CN213566452U - High unmanned aerial vehicle of security - Google Patents
High unmanned aerial vehicle of security Download PDFInfo
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- CN213566452U CN213566452U CN202022504072.3U CN202022504072U CN213566452U CN 213566452 U CN213566452 U CN 213566452U CN 202022504072 U CN202022504072 U CN 202022504072U CN 213566452 U CN213566452 U CN 213566452U
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- 238000001514 detection method Methods 0.000 claims description 9
- 238000013016 damping Methods 0.000 claims description 7
- 230000001681 protective effect Effects 0.000 claims description 7
- 239000006260 foam Substances 0.000 claims description 6
- 238000004891 communication Methods 0.000 claims description 5
- 230000007246 mechanism Effects 0.000 claims description 5
- 229920003023 plastic Polymers 0.000 claims description 3
- 239000004033 plastic Substances 0.000 claims description 3
- 238000013461 design Methods 0.000 abstract description 2
- 230000000694 effects Effects 0.000 description 12
- 238000005516 engineering process Methods 0.000 description 6
- 238000000034 method Methods 0.000 description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 4
- 238000010276 construction Methods 0.000 description 3
- 230000003139 buffering effect Effects 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
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Abstract
The utility model discloses an unmanned aerial vehicle with high safety, including the unmanned aerial vehicle main part, unmanned aerial vehicle main part bottom is provided with four connecting blocks, the unmanned aerial vehicle main part bottom is through connecting block fixedly connected with landing leg, landing leg bottom fixedly connected with damper, unmanned aerial vehicle main part side surface equidistance fixedly connected with support, support one end fixedly connected with brace table, brace table top fixedly connected with round platform, the round platform is through pivot fixedly connected with paddle, unmanned aerial vehicle main part top fixedly connected with housing, the inside battery that is provided with of housing, housing top equidistance is provided with four draw-in grooves, the housing top is provided with GPS, unmanned aerial vehicle main part bottom fixedly connected with camera, the inside, this kind of high unmanned aerial vehicle of security, simple structure is reasonable, and the modern design has higher practicality in the aspect of the unmanned aerial vehicle to the security height.
Description
Technical Field
The utility model relates to a high unmanned aerial vehicle technical field of security specifically is a high unmanned aerial vehicle of security.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle controlled by a radio remote control device or an onboard computer program control system. The unmanned aerial vehicle is simple in structure and low in use cost, not only can complete the task executed by the piloted aircraft, but also is more suitable for the task which is not suitable for being executed by the piloted aircraft. The emergency early warning device has great effect on emergency and early warning of emergencies. The unmanned aerial vehicle aerial photography uses an unmanned aerial vehicle as an aerial platform, uses airborne remote sensing equipment such as a high-resolution digital camera, a light optical camera, an infrared scanner, a laser scanner, a magnetic measuring instrument and the like to acquire information, processes image information by using a computer, and makes images according to certain precision requirements. The whole system has outstanding characteristics in the aspects of design and optimal combination, and is a novel application technology integrating high-altitude shooting, remote control, remote measuring technology, video image microwave transmission and computer image information processing. The unmanned aerial vehicle is used for carrying out the small-area remote sensing aerial photography technology, and obvious effect and experience are obtained in practice. The micro aerial remote sensing technology with the unmanned aerial vehicle as the aerial remote sensing platform adapts to the requirements of national economic and cultural construction development, and provides an effective remote sensing technology service means for economic and cultural construction of small and medium-sized cities, particularly cities, towns, counties, villages and other areas. The remote sensing aerial photography technology has an important promotion effect on the development of the economy of China. And the unmanned aerial vehicle security performance for the inspection plate storehouse in the existing market is poor, runs into the collision back, and the paddle is difficult to rotate for unmanned aerial vehicle can't fly, causes unmanned aerial vehicle to fall, thereby can bring the loss for the economy, does not have safeguard measure after falling moreover. Therefore, the unmanned aerial vehicle with high safety is provided by improving the unmanned aerial vehicle.
