CN206088902U - Vehicular unmanned aerial vehicle lift platform system - Google Patents
Vehicular unmanned aerial vehicle lift platform system Download PDFInfo
- Publication number
- CN206088902U CN206088902U CN201620986772.1U CN201620986772U CN206088902U CN 206088902 U CN206088902 U CN 206088902U CN 201620986772 U CN201620986772 U CN 201620986772U CN 206088902 U CN206088902 U CN 206088902U
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- unmanned plane
- platform system
- sprocket
- lifting platform
- chain
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- 238000005183 dynamical system Methods 0.000 claims description 10
- 230000005540 biological transmission Effects 0.000 claims description 8
- 238000012546 transfer Methods 0.000 claims description 4
- 230000000630 rising effect Effects 0.000 abstract 1
- 230000007704 transition Effects 0.000 description 3
- 241000276425 Xiphophorus maculatus Species 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000008859 change Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
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- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model discloses a vehicular unmanned aerial vehicle lift platform system, the motion of constituteing including drive sprocket, chain and driven sprocket, wherein, drive sprocket and driven sprocket are used for support and drive chain, and drive sprocket is connected with driving system, drive chain connects through cantilever and nacelle hinge, has realized unmanned aerial vehicle direct automatic rising on on -vehicle lift platform, the function that goes out to put in storage, need not to carry dedicated lift platform with unmanned aerial vehicle from the car and goes up and down, has practiced thrift the human cost, can on -vehicle transportation can be used for field work, flexible nature simultaneously.
Description
Technical field
The utility model is related to unmanned plane hoistable platform field, more particularly to vehicular unmanned plane lifting platform system.
Background technology
UAV abbreviation unmanned plane, is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft.Obtain in fields such as police, city management, agricultural, mapping, electric inspection process, rescue and relief work, movies-makings at present
Extensively application.If unmanned plane high-volume is used for into safety-security area, then a kind of vehicle-mounted transport cabin of maneuverability and lifting are flat
Platform just becomes very necessary；However, at present vehicle-mounted unmanned aerial vehicle equipment is only used for transport, storage or the charging of unmanned plane, can not
For the direct landing of unmanned plane, vehicular unmanned plane hoistable platform technology also be nobody shows any interest in.
The content of the invention
To realize the function of the direct landing of the unmanned plane of vehicle-mounted unmanned aerial vehicle equipment, the purpose of this utility model is to provide
Vehicular unmanned plane lifting platform system, the hoistable platform high working efficiency, maneuverability is strong, has saved human cost.
To solve above-mentioned technical problem, the utility model is adopted the following technical scheme that：
Vehicular unmanned plane lifting platform system, including the motion of drive sprocket, chain and driven sprocket composition, its
In, drive sprocket and driven sprocket are used to support and drive chain, and drive sprocket is connected with dynamical system；The drive chain is led to
Cross cantilever and gondola hinge-connection.
The drive sprocket and driven sprocket are vertically arranged, and drive sprocket is located at the lower section of driven sprocket, institute
Driven sprocket is stated for tightener sprocket.
The motion includes symmetrically arranged two sets, wherein, connected by power transmission shaft between two drive sprockets, two
Connected by power transmission shaft between driven sprocket.
The length and gondola height sum of the distance between the chain lowermost end and ground more than cantilever.
The gondola includes lifter plate and is arranged on lifter plate border, and the connector parallel with cantilever.
The connector is platy structure.
The cantilever has 6, is uniformly fixed on chain.
The dynamical system includes servomotor, and servomotor output end is connected with decelerator, also including frame, in frame
The bearing for supporting drive sprocket and driven sprocket is provided with, described cantilever one end is fixed on chain, other end hinge-connection
In the lateral surface of gondola.
The servomotor be arranged on frame on, the power direction of transfer of servomotor is parallel with frame, decelerator it is defeated
Go out end to be connected with the wheel shaft of drive sprocket by commutator.
The commutator is bevel gear commutator.
Prior art is compared, and the utility model at least has the advantages that, the utility model is flat by unmanned plane lifting
Platform is incorporated on mobile unit, there is provided it is a kind of can for unmanned plane automatic lifting vehicular multistation wheel make the transition unmanned plane liter
Drop platform, realize unmanned plane on vehicle-mounted lifting platform direct automatic lifting, go out the function of putting in storage, without the need for by unmanned plane from car
On be transported on special hoistable platform and lifted, human cost has been saved, while vehicle-mounted transport and field can be can be used for
Work, maneuverability.
Further, drive sprocket and driven sprocket are vertically arranged, and drive sprocket is located under driven sprocket
Side, by being arranged using vertical direction, can effectively increase rotate to top gondola height, drive sprocket be arranged on from
The lower section of movable sprocket, driven sprocket is tightener sprocket, the convenient access for arranging dynamical system, can constantly keep the tensioning of chain
State, is prevented effectively from the stability that cantilever is fixed on chain.
Further, motion includes symmetrically arranged two sets, wherein, connected by power transmission shaft between two drive sprockets
Connect, connected by power transmission shaft between two driven sprockets, both improve the stability of whole platform, it is ensured that it is same that two chains run
Step, and a set of dynamical system is only needed to, save equipment space and be manufactured into, convenient control.
