CN105857609A - Vehicular multi-station rotatory unmanned aerial vehicle lifting platform - Google Patents
Vehicular multi-station rotatory unmanned aerial vehicle lifting platform Download PDFInfo
- Publication number
- CN105857609A CN105857609A CN201610226116.6A CN201610226116A CN105857609A CN 105857609 A CN105857609 A CN 105857609A CN 201610226116 A CN201610226116 A CN 201610226116A CN 105857609 A CN105857609 A CN 105857609A
- Authority
- CN
- China
- Prior art keywords
- unmanned plane
- hoistable platform
- chain
- vehicular
- unmanned aerial
- 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.)
- Pending
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66F—HOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
- B66F7/00—Lifting frames, e.g. for lifting vehicles; Platform lifts
- B66F7/28—Constructional details, e.g. end stops, pivoting supporting members, sliding runners adjustable to load dimensions
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U80/00—Transport or storage specially adapted for UAVs
- B64U80/80—Transport or storage specially adapted for UAVs by vehicles
- B64U80/86—Land vehicles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66F—HOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
- B66F11/00—Lifting devices specially adapted for particular uses not otherwise provided for
Abstract
The invention discloses a vehicular multi-station rotatory unmanned aerial vehicle lifting platform, comprising a servo motor, a reducer, a commutator, a drive sprocket, a tension sprocket, a chain, cantilever plates and unmanned aerial vehicle lifting platforms. The output end of the servo motor is provided with the reducer, the output end of the reducer is provided with the commutator, the commutator is connected with the drive sprocket through a drive shaft, the drive sprocket is meshed with the chain, the chain is connected with the tension sprocket, the cantilever plates are installed on chain links of the chain, and the cantilever plates are connected with the unmanned aerial vehicle lifting platforms. The multiple unmanned aerial vehicle lifting platforms are driven to rotate and work through the chain, the multi-station rotatory unmanned aerial vehicle lifting platform which is flexible, can be transported by vehicles, and can conduct field work is provided, and a solid technical foundation is laid for the development of applying a large scale of unmanned aerial vehicles to the security field.
Description
Technical field
The present invention relates to the technical field of unmanned plane hoistable platform, particularly vehicular multistation wheel unmanned plane hoistable platform transition.
Background technology
Along with developing rapidly of science and technology, unmanned plane during flying and control technology are the most advanced and ripe.If by large batch of for unmanned plane for safety-security area, then the vehicle-mounted transport cabin of a kind of maneuverability and hoistable platform just become the most necessary；But at present vehicle-mounted unmanned aerial vehicle equipment only transport, store in a warehouse, use of charge, and be not useable for directly lifting of unmanned plane.Vehicular unmanned plane hoistable platform field also be nobody shows any interest at present.Mobile unit due to it limited space, power source limited, also require that designer sufficiently to consider space and the energy utilization rate of equipment.
Goal of the invention
It is an object of the invention to fill up the blank of vehicular multistation unmanned plane hoistable platform technical field, it is provided that full-automatic multistation wheel unmanned plane hoistable platform transition that a kind of space availability ratio is high.
Summary of the invention
The object of the present invention is achieved like this: includes servomotor, decelerator, diverter, drive sprocket, tightener sprocket, chain, cantilever slab, unmanned plane hoistable platform.Described servomotor outfan is provided with described decelerator, described decelerator outfan is provided with described diverter, described diverter connects described drive sprocket by power transmission shaft, described drive sprocket engages with described chain, described chain connects described tightener sprocket, it is filled with described cantilever slab on described chain link plate, described cantilever slab is connected to described unmanned plane hoistable platform.Moved by chain-driving multiple hoistable platform round, thus realize the round work of multistation unmanned plane hoistable platform.
Accompanying drawing explanation
In order to be illustrated more clearly that the embodiment of the present invention or technical scheme of the prior art, the accompanying drawing used required in embodiment or description of the prior art will be briefly described below, apparently, accompanying drawing in describing below is only one embodiment of the present of invention, for those of ordinary skill in the art, on the premise of not paying creative work, it is also possible to obtain other accompanying drawing according to these accompanying drawings.
Fig. 1 is the receipts cabin status architecture schematic diagram of the present invention a kind of vehicular multistation wheel unmanned plane hoistable platform transition；
Fig. 2 be the present invention a kind of vehicular multistation wheel transition unmanned plane hoistable platform go out cabin status architecture schematic diagram.
1-servomotor, 2-decelerator, 3-diverter, 4-drive sprocket, 5-chain, 6-tightener sprocket, 7-cantilever slab, 8-unmanned plane hoistable platform.
Detailed description of the invention
Below in conjunction with the accompanying drawings the preferred embodiments of the present invention are described in detail.
Refering to shown in accompanying drawing 1 and accompanying drawing 2, a kind of vehicular multistation wheel unmanned plane hoistable platform transition, including servomotor 1, and the decelerator 2 being connected with servomotor, and and the diverter 3 that connects of decelerator, and and the drive sprocket 4 that connects of diverter, and and drive sprocket 4 connect chain 5, and and the tightener sprocket 6 that connects of chain 5, and the cantilever slab 7 ined succession on chain, and the unmanned plane hoistable platform 8 connected on cantilever slab.
Described servomotor 1 export power through decelerator 2 slow down after, then by diverter 3(bevel gear box) transfer power to horizontal output.Described diverter 3 drives described drive sprocket 4 to rotate, and described drive sprocket 4 engages with described chain 5.Described chain 5 drives described tightener sprocket 6 to slowly run.It is connected to described cantilever slab 7 on described chain 5, described cantilever slab 7 is connected to described unmanned plane hoistable platform 8.Described chain 5 drives described cantilever slab 7 to do low speed batch (-type) gyration together, and described unmanned plane hoistable platform 8 slowly rises along with the low speed batch (-type) of described cantilever slab 7 turns round, declines intermittent cycle motion.Being work station when described unmanned plane hoistable platform 8 moves to peak, servomotor 1 stops operating, and described unmanned plane hoistable platform 8 is parked in peak and acts, for unmanned plane, the cabin that flies out.Complete rear motor to be rotated further, when described unmanned plane hoistable platform 8 moves to peak next time, unmanned plane landing, receive cabin.
In this preferred embodiment, on described chain 5, average mark can accommodate six unmanned planes and carries out transporting, goes out cabin, enters cabin in being furnished with six described cantilever slabs 7 and described unmanned plane hoistable platform 8, i.e. this example.Six described unmanned plane hoistable platforms 8 arrive peak successively, act the cabin that flies out successively；Then, after unmanned plane has worked, six described unmanned plane hoistable platforms 8 arrive peak the most successively, and cabin is received in landing successively.
In other embodiments of the present invention, can be according to some parameter in the space allocation present invention of cabin.Such as, on described chain 5, average mark is furnished with six described cantilever slabs 7 and described unmanned plane hoistable platform 8, but being not limited only to six can also be other quantity, can increase or reduce the number of unmanned plane hoistable platform according to the height of cabin, to realize the maximization of space availability ratio.
Compared with conventional art, unmanned plane hoistable platform is incorporated on mobile unit by the present invention, it is provided that a kind of can for unmanned plane automatic lifting vehicular multistation take turns transition unmanned plane hoistable platform.From car, action is manually moved to take to hoistable platform when eliminating unmanned plane work, it can realize unmanned plane on vehicle-mounted lifting platform direct automatic lifting, go out to put in storage, and multiple unmanned plane hoistable platform can be accommodated simultaneously transfer from one department to another the dynamic lower automatic wheel of regiment commander at chain wheel and change a job work.Substantially increase the work efficiency of vehicular unmanned plane hoistable platform, saved cost of labor, improve the maneuverability of unmanned plane hoistable platform work.
The invention provides a kind of maneuverability can multistation wheel unmanned plane hoistable platform transition of vehicle-mounted transport and field work, filled up the blank of this technical field, also established certain technical foundation for unmanned plane high-volume for the development of safety-security area.
The above, only a preferred embodiment of the present invention, but protection scope of the present invention is not limited thereto, any change expected without creative work or replacement, all should contain in scope.
Claims (6)
1. vehicular multistation wheel unmanned plane hoistable platform transition, it is characterised in that: include servomotor, decelerator, diverter, drive sprocket, tightener sprocket, chain, cantilever slab, unmanned plane hoistable platform.
2. vehicular multistation wheel unmanned plane hoistable platform transition, it is characterised in that: described servomotor outfan is provided with described decelerator, and described decelerator outfan is provided with described diverter.
3. vehicular multistation wheel unmanned plane hoistable platform transition, it is characterised in that: described diverter connects described drive sprocket by power transmission shaft, and described drive sprocket engages with described chain, and described chain connects described tightener sprocket.
4. vehicular multistation wheel unmanned plane hoistable platform transition, it is characterised in that: it is filled with described cantilever slab on described chain link plate, described cantilever slab is connected to described unmanned plane hoistable platform.
5. vehicular multistation wheel unmanned plane hoistable platform transition, it is characterised in that: it is evenly distributed six described cantilever slabs and described unmanned plane hoistable platform on described chain, but being not limited only to six can also be other quantity.
6. vehicular multistation wheel unmanned plane hoistable platform transition, it is characterised in that: moved by chain-driving multiple hoistable platform round, thus realize the round work of multistation unmanned plane hoistable platform.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610226116.6A CN105857609A (en) | 2016-04-13 | 2016-04-13 | Vehicular multi-station rotatory unmanned aerial vehicle lifting platform |
| CN201610767296.9A CN106185716B (en) | 2016-04-13 | 2016-08-29 | A kind of vehicular unmanned plane lifting platform system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610226116.6A CN105857609A (en) | 2016-04-13 | 2016-04-13 | Vehicular multi-station rotatory unmanned aerial vehicle lifting platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105857609A true CN105857609A (en) | 2016-08-17 |
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Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610226116.6A Pending CN105857609A (en) | 2016-04-13 | 2016-04-13 | Vehicular multi-station rotatory unmanned aerial vehicle lifting platform |
| CN201610767296.9A Active CN106185716B (en) | 2016-04-13 | 2016-08-29 | A kind of vehicular unmanned plane lifting platform system |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201610767296.9A Active CN106185716B (en) | 2016-04-13 | 2016-08-29 | A kind of vehicular unmanned plane lifting platform system |
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| CN (2) | CN105857609A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108341070A (en) * | 2018-02-09 | 2018-07-31 | 重庆三峡学院 | A kind of bridge machinery unmanned plane undercarriage |
| CN110409899A (en) * | 2019-08-21 | 2019-11-05 | 上海复亚智能科技有限公司 | The circulating unmanned plane of multimachine automates hangar |
| CN111717408A (en) * | 2020-06-29 | 2020-09-29 | 山东科技大学 | Marine launching platform capable of bearing multiple unmanned aerial vehicles |
| CN112153348A (en) * | 2020-09-28 | 2020-12-29 | 斯舰力(上海)电梯有限公司 | Engineering supervision system based on VR technology |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN106938706B (en) * | 2017-03-09 | 2019-05-03 | 王亮 | A kind of unmanned plane landing platform waggon |
| CN107943063A (en) * | 2017-11-15 | 2018-04-20 | 广东容祺智能科技有限公司 | A kind of unmanned plane landing is from steady platform and its method of work |
| CN111719927B (en) * | 2019-03-21 | 2021-12-31 | 北京京东乾石科技有限公司 | Unmanned aerial vehicle hangar |
| CN114708715A (en) * | 2022-04-08 | 2022-07-05 | 中国环境科学研究院 | Natural protected area ecological environment risk early warning system and method |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2693880Y (en) * | 2004-05-08 | 2005-04-20 | 陈忠孝 | Roller chain wheel suspension space parking place |
| CN102425322B (en) * | 2011-09-23 | 2013-12-04 | 许卫军 | Circulation type stereoscopic garage |
| CN104058100A (en) * | 2014-06-23 | 2014-09-24 | 杨举 | Device for launching and landing aircrafts |
| CN104494503A (en) * | 2014-11-25 | 2015-04-08 | 中国兵器工业计算机应用技术研究所 | Comprehensive shelter system of unmanned aerial vehicle |
| CN104670516B (en) * | 2015-02-15 | 2016-07-06 | 南京理工大学 | The quick lifting gear of aircraft |
| CN104787351B (en) * | 2015-04-17 | 2016-10-19 | 东北大学 | A kind of unmanned plane is launched and retracting device |
| CN206088902U (en) * | 2016-04-13 | 2017-04-12 | 西安天鹰防务科技有限公司 | Vehicular unmanned aerial vehicle lift platform system |
-
2016
- 2016-04-13 CN CN201610226116.6A patent/CN105857609A/en active Pending
- 2016-08-29 CN CN201610767296.9A patent/CN106185716B/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108341070A (en) * | 2018-02-09 | 2018-07-31 | 重庆三峡学院 | A kind of bridge machinery unmanned plane undercarriage |
| CN108341070B (en) * | 2018-02-09 | 2021-04-20 | 重庆三峡学院 | Bridge detection unmanned aerial vehicle undercarriage |
| CN110409899A (en) * | 2019-08-21 | 2019-11-05 | 上海复亚智能科技有限公司 | The circulating unmanned plane of multimachine automates hangar |
| CN111717408A (en) * | 2020-06-29 | 2020-09-29 | 山东科技大学 | Marine launching platform capable of bearing multiple unmanned aerial vehicles |
| CN112153348A (en) * | 2020-09-28 | 2020-12-29 | 斯舰力(上海)电梯有限公司 | Engineering supervision system based on VR technology |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106185716B (en) | 2019-03-26 |
| CN106185716A (en) | 2016-12-07 |
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Application publication date: 20160817 |