CN214336129U

CN214336129U - Detachable unmanned aerial vehicle for teaching

Info

Publication number: CN214336129U
Application number: CN202022808879.6U
Authority: CN
Inventors: 陈志明
Original assignee: Wuhan Skater Intelligent Creator Technology Co ltd
Current assignee: Wuhan Skater Intelligent Creator Technology Co ltd
Priority date: 2020-11-27
Filing date: 2020-11-27
Publication date: 2021-10-01
Anticipated expiration: 2030-11-27

Abstract

The utility model discloses a teaching is with dismantlable unmanned aerial vehicle, the device comprises a host computer, the host computer right flank is provided with the balancing pole, and the balancing pole right side tip installs rotatory storehouse to rotatory storehouse surface evenly is provided with the slotted hole, the monitor is installed to the host computer bottom surface, and the department's internal surface contact is connected with the transmission shaft in the middle of the host computer, the transmission shaft internal surface is provided with the axostylus axostyle, and axostylus axostyle surface mounting has the lug, lug surface contact is connected with the push rod, and the push rod tip installs the positive electrode, positive electrode surface contact is connected with the negative electrode, and the negative electrode right flank installs the vertical axis, vertical axis pole right flank is provided with screw mechanism, and the screw mechanism surface evenly is provided with the fixture block. This teaching is with dismantling unmanned aerial vehicle can be with the quick installation of balancing pole with fix in the host computer through simple operation to can drive the rotation of axis of rotation through the installation motor, make the installation become the integration with dismantling, solve current unmanned aerial vehicle installation and dismantle the inconvenient problem.

Description

Detachable unmanned aerial vehicle for teaching

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is a teaching is with dismantling unmanned aerial vehicle.

Background

With the arrival of the electronic era, the everywhere visible artificial intelligence has gradually come into our lives, and the multifunctional electronic equipment can actually bring convenience and rapidness to our lives, and more attention is paid to the diversity of the performances of the electronic equipment on the premise of improving the quality of life.

Unmanned aerial vehicle is often used for measuring and monitoring by people, extensively is arranged in garden forestry and building industry, and unmanned aerial vehicle's technical scope also is constantly promoting and is expanding, becomes to expand to the education trade from the use in garden forestry and the building industry in the past, in the use of education trade, has improved the requirement to unmanned aerial vehicle's installation and dismantlement again, also can light convenient dismantlement when will making the quick convenient installation of unmanned aerial vehicle ability.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a teaching is with dismantling unmanned aerial vehicle to provide the inconvenient installation of current teaching with unmanned aerial vehicle and the problem of dismantling in solving above-mentioned background.

In order to achieve the above object, the utility model provides a following technical scheme: a detachable unmanned aerial vehicle for teaching comprises a host, wherein a balancing rod is arranged on the right side face of the host, a rotating bin is installed at the end part of the right side of the balancing rod, a slotted hole is uniformly formed in the surface of the rotating bin, a monitor is installed on the bottom face of the host, a transmission shaft is connected with the middle of the host in an inner surface contact manner, a shaft rod is arranged on the inner surface of the transmission shaft, a lug is installed on the surface of the shaft rod, a push rod is connected with the surface of the lug in a contact manner, an positive electrode is installed at the end part of the push rod, a first spring is installed at the bottom end of the positive electrode, a negative electrode is connected with the surface of the positive electrode in a contact manner, a vertical shaft is installed on the right side face of the negative electrode, a second spring is arranged on the surface of the negative electrode, a screw mechanism is arranged on the right side face of the vertical shaft, clamping blocks are uniformly arranged on the surface of the screw mechanism, clamping grooves are connected with the surface in a contact manner, and are arranged on the inner surface of the transverse grooves, the transmission shaft surface part is connected with a gear, the surface of the gear is meshed with a rack, and the rack is arranged on the lower bottom surface of the motor.

Preferably, the slotted hole is round at one side and long-strip at one side, and the shape of the slotted hole is matched with the shape of the end part of the fan blade to be installed.

Preferably, the lug is fixedly connected to the surface of the transmission shaft, 2 lugs are arranged on the lug, the lug is in a sickle shape, and the 2 lugs are symmetrically distributed around the center of the transmission shaft.

Preferably, the positive electrode and the negative electrode are contacted with each other and then drive the screw mechanism to rotate on the surface of the vertical shaft.

Preferably, the fixture block is fixedly installed on the outer surface of the screw mechanism, the fixture block is in an inverted L shape, and 2 fixture blocks are arranged.

Preferably, the number of the clamping grooves is 2, and the length of each clamping groove is matched with that of each clamping block.

