

Many rotor unmanned aerial vehicle is the aircraft that begins to put into practical use gradually at present, and it has flexible, the reaction is quick, unmanned aerial vehicle, operation require advantage such as low, loads multiclass sensor on unmanned aerial vehicle, for example the camera, can realize image real-time transmission, high-risk area and survey the function, and the wide application is in each field to the realization is to the shooting of cruising and the supervision of specified area.

Most many rotor unmanned aerial vehicle at present is because the rotor is more, so the volume ratio is bigger, and the rotor can not be folded, but some rotors can be dismantled, all need the dismouting rotor in the use at every turn, put into the case, consequently use and carry the time very loaded down with trivial details, therefore we have proposed a portable many rotor unmanned aerial vehicle.

SUMMERY OF THE UTILITY MODEL

Not enough to prior art, the utility model discloses a portable many rotor unmanned aerial vehicle to solve the problem that proposes in the above-mentioned background art.

In order to achieve the above purpose, the utility model discloses a following technical scheme realizes: a portable multi-rotor unmanned aerial vehicle comprises a vehicle body, wherein four first clamping grooves are formed in the upper surface of the vehicle body, the inner walls of the four first clamping grooves are rotatably connected with first rotating rods, first sliding grooves are formed in the inner walls of the first clamping grooves, first elastic pieces are fixedly connected to the inner side walls of the first sliding grooves, one ends of the first elastic pieces are fixedly connected with pressing blocks, the outer surfaces of the pressing blocks are attached to the inner side walls of the first sliding grooves, one ends, far away from the clamping grooves, of the first rotating rods are rotatably connected with first rotors, second clamping grooves are formed in two sides of the vehicle body, the inner walls of the second clamping grooves are rotatably connected with two second rotating rods, a limiting assembly is arranged on the upper surface of each second rotating rod, one ends, far away from the second clamping grooves, of the second rotating rods are rotatably connected with rotating blocks, and the upper surfaces of the rotating blocks are rotatably connected with second rotors, and one side of the second rotating rod is provided with a sliding component.

Preferably, the length of first draw-in groove is greater than the length of first rotor, and the width of first draw-in groove is greater than the length of first rotor.

Preferably, spacing subassembly is including leading to the groove, lead to the groove and set up the one end that is close to the second draw-in groove at the second dwang, and the inner wall sliding connection who leads to the groove has two stoppers, two fixedly connected with second elastic component between the stopper, and the both ends difference fixed connection of second elastic component is at the lower surface and the upper surface of two stoppers, two the one end of stopper runs through the second turning block, and one side of stopper is laminated mutually with one side of fuselage.

Preferably, the sliding assembly comprises a second sliding groove, the second sliding groove is formed in one side of the second rotating rod, a third elastic part is fixedly connected to the inner side wall of the second sliding groove, a sliding block is fixedly connected to the other end of the third elastic part, and one side of the sliding block is respectively attached to one side of the second rotating rod and one side of the rotating block.

Preferably, the upper surface of the machine body is symmetrically and fixedly connected with two fixed blocks, a handle is rotatably connected between the two fixed blocks, the lower surface of the machine body is fixedly connected with four supporting rods, and a connecting rod is fixed between every two supporting rods.

Preferably, the length of the second clamping groove is greater than the lengths of the two second rotating rods, and the upper surface and the lower surface of the second clamping groove are attached to the upper surface and the lower surface of the second rotating rod.

The utility model discloses a portable many rotor unmanned aerial vehicle, its beneficial effect who possesses as follows:

1. this portable many rotor unmanned aerial vehicle through the cooperation of the first draw-in groove, second draw-in groove, first dwang, second dwang and the turning block that sets up for unmanned aerial vehicle can fold eight rotors when not using and withdraw, reduces the space, conveniently carries, and also more swiftly when using convenient.

2. This portable many rotor unmanned aerial vehicle can mention many rotor unmanned aerial vehicle like the case through the handle that sets up, and the bottom is provided with the bracing piece, can support unmanned aerial vehicle, can play certain guard action when making unmanned aerial vehicle descend.

