CN211663445U - High-endurance electric multifunctional unmanned aerial vehicle - Google Patents
High-endurance electric multifunctional unmanned aerial vehicle Download PDFInfo
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- CN211663445U CN211663445U CN202020027702.XU CN202020027702U CN211663445U CN 211663445 U CN211663445 U CN 211663445U CN 202020027702 U CN202020027702 U CN 202020027702U CN 211663445 U CN211663445 U CN 211663445U
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- 230000006835 compression Effects 0.000 claims description 22
- 238000007906 compression Methods 0.000 claims description 22
- 235000017166 Bambusa arundinacea Nutrition 0.000 claims description 8
- 235000017491 Bambusa tulda Nutrition 0.000 claims description 8
- 241001330002 Bambuseae Species 0.000 claims description 8
- 235000015334 Phyllostachys viridis Nutrition 0.000 claims description 8
- 239000011425 bamboo Substances 0.000 claims description 8
- 238000000926 separation method Methods 0.000 claims description 7
- 238000009434 installation Methods 0.000 claims description 5
- 230000003139 buffering effect Effects 0.000 abstract description 21
- 230000035939 shock Effects 0.000 abstract description 9
- 230000000712 assembly Effects 0.000 abstract description 2
- 238000000429 assembly Methods 0.000 abstract description 2
- 230000000903 blocking effect Effects 0.000 description 5
- 238000013016 damping Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
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Abstract
The utility model relates to the field of unmanned aerial vehicle equipment, in particular to an electric multifunctional unmanned aerial vehicle with high endurance, which comprises an unmanned aerial vehicle body; the unmanned aerial vehicle comprises an unmanned aerial vehicle body and is characterized in that the upper end of the unmanned aerial vehicle body is provided with four solar cell modules, the lower end of the unmanned aerial vehicle body is provided with a mounting plate, the lower end of the mounting plate is movably provided with a base through a buffer assembly, the lower end of the base is provided with a supporting leg, the lower end of the supporting leg is provided with a mounting seat, and the lower end of the mounting seat is hinged with; the left side and the right side of the lower end of the unmanned aerial vehicle body are provided with supports, the lower end of each support is provided with a centering assembly, and the left side and the right side of the base are arranged at the lower ends of the supports through the centering assemblies; high electronic multi-functional unmanned aerial vehicle of continuation of journey plays the buffering shock attenuation through the buffering subassembly when descending, guarantees through the subassembly of rightting that sets up when high electronic multi-functional unmanned aerial vehicle of continuation of journey descends the difficult position of bottom just has the buffering shock attenuation when deflecting the slope.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle equipment field specifically is an electronic multi-functional unmanned aerial vehicle of high continuation of journey.
Background
The pilotless aircraft is commonly known as an unmanned aircraft, an unmanned aerial vehicle, an unmanned combat aircraft and a bee-type aircraft, is a wide variety of remote control aircrafts without a pilot to board and drive in a broad sense, and is generally referred to as an unmanned reconnaissance aircraft in the military. The unmanned aerial vehicle is provided with no cockpit, but is provided with an automatic pilot, a program control device and other equipment. Unmanned aerial vehicles, as an embodiment of emerging technological forces, have penetrated the drip in modern civilization society.
Unmanned aerial vehicle among the prior art is because need go up and down many times, when descending, can cause great impact force to ground, if unmanned aerial vehicle does not set up better buffer, the huge impact force that produces when descending so will cause the damage to the inside accurate electron device of unmanned aerial vehicle, for reducing manufacturing cost among the prior art, adopt the mode of installation buffering frame to realize this technological effect usually, but the buffering shock attenuation effect of buffering frame is not too good, and still take place the offset easily when descending.
