CN218806531U - Portable unmanned aerial vehicle - Google Patents
Portable unmanned aerial vehicle Download PDFInfo
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- CN218806531U CN218806531U CN202222873407.8U CN202222873407U CN218806531U CN 218806531 U CN218806531 U CN 218806531U CN 202222873407 U CN202222873407 U CN 202222873407U CN 218806531 U CN218806531 U CN 218806531U
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
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Abstract
The utility model belongs to the technical field of unmanned aerial vehicles, in particular to a portable unmanned aerial vehicle; the unmanned aerial vehicle comprises an unmanned aerial vehicle main body, wherein a disc is fixedly mounted in the unmanned aerial vehicle main body, four through grooves are uniformly formed in the upper end of the disc, sliding blocks are assembled in the four through grooves in a sliding manner, assembling blocks are fixedly mounted at the upper ends of the four sliding blocks, connecting arms are fixedly mounted on one sides, away from the center of the interior of the unmanned aerial vehicle main body, of the four assembling blocks, connecting rods are fixedly mounted at the lower ends of the four sliding blocks, and a turntable is fixedly mounted on one side of the circumference of the disc; can accomodate the protection to four linking arms and four screw-thread paddle when using, like this when accomodating the unmanned aerial vehicle main part, required storage space is littleer, portable and storage more, and when accomodating, the staff only need the carousel of rotating, alright with the cooperation that leads to the groove with four connecting rods and four arcs, accomplish accomodating to four linking arms and four screw-thread paddle in stretching out.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle, concretely relates to portable unmanned aerial vehicle.
Background
Nowadays, unmanned aerial vehicle's application is very extensive, unmanned aerial vehicle can be used for taking photo by plane, the movie & TV is shot, disaster detection and electric power are patrolled and examined, wherein in the aspect of geographic survey, the most commonly used is just unmanned aerial vehicle, present unmanned aerial vehicle has more and more intelligent, unmanned aerial vehicle can utilize remote control equipment to carry out remote control, partly unmanned aerial vehicle can also be under the help of electronic calculation, independently fly, it is very convenient to use, current portable unmanned aerial vehicle, like the portable unmanned aerial vehicle of application patent number "CN202122196306.7", can accomodate a plurality of wings and enter into inside the unmanned aerial vehicle casing when accomodating, reduce unmanned aerial vehicle and deposit required space, play portable effect, but when accomodating, can only carry out the accomodating of a plurality of wings step by step, can's accomodating when unable to realize a plurality of wings, the speed of accomodating is slower, consequently, need improve.
SUMMERY OF THE UTILITY MODEL
The utility model aims at: aim at providing a portable unmanned aerial vehicle, can accomodate the protection to four linking arms and four screw thread paddle when using, like this when accomodating the unmanned aerial vehicle main part, required storage space is littleer, portable and storage more, and when accomodating, the staff only need the carousel of rotating, alright in order to utilize the cooperation that four connecting rods and four arc led to the groove, accomplish accomodating in stretching out four linking arms and four screw thread paddle, it is quick simple and convenient to operate.
In order to realize the technical purpose, the utility model discloses a technical scheme as follows:
a portable unmanned aerial vehicle comprises an unmanned aerial vehicle main body, wherein a disc is fixedly arranged in the unmanned aerial vehicle main body, four through grooves are uniformly formed in the upper end of the disc, sliding blocks are assembled in the four through grooves in a sliding mode, assembling blocks are fixedly arranged at the upper ends of the four sliding blocks, connecting arms are fixedly arranged on one sides, away from the center of the interior of the unmanned aerial vehicle main body, of the four assembling blocks, propeller blades are arranged on one ends, away from the unmanned aerial vehicle main body, of the four connecting arms, and four openings matched with the four propeller blades in position are formed in one side of the circumference of the unmanned aerial vehicle main body;
the disc lower extreme rotates and is equipped with the disk, four the equal fixed mounting of slider lower extreme has the connecting rod, disk circumference one side fixed mounting has the carousel, the carousel lower extreme seted up respectively with four connecting rod position assorted arc logical grooves, four the connecting rod leads to groove sliding connection with four arcs respectively, the disk lower extreme stretches out unmanned aerial vehicle main part fixed mounting has the disc, be equipped with locking Assembly between disc and the unmanned aerial vehicle main part, unmanned aerial vehicle main part lower extreme front side is equipped with the camera.