Further, the distance between chain lowermost end and ground are prevented more than the length and gondola height sum of cantilever
Because being rotated further by ground drag when cantilever and gondola go to least significant end.
Further, the gondola includes lifter plate and is arranged on lifter plate border, and the connector parallel with cantilever, institute
Connector is stated for platy structure, good stability.
Further, cantilever has 6, is uniformly fixed on chain, can simultaneously accommodate multiple unmanned plane hoistable platforms and exist
Transmission mechanism drives lower automatic wheel to change a job work, substantially increases operating efficiency.
Further, dynamical system includes servomotor, and servomotor output end is connected with decelerator, also including frame,
The bearing for supporting drive sprocket and driven sprocket is provided with frame, described cantilever one end is fixed on chain, the other end
Hinge is connected to the lateral surface of gondola, improves the stability of whole device, while realizing the precise control to gondola.
Further, servomotor is arranged in frame, and the power direction of transfer of servomotor is parallel with frame, adopts this
Structure design can effectively reduce the volume of the system, save interior space.
Description of the drawings
In order to be illustrated more clearly that the utility model embodiment or technical scheme of the prior art, below will be to embodiment
Or the accompanying drawing to be used needed for description of the prior art is briefly described, it should be apparent that, drawings in the following description are only
It is one embodiment of the present utility model, for those skilled in the art, on the premise of not paying creative work, also
Other accompanying drawings can be obtained according to these accompanying drawings.
Front view when Fig. 1 is the utility model receipts cabin state；
Side view when Fig. 2 is the utility model receipts cabin state；
Top view when Fig. 3 is the utility model receipts cabin state；
Fig. 4 goes out the front view during state of cabin for the utility model.
Description of reference numerals：
1- servomotors, 2- decelerators, 3- commutators, 4- drive sprockets, 5- chains, 6- driven sprockets, 7- cantilevers, 8- liters
Drop plate, 9- frames, 10- gondolas.
Specific embodiment
The utility model is described in further detail with reference to the accompanying drawings and detailed description.
As shown in Figure 1, Figure 2 and Figure 3, the utility model vehicular unmanned plane lifting platform system, including drive sprocket 4,
Motion, cantilever 7, gondola 10 and frame 9 that chain 5 and driven sprocket 6 are constituted, drive sprocket 4 and driven sprocket 6 are used to prop up
Support and drive chain 5, drive sprocket 4 and driven sprocket 6 are vertically arranged, and drive sprocket 4 is located under driven sprocket 6
Side, by arranging using vertical direction, can effectively increase the height of the gondola 10 for rotating to top, and drive sprocket 4 is arranged
In the lower section of driven sprocket 6, the convenient access for arranging dynamical system, the gondola includes lifter plate 8 and is arranged on the side of lifter plate 8
Boundary, and the side plate parallel with cantilever 7, one end of cantilever 7 is fixed on chain 5, the other end and the hinge-connection of gondola 10, the most bottom of chain 5
The distance between end and ground are provided with for supporting drive sprocket more than the length and gondola height sum of cantilever 7 in frame 9
4 and the bearing of driven sprocket 6, drive sprocket 4 is connected with dynamical system, and dynamical system includes servomotor 1, and servomotor 1 is pacified
It is mounted in frame 9, its power direction of transfer is parallel with frame, defeated its goes out end and be connected with decelerator 2, and the output end of decelerator 2 is led to
Cross bevel gear commutator 3 to be connected with the wheel shaft of drive sprocket 4, be capable of achieving the precise control to gondola 10, save space.This reality
Can be realized for the vehicular multistation wheel of unmanned plane automatic lifting transition unmanned plane hoistable platform there is provided a kind of with new
Unmanned plane on vehicle-mounted lifting platform direct automatic lifting, go out the function of putting in storage, it is special without the need for unmanned plane is transported to from car
Hoistable platform on lifted, saved human cost, while vehicle-mounted transport and field work can be can be used for, maneuverability
Property.
Preferably, the motion and frame 9 include symmetrically arranged two sets, wherein, lead between two drive sprockets 4
Power transmission shaft connection is crossed, is connected by power transmission shaft between two driven sprockets 6, both improve the stability of whole platform, and by wherein
One driving wheel drives another driving wheel to rotate by rotary shaft, saves the energy.
Preferably, driven sprocket 6 is tightener sprocket, and cantilever 7 can be avoided to occur position skew in rotation process.
Preferably, cantilever 7 has 6, and each cantilever 7 hinge-connection, one gondola 10, the cantilever 7 is uniformly fixed on chain
On 5,6 unmanned planes can be accommodated and transported, go out cabin, entered cabin, 6 gondolas 10 reach successively peak, its accommodate nobody
Machine acts successively the cabin that flies out；Then after the completion for the treatment of unmanned plane work, 6 gondolas 10 reach successively peak again, and unmanned plane drops successively
Fall to receiving cabin, substantially increase operating efficiency.
