CN211810193U

CN211810193U - Foldable unmanned aerial vehicle

Info

Publication number: CN211810193U
Application number: CN201921825504.1U
Authority: CN
Inventors: 杜华荣
Original assignee: Hangying Jiangsu Information Technology Co ltd
Current assignee: Hangying Jiangsu Information Technology Co ltd
Priority date: 2019-10-29
Filing date: 2019-10-29
Publication date: 2020-10-30
Anticipated expiration: 2029-10-29

Abstract

The utility model belongs to the technical field of the unmanned air vehicle technique and specifically relates to a foldable unmanned aerial vehicle, which comprises a bod, the spread groove has been seted up in the four corners of organism, the spread groove is all connected the horn through the pivot, the horn is kept away from the fixed rotating electrical machines that is equipped with in one end top of spread groove, the top of rotating electrical machines is equipped with thick liquid seat, the top of thick liquid seat is equipped with the screw, the first groove of accomodating has been seted up to the bottom of horn, and this foldable unmanned aerial vehicle contrast has the current unmanned aerial vehicle advantage to lie in through rolling over the undercarriage first inslot of accomodating, again through rolling over the horn into the second accomodate the inslot, can realize accomodating and expand, and the unmanned aerial vehicle's of being convenient for carry and.

Description

Foldable unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned air vehicle technique field especially relates to a foldable unmanned aerial vehicle.

Background

The unmanned plane is called unmanned plane for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device. From a technical point of view, the definition can be divided into: unmanned fixed wing aircraft, unmanned vertical take-off and landing aircraft, unmanned airship, unmanned helicopter, unmanned multi-rotor aircraft, unmanned paravane aircraft, and the like. Although, current unmanned aerial vehicle has got into civilian field, but it is still bulky, so be unfavorable for unmanned aerial vehicle accomodate and carry, for this reason, we propose a foldable unmanned aerial vehicle and solve above problem.

SUMMERY OF THE UTILITY MODEL

The utility model aims at solving and having had current unmanned aerial vehicle to get into civilian field among the prior art, but it is still bulky, so be unfavorable for unmanned aerial vehicle's the shortcoming of accomodating and carrying, and the foldable unmanned aerial vehicle who provides.

In order to achieve the above purpose, the utility model adopts the following technical scheme:

a folding unmanned aerial vehicle is designed, and comprises a vehicle body, wherein connecting grooves are formed in four corners of the vehicle body, the connecting grooves are connected with a vehicle arm through rotating shafts, a rotating motor is fixedly arranged at the top of one end, away from the connecting grooves, of the vehicle arm, a slurry seat is arranged at the top of the rotating motor, a propeller is arranged at the top of the slurry seat, a first accommodating groove is formed in the bottom of the vehicle arm, one end, away from the connecting grooves, of the first accommodating groove is connected with an undercarriage through a rotating shaft, one end, away from the undercarriage, of the first accommodating groove is internally and fixedly provided with a positive magnet, one end, away from the first accommodating groove, of the undercarriage is internally and fixedly provided with a negative magnet, a second accommodating groove is formed in the four sides, adjacent to the connecting grooves, of the vehicle body cavity, at the top of the second accommodating groove, a first limiting mechanism is formed in the top of the second accommodating, the machine body is positioned at the top of the clamping groove and is provided with a first moving groove, two opposite sides of the first moving groove are provided with first limiting grooves, an inner cavity of the first moving groove is provided with a button, one end of the first moving groove penetrates to the top of the machine body, the button is positioned at two sides of the first limiting groove and is fixedly provided with a matched first limiting block, the first limiting groove is positioned at the bottom of the first limiting block and is fixedly provided with a first spring and is fixedly connected with the first limiting block, the top of the machine arm is provided with a first buckling mechanism which is a clamping block positioned at the top of the machine arm, the bottom of the clamping block positioned on the machine arm is provided with a matched second moving groove, the bottom of the second moving groove is fixedly provided with a second spring and is fixedly connected with the clamping block, two opposite sides of the second moving groove are provided with second limiting grooves, the clamping block is positioned at two opposite sides of the second limiting groove and is fixedly provided with a matched second limiting block, the four corners that the organism was located are located the fixed lug that is equipped with in top of horn, the bottom of lug is equipped with second stop gear, the top of horn is equipped with the perpendicular to second stop gear's second buckle mechanism.

Preferably, the propeller can be folded through the paddle seat, a rubber cushion pad is fixedly arranged at the bottom of the undercarriage, and a rotating buckle is arranged between the undercarriage and the horn through a rotating shaft.

Preferably, the bottom of the machine body is provided with a charging port, and the second accommodating groove is matched with the machine arm, the rotating motor and the folded propeller.

The utility model provides a pair of foldable unmanned aerial vehicle, beneficial effect lies in: this foldable unmanned aerial vehicle is through rolling over into the undercarriage first accomodating the inslot, again through rolling over into the second with the horn and accomodate the inslot, can realize accomodating and expand, and unmanned aerial vehicle's of being convenient for carry and use has overcome unmanned aerial vehicle among the prior art accomodate and has deposited inconvenient problem.

Drawings

Fig. 1 is a schematic structural view of a foldable unmanned aerial vehicle provided by the present invention;

fig. 2 is a schematic side view of a foldable unmanned aerial vehicle according to the present invention;

fig. 3 is a schematic front structural view of a foldable unmanned aerial vehicle according to the present invention;

fig. 4 is a schematic view of a first buckle structure of a foldable unmanned aerial vehicle according to the present invention;

fig. 5 is the utility model provides a foldable unmanned aerial vehicle's first limit structure schematic diagram.

In the figure: organism 1, spread groove 2, horn 3, rotating electrical machines 4, thick liquid seat 5, screw 6, first groove 7 of accomodating, undercarriage 8, anodal magnet 9, negative pole magnet 10, second groove 11 of accomodating, first stop gear 12, draw-in groove 13, first shifting chute 14, first spacing groove 15, button 16, first stopper 17, first spring 18, first buckle mechanism 19, fixture block 20, second shifting chute 21, second spring 22, second spacing groove 23, second stopper 24, lug 25, second stop gear 26, second buckle mechanism 27.

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.

Referring to fig. 1-5, a folding type unmanned aerial vehicle comprises a machine body 1, connecting grooves 2 are formed at four corners of the machine body 1, the connecting grooves 2 are all connected with a machine arm 3 through rotating shafts, a rotating motor 4 is fixedly arranged at the top of one end of the machine arm 3 far away from the connecting grooves 2, a slurry seat 5 is arranged at the top of the rotating motor 4, a propeller 6 is arranged at the top of the slurry seat 5, a first accommodating groove 7 is formed at the bottom of the machine arm 3, one end of the first accommodating groove 7 far away from the connecting grooves 2 is connected with an undercarriage 8 through the rotating shafts, a positive magnet 9 is fixedly arranged inside one end of the first accommodating groove 7 far away from the undercarriage 8, a negative magnet 10 is fixedly arranged inside one end of the undercarriage 8 far away from the first accommodating groove 7, second accommodating grooves 11 are formed on four adjacent sides of the machine body 1, a first limiting mechanism 12 is arranged at the top of the second accommodating groove 11 in the cavity of the machine body 1, a, the machine body 1 is provided with a first moving groove 14 at the top of the clamping groove 13, first limiting grooves 15 are arranged at two opposite sides of the first moving groove 14, a button 16 is arranged in an inner cavity of the first moving groove 14, one end of the first moving groove penetrates to the top of the machine body 1, matched first limiting blocks 17 are fixedly arranged at two opposite sides of the first limiting groove 15, a first spring 18 is fixedly arranged at the bottom of the first limiting block 17 of the first limiting groove 15 and is fixedly connected with the first limiting block 17, a first buckling mechanism 19 is arranged at the top of the machine arm 3, the first buckling mechanism 19 is a clamping block 20 arranged at the top of the machine arm 3, a matched second moving groove 21 is arranged at the bottom of the clamping block 20 of the machine arm 3, a second spring 22 is fixedly arranged at the bottom of the second moving groove 21 and is fixedly connected with the clamping block 20, second limiting grooves 23 are arranged at two opposite sides of the second moving groove 21, matched second limiting blocks 24 are fixedly arranged at two opposite sides of the clamping block 20, the four corners that organism 1 is located are located the fixed lug 25 that is equipped with in top of horn 3, and the bottom of lug 25 is equipped with second stop gear 26, and the top of horn 3 is equipped with the second buckle mechanism 27 of perpendicular to second stop gear 26.