To the problem among the above-mentioned background art, the utility model discloses a brand-new structural design produces a high continuation of journey electronic multi-functional unmanned aerial vehicle.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an electronic multi-functional unmanned aerial vehicle of high continuation of journey to solve the problem that proposes in the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme:
the utility model provides an electronic multi-functional unmanned aerial vehicle of high continuation of journey, it includes: the unmanned aerial vehicle comprises an unmanned aerial vehicle body, wherein the unmanned aerial vehicle body is in a regular hexagon shape, wings are arranged around the edge of the unmanned aerial vehicle body, propellers are arranged on the wings, the number of the propellers is six, and the six propellers are distributed around the edge of the unmanned aerial vehicle body; the high-endurance electric multifunctional unmanned aerial vehicle is characterized in that the upper end of the unmanned aerial vehicle body is provided with four solar cell modules, the four solar cell modules can supply power independently and can also supply power by two, three or four functions simultaneously, and the high-endurance electric multifunctional unmanned aerial vehicle can realize long-time endurance;
the lower end of the unmanned aerial vehicle body is provided with a mounting plate, the lower end of the mounting plate is movably provided with a base through a buffering assembly, the lower end of the base is provided with a supporting leg, the lower end of the supporting leg is provided with a mounting seat, and the lower end of the mounting seat is hinged and movably provided with a roller; the unmanned aerial vehicle body lower extreme left and right sides is equipped with the support, and the subassembly of rightting is installed to the support lower extreme, and the base left and right sides is through righting the subassembly and installing at the support lower extreme.
As a further aspect of the present invention: the unmanned aerial vehicle body upper end is seted up flutedly, the inside rubber pad that is equipped with of recess, and the rubber pad lower extreme passes through fourth compression spring and the contact of recess inner wall, and when equipment solar cell module, place the back on the inside rubber pad of recess with solar cell module, the solar cell module left and right sides passes through the bolt erection fixed on the unmanned aerial vehicle body, can make the firm convenient to detach equipment of solar cell module installation through this kind of mode installation solar cell module, can guarantee again when high continuation of journey electronic multi-functional unmanned aerial vehicle receives violent striking, solar cell module bottom can cushion the shock attenuation, self can obtain effective protection.
As a further aspect of the present invention: the righting component comprises two limiting rods, the two limiting rods are respectively installed inside the groove, and the groove is formed in the lower end of the support.
As a further aspect of the present invention: base one end movable mounting all is equipped with first gleitbretter and first compression spring on the part of two gag lever posts upper and lower extreme position on the base simultaneously on two gag lever posts, and first gleitbretter and first compression spring echelon are arranged.
As a further aspect of the present invention: buffering subassembly includes loop bar, first separation blade and a movable section of thick bamboo, the installation of loop bar upper end is fixed on the mounting panel inner wall, and movable mounting is inside a movable section of thick bamboo behind the loop bar lower extreme passes first separation blade, first separation blade sets up in a movable section of thick bamboo upper end, and a movable section of thick bamboo lower extreme passes the mounting panel and connects the base.
As a further aspect of the present invention: inside the mounting panel, slidable mounting has second gleitbretter and third compression spring on the loop bar, and the second compression spring is installed to the movable cylinder on the part between first separation blade and mounting panel bottom inner wall.
Compared with the prior art, the beneficial effects of the utility model are that:
high continuation of journey electronic multi-functional unmanned aerial vehicle structural design reasonable, the function is various, has following advantage:
the long-time cruising operation is realized through the four solar battery modules, and the solar battery modules can be firmly installed and are convenient to disassemble and assemble, and can ensure that the bottom ends of the solar battery modules can buffer and absorb shock when the high cruising electric multifunctional unmanned aerial vehicle is violently impacted, so that the solar battery modules can be effectively protected;
the buffering and damping function is achieved through the buffering component during landing, and the buffering and damping function is achieved while the bottom end of the high-endurance electric multifunctional unmanned aerial vehicle is enabled not to deflect and incline easily during landing through the arranged righting component;
and thirdly, the high-endurance electric multifunctional unmanned aerial vehicle is convenient to move through the arranged idler wheels.