Drawings

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

FIG. 2 is an enlarged schematic view of the utility model at A;

fig. 3 is a schematic view of the internal structure of the first slot of the present invention;

fig. 4 is a schematic view of the internal structure of the second rotating rod of the present invention;

fig. 5 is a schematic side view of the second rotating rod of the present invention.

In the figure: 1. a body; 101. a support bar; 102. a connecting rod; 103. a first card slot; 104. a handle; 105. a first rotating lever; 106. a first rotor; 107. pressing the block; 108. a first chute; 109. a first elastic member; 2. a second rotating lever; 201. rotating the block; 202. a second rotor; 203. a through groove; 204. a limiting block; 205. a second elastic member; 206. a second chute; 207. a slider; 208. a third elastic member; 209. and a second card slot.

Detailed Description

The embodiment of the utility model discloses a portable multi-rotor unmanned aerial vehicle, as shown in fig. 1-5, comprising a main body 1, two fixed blocks are symmetrically and fixedly connected to the upper surface of the main body 1, a handle 104 is rotatably connected between the two fixed blocks, four support rods 101 are fixedly connected to the lower surface of the main body 1, a connecting rod 102 is fixed between every two support rods 101, four first slots 103 are arranged on the upper surface of the main body 1, the length of the first slots 103 is greater than that of the first rotating rods 105, the width of the first slots 103 is greater than that of the first rotors 106, the inner walls of the four first slots 103 are rotatably connected with the first rotating rods 105, a first chute 108 is arranged on the inner wall of the first slots 103, a first elastic member 109 is fixedly connected to the inner side wall of the first chute 108, a pressing block 107 is fixedly connected to one end of the first elastic member 109, and the outer surface of the pressing block 107 is attached to the inner side wall of the first chute 108, one end, far away from the clamping grooves, of the first rotating rod 105 is rotatably connected with a first rotor 106, second clamping grooves 209 are formed in the two sides of the fuselage 1, the length of each second clamping groove 209 is larger than that of each of the two second rotating rods 2, the upper surface and the lower surface of each second clamping groove 209 are attached to the upper surface and the lower surface of each second rotating rod 2, the inner walls of the second clamping grooves 209 are rotatably connected with the two second rotating rods 2, and the upper surfaces of the second rotating rods 2 are provided with limiting assemblies;

the limiting assembly comprises a through groove 203, the through groove 203 is arranged at one end of the second rotating rod 2 close to the second clamping groove 209, the inner wall of the through groove 203 is connected with two limiting blocks 204 in a sliding manner, a second elastic part 205 is fixedly connected between the two limiting blocks 204, two ends of the second elastic part 205 are respectively and fixedly connected with the lower surfaces and the upper surfaces of the two limiting blocks 204, one ends of the two limiting blocks 204 penetrate through the second rotating block 201, one side of each limiting block 204 is attached to one side of the machine body 1, one end of the second rotating rod 2 far away from the second clamping groove 209 is rotatably connected with the rotating block 201, the upper surface of the rotating block 201 is rotatably connected with the second rotor 202, one side of the second rotating rod 2 is provided with a sliding assembly, the sliding assembly comprises a second sliding groove 206, the second sliding groove 206 is arranged at one side of the second rotating rod 2, and the inner side wall of the second sliding groove 206 is fixedly connected with a third elastic part 208, the other end of the third elastic member 208 is fixedly connected with a sliding block 207, and one side of the sliding block 207 is respectively attached to one side of the second rotating rod 2 and one side of the rotating block 201.

The working principle is as follows: when the portable multi-rotor unmanned aerial vehicle is used, firstly, the pressing block 107 is pressed inwards to enable the pressing block 107 to move inwards and compress the first elastic piece 109, then the first rotating rod 105 is rotated to enable the first rotating rod 105 to be unfolded, the pressing block 107 is loosened, the first elastic piece 109 rebounds to drive the pressing block 107 to move outwards, so that the first rotating rod 105 cannot be accidentally withdrawn, the four first rotating rods 105 are unfolded by the same operation, then the second rotating block 201 is pulled outwards to enable the second rotating block 201 to be unfolded completely, therefore, the limiting block 204 loses the extrusion of the second clamping groove 209, the second elastic piece 205 rebounds to drive the limiting block 204 to move outwards and is attached to the outer surface of the machine body 1 to fix the second rotating rod 2, then the sliding block 207 is pulled to compress the third elastic piece 208, the sliding block 207 is not in contact with the rotating block 201, then the rotating block 201 is rotated to rotate the second rotor 202 upwards, then the third elastic piece 208 of the sliding block 207 is loosened to bounce, so that the sliding block 207 is attached to the rotating block 201, the rotating block 201 cannot rotate, and other second rotating rods 2 are operated and unfolded as above, so that the unmanned aerial vehicle can be used;

after unmanned aerial vehicle finishes using, with the principle of going up, press earlier and press piece 107, then rotate first rotor 105, make first rotor 105 and first rotor 106 get into in first draw-in groove 103, then remove slider 207 again, rotate turning block 201, make second rotor 202 rotate to both sides, then press two stopper 204, make stopper 204 enter into inside second dwang 2, rotate second dwang 2 again, make second dwang 2 laminate with second draw-in groove 209 mutually, unmanned aerial vehicle packs up and finishes, then grasp handle 104 and carry unmanned aerial vehicle.

The basic principles and the main features of the invention and the advantages of the invention have been shown and described above. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims

1. The utility model provides a portable many rotor unmanned aerial vehicle, includes fuselage (1), its characterized in that: the upper surface of the fuselage (1) is provided with four first clamping grooves (103), the inner walls of the four first clamping grooves (103) are connected with a first rotating rod (105) in a rotating mode, the inner wall of the first clamping groove (103) is provided with a first sliding groove (108), the inner side wall of the first sliding groove (108) is fixedly connected with a first elastic part (109), one end of the first elastic part (109) is fixedly connected with a pressing block (107), the outer surface of the pressing block (107) is attached to the inner side wall of the first sliding groove (108), one end, far away from the clamping grooves, of the first rotating rod (105) is connected with a first rotor (106) in a rotating mode, the two side faces of the fuselage (1) are provided with second clamping grooves (209) in a rotating mode, the inner wall of the second clamping grooves (209) is connected with two second rotating rods (2) in a rotating mode, the upper surface of the second rotating rod (2) is provided with a limiting component, and one end, far away from the second clamping grooves (209) of the second rotating rod (2) is connected with a rotating block (201), the upper surface of turning block (201) rotates and is connected with second rotor (202), and one side of second dwang (2) is provided with sliding assembly.

2. A portable multi-rotor drone according to claim 1, characterized in that: the length of the first clamping groove (103) is larger than that of the first rotating rod (105), and the width of the first clamping groove (103) is larger than that of the first rotating wing (106).

3. A portable multi-rotor drone according to claim 1, characterized in that: spacing subassembly is including leading to groove (203), lead to groove (203) and set up the one end that is close to second draw-in groove (209) at second dwang (2), and the inner wall sliding connection who leads to groove (203) has two stopper (204), two fixedly connected with second elastic component (205) between stopper (204), and the both ends difference fixed connection of second elastic component (205) is at the lower surface and the upper surface of two stopper (204), two the one end of stopper (204) runs through second turning block (201), and the one side of stopper (204) is laminated with one side of fuselage (1) mutually.

4. A portable multi-rotor drone according to claim 1, characterized in that: the sliding assembly comprises a second sliding groove (206), the second sliding groove (206) is arranged on one side of the second rotating rod (2), a third elastic part (208) is fixedly connected to the inner side wall of the second sliding groove (206), a sliding block (207) is fixedly connected to the other end of the third elastic part (208), and one side of the sliding block (207) is respectively attached to one side of the second rotating rod (2) and one side of the rotating block (201).

5. A portable multi-rotor drone according to claim 1, characterized in that: the novel multifunctional aircraft is characterized in that two fixed blocks are symmetrically and fixedly connected to the upper surface of the aircraft body (1), a handle (104) is rotatably connected between the two fixed blocks, four support rods (101) are fixedly connected to the lower surface of the aircraft body (1), and a connecting rod (102) is fixed between every two support rods (101).

6. A portable multi-rotor drone according to claim 1, characterized in that: the length of second draw-in groove (209) is greater than the length of two second dwang (2), and the upper surface and the lower surface of second draw-in groove (209) laminate mutually with the upper surface and the lower surface of second dwang (2).