Compared with the prior art, the beneficial effects of the utility model are that: this teaching is with dismantling unmanned aerial vehicle can be with the quick installation of balancing pole with fix in the host computer through simple operation to can drive the rotation of axis of rotation through the installation motor, make the installation become the integration with dismantling, solve current unmanned aerial vehicle installation and dismantle the inconvenient problem.

1. The motor is installed in the rotating bin, the rack at the bottom of the motor drives the gear to rotate, the transmission shaft rotates, the shaft rod rotates, the positive electrode slowly approaches the negative electrode, the two electrodes are connected, the spiral mechanism rotates, and the clamping block can be slowly clamped into the clamping groove to complete installation and fixation of the balance rod;

2. through down taking out the motor for the rack up drives the antiport of gear, makes fixture block and draw-in groove not at the block, and the fixture block slowly rolls out from the draw-in groove, makes that can be light take off the balancing pole from the host computer, accomplishes the purpose of light dismantlement.

Drawings

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

FIG. 2 is a schematic side view of the main body of the present invention;

FIG. 3 is an enlarged schematic view of point A of FIG. 1 according to the present invention;

FIG. 4 is a schematic diagram of the right-side view structure of the screw mechanism of the present invention;

fig. 5 is a schematic view of the sectional structure of the rotary bin of the present invention.

In the figure: 1. a host; 2. a balancing pole; 3. rotating the bin; 4. a slot; 5. a monitor; 6. a drive shaft; 7. a bump; 8. a shaft lever; 9. a positive electrode; 10. a push rod; 11. a negative electrode; 12. a transverse groove; 13. A vertical axis; 14. a screw mechanism; 15. a clamping block; 16. a card slot; 17. a motor; 18. a rack; 19. a gear; 20. a first spring; 21. a second spring.

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. 1-5, the present invention provides a technical solution: a detachable unmanned aerial vehicle for teaching comprises a main machine 1, a balancing rod 2 is arranged on the right side of the main machine 1, a rotary bin 3 is mounted at the right side end of the balancing rod 2, a slotted hole 4 is uniformly formed in the surface of the rotary bin 3, a monitor 5 is mounted on the bottom surface of the main machine 1, a transmission shaft 6 is connected to the middle of the main machine 1 in a surface contact manner, a shaft rod 8 is arranged on the inner surface of the transmission shaft 6, a lug 7 is mounted on the surface of the shaft rod 8, a push rod 10 is connected to the surface of the lug 7 in a surface contact manner, an anode 9 is mounted at the end of the push rod 10, a first spring 20 is mounted at the bottom end of the anode 9, a cathode 11 is connected to the surface of the anode 9 in a surface contact manner, a vertical shaft 13 is mounted on the right side of the cathode 11, a second spring 21 is arranged on the surface of the cathode 11, a screw mechanism 14 is arranged on the right side of the vertical shaft 13, a clamping block 15 is uniformly arranged on the surface of the screw mechanism 15, a clamping groove 16 is connected in a surface contact manner, and the clamping groove 16 is arranged on the inner surface of the transverse groove 12, the surface part of the transmission shaft 6 is connected with a gear 19, the surface of the gear 19 is engaged with a rack 18, and the rack 18 is arranged on the lower bottom surface of the motor 17.

Slotted hole 4 sets up to one side circular, one side rectangular shape, and slotted hole 4 shape is identical with the flabellum tip shape that needs the installation, and the identical flabellum of size of slotted hole 4 on unmanned aerial vehicle rotary bin 3 surface is installed in slotted hole 4.

The lug 7 is fixedly connected on the surface of the

transmission shaft

6, 2 lugs 7 are arranged, the lug 7 is in a shape of a sickle, meanwhile, the 2 lugs 7 are symmetrically distributed on the center of the transmission shaft 6, the push rod 10 is slowly pushed outwards by the slow rotation of the lugs 7, and the positive electrode 9 at the end part of the push rod 10 is contacted with the negative electrode 11.

After the surfaces of the positive electrode 9 and the negative electrode 11 are contacted, the screw mechanism 14 is driven to rotate on the surface of the vertical shaft 13, and after the positive electrode 9 is contacted with the negative electrode 11, the screw mechanism 14 on the surface of the vertical shaft 13 is triggered to rotate.

Fixture block 15 fixed mounting is at 14 external surfaces of screw mechanism, and fixture block 15 is "L" shape of falling to fixture block 15 is provided with 2, and fixture block 15's rotation can slowly the block advance draw-in groove 16 internal fixation, whole unmanned aerial vehicle can normal use and lift off.

The number of the clamping grooves 16 is 2, the length of each clamping groove 16 is identical to that of the corresponding clamping block 15, so that the transmission shaft 6 can rotate reversely, the clamping blocks 15 and the clamping grooves 16 are not clamped, and the balancing rod 2 can be easily taken out of the main machine 1.