Drawings
Fig. 1 is the utility model discloses electronic multi-functional unmanned aerial vehicle's of high duration top view.
Fig. 2 is the utility model discloses a high continuation of journey electronic multi-functional unmanned aerial vehicle's elevation.
Fig. 3 is the utility model discloses a high continuation of the journey electronic multi-functional unmanned aerial vehicle's righting subassembly schematic structure.
Fig. 4 is the utility model discloses a high continuation of journey electronic multi-functional unmanned aerial vehicle's buffering subassembly schematic structure.
Fig. 5 is the utility model discloses a high continuation of the journey electronic multi-functional unmanned aerial vehicle's a department structure schematic diagram.
In the figure: the unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, a wing 2, a propeller 3, a solar cell module 4, a bracket 5, a righting assembly 6, a base 7, supporting legs 8, a mounting seat 9, rollers 10, a buffering assembly 11, a mounting plate 12, a slot 13, a first sliding sheet 14, a first compression spring 15, a limiting rod 16, a movable barrel 17, a second compression spring 18, a first blocking sheet 19, a loop bar 20, a second sliding sheet 21, a third compression spring 22, a rubber pad 23, a fourth compression spring 24 and a bolt 25.
Detailed Description
The technical solution of the present invention will be described in further detail with reference to the following embodiments.
Example 1
Referring to fig. 1 and 2, in embodiment 1 of the present invention, an electric multifunctional unmanned aerial vehicle with high endurance includes: the unmanned aerial vehicle comprises an unmanned aerial vehicle body 1, wherein the unmanned aerial vehicle body 1 is in a regular hexagon shape, wings 2 are arranged around the edge of the unmanned aerial vehicle body 1, propellers 3 are arranged on the wings 2, the number of the propellers 3 is six, and the six propellers 3 are distributed around the edge of the unmanned aerial vehicle body 1; the solar battery modules 4 are arranged at the upper end of the unmanned aerial vehicle body 1, the number of the solar battery modules 4 is four, and the four solar battery modules 4 can supply power independently and can also supply power by two, three or four functions simultaneously, so that the high-endurance electric multifunctional unmanned aerial vehicle can realize long-time endurance;
the lower end of the unmanned aerial vehicle body 1 is provided with a mounting plate 12, the lower end of the mounting plate 12 is movably provided with a base 7 through a buffer assembly 11, the lower end of the base 7 is provided with a supporting leg 8, the lower end of the supporting leg 8 is provided with a mounting seat 9, and the lower end of the mounting seat 9 is hinged and movably provided with a roller 10; the left side and the right side of the lower end of the unmanned aerial vehicle body 1 are provided with supports 5, the lower end of each support 5 is provided with a centering assembly 6, and the left side and the right side of the base 7 are arranged at the lower end of each support 5 through the centering assemblies 6;
high electronic multi-functional unmanned aerial vehicle of duration realize long-time duration operation through four solar cell modules 4 that set up, in addition, high electronic multi-functional unmanned aerial vehicle of duration plays the buffering shock attenuation through buffering subassembly 11 when descending, guarantees through the subassembly 6 of rightting that sets up when descending high electronic multi-functional unmanned aerial vehicle of duration is difficult for the position to deflect when inclining and has the buffering shock attenuation, is convenient for through gyro wheel 10 in addition high electronic multi-functional unmanned aerial vehicle of duration removes.
Please refer to fig. 5, further, a groove is formed in the upper end of the unmanned aerial vehicle body 1, a rubber pad 23 is arranged in the groove, the lower end of the rubber pad 23 contacts with the inner wall of the groove through a fourth compression spring 24, when the solar battery module 4 is assembled, the solar battery module 4 is placed on the rubber pad 23 in the groove, the left side and the right side of the solar battery module 4 are fixed on the unmanned aerial vehicle body 1 through bolts 25, and the solar battery module 4 is installed in such a way that the solar battery module 4 can be firmly installed and is convenient to disassemble and assemble, and the high-endurance electric multifunctional unmanned aerial vehicle can be guaranteed to be impacted violently, and the bottom end of the solar battery module 4 can be buffered and damped, so that the high-endurance electric multifunctional unmanned aerial vehicle can be.