Locking Assembly includes the threaded rod, unmanned aerial vehicle main part lower extreme encircles around the fritter and has seted up a plurality of first screw holes, the disc lower extreme set up with a plurality of first screw hole position assorted second screw hole, it is a plurality of first screw hole and second screw hole all with threaded rod threaded connection, threaded rod threaded connection is in second screw threaded connection inside, the twist hand is installed to the threaded rod lower extreme.
The lower end of the unmanned aerial vehicle main body is detachably provided with a supporting mechanism, the supporting mechanism comprises two supporting components, and the two supporting components are respectively arranged on the left side and the right side of the lower end of the unmanned aerial vehicle main body;
the supporting component comprises two mounting blocks and a connecting rod, the mounting blocks are symmetrically mounted at the lower end of the unmanned aerial vehicle body in a front-back mode, the mounting blocks are close to one end and are provided with square grooves, matching grooves matched with the two square grooves in position are formed in the front end and the back end of the connecting rod respectively, the square blocks are assembled in the matching grooves in a sliding mode and are provided with springs and two springs, the spring other ends are fixedly connected with the inner walls of the two matching grooves respectively, the connecting rod is far away from one end of a disc and is provided with two communicating grooves, the communicating grooves are communicated with the two matching grooves respectively and are provided with stirring blocks in a sliding mode, the stirring blocks are two, one end of each stirring block is fixedly connected with the two square blocks respectively, and a stabilizing frame is mounted at the lower end of the connecting rod.
And shock pads are arranged at the lower ends of the two stabilizing frames.
Position tracker is installed to unmanned aerial vehicle main part upper end.
And an anti-slip pad is arranged on one side of the circumference of the disc.
The utility model discloses can accomodate the protection to four linking arms and four screw thread paddles when using, like this when accomodating the unmanned aerial vehicle main part, required storage space is littleer, portable and storage more, and when accomodating, the staff only need the rotating disc, alright in order to utilize the cooperation that four connecting rods and four arc led to the groove, accomplish to four linking arms and four screw thread paddles accomodate in stretching out, it is easy and simple to handle fast, can effectively promote staff's work efficiency.
Drawings
The invention can be further illustrated by means of non-limiting examples given in the figures.
Fig. 1 is a schematic structural diagram of a portable unmanned aerial vehicle according to the present invention;
fig. 2 is a schematic structural diagram of a portable unmanned aerial vehicle of the present invention;
fig. 3 is a third schematic structural view of the portable unmanned aerial vehicle of the present invention;
fig. 4 is a schematic structural diagram of a portable unmanned aerial vehicle according to the present invention;
fig. 5 is a schematic structural diagram of a portable unmanned aerial vehicle according to the present invention;
fig. 6 is a sixth schematic structural view of the portable unmanned aerial vehicle of the present invention;
fig. 7 is a first schematic structural diagram of a supporting mechanism of the portable unmanned aerial vehicle according to the present invention;
fig. 8 is a schematic structural view of a locking assembly of the portable unmanned aerial vehicle of the present invention;
fig. 9 is a schematic structural diagram of a supporting mechanism of a portable unmanned aerial vehicle according to the present invention;
fig. 10 is the utility model relates to a portable unmanned aerial vehicle's structural schematic diagram seven.
The main element symbols are as follows:
unmanned aerial vehicle main part 1, mounting disc 11, logical groove 12, slider 13, assembly piece 14, connecting arm 15, propeller blade 151, opening 16, circle piece 17, connecting rod 19, carousel 20, arc logical groove 201, disc 21, camera 22, threaded rod 23, first screw hole 24, second screw hole 25, twist hand 26, installation piece 27, connecting rod 28, square groove 281, matching groove 29, square piece 30, spring 31, intercommunication groove 32, stir piece 33, steady rest 34, shock pad 35, position tracker 36, slipmat 37.
Detailed Description
In order to make the present invention better understood by those skilled in the art, the technical solutions of the present invention are further described below with reference to the accompanying drawings and examples.
