CN220430584U - Vehicle-mounted unmanned aerial vehicle take-off and landing device - Google Patents
Vehicle-mounted unmanned aerial vehicle take-off and landing device Download PDFInfo
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- CN220430584U CN220430584U CN202321816907.6U CN202321816907U CN220430584U CN 220430584 U CN220430584 U CN 220430584U CN 202321816907 U CN202321816907 U CN 202321816907U CN 220430584 U CN220430584 U CN 220430584U
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- 239000000872 buffer Substances 0.000 claims abstract description 50
- 239000003550 marker Substances 0.000 claims description 11
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 6
- 238000007789 sealing Methods 0.000 claims description 4
- 238000013016 damping Methods 0.000 claims description 3
- 229910052742 iron Inorganic materials 0.000 claims description 3
- 238000009434 installation Methods 0.000 abstract description 2
- 238000012423 maintenance Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 230000007246 mechanism Effects 0.000 description 3
- 230000008439 repair process Effects 0.000 description 3
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000013480 data collection Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
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Abstract
The utility model provides a vehicle-mounted unmanned aerial vehicle lifting device, which comprises: the lifting platform comprises a lifting platform and a vehicle-mounted platform, wherein the vehicle-mounted platform is arranged below the lifting platform, the upper surface of the vehicle-mounted platform is sunken downwards to form a landing buffer groove, a plurality of groups of spring buffers are arranged in the landing buffer groove, and two electromagnetic chucks are respectively arranged on the left side and the right side of the upper surface of the lifting platform. Through setting up dashpot and multiunit spring buffer, when unmanned aerial vehicle falls on the landing platform, can cushion the impact force that brings when descending unmanned aerial vehicle, make unmanned aerial vehicle's undercarriage not fragile, promote the life of undercarriage, through setting up electromagnet and pre-installation piece, through installing the pre-loading board in unmanned aerial vehicle undercarriage below, when unmanned aerial vehicle falls on the landing platform, can adsorb the pre-loading board through making electromagnet lead to, thereby make unmanned aerial vehicle be difficult for removing after the landing platform, stability is better.
Description
Technical Field
The utility model belongs to the technical field of vehicle-mounted unmanned aerial vehicles, and particularly relates to a vehicle-mounted unmanned aerial vehicle take-off and landing device.
Background
The vehicle-mounted unmanned aerial vehicle is an unmanned aerial vehicle system arranged on a vehicle. The device has the functions of autonomous flight, hovering, image acquisition and the like, and can be used in the fields of aerial photography, monitoring, rescue and the like. The unmanned plane has the characteristics of small portability, rapid deployment and flexible operation, can perform remote monitoring and data collection in the running process of the vehicle, provides real-time information and visual angles, and provides practical value for various tasks. The lack of a buffer mechanism while the drone is landing can lead to a series of drawbacks and problems.
Landing gear damage: due to the non-cushioning mechanism, the landing gear of the unmanned aerial vehicle is subjected to large impacts and pressures at each landing. Such impacts may cause structural deformation, material fatigue and damage to the landing gear, reducing its reliability and life.
Unmanned aerial vehicle damages: damage to the landing gear of a vehicle-mounted unmanned aerial vehicle may cause more serious problems, directly leading to damage or even failure of the unmanned aerial vehicle. For example, landing gear damage may cause the drone to lose balance during landing, roll over or strike the ground, causing serious damage to the drone.
Safety risk: damage to the landing gear may raise a safety hazard. For example, if the landing gear breaks or fails while the drone is landing, it may not land smoothly, resulting in an accident. This not only endangers the drone itself, but may also cause damage to the surrounding environment and personnel.
The maintenance cost is increased: vehicle-mounted unmanned aerial vehicle landing gear damage requires repair or replacement, which increases maintenance and repair costs. Frequent landing gear repairs may result in unstable unmanned aerial vehicle operation, requiring more maintenance time and capital investment. This can have a negative impact on the operating costs of the drone.
Limiting task capabilities: the risk of landing gear damage may limit the range and capabilities of the unmanned aerial vehicle's tasks. Unmanned aerial vehicles that cannot land safely may not land and take off in place, limiting their ability to be used in complex environments.
In summary, the lack of a buffer mechanism of the vehicle-mounted unmanned aerial vehicle during landing can cause serious drawbacks such as damage to the landing gear and damage to the unmanned aerial vehicle, so that we have developed a vehicle-mounted unmanned aerial vehicle landing device to solve the above problems.
Disclosure of Invention
Aiming at the defects existing in the prior art, the utility model aims to provide a vehicle-mounted unmanned aerial vehicle lifting device, which solves the problems in the background art.
The utility model is realized by the following technical scheme: a vehicle-mounted unmanned aerial vehicle landing gear, comprising: the lifting platform and the vehicle-mounted platform are arranged below the lifting platform, and the upper surface of the vehicle-mounted platform is sunken downwards to form a landing buffer groove;
a plurality of groups of spring buffers are arranged in the landing buffer groove, and two electromagnetic chucks are respectively arranged on the left side and the right side of the upper surface of the landing platform;
two preassembling sheets are arranged above the lifting platform, outline marker light bars are arranged on the periphery of the upper surface of the lifting platform, and sealing rubber bars are arranged on Fang Sizhou of the landing buffer groove.
As a preferable implementation mode, the length and the width of the landing buffer groove are larger than those of the landing platform, the lower part of the landing platform stretches into the landing buffer groove to be connected with the upper surfaces of the plurality of groups of spring buffers, and the unmanned aerial vehicle can land above the landing platform.
As a preferred embodiment, four spring buffers are arranged in each group, and a plurality of groups of the spring buffers are distributed in a rectangular shape in a top view.
As a preferable implementation mode, the lower surface of the vehicle-mounted table is glued with a double-sided adhesive sheet, and the lower surface of the double-sided adhesive sheet is glued with release paper.
As a preferred embodiment, the top surface of the preassembled sheet is of a circular structure, and the lower parts of the spring bumpers are connected with the lower parts of the inner parts of the landing buffer grooves.
As a preferred embodiment, the electromagnetic chuck is a ZYE06 circular electromagnetic chuck, the outline marker light bar is an LED light bar, and the outline marker light bar can display the outline of the lifting platform 100 after being lighted
As a preferred embodiment, the spring buffer is an HT3-1250 small damping spring buffer, the material of the pre-installed sheet is iron, and the spring buffer can buffer and absorb impact force.
After the technical scheme is adopted, the utility model has the beneficial effects that: through setting up dashpot and multiunit spring buffer, when unmanned aerial vehicle falls on the landing platform, can cushion the impact force that brings when descending unmanned aerial vehicle, make unmanned aerial vehicle's undercarriage not fragile, promote the life of undercarriage, through setting up electromagnet and pre-installation piece, through installing the pre-loading board in unmanned aerial vehicle undercarriage below, when unmanned aerial vehicle falls on the landing platform, can adsorb the pre-loading board through making electromagnet lead to, thereby make unmanned aerial vehicle be difficult for removing after the landing platform, stability is better.
Drawings
In order to more clearly illustrate the embodiments of the utility model or the technical solutions of the prior art, the drawings which are used in the description of the embodiments or the prior art will be briefly described, it being obvious that the drawings in the description below are only some embodiments of the utility model, and that other drawings can be obtained according to these drawings without inventive faculty for a person skilled in the art.
Fig. 1 is a schematic diagram of the overall structure of a take-off and landing device of a vehicle-mounted unmanned aerial vehicle.
Fig. 2 is a schematic diagram of a front section of a vehicle-mounted table in the lifting device of the vehicle-mounted unmanned aerial vehicle.
Fig. 3 is an enlarged schematic view of a portion a of fig. 1.
Fig. 4 is a schematic view of a vehicle-mounted table in the lifting device of the vehicle-mounted unmanned aerial vehicle.
In the figure, a 100-lifting platform, a 200-vehicle-mounted platform, a 300-landing buffer tank, a 400-preassembled sheet, a 500-electromagnetic chuck, a 700-marker light bar, an 800-spring buffer, a 900-double-sided film and 110-release paper.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
Referring to fig. 1 to 4, the present utility model provides a technical solution: a vehicle-mounted unmanned aerial vehicle landing gear, comprising: the lifting platform 100 and the vehicle-mounted platform 200, wherein the vehicle-mounted platform 200 is arranged below the lifting platform 100, and the upper surface of the vehicle-mounted platform 200 is recessed downwards to form a landing buffer groove 300;
a plurality of groups of spring buffers 800 are arranged in the landing buffer tank 300, and two electromagnetic chucks 500 are respectively arranged on the left side and the right side of the upper surface of the landing platform 100;
two preassembling sheets 400 are arranged above the lifting platform 100, outline marker light bars 700 are arranged on the periphery of the upper surface of the lifting platform 100, sealing rubber bars are arranged on the periphery of the upper side of the landing buffer tank 300, and the sealing rubber bars can seal gaps around the landing buffer tank 300.
The length and width of the landing buffer slot 300 are greater than those of the landing platform 100, the lower part of the landing platform 100 stretches into the landing buffer slot 300 to be connected with the upper surfaces of the plurality of groups of spring buffers 800, and the unmanned aerial vehicle can land above the landing platform 100.
Four spring buffers 800 are arranged in each group, and the spring buffers 800 are distributed in a rectangular shape in a top view.
The lower surface of the vehicle-mounted table 200 is glued with a double-sided tape 900, the lower surface of the double-sided tape 900 is glued with release paper 110, and the vehicle-mounted table 200 can be glued and fixed on a vehicle body through the double-sided tape 900.
The top surface of the pre-loading piece 400 is in a circular structure, the lower parts of the plurality of groups of spring buffers 800 are connected with the lower part of the inner part of the falling buffer groove 300, and the electromagnetic chuck 500 can absorb the pre-loading piece 400.
The electromagnetic chuck 500 is a ZYE06 round electromagnetic chuck, the outline marker light bar 700 is an LED light bar, and the outline marker light bar 700 can display the outline of the lifting platform 100 after being lighted.
The spring damper 800 is a HT3-1250 small damping spring damper, the material of the pre-installed sheet 400 is iron, and the spring damper 800 can buffer and absorb impact force.
Referring to fig. 1 to 4, as a first embodiment of the present utility model: before using, tear release paper 110, make on-vehicle platform 200 glue through double-sided film 900 to be fixed on the automobile body, when unmanned aerial vehicle falls in landing platform 100, landing platform 100 below descends in landing buffer tank 300, and the impact force that produces when unmanned aerial vehicle falls simultaneously is transmitted to multiunit spring buffer 800 department through landing platform 100, multiunit spring buffer 800 can cushion and absorb the impact force to can make the unmanned aerial vehicle undercarriage not fragile when falling.
Referring to fig. 1, as a second embodiment of the present utility model: according to the first embodiment, two preassembling sheets 400 can be fixed below the landing gear of the unmanned aerial vehicle in advance, when the unmanned aerial vehicle is lowered onto the take-off and landing platform 100, the four electromagnetic chucks 500 are electrified to generate magnetic force, so that the preassembling sheets 400 can be adsorbed by the electromagnetic chucks 500, the unmanned aerial vehicle is not easy to move after being lowered onto the take-off and landing platform 100, the stability is better, when the unmanned aerial vehicle needs to take off, the four electromagnetic chucks 500 are powered off, the electromagnetic chucks 500 do not adsorb the preassembling sheets 400 any more, and then the unmanned aerial vehicle can take off.
Referring to fig. 1 and 3, as a third embodiment of the present utility model: when the unmanned aerial vehicle is at night, the outline marker lamp bar 700 can be electrified to be lighted, and the outline of the take-off and landing platform 100 can be displayed after the outline marker lamp bar 700 is lighted, so that the position of the take-off and landing platform 100 can be conveniently observed at night, and the unmanned aerial vehicle can conveniently land above the take-off and landing platform at night.
The foregoing description of the preferred embodiments of the utility model is not intended to be limiting, but rather is intended to cover all modifications, equivalents, alternatives, and improvements that fall within the spirit and scope of the utility model.
Claims (7)
1. A vehicle-mounted unmanned aerial vehicle landing gear, comprising: take off and land platform (100) and on-vehicle platform (200), take off and land platform (100) below is provided with on-vehicle platform (200), its characterized in that: the upper surface of the vehicle-mounted table (200) is recessed downwards to form a landing buffer groove (300);
a plurality of groups of spring buffers (800) are arranged in the landing buffer groove (300), and two electromagnetic chucks (500) are respectively arranged on the left side and the right side of the upper surface of the landing platform (100);
two preassembling sheets (400) are arranged above the lifting platform (100), outline marker light bars (700) are arranged on the periphery of the upper surface of the lifting platform (100), and sealing rubber bars are arranged on Fang Sizhou of the landing buffer groove (300).
2. The vehicle-mounted unmanned aerial vehicle take-off and landing device according to claim 1, wherein: the length and the width of the landing buffer groove (300) are larger than those of the landing platform (100), and the lower part of the landing platform (100) stretches into the landing buffer groove (300) to be connected with the upper surfaces of the plurality of groups of spring buffers (800).
3. The vehicle-mounted unmanned aerial vehicle take-off and landing device according to claim 2, wherein: four spring buffers (800) are arranged in each group, and a plurality of groups of the spring buffers (800) are distributed in a rectangular shape in the overlook plane.
4. The vehicle-mounted unmanned aerial vehicle take-off and landing device according to claim 1, wherein: the lower surface of the vehicle-mounted table (200) is glued with a double-sided film (900), and the lower surface of the double-sided film (900) is glued with release paper (110).
5. The vehicle-mounted unmanned aerial vehicle take-off and landing device according to claim 1, wherein: the top view surface of the preassembled sheet (400) is of a circular structure, and the lower parts of the plurality of groups of spring buffers (800) are connected with the inner lower parts of the falling buffer grooves (300).
6. The vehicle-mounted unmanned aerial vehicle take-off and landing device according to claim 1, wherein: the electromagnetic chuck (500) is a ZYE06 round electromagnetic chuck, and the outline marker light bar (700) is an LED light bar.
7. The vehicle-mounted unmanned aerial vehicle take-off and landing device of claim 5, wherein: the spring damper (800) is an HT3-1250 small damping spring damper, and the pre-installed sheet (400) is made of iron.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321816907.6U CN220430584U (en) | 2023-07-11 | 2023-07-11 | Vehicle-mounted unmanned aerial vehicle take-off and landing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321816907.6U CN220430584U (en) | 2023-07-11 | 2023-07-11 | Vehicle-mounted unmanned aerial vehicle take-off and landing device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220430584U true CN220430584U (en) | 2024-02-02 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321816907.6U Active CN220430584U (en) | 2023-07-11 | 2023-07-11 | Vehicle-mounted unmanned aerial vehicle take-off and landing device |
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| Country | Link |
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| CN (1) | CN220430584U (en) |
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2023
- 2023-07-11 CN CN202321816907.6U patent/CN220430584U/en active Active
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