SUMMERY OF THE UTILITY MODEL
In order to solve the technical problem, the utility model provides a following technical scheme:
the utility model relates to a high unmanned aerial vehicle of security, including the unmanned aerial vehicle main part, unmanned aerial vehicle main part bottom is provided with four connecting blocks, connecting block fixedly connected with landing leg is passed through to unmanned aerial vehicle main part bottom, landing leg bottom fixedly connected with damper, unmanned aerial vehicle main part side surface equidistance fixedly connected with support, support one end fixedly connected with brace table, brace table top fixedly connected with round platform, the round platform is through pivot fixedly connected with paddle, unmanned aerial vehicle main part top fixedly connected with housing, the inside battery that is provided with of housing, housing top equidistance is provided with four draw-in grooves, the housing top is provided with GPS, unmanned aerial vehicle main part bottom fixedly connected with camera, the inside wireless communication module that is provided with of unmanned.
As an optimal technical scheme of the utility model, four the equal fixedly connected with protecting crust in paddle outside, the protecting crust is made by plastics and is the lattice construction.
As a preferred technical scheme of the utility model, unmanned aerial vehicle main part bottom fixedly connected with acceleration sensor, unmanned aerial vehicle main part bottom fixedly connected with magnetic sensor, acceleration sensor and magnetic sensor and wireless communication module electric connection.
As an optimal technical scheme of the utility model, fixedly connected with horizontal pole between the landing leg, the outside parcel of horizontal pole has the showy foam.
As a preferred technical scheme of the utility model, the inside swing joint of draw-in groove has the stand, stand top fixedly connected with chassis, chassis top fixedly connected with parachute box, the inside shrink parachute that is provided with of parachute box, shrink parachute electric connection has acceleration sensor.
As a preferred technical scheme of the utility model, damper includes fixed landing leg, activity landing leg and elastic component, and the elastic component has all been welded to the inner chamber bottom of activity landing leg and the bottom of fixed landing leg, and the bottom of activity landing leg all has the gyro wheel through bolt fixed mounting.
As a preferred technical scheme of the utility model, unmanned aerial vehicle main part electric connection has the controller, the inside detection module that is provided with of battery, detection module electric connection has the controller.
As an optimized technical scheme of the utility model, four brace table bottom is provided with the pilot lamp, pilot lamp electric connection has acceleration sensor.
The utility model has the advantages that: by arranging the protective shell, the protective shell can keep rotating continuously to fly when encountering collision, and the rotating blades can not hurt people by mistake; through being provided with acceleration sensor and magnetic sensor, acceleration sensor can run into when the special conditions descends rapidly at unmanned aerial vehicle, and acceleration sensor can detect and convey to the controller, and magnetic sensor can provide the direction sense for unmanned aerial vehicle, and it can provide the device at the data of each axial of XYZ born the magnetic field. Then, relevant data can be imported into an operation method of the microcontroller to provide a heading angle relevant to magnetic north pole, and then the information can be used for detecting the geographic position, so that normal navigation can be performed no matter whether rain or snow weather exists, and the safety is high; by arranging the cross rod, the strength between the support legs can be enhanced, and the wrapping foam is arranged, so that the unmanned aerial vehicle cannot fall into water when falling into the water, can float, protect the unmanned aerial vehicle and prevent damage; by arranging the parachute box, when the unmanned aerial vehicle drops emergently, the unmanned aerial vehicle can be buffered through the parachute, so that the unmanned aerial vehicle can slowly land without serious damage, and the safety is greatly improved; by arranging the damping mechanism, when the unmanned aerial vehicle lands, the unmanned aerial vehicle can be damped and buffered, so that the unmanned aerial vehicle cannot be damaged, and the damping effect is better and the safety is improved through the rollers; through being provided with detection module, can detect the electric quantity of battery, cross when the electric quantity low and remind, prevent that unmanned aerial vehicle does not have the electric quantity to take place to fall.
Drawings
The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention. In the drawings:
fig. 1 is a schematic view of a main structure of an unmanned aerial vehicle with high safety;
fig. 2 is a schematic plan view of the unmanned aerial vehicle with high safety of the present invention;
fig. 3 is a schematic view of the parachute structure of the unmanned aerial vehicle with high safety;
fig. 4 is the utility model relates to a high unmanned aerial vehicle's of security damper structure schematic diagram.
In the figure: 1. an unmanned aerial vehicle main body; 2. a support leg; 3. a damping mechanism; 301. fixing the supporting legs; 302. A movable leg; 303. an elastic member; 304. a roller; 4. a support; 5. a support table; 6. a circular truncated cone; 7. a paddle; 701. a protective shell; 8. a housing; 9. a card slot; 10. a GPS; 11. a camera; 12. an acceleration sensor; 13. a magnetic sensor; 14. a cross bar; 15. a column; 16. A chassis; 17. a parachute box.
Detailed Description
In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.
As shown in fig. 1-4, the utility model relates to a high unmanned aerial vehicle of security, including unmanned aerial vehicle main part 1, 1 bottom of unmanned aerial vehicle main part is provided with four connecting blocks, connecting block fixedly connected with landing leg 2 is passed through to 1 bottom of unmanned aerial vehicle main part, 2 bottom fixedly connected with damper 3 of landing leg, 1 side surface equidistance fixedly connected with support 4 of unmanned aerial vehicle main part, 4 one end fixedly connected with brace table 5 of support, 5 top fixedly connected with round platform 6 of brace table, round platform 6 is through pivot fixedly connected with paddle 7, 1 top fixedly connected with housing 8 of unmanned aerial vehicle main part, the inside battery that is provided with of housing 8, 8 top equidistance of housing are provided with four draw-in grooves 9, 8 tops of housing are provided with GPS10, 1 bottom.
Wherein, the equal fixedly connected with protecting crust 701 in four paddle 7 outsides, protecting crust 701 is made by plastics and is the grid structure, and through being provided with the protecting crust, the protecting crust can keep continuing the rotation when meetting the collision, flies, and the people can not be hindered to the paddle in the rotation by mistake.
Wherein, 1 bottom fixedly connected with acceleration sensor 12 of unmanned aerial vehicle main part, 1 bottom fixedly connected with magnetic sensor 13 of unmanned aerial vehicle main part, acceleration sensor 12 and magnetic sensor 13 and wireless communication module electric connection, through being provided with acceleration sensor and magnetic sensor, acceleration sensor can meet when the special conditions descends rapidly at unmanned aerial vehicle, acceleration sensor can detect and convey the controller to, magnetic sensor can provide the direction sense for unmanned aerial vehicle, it can provide the device at the data in each axial magnetic field that XYZ bore. Then the related data can be imported into an operation method of the microcontroller to provide a heading angle related to magnetic north pole, and then the information can be used for detecting the geographic position, so that normal navigation can be performed no matter whether the weather is rainy or snowy, and the safety is high.
Wherein, fixedly connected with horizontal pole 14 between landing leg 2, 14 outside parcels of horizontal pole have showy foam, and through being provided with the horizontal pole, intensity between the landing leg can be strengthened to the horizontal pole, and is provided with the parcel foam and can not fall into the aquatic when can making unmanned aerial vehicle fall to the aquatic, can float, protects unmanned aerial vehicle, prevents to damage.
Wherein, the inside swing joint of draw-in groove 9 has stand 15, 15 top fixedly connected with chassis 16 of stand, 16 top fixedly connected with parachute box 17 on chassis, the inside shrink parachute that is provided with of parachute box 17, shrink parachute electric connection has acceleration sensor 12, through being provided with the parachute box, can cushion through the parachute when unmanned aerial vehicle promptly drops, makes unmanned aerial vehicle can slowly descend, can not damage seriously, greatly increased the security.
Wherein, damper 3 includes fixed landing leg 301, activity landing leg 302 and elastic component 303, the elastic component 303 of all welding in the inner chamber bottom of activity landing leg 302 and the bottom of fixed landing leg 301, there is gyro wheel 304 bottom of activity landing leg 302 all through bolt fixed mounting, through being provided with damper, when unmanned aerial vehicle descends, can carry out the shock attenuation buffering to unmanned aerial vehicle, make unmanned aerial vehicle can not receive the damage, and it is better to make the buffering shock attenuation effect through the gyro wheel, increase the security.
Wherein, 1 electric connection of unmanned aerial vehicle main part has the controller, and the inside detection module that is provided with of battery, detection module electric connection have the controller, through being provided with detection module, can detect the electric quantity of battery, crosses when the electric quantity low and reminds, prevents that unmanned aerial vehicle does not have the electric quantity to take place to fall.
Wherein, four brace table 5 bottoms are provided with the pilot lamp, and pilot lamp electric connection has acceleration sensor 12.
When the aircraft works, the protective shell 701 is arranged, so that the protective shell 701 can keep rotating continuously to fly when colliding, and the rotating blades cannot hurt people by mistake; through being provided with acceleration sensor 12 and magnetic sensor 13, acceleration sensor 12 can be when unmanned aerial vehicle meets special conditions and descends rapidly, and acceleration sensor 12 can detect and convey to the controller, and magnetic sensor 13 can provide the direction sense for unmanned aerial vehicle, and it can provide the device in the data of the each axial magnetic field that bears of XYZ. Then, relevant data can be imported into an operation method of the microcontroller to provide a heading angle relevant to magnetic north pole, and then the information can be used for detecting the geographic position, so that normal navigation can be performed no matter whether rain or snow weather exists, and the safety is high; by arranging the cross rod 14, the strength between the support legs 2 can be enhanced by the cross rod 14, and the wrapping foam is arranged, so that the unmanned aerial vehicle cannot fall into water when falling into the water, can float, protect the unmanned aerial vehicle and prevent damage; by arranging the parachute box 17, when the unmanned aerial vehicle drops emergently, the unmanned aerial vehicle can be buffered through the parachute, so that the unmanned aerial vehicle can slowly land without serious damage, and the safety is greatly improved; by arranging the damping mechanism 3, when the unmanned aerial vehicle lands, the unmanned aerial vehicle can be damped and buffered, so that the unmanned aerial vehicle cannot be damaged, and the damping effect is better and the safety is improved through the rollers 304; through being provided with detection module, can detect the electric quantity of battery, cross when the electric quantity low and remind, prevent that unmanned aerial vehicle does not have the electric quantity to take place to fall.
Finally, it should be noted that: in the description of the present invention, it should be noted that the terms "vertical", "upper", "lower", "horizontal", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed in a specific orientation, and be operated, and thus should not be construed as limiting the present invention.
In the description of the present invention, it should also be noted that, unless otherwise explicitly specified or limited, the terms "disposed," "mounted," "connected," and "connected" are to be construed broadly, e.g., as meaning either a fixed connection, a removable connection, or an integral connection; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.
Although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the embodiments described in the foregoing embodiments, or equivalents may be substituted for elements thereof. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (8)
1. An unmanned aerial vehicle with high safety comprises an unmanned aerial vehicle main body (1) and is characterized in that four connecting blocks are arranged at the bottom end of the unmanned aerial vehicle main body (1), supporting legs (2) are fixedly connected to the bottom end of the unmanned aerial vehicle main body (1) through the connecting blocks, a damping mechanism (3) is fixedly connected to the bottom ends of the supporting legs (2), a support (4) is fixedly connected to the surface of the side surface of the unmanned aerial vehicle main body (1) at equal intervals, a supporting table (5) is fixedly connected to one end of the support (4), a round table (6) is fixedly connected to the top end of the supporting table (5), paddles (7) are fixedly connected to the round table (6) through a rotating shaft, a housing (8) is fixedly connected to the top end of the unmanned aerial vehicle main body (1), a storage battery is arranged inside the housing, unmanned aerial vehicle main part (1) bottom fixedly connected with camera (11), unmanned aerial vehicle main part (1) inside is provided with wireless communication module.
2. An unmanned aerial vehicle with high safety as claimed in claim 1, wherein a protective shell (701) is fixedly connected to the outside of each of the four blades (7), and the protective shell (701) is made of plastic and is of a grid structure.
3. The unmanned aerial vehicle with high safety as claimed in claim 1, wherein the bottom end of the unmanned aerial vehicle main body (1) is fixedly connected with an acceleration sensor (12), the bottom end of the unmanned aerial vehicle main body (1) is fixedly connected with a magnetic sensor (13), the acceleration sensor (12) and the magnetic sensor (13) are electrically connected with a wireless communication module, and the acceleration sensor is CT1005 LC.
4. The unmanned aerial vehicle with high safety as claimed in claim 1, wherein a cross bar (14) is fixedly connected between the supporting legs (2), and floating foam is wrapped outside the cross bar (14).
5. The high unmanned aerial vehicle of a security according to claim 1, characterized in that, inside swing joint of draw-in groove (9) has stand (15), stand (15) top fixedly connected with chassis (16), chassis (16) top fixedly connected with parachute box (17), the inside shrink parachute that is provided with of parachute box (17), shrink parachute electric connection has acceleration sensor (12).
6. The unmanned aerial vehicle with high safety as claimed in claim 1, wherein the damping mechanism (3) comprises a fixed leg (301), a movable leg (302) and an elastic part (303), the elastic part (303) is welded to the bottom of the inner cavity of the movable leg (302) and the bottom of the fixed leg (301), and rollers (304) are fixedly mounted on the bottoms of the movable legs (302) through bolts.
7. The unmanned aerial vehicle with high safety according to claim 1, wherein the unmanned aerial vehicle body (1) is electrically connected with a controller, the storage battery is internally provided with a detection module, and the detection module is electrically connected with the controller.
8. An unmanned aerial vehicle with high safety according to claim 1, wherein indicator lamps are arranged at the bottoms of the four support platforms (5), and the indicator lamps are electrically connected with acceleration sensors (12).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022504072.3U CN213566452U (en) | 2020-11-03 | 2020-11-03 | High unmanned aerial vehicle of security |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022504072.3U CN213566452U (en) | 2020-11-03 | 2020-11-03 | High unmanned aerial vehicle of security |
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| Publication Number | Publication Date |
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| CN213566452U true CN213566452U (en) | 2021-06-29 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202022504072.3U Expired - Fee Related CN213566452U (en) | 2020-11-03 | 2020-11-03 | High unmanned aerial vehicle of security |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113859525A (en) * | 2021-11-16 | 2021-12-31 | 山东省国土测绘院 | High remote sensing survey and drawing unmanned aerial vehicle of security |
| CN113895622A (en) * | 2021-10-20 | 2022-01-07 | 新沂阿凡达智能科技有限公司 | Unmanned aerial vehicle's safety protection structure |
-
2020
- 2020-11-03 CN CN202022504072.3U patent/CN213566452U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113895622A (en) * | 2021-10-20 | 2022-01-07 | 新沂阿凡达智能科技有限公司 | Unmanned aerial vehicle's safety protection structure |
| CN113859525A (en) * | 2021-11-16 | 2021-12-31 | 山东省国土测绘院 | High remote sensing survey and drawing unmanned aerial vehicle of security |
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210629 |
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| CF01 | Termination of patent right due to non-payment of annual fee |