Operationally, the servomotor 1 is defeated for vehicular multistation wheel transition unmanned plane hoistable platform of the present utility model
Go out power and power is switched to into horizontal output after the deceleration of decelerator 2, then by commutator 3, commutator 3 drives drive sprocket 4
Rotate, drive sprocket 4 is engaged with chain 5, chain 5 drives tightener sprocket to slowly run, and cantilever 7, cantilever 7 are provided with chain 5
With the hinge-connection of gondola 10, therefore chain 5 drive cantilever 7 do low speed batch (-type) gyration together, gondola 10 is then with cantilever 7
The revolution of low speed batch (-type) is slow to be risen, declines intermittent cycle motion.As shown in figure 4, when gondola 10 moves to peak
For work station, servomotor 1 stops operating, and gondola 10 is parked in peak so that unmanned plane acts the cabin that flies out.Then motor continues
Rotate, when gondola 10 moves to peak next time, unmanned plane landing, receive cabin.
The utility model can be according to some of space allocation the utility model of cabin parameter.For example, the chain 5
Upper average mark is furnished with 6 cantilevers 7 and 6 gondolas 10, but it can also be other quantity to be not limited only to 6, can be according to cabin
Highly increase or reduce the number of unmanned plane hoistable platform, to realize the maximization of space availability ratio.
Above example is merely to illustrate the technical solution of the utility model, not for restriction model of the present utility model
Enclose, any those skilled in the art, in without departing from spirit and scope of the present utility model, can make various replacements and modification,
Therefore protection domain of the present utility model should be defined by claim limited range.
Claims (10)
1. vehicular unmanned plane lifting platform system, it is characterised in that including drive sprocket (4), chain (5) and driven sprocket
(6) motion of composition, wherein, drive sprocket (4) and driven sprocket (6) are for support and drive chain (5), drive sprocket
(4) dynamical system is connected with, the drive chain (5) is by cantilever (7) and gondola (10) hinge-connection.
2. vehicular unmanned plane lifting platform system according to claim 1, it is characterised in that the drive sprocket (4)
Vertically arrange with driven sprocket (6), and drive sprocket (4) is positioned at the lower section of driven sprocket (6), the driven sprocket
(6) it is tightener sprocket.
3. vehicular unmanned plane lifting platform system according to claim 1, it is characterised in that the motion includes
Symmetrically arranged two sets, wherein, connected by power transmission shaft between two drive sprockets (4), by passing between two driven sprockets (6)
Moving axis connects.
4. vehicular unmanned plane lifting platform system according to claim 1, it is characterised in that chain (5) the most bottom
The length and gondola (10) height sum of the distance between end and ground more than cantilever (7).
5. vehicular unmanned plane lifting platform system according to claim 1, it is characterised in that the gondola (10) includes
Lifter plate (8) and lifter plate (8) border is arranged on, and the connector parallel with cantilever (7).
6. vehicular unmanned plane lifting platform system according to claim 5, it is characterised in that the connector is tabular
Structure.
7. vehicular unmanned plane lifting platform system according to claim 1, it is characterised in that the cantilever (7) has 6
It is individual, uniformly it is fixed on chain (5).
8. vehicular unmanned plane lifting platform system according to claim 1, it is characterised in that the dynamical system includes
Servomotor (1), servomotor (1) output end is connected with decelerator (2), and also including frame (9), frame is provided with use on (9)
In supporting drive sprocket (4) and the bearing of driven sprocket (6), described cantilever (7) one end is fixed on chain (5), other end hinge
It is linked in the lateral surface of gondola.
9. vehicular unmanned plane lifting platform system according to claim 8, it is characterised in that the servomotor (1)
In frame (9), the power direction of transfer of servomotor (1) is parallel with frame, and the output end of decelerator (2) is by commutation
Device (3) is connected with the wheel shaft of drive sprocket (4).
10. vehicular unmanned plane lifting platform system according to claim 9, it is characterised in that the commutator (3)
For bevel gear commutator.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620304320 | 2016-04-13 | ||
| CN2016203043200 | 2016-04-13 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206088902U true CN206088902U (en) | 2017-04-12 |
Family
ID=58473911
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620986772.1U Expired - Fee Related CN206088902U (en) | 2016-04-13 | 2016-08-29 | Vehicular unmanned aerial vehicle lift platform system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206088902U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106185716A (en) * | 2016-04-13 | 2016-12-07 | 西安天鹰防务科技有限公司 | A kind of vehicular unmanned plane lifting platform system |
| 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 |
| CN111959808A (en) * | 2019-05-20 | 2020-11-20 | 北京京东尚科信息技术有限公司 | Carrying structure |
-
2016
- 2016-08-29 CN CN201620986772.1U patent/CN206088902U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106185716A (en) * | 2016-04-13 | 2016-12-07 | 西安天鹰防务科技有限公司 | A kind of vehicular unmanned plane lifting platform system |
| CN106185716B (en) * | 2016-04-13 | 2019-03-26 | 西安天鹰防务科技有限公司 | A kind of vehicular unmanned plane lifting platform system |
| CN111959808A (en) * | 2019-05-20 | 2020-11-20 | 北京京东尚科信息技术有限公司 | Carrying structure |
| 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 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170412 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |