CN205952339U - Staying unmanned aerial vehicle receive and releases cabin device - Google Patents
Staying unmanned aerial vehicle receive and releases cabin device Download PDFInfo
- Publication number
- CN205952339U CN205952339U CN201620660472.4U CN201620660472U CN205952339U CN 205952339 U CN205952339 U CN 205952339U CN 201620660472 U CN201620660472 U CN 201620660472U CN 205952339 U CN205952339 U CN 205952339U
- Authority
- CN
- China
- Prior art keywords
- folding
- cabin device
- hoistable platform
- tethered
- unmanned plane
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- 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.)
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Abstract
The utility model relates to a staying unmanned aerial vehicle receive and releases cabin device, it includes cabin cover, the cabin body, lift platform, support and guide, the cabin cover setting is in the top of the cabin body is opened and is closed in order being used for the inner space of the cabin body, lift platform is located the inner space of the cabin body is parked for staying unmanned aerial vehicle, the guide is located the bottom of the inner space of the cabin body, support respectively with lift platform with the guide is connected in order to be used for the support lift platform. This device can be parked, preserve and protect it through the cabin body device that can close for supplying it at staying unmanned aerial vehicle during at perform tasks not for a long time, when needs took off, the device can in time open and lift preset position with it through elevating gear, made it conveniently put the departure from former off -position, the device can in time open when needs navigate back the descending to navigate back to the assigned position through its accuracy of align member precise guidance assurance, accomplish recovery work.
Description
Technical field
Basis is new to be related to aircraft field.More specifically, originally new be related to a kind of folding and unfolding cabin device being tethered at unmanned plane.
Background technology
Being tethered at unmanned plane is a kind of unmanned plane quickly growing now.Due to being tethered at the flight of unmanned plane and controlling requirement negative
Carry high voltage and high current, therefore, major part is tethered at unmanned plane and has been configured without power supply unit, or the confession of its power supply unit in itself
Electricity is very little.Generally, it is tethered at unmanned plane dependence one or multi-cable to be attached with ground power supply system and rely on ground to supply
Electric system provides continuation of the journey required electricity for it.Therefore, it is tethered at unmanned plane and always pulls cable in flight course, be tethered at no
Man-machine also hence obtain one's name.
And the folding and unfolding technology being tethered at unmanned plane is the important component part being tethered at unmanned air vehicle technique, rise to being tethered at unmanned plane
Drop and park protection etc. and play important guaranteeing role.And also not can effectively solve the problem that in prior art and be tethered at unmanned plane folding and unfolding
Problem, meets the device being tethered at unmanned plane landing, the corresponding requirement such as reclaiming, park, protecting.
Utility model content
In order to solve the problems, such as the above-mentioned folding and unfolding being tethered at unmanned plane, a kind of folding and unfolding cabin dress being tethered at unmanned plane of this new offer
Put, it includes hatchcover, nacelle, hoistable platform, support and guide, wherein, described hatchcover be arranged on the top of described nacelle with
For opening and closing the inner space of described nacelle；Described hoistable platform is located at the inner space of described nacelle for being tethered at no
Man-machine stop is parked；Described guide is located at the bottom of the inner space of described nacelle, and described support is flat with described lifting respectively
Platform and described guide connect for supporting described hoistable platform.
Further, described guide includes：Guide rail slide unit and guide rail slide block, wherein, described guide rail slide block with described
Frame connects, and described guide rail slide block moves up and down to drive described support to move up and down in described guide rail slide unit, and then carries
Move described hoistable platform to move up and down.
Further, described hatchcover is slidably hatchcover, and described slidably hatchcover includes lid and slide rail, and described lid exists
Slide to open and close the inner space of described nacelle in described slide rail.
Further, described folding and unfolding cabin device further includes the motor being connected with described guide, and described motor is used for
Drive described guide motion, and then drive described hoistable platform to move up and down.
Further, described folding and unfolding cabin device further includes motor, and described motor is connected with described guide to drive
Described guide rail slide block moves up and down in described guide rail slide unit, and then drives described hoistable platform to move up and down.
Further, described folding and unfolding cabin device further includes the motor being connected with described hatchcover, and described motor is used for driving
Dynamic described hatchcover moves to open and close the inner space of described nacelle.
Further, described folding and unfolding cabin device further includes the motor being connected with described slidably hatchcover, described motor
For driving described lid to slide to open and close the inner space of described nacelle in described slide rail.
Further, described hoistable platform is provided with the cable hole passing through for cable, described cable hole is arranged with to be led
Line device.
Further, described folding and unfolding cabin device further includes for being tethered at, to described, the align member that unmanned plane positions,
It is tethered at, described in can making, the specified location that unmanned plane docks at described hoistable platform.
Further, described align member includes the relative position for being tethered at unmanned plane and described hoistable platform described in obtaining
The differential GPS localizer of confidence breath.
Basis is new compared with prior art to be had the advantages that：
First, this device can be tethered at unmanned plane when not executing task, for parking storage for a long time for it, and passes through
Closable nacelle device is protected to it；
2nd, when being tethered at unmanned plane and needing to take off, this device can be opened in time, and is lifted by lowering or hoisting gear
Precalculated position flies out so as to easily put from former off-position；
3rd, be tethered at unmanned plane need make a return voyage landing when, this device can be opened in time, and is accurately made by align member
It accurately makes a return voyage to specified location to lead guarantee, completes recovery operation.
Brief description
Fig. 1 is that the closed mode of the folding and unfolding cabin device for being tethered at unmanned plane according to this new embodiment is illustrated
Figure.
Fig. 2 is to be opened according to the folding and unfolding cabin device of this new another embodiment and hoistable platform will be tethered at unmanned plane and hold out
View.
Specific embodiment
It is described in further details with reference to the Figure of description technical scheme new to this.
As illustrated in fig. 1 and 2, this new extension and retraction system for being tethered at unmanned plane includes being tethered at unmanned plane 10 for accommodating
Folding and unfolding cabin device nacelle 20, it includes an inner space.Have in this nacelle 20：Hatchcover, hoistable platform 211, support 212,
Guide and cable 230.Wherein, hoistable platform 211 is arranged in the inner space of nacelle 20 for making to be tethered at unmanned plane 10
Stop thereon.Specifically, the top surface of hoistable platform 211 is tethered at unmanned plane 10 for arrangement；Support 212, it is used for supporting
Hoistable platform 211；Guide, it is located at the bottom of the inner space of nacelle 20, and this guide includes guide rail slide unit 213, guide rail
Slide block 214, arranges the guide rail slide block 214 sliding along in guide rail slide unit 213, one end of support 212 connects to guide rail slide block
214 and the other end connects to hoistable platform 211, guide is connected with motor, this Motor drive guide rail slide block 214 guide rail slide
The elevating movement carrying out in platform 213 can drive support 212 to move up and down, so can drive hoistable platform 211 and thereon be
Unmanned plane 10 is stayed to move up and down.Preferably, hoistable platform 211 can rise to the height substantially parallel with slidably hatchcover 220,
Even exceed certain altitude than slidably hatchcover 220 upper surface, to be conducive to being tethered at taking off and landing of unmanned plane 10.
Further, hatchcover is slidably hatchcover 220, and it is arranged on the top of nacelle 20 for opening and closing nacelle
20 inner space.Specifically, slidably hatchcover 220 includes lid 221, slide rail 222, and slidably hatchcover 220 is connected with motor,
This Motor drive lid 221 level in slide rail 222 is slided to open and close inner space.
Further, it is tethered at unmanned plane 10 because cable 230 can followed by always, so being the entanglement avoiding cable 230
With guarantee cable 230, there is correct outlet direction, hoistable platform 211 is additionally provided with cable hole 211a and is arranged at this cable
Cable guiding device below the 211a of hole（Not shown）, cable 230 passes through cable hole 211a and cable guiding device and connects to being tethered at unmanned plane 10.
Preferably, cable 230 can be tethered at cable for aviation, and it includes two alloy lead wires and an optical fiber cable, and it has
Resist big pulling force, characteristic soft, that recovery, anti-high pressure and heavy current can be coiled, single-mode optics fibre core can be used for communicating.
Further, also include in this folding and unfolding cabin device described be tethered at unmanned plane and take off, make a return voyage, hovering and be servo-actuated when
Be tethered at, to described, the align member that unmanned plane is positioned, this align member can make described in be tethered at unmanned plane and dock at described liter
The specified location of fall platform.In a preferred embodiment, this align member is arranged in nacelle 20.
Further, this align member includes a differential GPS localizer（Not shown）, its be used for obtaining described in be tethered at unmanned
Machine and the relative position information of described hoistable platform, this information includes the number relevant with centralized positioning coordinate of hoistable platform 211
According to accurately stopping to drop on hoistable platform 211 thus contributing to control and being tethered at unmanned plane 10.
In the case of not execution task, lid 221 is in the state of the interior space of nacelle 20 of closing, such as schemes
Shown in 1.It is tethered in the internally positioned space of unmanned plane 10 and rests on the top surface of hoistable platform 211.So, nacelle 20 is used for
The a whole set of UAS of protection and mechanism.After being connected to the instruction of execution aerial mission, Motor drive lid 221 is to two Slideslips
To open inner space, subsequently or simultaneously hoistable platform 211 is actuated to preferably rise up to the height substantially parallel with lid 221
Degree, completes flight preparation action, as shown in Figure 2.Then, being tethered at unmanned plane 10 drags city's cable 230 to take off to setting height execution
Task.After the completion of task, it is tethered at unmanned plane and makes a return voyage to hoistable platform 211, hoistable platform 211 drives and is tethered at unmanned plane 10 and drops to
The inner space of nacelle 20, then or therewith lid 221 slide to middle part to close this inner space, thus completing this flight
Task.
In one embodiment, it is tethered at unmanned plane 10 and includes many rotor wing unmanned aerial vehicles body, fly control unit, IMU unit, communication
Unit, the second differential GPS unit, power module, TU task unit etc..Communication unit may be configured with optical transmitter and receiver, passes through Aviation cable
The information such as position and flying quality are transmitted back to GCU by optical fiber, are tethered at unmanned described in the second differential GPS unit acquisition
The position data of machine 10, thus realizing being accurately positioned, is realized unmanned plane and is taken off, makes a return voyage, hovers and automatically follow.
As described above, originally new disclose a kind of folding and unfolding cabin device for being tethered at unmanned plane.When not executing task, such as
Shown in Fig. 1, it is tethered at unmanned plane and is encapsulated in folding and unfolding cabin；When needing execution task, comment platform by controlling lifting as shown in Figure 2
Slidably hatchcover will be tethered at unmanned plane and hold out in folding and unfolding cabin, be tethered at unmanned plane and can leave folding and unfolding cabin and rise and execute and be tethered at
Task, after the completion of task, the centralized positioning coordinate by means of the differential GPS unit of its own and the hoistable platform obtaining realizes essence
Really land in hoistable platform, and then hoistable platform automatically retracts in folding and unfolding cabin, complete the recovery action of unmanned plane.Whole mistake
Journey can control via GCU and the controller being arranged in drawing cable equipment, without manual operation.Therefore, originally
New solve the problems, such as to be tethered at the accurate takeoff and landing of unmanned plane, the problem that precise guidance is maked a return voyage, unmanned plane digital preservation, storage
The problem hidden, and long-time to being tethered at the problem that unmanned plane is powered.
This new applicant describes in detail with reference to the Figure of description embodiment new to this and describes, but this
Skilled person, it should be understood that above example is only a kind of this new embodiment, is merely to illustrate new, wherein
The structure of each part, connected mode etc. all can change, and explanation in detail is intended merely to help reader to more fully understand this
New spirit, and the not restriction to the novel protected scope of basis, on the contrary, it is any that any new spirit new based on basis is made
Improve modification and equivalents and improvement all should not excluded outside this new protection domain.
Claims (10)
1. a kind of folding and unfolding cabin device being tethered at unmanned plane is it is characterised in that include hatchcover, nacelle, hoistable platform, support and guiding
Part,
Wherein, described hatchcover is arranged on the top of described nacelle for opening and closing the inner space of described nacelle；
The inner space that described hoistable platform is located at described nacelle is parked for being tethered at unmanned plane；
Described guide is located at the bottom of the inner space of described nacelle,
Described support is connected with described hoistable platform and described guide respectively for supporting described hoistable platform.
2. folding and unfolding cabin device according to claim 1 is it is characterised in that described guide includes：
Guide rail slide unit and guide rail slide block,
Wherein, described guide rail slide block is connected with described support, described guide rail slide block move up and down in described guide rail slide unit with
Drive described support to move up and down, and then drive described hoistable platform to move up and down.
3. folding and unfolding cabin device according to claim 1 is it is characterised in that described hatchcover is slidably hatchcover, described slides
Dynamic hatchcover includes lid and slide rail, and described lid slides to open and close the inner space of described nacelle in described slide rail.
4. folding and unfolding cabin device according to claim 1 it is characterised in that described folding and unfolding cabin device further include with described
The motor that guide connects, described motor is used for driving described guide motion, and then drives described hoistable platform to do lifting fortune
Dynamic.
5. folding and unfolding cabin device according to claim 2 is it is characterised in that described folding and unfolding cabin device further includes motor,
Described motor is connected with described guide to drive described guide rail slide block to move up and down in described guide rail slide unit, and then drives
Described hoistable platform moves up and down.