The working principle is as follows: when the unmanned aerial vehicle is needed, firstly, the fan blades matched with the size of the slotted holes 4 on the surface of the rotating bin 3 of the unmanned aerial vehicle are installed in the slotted holes 4, the technology for installing the fan blades is the prior art, and the motor 17 is installed in the rotating bin 3 to complete the work before the unmanned aerial vehicle flies;

the balance rod 2 of the rotating bin 3 with the installed fan blades is inserted into the corresponding position of the host 1, the motor 17 is installed in the rotating bin 3, the rack 18 at the bottom of the motor 17 drives the gear 19 to rotate, so that the gear 19 rotates to drive the transmission shaft 6 to rotate, the transmission shaft 6 rotates to enable the bump 7 to rotate to be in contact with the push rod 10, the push rod 10 is slowly pushed outwards by the slow rotation of the bump 7, the screw mechanism 14 on the surface of the vertical shaft 13 is triggered to rotate after the positive electrode 9 at the end of the push rod 10 is in contact with the negative electrode 11, the fixture block 15 on the surface is driven to rotate by the rotation of the screw mechanism 14, the fixture block 15 rotates to be slowly clamped into the clamping groove 16 to be fixed, and the whole unmanned aerial vehicle can be normally used and lifted;

when the motor 17 needs to be disassembled, the motor 17 is taken out upwards, the rack 18 moves upwards, the gear 19 rotates reversely, the transmission shaft 6 also rotates reversely, the positive electrode 9 is separated from the negative electrode 11 due to the first spring 20 arranged at the bottom of the positive electrode 9, the negative electrode 11 and the positive electrode 9 cannot be connected under the action of the second spring 21 at the bottom end of the negative electrode 11, the clamping block 15 and the clamping groove 16 are not clamped, the balance rod 2 is easily taken out of the main machine 1, the disassembly and the storage are easy, and the next use is convenient.

It is to be understood that the terms "central," "longitudinal," "lateral," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like are used in the orientations and positional relationships indicated in the drawings for the purpose of convenience and simplicity of description, and are not intended to indicate or imply that the referenced devices or elements must be in a particular orientation, constructed and operated in a particular orientation, and are not to be construed as limiting the scope of the present invention.

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 teaching is with dismantlable unmanned aerial vehicle, includes host computer (1), its characterized in that: the device is characterized in that a balance rod (2) is arranged on the right side face of a host (1), a rotary bin (3) is installed at the right side end of the balance rod (2), slotted holes (4) are uniformly formed in the surface of the rotary bin (3), a monitor (5) is installed on the bottom face of the host (1), a transmission shaft (6) is connected to the middle of the host (1) in a contact mode, a shaft rod (8) is arranged on the inner surface of the transmission shaft (6), a bump (7) is installed on the surface of the shaft rod (8), a push rod (10) is connected to the bump (7) in a surface contact mode, an anode (9) is installed at the end of the push rod (10), a first spring (20) is installed at the bottom end of the anode (9), a cathode (11) is connected to the anode (9) in a surface contact mode, a vertical shaft (13) is installed on the right side face of the cathode (11), and a second spring (21) is installed on the surface of the cathode (11), the vertical shaft (13) right flank is provided with screw mechanism (14), and screw mechanism (14) surface evenly is provided with fixture block (15), fixture block (15) surface contact is connected with draw-in groove (16), and draw-in groove (16) set up at cross slot (12) internal surface, transmission shaft (6) surface part is connected with gear (19), and gear (19) surface meshing is connected with rack (18) to install bottom surface under motor (17) rack (18).

2. The detachable unmanned aerial vehicle for teaching of claim 1, wherein: the slotted hole (4) is round at one side and long in strip shape at one side, and the shape of the slotted hole (4) is matched with the shape of the end part of the fan blade to be installed.

3. The detachable unmanned aerial vehicle for teaching of claim 1, wherein: lug (7) fixed connection is in transmission shaft (6) surface, and lug (7) are provided with 2 to lug (7) shape is "sickle" shape, and 2 lugs (7) are simultaneously about transmission shaft (6) central symmetry distribution.

4. The detachable unmanned aerial vehicle for teaching of claim 1, wherein: after the surfaces of the positive electrode (9) and the negative electrode (11) are contacted, the screw mechanism (14) is driven to rotate on the surface of the vertical shaft (13).

5. The detachable unmanned aerial vehicle for teaching of claim 1, wherein: the fixture blocks (15) are fixedly installed on the outer surface of the screw mechanism (14), the fixture blocks (15) are inverted L-shaped, and 2 fixture blocks (15) are arranged.

6. The detachable unmanned aerial vehicle for teaching of claim 1, wherein: the number of the clamping grooves (16) is 2, and the length of each clamping groove (16) is matched with that of each clamping block (15).