6 accessible thick liquid seats of screw 5 are folding, the fixed rubber buffer pad that is equipped with in bottom of undercarriage 8, reduce the vibrations of this foldable unmanned aerial vehicle when descending, prevent to cause the internals damage, be equipped with rotatory buckle through the pivot between undercarriage 8 and the horn 3, it is fixed when making undercarriage 8 can reopen, 1 bottom of organism is equipped with the mouth that charges, groove 11 and horn 3 are accomodate to the second, rotating electrical machines 4 and the screw 6 phase-match after folding, make horn 3 and screw 6 can accomodate into in the second accomodates groove 11, this foldable unmanned aerial vehicle is through rolling over undercarriage 8 into first accomodating in the groove 7, again through rolling over horn 3 into the second accomodate in the groove 11, can realize accomodating and expand, be convenient for unmanned aerial vehicle's carrying and use, unmanned aerial vehicle's accomodating and depositing inconvenient problem among the prior art has been overcome.

The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.

Claims

1. A folding unmanned aerial vehicle comprises a machine body (1) and is characterized in that connecting grooves (2) are formed in four corners of the machine body (1), the connecting grooves (2) are connected with a machine arm (3) through rotating shafts, a rotating motor (4) is fixedly arranged at the top of one end, far away from the connecting grooves (2), of the machine arm (3), a slurry seat (5) is arranged at the top of the rotating motor (4), a propeller (6) is arranged at the top of the slurry seat (5), a first accommodating groove (7) is formed in the bottom of the machine arm (3), one end, far away from the connecting grooves (2), of the first accommodating groove (7) is connected with a rotating shaft of an undercarriage (8), one end, far away from the undercarriage (8), of the first accommodating groove (7) is fixedly arranged in an anode magnet (9), a cathode magnet (10) is fixedly arranged in one end, far away from the undercarriage (8), of the first accommodating groove (7), the machine body (1) is positioned on four adjacent sides of the connecting groove (2) and is provided with a second accommodating groove (11), the cavity of the machine body (1) is positioned on the top of the second accommodating groove (11) and is provided with a first limiting mechanism (12), the first limiting mechanism (12) is a clamping groove (13) arranged on the top of the second accommodating groove (11), the machine body (1) is positioned on the top of the clamping groove (13) and is provided with a first moving groove (14), two opposite sides of the first moving groove (14) are provided with first limiting grooves (15), the inner cavity of the first moving groove (14) is provided with a button (16), one end of the inner cavity of the first moving groove (14) penetrates through the top of the machine body (1), the button (16) is positioned on two sides of the first limiting grooves (15) and is fixedly provided with first limiting blocks (17) matched, the first limiting grooves (15) are positioned on the bottom of the first limiting blocks (17) and are fixedly provided with first springs (18) and fixedly connected with the first limiting blocks (17), a first buckling mechanism (19) is arranged at the top of the horn (3), the first buckling mechanism (19) is a clamping block (20) positioned at the top of the horn (3), the bottom of the machine arm (3) positioned at the clamping block (20) is provided with a matched second moving groove (21), a second spring (22) is fixedly arranged at the bottom of the second moving groove (21) and is fixedly connected with the clamping block (20), two opposite sides of the second moving groove (21) are provided with second limit grooves (23), the fixture block (20) is fixedly provided with matched second limit blocks (24) at two sides of the second limit groove (23), the four corners of the machine body (1) are positioned at the top of the machine arm (3) and are fixedly provided with convex blocks (25), the bottom of the bump (25) is provided with a second limiting mechanism (26), and the top of the horn (3) is provided with a second buckling mechanism (27) which is perpendicular to the second limiting mechanism (26).

2. A folding unmanned aerial vehicle according to claim 1, wherein the propeller (6) is foldable through the paddle seat (5), a rubber cushion pad is fixed on the bottom of the landing gear (8), and a rotary buckle is arranged between the landing gear (8) and the horn (3) through a rotating shaft.

3. A folding unmanned aerial vehicle according to claim 1, wherein a charging port is provided at the bottom of the body (1), and the second accommodating groove (11) is matched with the horn (3), the rotating motor (4) and the folded propeller (6).