The first embodiment is as follows:
as shown in fig. 1-10, the utility model discloses a portable unmanned aerial vehicle, including unmanned aerial vehicle main part 1, fixed mounting plate 11 is installed inside unmanned aerial vehicle main part 1, four through grooves 12 have evenly been seted up to mounting plate 11 upper end, slider 13 has all been assembled to four through grooves 12 inside sliding, assembly block 14 has all been installed to four slider 13 upper ends, four assembly blocks 14 keep away from unmanned aerial vehicle main part 1 inside central one side all fixed mounting have linking arm 15, four linking arms 15 keep away from unmanned aerial vehicle main part 1 one end all install propeller blade 151, unmanned aerial vehicle main part 1 circumference one side is seted up with four openings 16 of propeller blade 151 position phase-match;
11 lower extremes of mounting disc rotate and are equipped with the disk 17, the equal fixed mounting of four slider 13 lower extremes has connecting rod 19, disk 17 circumference one side fixed mounting has carousel 20, 20 lower extremes of carousel are seted up respectively with four connecting rod 19 position assorted four arcs through groove 201, four connecting rod 19 lead to groove 201 sliding connection with four arcs respectively, disk 21 is stretched out to disk 17 lower extreme 1 fixed mounting of unmanned aerial vehicle main part, be equipped with locking Assembly between disk 21 and the unmanned aerial vehicle main part 1, 1 lower extreme front side of unmanned aerial vehicle main part is equipped with camera 22.
In an original state, the four propeller blades 151 including the four propeller blades 151 are all stored in the main unmanned aerial vehicle body 1, so that when the main unmanned aerial vehicle body 1 is stored, a smaller storage tool can be used for storing, so that the required occupied space is smaller, and the portable effect is achieved, the stored propeller blades 151 and the stored propeller blades 151 are more convenient for a user to take the main unmanned aerial vehicle body 1, when the worker needs to push the four propeller blades 151 out of the main unmanned aerial vehicle body 1, in the original state, the locking assembly is in a locking state, so that the disc 21 cannot rotate, the disc 18 cannot rotate, because the positions between the four arc-shaped through grooves 201 and the through grooves 12 are in a staggered arrangement, when the disc 18 cannot rotate, the position of the turntable 20 is locked, then the connecting rod 19 cannot slide in the arc-shaped through groove 201, and then the position of the connecting rod 19 is locked, in such a state, even if the main unmanned aerial vehicle body 1 falls, the four propeller blades 151 cannot extend out of the opening 16 due to vibration;
when the unmanned aerial vehicle main body 1 needs to be used, a worker firstly releases locking of the locking assemblies, then rotates the disc 21, the disc can drive the round block 17 to rotate, when the round block 17 rotates, the rotary disc 20 can be driven to rotate, because the four connecting rods 19 are in sliding connection with the four arc-shaped through grooves 201, when the rotary disc 20 rotates, the inclined planes on the inner sides of the arc-shaped through grooves 201 generate outward driving force, then the four connecting rods 19 are pushed out outwards at the same time, because the four sliding blocks 18 are in sliding connection with the four through grooves 12, the rotary block 17 needs to rotate at the moment, the sliding blocks 18 can be pushed by the driving force generated by the connecting rods 19, then the four sliding blocks 18 slide towards one side far away from the unmanned aerial vehicle main body 1 at the same time, then the assembling block 14 drives the connecting arms 15 and the propeller blades 151 to extend out of the unmanned aerial vehicle main body 1 through the openings 16, so that the extension of the plurality of the propeller blades 151 is completed at the same time, finally, the disc 21 is locked by the locking assemblies, and the limiting of the connecting rods 19 is completed;
when the storage is needed, after the staff contacts with the locking of the locking assembly, the staff rotates the disc 21 towards the other direction, the disc 21 drives the turntable 20 to rotate, the turntable 20 can drive the four arc-shaped through grooves 201 to rotate when rotating, at the moment, the inclined planes outside the arc-shaped through grooves 201 generate inward pushing force, the connecting rods 19 slide inwards in the arc-shaped through grooves 201, the simultaneous storage of the four connecting arms 15 and the four propeller blades 151 is realized, the locking assembly is used for locking after the storage is finished, and therefore the storage of the four propeller blades 151 is finished simultaneously;
the utility model discloses can accomodate the protection to four linking arms 15 and four screw thread paddle 151 when using, like this when accomodating unmanned aerial vehicle main part 1, required storage space is littleer, portable and storage more, and when accomodating, the staff only need the rotating disc 21, alright in order to utilize the cooperation that four connecting rods 19 and four arc lead to groove 201, accomplish accomodating in stretching out four linking arms 15 and four screw thread paddle 151, it is quick simple and convenient to operate, can effectively promote staff's work efficiency.
The locking assembly comprises a threaded rod 23, the lower end of the unmanned aerial vehicle main body 1 is provided with a plurality of first threaded holes 24 in a surrounding mode around the round block 17, the lower end of the disc 21 is provided with second threaded holes 25 matched with the first threaded holes 24 in position, the first threaded holes 24 and the second threaded holes 25 are in threaded connection with the threaded rod 23, the threaded rod 23 is in threaded connection with the inner portion of the second threaded hole 25, and the lower end of the threaded rod 23 is provided with a twisting hand 26; in an original state, the threaded rod 23 is in threaded connection with the second threaded hole 25 and is in threaded connection with one of the first threaded holes 25 at the same time, the disc 21 cannot rotate in the state, when the disc 21 needs to be rotated, a worker twists the twisting handle 26 to enable the threaded rod 23 to be separated from the connection with one of the first threaded holes 24, the disc 21 can be normally rotated, after the rotation is finished, the worker rotates the twisting handle 26 again to enable the twisting handle 26 to drive the threaded rod 23 to be connected with one of the first threaded holes 24 again, the locking can be completed, the locking is simple and convenient, and the locking is reliable.
Example two:
the unmanned aerial vehicle is further improved on the basis of the first embodiment, a supporting mechanism is detachably mounted at the lower end of the unmanned aerial vehicle main body 1, the supporting mechanism comprises two supporting components, and the two supporting components are respectively mounted at the left side and the right side of the lower end of the unmanned aerial vehicle main body 1;
the supporting assembly comprises two mounting blocks 27 and a connecting rod 28, the two mounting blocks 27 are symmetrically mounted at the lower end of the unmanned aerial vehicle main body 1 in a front-back mode, a square groove 281 is formed in one end, close to each other, of each mounting block 27, matching grooves 29 matched with the positions of the two square grooves 281 are formed in the front end and the rear end of the connecting rod 28 respectively, square blocks 30 are assembled in the two matching grooves 29 in a sliding mode, springs 31 are fixedly mounted at one ends, close to each other, of the two square blocks 30, the other ends of the two springs 31 are fixedly connected with the inner walls of the two matching grooves 29 respectively, two communicating grooves 32 are formed in one end, far away from the disc 21, of the connecting rod 28, the two communicating grooves 32 are communicated with the two matching grooves 29 respectively, shifting blocks 33 are assembled in the two communicating grooves 32 in a sliding mode, one ends of the two shifting blocks 33 are fixedly connected with the two square blocks 30 respectively, and a stabilizing frame 34 is mounted at the lower end of the connecting rod 28; under original state, four square blocks 30 are under four spring 31's effect, respectively partly stretch into in four square groove 281, accomplished the fixed mounting to two connecting rods 28 like this, two sets of stabilizer 34 can provide stable supporting power for unmanned aerial vehicle main part 1 like this, when needs are accomodate unmanned aerial vehicle main part 1, can dismantle two sets of stabilizer 34, when dismantling one of them group supporting component by priority when dismantling, the staff makes two stirring piece 33 be close to each other, then drive two square blocks 30 by two stirring piece 33 and be close to each other, thereby release among two square groove 281, just so accomplish the dismantlement to one of them group supporting component, dismantle two sets of supporting component alright like this in proper order, and easy operation is convenient, and the mounting means is similar with the dismantlement mode, do not have here to describe repeatedly.
The lower ends of the two stabilizing frames 34 are provided with shock-absorbing pads 35; when unmanned aerial vehicle body 1 rises and falls, shock pad 35 can play buffering cushioning effect, provides the protection to unmanned aerial vehicle body 1.
A position tracker 36 is arranged at the upper end of the unmanned aerial vehicle main body 1; like this when unmanned aerial vehicle main part 1 loses power and takes place to drop, position tracker 36 can be convenient for look for the position of unmanned aerial vehicle main part 1.
An anti-skid pad 37 is arranged on one side of the circumference of the disc 21; this makes it more comfortable for the worker to turn the disc 21.
The above embodiments are merely illustrative of the principles and effects of the present invention, and are not to be construed as limiting the invention. Modifications and variations can be made to the above-described embodiments by those skilled in the art without departing from the spirit and scope of the present invention. Accordingly, it is intended that all equivalent modifications or changes which may be made by those skilled in the art without departing from the spirit and technical spirit of the present invention be covered by the claims of the present invention.
Claims (6)
1. The utility model provides a portable unmanned aerial vehicle, includes the unmanned aerial vehicle main part, its characterized in that: the mounting disc is fixedly mounted inside the unmanned aerial vehicle main body, four through grooves are uniformly formed in the upper end of the mounting disc, sliding blocks are assembled inside the four through grooves in a sliding mode, assembling blocks are fixedly mounted at the upper ends of the four sliding blocks, connecting arms are fixedly mounted on the sides, away from the center of the inside of the unmanned aerial vehicle main body, of the four assembling blocks, propeller blades are mounted on the ends, away from the unmanned aerial vehicle main body, of the four connecting arms, and four openings matched with the four propeller blades in position are formed in one side of the circumference of the unmanned aerial vehicle main body;
the mounting disc lower extreme rotates and is equipped with the disk, four the equal fixed mounting of slider lower extreme has the connecting rod, disk circumference one side fixed mounting has the carousel, the carousel lower extreme seted up respectively with four connecting rod position assorted arc logical grooves, four the connecting rod leads to groove sliding connection with four arcs respectively, the disk lower extreme stretches out unmanned aerial vehicle main part fixed mounting has the disk, be equipped with locking Assembly between disk and the unmanned aerial vehicle main part, unmanned aerial vehicle main part lower extreme front side is equipped with the camera.
2. A portable drone according to claim 1, characterised in that: locking Assembly includes the threaded rod, unmanned aerial vehicle main part lower extreme encircles around the disk and has seted up a plurality of first screw holes, the disc lower extreme seted up with a plurality of first screw hole position assorted second screw hole, it is a plurality of first screw hole and second screw hole all with threaded rod threaded connection, threaded rod threaded connection is in second threaded hole inside, the twist hand is installed to the threaded rod lower extreme.
3. A portable drone according to claim 1, characterised in that: the lower end of the unmanned aerial vehicle main body is detachably provided with a supporting mechanism, the supporting mechanism comprises two supporting components, and the two supporting components are respectively arranged on the left side and the right side of the lower end of the unmanned aerial vehicle main body;
the supporting component comprises two mounting blocks and a connecting rod, the mounting blocks are symmetrically mounted at the lower end of the unmanned aerial vehicle body in a front-back mode, the mounting blocks are close to one end and are provided with square grooves, matching grooves matched with the two square grooves in position are formed in the front end and the back end of the connecting rod respectively, the square blocks are assembled in the matching grooves in a sliding mode and are provided with springs and two springs, the spring other ends are fixedly connected with the inner walls of the two matching grooves respectively, the connecting rod is far away from one end of a disc and is provided with two communicating grooves, the communicating grooves are communicated with the two matching grooves respectively and are provided with stirring blocks in a sliding mode, the stirring blocks are two, one end of each stirring block is fixedly connected with the two square blocks respectively, and a stabilizing frame is mounted at the lower end of the connecting rod.
4. A portable drone according to claim 3, characterised in that: and shock pads are arranged at the lower ends of the two stabilizing frames.
5. A portable drone according to claim 1, characterised in that: position tracker is installed to unmanned aerial vehicle main part upper end.
6. A portable drone according to claim 1, characterised in that: and an anti-slip pad is arranged on one side of the circumference of the disc.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222873407.8U CN218806531U (en) | 2022-10-28 | 2022-10-28 | Portable unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222873407.8U CN218806531U (en) | 2022-10-28 | 2022-10-28 | Portable unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218806531U true CN218806531U (en) | 2023-04-07 |
Family
ID=87268336
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222873407.8U Active CN218806531U (en) | 2022-10-28 | 2022-10-28 | Portable unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218806531U (en) |
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2022
- 2022-10-28 CN CN202222873407.8U patent/CN218806531U/en active Active
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