6. folding and unfolding cabin device according to claim 1 it is characterised in that described folding and unfolding cabin device further include with described
The motor that hatchcover connects, described motor is used for driving described hatchcover to move to open and close the inner space of described nacelle.
7. folding and unfolding cabin device according to claim 3 it is characterised in that described folding and unfolding cabin device further include with described
The motor that slidably hatchcover connects, it is described to open and close that described motor is used for driving described lid to slide in described slide rail
The inner space of nacelle.
8. the folding and unfolding cabin device according to claim 1-7 any one claim is it is characterised in that on described hoistable platform
It is provided with the cable hole passing through for cable, described cable hole is arranged with cable guiding device.
9. the folding and unfolding cabin device according to claim 1-7 any one claim is it is characterised in that described folding and unfolding cabin device
Further include for the described align member being tethered at unmanned plane positioning, its can make described in be tethered at unmanned plane dock at described
The specified location of hoistable platform.
10. folding and unfolding cabin device according to claim 9 it is characterised in that described align member include described for obtaining
It is tethered at the differential GPS localizer of unmanned plane and the relative position information of described hoistable platform.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620660472.4U CN205952339U (en) | 2016-06-29 | 2016-06-29 | Staying unmanned aerial vehicle receive and releases cabin device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620660472.4U CN205952339U (en) | 2016-06-29 | 2016-06-29 | Staying unmanned aerial vehicle receive and releases cabin device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205952339U true CN205952339U (en) | 2017-02-15 |
Family
ID=57969889
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620660472.4U Expired - Fee Related CN205952339U (en) | 2016-06-29 | 2016-06-29 | Staying unmanned aerial vehicle receive and releases cabin device |
Country Status (1)
| Country | Link |
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| CN (1) | CN205952339U (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106672255A (en) * | 2017-03-16 | 2017-05-17 | 四方继保（武汉）软件有限公司 | Cabin control system for unmanned aerial vehicle on unmanned ship |
| CN107238907A (en) * | 2017-07-18 | 2017-10-10 | 沈阳亨通光通信有限公司 | Aerial optical cable laying system and aerial optical cable laying method |
| CN107512391A (en) * | 2017-08-23 | 2017-12-26 | 长春长光精密仪器集团有限公司 | Based on the rotor unmanned aircraft for being tethered at cable power supply |
| CN107539199A (en) * | 2017-09-14 | 2018-01-05 | 张欣 | One key discharges key recovery vehicle-mounted unmanned aerial vehicle storage device and accommodation method |
| CN108755491A (en) * | 2018-05-29 | 2018-11-06 | 广东泓胜科技股份有限公司 | A kind of non-at-scene enforcement system of highway overload remediation load |
| CN109747859A (en) * | 2017-11-02 | 2019-05-14 | 天津职业技术师范大学 | A kind of unmanned plane carrying power and data line rises and falls plateform system |
| CN109835498A (en) * | 2017-11-24 | 2019-06-04 | 天津职业技术师范大学 | The UAV system and its implementation transmitted based on wired power supply and data |
-
2016
- 2016-06-29 CN CN201620660472.4U patent/CN205952339U/en not_active Expired - Fee Related
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106672255A (en) * | 2017-03-16 | 2017-05-17 | 四方继保（武汉）软件有限公司 | Cabin control system for unmanned aerial vehicle on unmanned ship |
| CN107238907A (en) * | 2017-07-18 | 2017-10-10 | 沈阳亨通光通信有限公司 | Aerial optical cable laying system and aerial optical cable laying method |
| CN107512391A (en) * | 2017-08-23 | 2017-12-26 | 长春长光精密仪器集团有限公司 | Based on the rotor unmanned aircraft for being tethered at cable power supply |
| CN107512391B (en) * | 2017-08-23 | 2020-07-24 | 佛山长光智能制造研究院有限公司 | Rotor unmanned aerial vehicle based on mooring cable power supply |
| CN107539199A (en) * | 2017-09-14 | 2018-01-05 | 张欣 | One key discharges key recovery vehicle-mounted unmanned aerial vehicle storage device and accommodation method |
| CN109747859A (en) * | 2017-11-02 | 2019-05-14 | 天津职业技术师范大学 | A kind of unmanned plane carrying power and data line rises and falls plateform system |
| CN109835498A (en) * | 2017-11-24 | 2019-06-04 | 天津职业技术师范大学 | The UAV system and its implementation transmitted based on wired power supply and data |
| CN108755491A (en) * | 2018-05-29 | 2018-11-06 | 广东泓胜科技股份有限公司 | A kind of non-at-scene enforcement system of highway overload remediation load |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170215 Termination date: 20190629 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |