CN220221172U - Horizontal take-off platform for unmanned aerial vehicle - Google Patents
Horizontal take-off platform for unmanned aerial vehicle Download PDFInfo
- Publication number
- CN220221172U CN220221172U CN202322210196.4U CN202322210196U CN220221172U CN 220221172 U CN220221172 U CN 220221172U CN 202322210196 U CN202322210196 U CN 202322210196U CN 220221172 U CN220221172 U CN 220221172U
- Authority
- CN
- China
- Prior art keywords
- fixedly connected
- unmanned aerial
- fixed plate
- wall
- platform
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 230000007306 turnover Effects 0.000 claims abstract description 12
- 238000013016 damping Methods 0.000 claims abstract description 10
- 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
- 230000000694 effects Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000001681 protective effect Effects 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 241000196324 Embryophyta Species 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
Landscapes
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The utility model discloses a horizontal take-off platform for an unmanned aerial vehicle, which comprises a fixed plate, wherein a hinge is fixedly connected to the outer wall of the fixed plate, a turnover plate is fixedly connected to the other end of the hinge, a rotating rod is fixedly connected to the middle position of the outer wall of the bottom of the fixed plate, a limiting plate penetrates through and is rotationally connected to the outer wall of the rotating rod, a threaded cylinder is fixedly connected to the middle position of the bottom of the fixed plate, a sliding rod penetrates through and is in threaded connection with the inner wall of the threaded cylinder, a sleeve is slidably connected to the outer wall of the sliding rod, and a damping spring is fixedly connected to the bottom of the sliding rod. According to the utility model, the solar panel can be protected through the protection pad, the unmanned aerial vehicle can be prevented from sliding on the platform, the leveling instrument can ensure the height level of the take-off and landing platform through judging the condition of the leveling instrument, and the height of the take-off and landing platform of the unmanned aerial vehicle can be adjusted through rotating the slide bars and the rubber blocks.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a horizontal take-off platform for an unmanned aerial vehicle.
Background
Unmanned plane is called "unmanned plane" for short, be the unmanned plane that utilizes radio remote control equipment and self-contained program control device to operate, or operate independently by on-vehicle computer is complete or intermittent type, along with technological rapid development, unmanned plane field application is more and more extensive, at present in the application in fields such as take photo by plane, agriculture, plant protection, miniature selfie, express delivery transportation, disaster rescue, observe wild animal, monitor infectious disease, survey, news report, electric power inspection, disaster relief, film and television shooting, manufacturing romantic etc., the purpose of unmanned plane itself has been greatly expanded, developed nations also are actively expanding trade application and developing unmanned plane technique, unmanned plane needs to provide stable holding power with the help of take off and land the platform when taking off.
At present, the unmanned aerial vehicle take-off and landing platform of the unmanned aerial vehicle is supported by adopting supporting legs with fixed length, the height cannot be adjusted, the unmanned aerial vehicle is difficult to balance on the ground with more complicated environment, the unmanned aerial vehicle can shake when taking off, no good protective measures exist on the platform, the unmanned aerial vehicle can easily slide off from the platform when taking off faults, and the unmanned aerial vehicle is inconvenient to carry, so that the horizontal take-off platform of the unmanned aerial vehicle needs to be improved.
Disclosure of Invention
The utility model aims to solve the defects in the prior art, and provides a horizontal take-off platform for an unmanned aerial vehicle.
In order to achieve the above purpose, the present utility model adopts the following technical scheme: the utility model provides a horizontal take-off platform for unmanned aerial vehicle, includes the fixed plate, fixedly connected with hinge on the outer wall position of fixed plate, fixedly connected with upset board on the other end position of hinge, fixedly connected with dwang on the bottom outer wall intermediate position of fixed plate, run through on the outer wall position of dwang and rotate and be connected with the limiting plate, fixedly connected with screw thread section of thick bamboo on the bottom intermediate position of fixed plate, run through on the inner wall position of screw thread section of thick bamboo and threaded connection has the slide bar, sliding connection has the sleeve on the outer wall position of slide bar, fixedly connected with damping spring on the bottom position of slide bar, all run through and be provided with the reflector strip on the top inner wall position of upset board, all run through and be provided with the reflector strip on the bottom outer wall position of upset board.
As a further description of the above technical solution:
the top four corners of the turnover plate are all penetrated and fixedly connected with first magic tapes.
As a further description of the above technical solution:
and the middle position of the top of the turnover plate is penetrated and fixedly connected with a solar panel.
As a further description of the above technical solution:
and a protection pad penetrates through the middle position of the top of the fixing plate and is fixedly connected with the fixing plate.
As a further description of the above technical solution:
the second magic tapes penetrate through and are fixedly connected to the four corners of the middle of the top of the fixing plate.
As a further description of the above technical solution:
the rubber block is connected to the bottom of the inner wall of the sleeve in a threaded manner and is fixedly connected with the damping spring.
As a further description of the above technical solution:
and the middle positions of the left side and the right side of the front side and the rear side of the top of the fixed plate are penetrated and fixedly connected with a level meter.
As a further description of the above technical solution:
a handle is fixedly connected between the rubber plugs.
The utility model has the following beneficial effects:
1. according to the utility model, the solar panel can be protected through the protection pad, the unmanned aerial vehicle can be prevented from sliding on the platform, the leveling instrument can ensure the height level of the take-off and landing platform through judging the condition of the leveling instrument, and the height of the take-off and landing platform of the unmanned aerial vehicle can be adjusted through rotating the slide bars and the rubber blocks.
2. According to the utility model, the turnover plate and the fixing plate can be unfolded and folded through the hinge, the turnover plate and the fixing plate can be fixed through the first magic tape and the second magic tape, and the rubber plug, the handle and the detachable support are convenient to carry.
Drawings
FIG. 1 is an exploded view of a horizontal takeoff platform for an unmanned aerial vehicle according to the present utility model;
FIG. 2 is a top view of a horizontal takeoff platform for a unmanned aerial vehicle according to the present utility model;
fig. 3 is a perspective view of a horizontal take-off platform for an unmanned aerial vehicle according to the present utility model.
Legend description:
1. a turnover plate; 2. a hinge; 3. a fixing plate; 4. a solar panel; 5. a first magic tape; 6. a reflective strip; 7. a level gauge; 8. the second magic tape; 9. a protective pad; 10. a rubber stopper; 11. a grip; 12. a rotating lever; 13. a limiting plate; 14. a thread cylinder; 15. a slide bar; 16. a damping spring; 17. a sleeve; 18. rubber blocks.
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.
In the description of the present utility model, it should be noted that, directions or positional relationships indicated by terms such as "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc., are based on directions or positional relationships shown in the drawings, are merely for convenience of description and simplification of description, and do not indicate or imply that the apparatus or element to be referred to must have a specific direction, be constructed and operated in the specific direction, and thus should not be construed as limiting the present utility model; the terms "first," "second," "third," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying relative importance, and furthermore, unless explicitly specified and limited otherwise, the terms "mounted," "connected," "coupled," and the like are to be construed broadly, and may be fixedly coupled, detachably coupled, or integrally coupled, for example; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present utility model will be understood in specific cases by those of ordinary skill in the art.
Referring to fig. 1-3, one embodiment provided by the present utility model is: the utility model provides a horizontal take-off platform for unmanned aerial vehicle, including fixed plate 3, fixedly connected with hinge 2 on the outer wall position of fixed plate 3, fixedly connected with turnover plate 1 on the other end position of hinge 2, fixedly connected with dwang 12 on the bottom outer wall intermediate position of fixed plate 3, run through on the outer wall position of dwang 12 and be connected with limiting plate 13 in the rotation, fixedly connected with screw thread section of thick bamboo 14 on the bottom intermediate position of fixed plate 3, run through on the inner wall position of screw thread section of thick bamboo 14 and threaded connection have slide bar 15, sliding connection has sleeve 17 on the outer wall position of slide bar 15, fixedly connected with damping spring 16 on the bottom position of slide bar 15, all run through on the top inner wall position of turnover plate 1 and be provided with reflection bar 6, install slide bar 15 at screw thread section of thick bamboo 14 inner wall through rotating limiting plate 13, can be spacing to turnover plate 1, can both give out light and can reflect light through reflection bar 6, even if at night, also can realize that the aircraft finds the landing platform position fast, run through and be provided with rubber stopper 10 on the bottom outer wall position of turnover plate 1.
The first magic subsides 5 of all running through and fixedly connected with on the top four corners position of roll-over plate 1, run through and fixedly connected with solar panel 4 on the top intermediate position of roll-over plate 1, run through and fixedly connected with protection pad 9 on the top intermediate position of fixed plate 3, all run through and fixedly connected with second magic subsides 8 on the top intermediate four corners position of fixed plate 3, threaded connection has rubber piece 18 and damping spring 16 fixed connection on the inner wall bottom position of sleeve 17, all run through and fixedly connected with spirit level 7 on both sides left and right sides intermediate position around the top of fixed plate 3, fixedly connected with handle 11 between the rubber plug 10, play shock-absorbing buffer effect through slide bar 15, damping spring 16, sleeve 17 and rubber piece 18, spirit level 7, through judging the spirit level condition, ensure the landing platform height level, can adjust unmanned aerial vehicle landing platform's height through rotating slide bar 15 and rubber piece 18, can make roll-over plate 1 and fixed plate 3 expand and close through hinge 2, conveniently carry with the support of closing with dismantling through rubber plug 10 and 11.
Working principle: during the use, install slide bar 15 at screw section of thick bamboo 14 inner wall, can carry out spacingly to the roll-over plate 1 through rotating limiting plate 13, can both give out light and can reflect light through reflection of light strip 6, even fly at night, also can realize that the aircraft finds the landing platform position fast, play shock attenuation cushioning effect through slide bar 15, damping spring 16, sleeve 17 and rubber piece 18, the spirit level 7, through judging the spirit level condition, ensure landing platform height level, can adjust unmanned aerial vehicle landing platform's height through rotating slide bar 15 and rubber piece 18, can make roll-over plate 1 and fixed plate 3 to expand and close through hinge 2, conveniently carry through rubber buffer 10 and grip 11 and the support of dismantlement.
Finally, it should be noted that: the foregoing description is only illustrative of the preferred embodiments of the present utility model, and although the present utility model 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, or equivalents may be substituted for elements thereof, and any modifications, equivalents, improvements or changes may be made without departing from the spirit and principles of the present utility model.
Claims (8)
1. Horizontal take-off platform for unmanned aerial vehicle, including fixed plate (3), its characterized in that: fixedly connected with hinge (2) on the outer wall position of fixed plate (3), fixedly connected with upset board (1) on the other end position of hinge (2), fixedly connected with dwang (12) on the bottom outer wall intermediate position of fixed plate (3), run through on the outer wall position of dwang (12) and rotate and be connected with limiting plate (13), fixedly connected with screw thread section of thick bamboo (14) on the bottom intermediate position of fixed plate (3), run through on the inner wall position of screw thread section of thick bamboo (14) and threaded connection have slide bar (15), sliding connection has sleeve (17) on the outer wall position of slide bar (15), fixedly connected with damping spring (16) on the bottom position of slide bar (15), all run through on the top inner wall position of upset board (1) and be provided with reflector strip (6), all run through on the top outer wall position of fixed plate (3) and be provided with reflector strip (10) on the bottom outer wall position of upset board (1).
2. A horizontal takeoff platform for unmanned aerial vehicles according to claim 1, wherein: the four corners of the top of the turnover plate (1) are penetrated through and fixedly connected with first magic tapes (5).