Example 2
Referring to fig. 3, further, the righting assembly 6 includes two limiting rods 16, the two limiting rods 16 are respectively installed inside the open slot 13, and the open slot 13 is formed at the lower end of the support 5;
specifically, one end of the base 7 is movably mounted on two limiting rods 16 at the same time, the parts of the two limiting rods 16 at the upper and lower end positions of the base 7 are both provided with a first sliding sheet 14 and a first compression spring 15, and the first sliding sheet 14 and the first compression spring 15 are arranged in a gradient manner;
when the landing device lands, the left side and the right side of the base 7 respectively move up and down in the open groove 13 at the lower end of the bracket 5, and the base 7 is limited left and right through the two limiting rods 16 of the centering component 6, so that the base 7 is not easy to shift when the landing device lands; in addition, in the process of the up-and-down movement of the base 7, the base 7 which moves up and down violently is buffered and damped through the cooperation of the first compression spring 15 and the first sliding piece 14.
Referring to fig. 4, further, the buffering assembly 11 includes a loop bar 20, a first blocking piece 19 and a movable cylinder 17, the upper end of the loop bar 20 is fixedly installed on the inner wall of the mounting plate 12, the lower end of the loop bar 20 passes through the first blocking piece 19 and is movably installed inside the movable cylinder 17, the first blocking piece 19 is arranged at the upper end of the movable cylinder 17, and the lower end of the movable cylinder 17 passes through the mounting plate 12 and then is connected to the base 7;
specifically, inside the mounting plate 12, a second sliding piece 21 and a third compression spring 22 are slidably mounted on the loop bar 20, and a second compression spring 18 is mounted on the part of the movable cylinder 17 between the first blocking piece 19 and the inner wall of the bottom end of the mounting plate 12;
when the high-endurance electric multifunctional unmanned aerial vehicle lands, the third compression spring 22 and the second compression spring 18 in the buffer assembly 11 are matched to play a role in buffering and damping the high-endurance electric multifunctional unmanned aerial vehicle up and down, so that the damping effect of the high-endurance electric multifunctional unmanned aerial vehicle is improved;
the rest of the structure of example 2 is the same as example 1.
The utility model discloses a theory of operation is:
high electronic multi-functional unmanned aerial vehicle of duration realize long-time duration operation through four solar cell modules 4 that set up, in addition, high electronic multi-functional unmanned aerial vehicle of duration plays the buffering shock attenuation through buffering subassembly 11 when descending, guarantees through the subassembly 6 of rightting that sets up when descending high electronic multi-functional unmanned aerial vehicle of duration descends the difficult deflection position slope of bottom in the time and have the buffering shock attenuation, is convenient for through gyro wheel 10 in addition high electronic multi-functional unmanned aerial vehicle of duration removes.
Although the preferred embodiments of the present invention have been described in detail, the present invention is not limited to the above embodiments, and various changes can be made without departing from the spirit of the present invention within the scope of knowledge possessed by those skilled in the art.
Claims (8)
1. The utility model provides an electronic multi-functional unmanned aerial vehicle of high continuation of journey, it includes: unmanned aerial vehicle body (1), its characterized in that: the unmanned aerial vehicle is characterized in that the unmanned aerial vehicle body (1) is regular hexagonal, the lower end of the unmanned aerial vehicle body (1) is provided with a mounting plate (12), the lower end of the mounting plate (12) is movably provided with a base (7) through a buffer assembly (11), the lower end of the base (7) is provided with a supporting leg (8), the lower end of the supporting leg (8) is provided with a mounting seat (9), and the lower end of the mounting seat (9) is hinged and movably provided with a roller (; unmanned aerial vehicle body (1) lower extreme left and right sides is equipped with support (5), and support (5) lower extreme is installed and is right subassembly (6), and base (7) left and right sides is installed at support (5) lower extreme through right subassembly (6).
2. The high endurance electric multifunctional unmanned aerial vehicle of claim 1, wherein: wings (2) are arranged on the periphery of the edge of the unmanned aerial vehicle body (1), the wings (2) are provided with six propellers (3), and the six propellers (3) are distributed on the periphery of the edge of the unmanned aerial vehicle body (1); unmanned aerial vehicle body (1) upper end is equipped with solar cell module (4), and the quantity of solar cell module (4) is four.
3. The high endurance electric multifunctional unmanned aerial vehicle of claim 1, wherein: the unmanned aerial vehicle body (1) upper end is seted up flutedly, and the recess is inside to be equipped with rubber pad (23), and rubber pad (23) lower extreme passes through fourth compression spring (24) and the contact of recess inner wall, and when equipment solar cell module (4), with solar cell module (4) place back on the inside rubber pad (23) of recess, the bolt (25) erection fixation is passed through on unmanned aerial vehicle body (1) in the solar cell module (4) left and right sides.
4. The high endurance electric multifunctional unmanned aerial vehicle of claim 1, wherein: righting subassembly (6) and including gag lever post (16), the quantity of gag lever post (16) is two, and two gag lever posts (16) are installed respectively inside fluting (13), and fluting (13) are seted up at support (5) lower extreme.
5. The high endurance electric multifunctional unmanned aerial vehicle of claim 4, wherein: one end of the base (7) is movably mounted on the two limiting rods (16), the two limiting rods (16) are respectively provided with a first sliding sheet (14) and a first compression spring (15) at the upper end and the lower end of the base (7), and the first sliding sheet (14) and the first compression spring (15) are arranged in a gradient manner.
6. The high endurance electric multifunctional unmanned aerial vehicle of claim 1, wherein: buffer unit (11) include loop bar (20), first separation blade (19) and a movable section of thick bamboo (17), loop bar (20) upper end installation is fixed on mounting panel (12) inner wall, and movable mounting is inside a movable section of thick bamboo (17) behind loop bar (20) lower extreme passing first separation blade (19), first separation blade (19) set up in a movable section of thick bamboo (17) upper end, and a movable section of thick bamboo (17) lower extreme passes mounting panel (12) back connection base (7).
7. The high endurance electric multifunctional unmanned aerial vehicle of claim 6, wherein: inside the mounting plate (12), a second sliding sheet (21) and a third compression spring (22) are slidably mounted on the loop bar (20).
8. The high endurance electric multifunctional unmanned aerial vehicle of claim 6, wherein: inside the mounting plate (12), a second compression spring (18) is mounted on the part of the movable cylinder (17) between the first baffle plate (19) and the inner wall of the bottom end of the mounting plate (12).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020027702.XU CN211663445U (en) | 2020-01-07 | 2020-01-07 | High-endurance electric multifunctional unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020027702.XU CN211663445U (en) | 2020-01-07 | 2020-01-07 | High-endurance electric multifunctional unmanned aerial vehicle |
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| CN211663445U true CN211663445U (en) | 2020-10-13 |
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| CN202020027702.XU Expired - Fee Related CN211663445U (en) | 2020-01-07 | 2020-01-07 | High-endurance electric multifunctional unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111071443A (en) * | 2020-01-07 | 2020-04-28 | 北京致媒科技有限公司 | A high-endurance electric multi-function unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111071443A (en) * | 2020-01-07 | 2020-04-28 | 北京致媒科技有限公司 | A high-endurance electric multi-function unmanned aerial vehicle |
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| CF01 | Termination of patent right due to non-payment of annual fee |