3. A horizontal takeoff platform for unmanned aerial vehicles according to claim 1, wherein: the solar panel (4) penetrates through and is fixedly connected with the middle position of the top of the turnover panel (1).
4. A horizontal takeoff platform for unmanned aerial vehicles according to claim 1, wherein: the middle position of the top of the fixed plate (3) is penetrated and fixedly connected with a protection pad (9).
5. A horizontal takeoff platform for unmanned aerial vehicles according to claim 1, wherein: the second magic tapes (8) are penetrated and fixedly connected at the four corners of the middle of the top of the fixed plate (3).
6. A horizontal takeoff platform for unmanned aerial vehicles according to claim 1, wherein: the rubber block (18) is connected to the bottom of the inner wall of the sleeve (17) in a threaded mode, and the rubber block (18) is fixedly connected with the damping spring (16).
7. A horizontal takeoff platform for unmanned aerial vehicles according to claim 1, wherein: and the middle positions of the left side and the right side of the front side and the rear side of the top of the fixed plate (3) are penetrated and fixedly connected with a level meter (7).
8. A horizontal takeoff platform for unmanned aerial vehicles according to claim 1, wherein: a handle (11) is fixedly connected between the rubber plugs (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322210196.4U CN220221172U (en) | 2023-08-17 | 2023-08-17 | Horizontal take-off platform for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322210196.4U CN220221172U (en) | 2023-08-17 | 2023-08-17 | Horizontal take-off platform for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220221172U true CN220221172U (en) | 2023-12-22 |
Family
ID=89187309
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322210196.4U Active CN220221172U (en) | 2023-08-17 | 2023-08-17 | Horizontal take-off platform for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220221172U (en) |
-
2023
- 2023-08-17 CN CN202322210196.4U patent/CN220221172U/en active Active
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US6808324B2 (en) | Image stabilization and balancing system | |
| CN220221172U (en) | Horizontal take-off platform for unmanned aerial vehicle | |
| EP3950491B1 (en) | Self-driving control apparatus and driverless apparatus provided with same | |
| CN108248815B (en) | Method and device for acquiring high-precision remote sensing data | |
| CN213566452U (en) | High unmanned aerial vehicle of security | |
| JPH0943753A (en) | Aerial photographic method for remote controlled aircraft | |
| CN112678172A (en) | Spherical unmanned aerial vehicle | |
| CN218537086U (en) | Surveying and mapping aerial photography aircraft | |
| CN112319782A (en) | Self-balancing unmanned aerial vehicle foot stand and balancing method thereof | |
| CN215972143U (en) | Environmental detection is with unmanned aerial vehicle that barrier propterty is good | |
| CN113202899B (en) | Airborne laser radar damping device | |
| CN207444615U (en) | A kind of control seat of display and control unit adjustable angle | |
| CN207141420U (en) | A kind of vertical stable clouds terrace system and unmanned plane | |
| CN213443093U (en) | Bird-driving unmanned aerial vehicle | |
| CN209988111U (en) | Plant protection unmanned aerial vehicle shock attenuation foot rest | |
| CN219619399U (en) | Unmanned aerial vehicle shock attenuation formula aerial survey equipment | |
| CN210555624U (en) | Aerial survey unmanned aerial vehicle bracket | |
| CN206978523U (en) | A kind of plant protection unmanned plane medication bottom seat | |
| CN216360018U (en) | Unmanned aerial vehicle descending protection device for geophysical prospecting | |
| CN209897069U (en) | Movable anti-unmanned aerial vehicle device | |
| CN210618499U (en) | Positioning support for luminance meter of cockpit | |
| CN219134581U (en) | Unmanned aerial vehicle landing platform with protective structure | |
| CN218703934U (en) | High-stability remote sensing surveying and mapping unmanned aerial vehicle | |
| CN218806643U (en) | Forestry investigation is with shooting device | |
| CN216246360U (en) | Topographic surveying and mapping device for architectural design |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |