CN206984419U - For carrying the vehicle of rotor wing unmanned aerial vehicle - Google Patents
For carrying the vehicle of rotor wing unmanned aerial vehicle Download PDFInfo
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- CN206984419U CN206984419U CN201720795169.XU CN201720795169U CN206984419U CN 206984419 U CN206984419 U CN 206984419U CN 201720795169 U CN201720795169 U CN 201720795169U CN 206984419 U CN206984419 U CN 206984419U
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- unmanned aerial
- telescopic component
- rotor wing
- wing unmanned
- aerial vehicle
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Abstract
A kind of vehicle for being used to carry rotor wing unmanned aerial vehicle is the utility model is related to, it includes：Vehicle body, including top and the receiving storehouse for being arranged at top；Rise and fall platform, including the first telescopic component and platform assembly, and one end of the first telescopic component is connected with accommodating the bottom in storehouse, and the other end is connected with platform assembly, and platform assembly is used to support rotor wing unmanned aerial vehicle；First telescopic component can stretching motion with by platform assembly eject or retract accommodate storehouse；Wherein, the platform that rises and falls of contraction state can be accommodated by accommodating storehouse.The vehicle of the present utility model for being used to carry rotor wing unmanned aerial vehicle, the platform for taking off or landing for rotor wing unmanned aerial vehicle can rapidly be built, operating personnel are no longer needed to find suitable place temporarily, reduce the time spent by delivery process and manpower so that simpler efficient during using rotor wing unmanned aerial vehicle progress article delivery work.
Description
Technical field
Equipment technology field of transport is the utility model is related to, more particularly to a kind of car for being used to carry rotor wing unmanned aerial vehicle
.
Background technology
With the development of science and technology, in production process of living, the use range of rotor wing unmanned aerial vehicle is more and more extensive.By
There is maneuverability in rotor wing unmanned aerial vehicle, the advantages that having a smooth flight, therefore rotor wing unmanned aerial vehicle is also applied to retail stores management at present
Transportation system, for carry, transport and delivery items.However, carry out article delivery process using rotor wing unmanned aerial vehicle at present
In, operator is frequently necessary to find suitable landing place near delivery point temporarily so that delivery process, which exists, expends the time
It is long, the cumbersome deficiency of operating process.
Utility model content
The utility model embodiment provides a kind of vehicle for being used to carry rotor wing unmanned aerial vehicle, can rapidly build for rotor
The platform that unmanned plane takes off or landed, it is no longer necessary to which operating personnel find suitable place temporarily, reduce delivery process and are consumed
The time taken and manpower so that simpler efficient during using rotor wing unmanned aerial vehicle progress article delivery work.
On the one hand, a kind of vehicle for being used to carry rotor wing unmanned aerial vehicle is proposed according to the utility model embodiment, it includes：
Vehicle body, including top and the receiving storehouse for being arranged at top；Rise and fall platform, including the first telescopic component and platform group
Part, one end of the first telescopic component are connected with accommodating the bottom in storehouse, and the other end is connected with platform assembly, and platform assembly is used for
Support rotor wing unmanned aerial vehicle；First telescopic component can stretching motion with by platform assembly eject or retract accommodate storehouse；Wherein, accommodate
Storehouse can accommodate the platform that rises and falls of contraction state.
According to the one side of the utility model embodiment, the first telescopic component include the first bearing, the first rod member and
For driving the first driver of the first rod member movement, the first bearing is connected with accommodating the bottom in storehouse, platform assembly and first
The free end of rod member is connected.
According to the one side of the utility model embodiment, platform assembly includes multiple splice plates and is arranged at each spelling
Driving element between fishplate bar and the first telescopic component, one end of each splice plate is rotatablely connected with the first telescopic component, each
Corresponding splice plate can be driven to rotate for driving element so that each splice plate folds or the horizontal exhibition in same horizontal plane
Open.
According to the one side of the utility model embodiment, driving element includes the second telescopic component, the second telescopic component
One end be connected to the first telescopic component, the other end is connected to splice plate, the second telescopic component can stretching motion so that splicing
Plate is swung around one end that splice plate is connected with the first telescopic component.
According to the one side of the utility model embodiment, the second telescopic component include the second bearing, the second rod member and
For driving the second driver of the second rod member movement, one end of the second bearing is rotatablely connected with the first telescopic component, the second bar
One end of part is rotatablely connected with splice plate.
According to the one side of the utility model embodiment, the first telescopic component and the second telescopic component are respectively hydraulic pressure
One or more in cylinder, electric cylinder and pneumatic linear actuator.
According to the one side of the utility model embodiment, vehicle body also includes being used to open or close accommodating opening for storehouse
The lid of mouth.
According to the one side of the utility model embodiment, sealing gasket is provided between lid and top.
According to the one side of the utility model embodiment, vehicle body also includes horizontal slide rail, and lid is sliding by level
Rail and top slidable connection.
According to the one side of the utility model embodiment, the height of the platform that rises and falls in contraction state, which is less than, accommodates storehouse
Depth.
The vehicle for being used to carry rotor wing unmanned aerial vehicle provided according to the utility model embodiment, it includes that itself can be passed through
The platform that rises and falls set rapidly erects to take off or landing platform for rotor wing unmanned aerial vehicle, so as to facilitate operating personnel to use
Rotor wing unmanned aerial vehicle carries out article delivery work, it is no longer necessary to which operating personnel find suitable place temporarily, reduce whole delivery
The labor intensity of work, save the whole time delivered spent by work.Vehicle is provided for accommodating the receiving for the platform that rises and falls
Storehouse, the platform that rises and falls can be effectively protected, while also make it that whole vehicle structure is compact, lifts aesthetics.Pass through operation first
Telescopic component is so that platform assembly moves up and down in storehouse is accommodated, it is no longer necessary to manual operation, improves automaticity, reduces
Human input during use.
Brief description of the drawings
The feature of the utility model exemplary embodiment, advantage and technique effect are described below by reference to accompanying drawing.
Fig. 1 is that the vehicle for being used to carry rotor wing unmanned aerial vehicle of the embodiment of the utility model one is used cooperatively with rotor wing unmanned aerial vehicle
When overall structure diagram.
Fig. 2 is the broken section structural representation for being used to carry the vehicle of rotor wing unmanned aerial vehicle of another embodiment of the utility model
Figure.
Fig. 3 is the overall structure diagram of the platform that rises and falls of the embodiment of the utility model one.
In the accompanying drawings, accompanying drawing is not drawn according to the ratio of reality.
Embodiment
Embodiment of the present utility model is described in further detail with reference to the accompanying drawings and examples.Following examples
The detailed description and the accompanying drawings be used to exemplarily illustrate principle of the present utility model, but can not be used for limiting model of the present utility model
Enclose, i.e., the utility model is not limited to described embodiment.
, it is necessary to which explanation, unless otherwise indicated, " multiple " are meant that two or two in description of the present utility model
More than individual；The orientation or position relationship of the instruction such as term " on ", " under ", "left", "right", " interior ", " outer " are for only for ease of and retouched
State the utility model and simplify and describe, rather than instruction or imply signified device or element must have specific orientation, with
Specific azimuth configuration and operation, therefore it is not intended that to limitation of the present utility model.In addition, term " first ", " second ",
Etc. be only used for describe purpose, and it is not intended that instruction or imply relative importance.In description of the present utility model, it is also necessary to
Illustrate, unless otherwise clearly defined and limited, term " installation ", " connected ", " connection " should be interpreted broadly, for example,
Can be fixedly connected or be detachably connected, or be integrally connected；Can be joined directly together, centre can also be passed through
Medium is indirectly connected.For the ordinary skill in the art, visual concrete condition understands that above-mentioned term is new in this practicality
Concrete meaning in type.
In order to more fully understand the utility model, it is used to carry according to the utility model embodiment with reference to Fig. 1 to 3
The vehicle of rotor wing unmanned aerial vehicle is described in detail.
The vehicle of the utility model embodiment is used to carry rotor wing unmanned aerial vehicle 99, and the vehicle includes vehicle body 10 and risen
Fall platform 20.After operating personnel, which drive the vehicle, reaches specified location, the platform 20 that rises and falls set on vehicle can be used fast
Construct fastly as rotor wing unmanned aerial vehicle 99 take off or place of landing.So, taking off during the use of rotor wing unmanned aerial vehicle 99
Or descent will not be affected by the ambient, look for being adapted to rotor without operating personnel's overspending energy and time
The place that unmanned plane 99 takes off or landed, so that it is simple using the process operation of the delivery items of rotor wing unmanned aerial vehicle 99, more
It is convenient and swift, time of delivery is substantially reduced, improves and delivers operating efficiency.
As shown in figure 1, the vehicle body 10 of the utility model embodiment includes top 101 and is arranged at top 101
Accommodate storehouse 102.The receiving storehouse 102 of the present embodiment can be the independent structure part or top that are fixedly connected with top 101
101 parts of itself.
In one embodiment, the platform 20 that rises and falls includes the first telescopic component 201 and platform assembly 202.First is flexible
One end of component 201 is connected with accommodating the bottom in storehouse 102, and the other end is connected with platform assembly 202.Platform assembly 202 is used
In support rotor wing unmanned aerial vehicle 99.In the present embodiment, one end of the first telescopic component 201 can be by way of bolt or welding
It is connected with the bottom for accommodating storehouse 102.The other end of first telescopic component 201 can be by way of bolt or welding with putting down
Platform component 202 is connected.Platform assembly 202 has smooth upper surface, provides landing site for rotor wing unmanned aerial vehicle 99, protects simultaneously
Demonstrate,prove the stationarity of the landing process of rotor wing unmanned aerial vehicle 99.In the present embodiment, the first telescopic component 201 can make up and down stretching motion with
Platform assembly 202 is ejected or retracted and accommodates storehouse 102, operating process is convenient.Accommodating storehouse 102 can accommodate in contraction state
The platform 20 that rises and falls.The height of the platform 20 that rises and falls in contraction state is less than the depth for accommodating storehouse 102, so as to accommodate storehouse 102
To rising and falling, platform 20 plays a protective role, while also causes the compact overall structure of vehicle body 10, appearance looks elegant.
As shown in figure 3, in the present embodiment, the first telescopic component 201 includes the first bearing 201a, the first rod member 201b and use
In the first driver 201c for driving the first rod member 201b to be moved relative to the first bearing 201a.First driver 201c drivings the
When one rod member 201b is moved, platform assembly 202 can be ejected or be retracted receiving storehouse 102.First bearing 201a is with accommodating storehouse 102
Bottom be connected.Platform assembly 202 is connected with the first rod member 201b free end.First bearing 201a passes through bolt or weldering
The mode connect is connected with accommodating the bottom in storehouse 102.Connection is socketed between first rod member 201b one end and the first bearing 201a.
First rod member 201b being moved axially with respect to the first bearing 201a along itself, moved down so as to drive on platform assembly 202
It is dynamic.
First telescopic component 201 of the utility model embodiment can be one kind in hydraulic cylinder, electric cylinder and pneumatic linear actuator
Or it is several, according to being actually needed carry out flexible configuration.Hydraulic cylinder, electric cylinder or pneumatic linear actuator driving platform assembly 202 move up and down
Process it is relatively stable.The quantity of first telescopic component 201 can be configured according to being actually needed.When the first telescopic component
When 201 quantity is more than three, first telescopic component 201 of more than three is in the bottom in platform assembly 202 and receiving storehouse 102
Between be uniformly distributed.
In one embodiment, platform assembly 202 can be the platy structure of a monoblock type, so as to only need by first
Telescopic component 201 ejects platform assembly 202 to precalculated position, you can rotor wing unmanned aerial vehicle 99 is placed into platform assembly 202
Upper standby, overall shorten takes off time.Meanwhile rotor wing unmanned aerial vehicle 99 land after, taken away from platform assembly 202 rotor without
Man-machine 99, then operate the first telescopic component 201 and directly retract platform assembly 202 in receiving storehouse 102, shorten recovery time.
In such manner, it is possible to improve the whole efficiency for delivering work.
In another embodiment, as shown in Fig. 2 platform assembly 202 includes multiple splice plate 202a and is arranged at every
Driving element 30 between individual splice plate 202a and the first telescopic component 201.One end of driving element 30 and the first telescopic component
201 are connected, and the other end is connected with splice plate 202a.In the present embodiment, the quantity of driving element 30 is with splice plate 202a's
Quantity is equal.Each splice plate 202a one end is rotatablely connected with the first telescopic component 201.Each splice plate 202a one end with
Rotating shaft is provided between first telescopic component 201, the axis that the rotating shaft can be surrounded so as to splice plate 202a is swung up and down.When
When one telescopic component 201 includes the first rod member 201b, splice plate 202a one end and the first rod member 201b top pass through level
Axis of rotation connects.Corresponding splice plate 202a can be driven to rotate for each driving element 30 so that each splice plate 202a rolls over
Folded or horizontal development.The splice plate 202a of the present embodiment is in sector structure.
When need to use this rise and fall platform 20 when, by the first telescopic component 201 by platform assembly 202 eject accommodate storehouse
102 and push up to behind precalculated position, then corresponding each splice plate 202a is driven from folded state by each driving element 30
Switch to horizontal development state, be maintained at the same horizontal plane so as to all splice plate 202a, now can by rotor nobody
Machine 99 is placed on platform assembly 202 and carries out takeoff operational.
After the completion of this rises and falls the use of platform 20, rotor wing unmanned aerial vehicle 99 is taken away, then phase is driven by each driving element 30
Corresponding each splice plate 202a switches to folded state from horizontal development state, will be flat finally by the first telescopic component 201
Platform component 202, which retracts, accommodates storehouse 102.
The platform assembly 202 of the present embodiment includes multiple foldable or expansion splice plate 202a, flat so as to change
The overall dimensions of platform component 202, platform assembly 202 convenient for collecting.When multiple splice plate 202a are in folded state, platform group
The overall volume of part 202 is small, therefore accordingly, the overall dimensions in receiving storehouse 102 are small, reduce and accommodate storehouse 102 and the platform that rises and falls
Space shared by 20, ensure vehicle compact overall structure.
The driving element 30 of the present embodiment includes the second telescopic component 301.Stretched with first one end of second telescopic component 301
Contracting component 201 is connected, and the other end is connected with splice plate 202a.Second telescopic component 301 can stretching motion so that splicing
Plate 202a is swung around one end that splice plate 202a is connected with the first telescopic component 201, so as to which splice plate 202a can folded
Switched between deployed condition.
Second telescopic component 301 of the present embodiment includes the second bearing 301a, the second rod member 301b and for driving the
Second driver of two rod member 301b movements.Second bearing 301a and the second rod member 301b socket connections.Second bearing 301a's
One end is rotatablely connected with the first telescopic component 201.Second rod member 301b one end is rotatablely connected with splice plate 202a.
Second telescopic component 301 of the present embodiment is the one or more in hydraulic cylinder, electric cylinder and pneumatic linear actuator, according to reality
Border needs to carry out flexible configuration.The action process of hydraulic cylinder, electric cylinder and pneumatic linear actuator driving platform assembly 202 is stable.Second stretches
The quantity of contracting component 301 can be configured according to being actually needed.When the quantity of the second telescopic component 301 is more than three,
Second telescopic component 301 of more than three is uniformly distributed between the bottom in platform assembly 202 and receiving storehouse 102.
As shown in Figure 1 or 2, the vehicle body 10 of the utility model embodiment also includes being used to open or close accommodating storehouse
The lid 40 of 102 opening.After the platform 20 that rises and falls, which is received into, to be accommodated in storehouse 102, lid 40 closes the opening for accommodating storehouse 102,
So as to form protection to accommodating storehouse 102 and the platform 20 that rises and falls, avoid the impurity such as dust or water droplet from entering and accommodate storehouse 102 and adhere to
Rising and falling on platform 20, ensureing to accommodate the cleanliness factor in storehouse 102 and the platform 20 that rises and falls.
Sealing gasket is provided between the lid 40 of the present embodiment and the top 101 of vehicle body 10.Sealing gasket is ring-type knot
Structure, size are engaged with accommodating the opening in storehouse 102.Sealing gasket can be filled between lid 40 and the top 101 of vehicle body 10
Gap, so as to form annular sealing surface, the sealing property of lid 40 is further lifted, with to accommodating storehouse 102 and rising and falling platform
20 form good protection.
The lid 40 of the present embodiment is slidably disposed in the top 101 of vehicle body 10.The top 101 of vehicle body 10
It is provided with horizontal slide rail (not shown).Lid 40 is slideably connected by the top 101 of horizontal slide rail and vehicle body 10
Connect.Lid 40 is horizontal on horizontal slide rail to be slided to close or open the opening in receiving storehouse 102, simple and quick.This implementation
The horizontal slide rail of example includes two bar blocks be arrangeding in parallel, is provided with dovetail groove in each bar blocks, is provided with lid 40
The dovetail boss being engaged with dove tail shape.
The vehicle for being used to carry rotor wing unmanned aerial vehicle 99 of the utility model embodiment, rising and falling for being set by itself are flat
Platform 20 rapidly erects to take off or landing platform for rotor wing unmanned aerial vehicle 99, so as to facilitate operating personnel using rotor nobody
Machine 99 carries out article delivery work, it is no longer necessary to which operating personnel find suitable place temporarily, reduce whole delivery work
Labor intensity, save the whole time delivered spent by work.Vehicle is provided for accommodating the receiving storehouse for the platform 20 that rises and falls
102, the platform 20 that rises and falls can be effectively protected, while also make it that whole vehicle structure is compact, lifts aesthetics.Pass through operation the
One telescopic component 201 is so that the platform 20 that rises and falls moves up and down in storehouse 102 is accommodated, it is no longer necessary to manual operation, improves automatic
Change degree, reduce the human input during use.
Although the utility model is described by reference to preferred embodiment, model of the present utility model is not being departed from
In the case of enclosing, various improvement can be carried out to it and part therein can be replaced with equivalent.Especially, as long as not depositing
The every technical characteristic being previously mentioned in structural hazard, each embodiment can combine in any way.The utility model
It is not limited to specific embodiment disclosed herein, but all technical schemes including falling within the scope of the appended claims.
Claims (10)
- A kind of 1. vehicle for being used to carry rotor wing unmanned aerial vehicle, it is characterised in that including：Vehicle body, including top and the receiving storehouse for being arranged at the top；Rise and fall platform, including the first telescopic component and platform assembly, one end of first telescopic component and the receiving storehouse Bottom be connected, the other end is connected with the platform assembly, the platform assembly be used for support the rotor wing unmanned aerial vehicle；First telescopic component can stretching motion to eject or retract the receiving storehouse by the platform assembly；Wherein, the storehouse that accommodates can accommodate the platform that rises and falls of contraction state.
- 2. the vehicle according to claim 1 for being used to carry rotor wing unmanned aerial vehicle, it is characterised in that first telescopic component Including the first bearing, the first rod member and the first driver for driving first rod member movement, first bearing with The bottom for accommodating storehouse is connected, and the platform assembly is connected with the free end of first rod member.
- 3. the vehicle according to claim 1 or 2 for being used to carry rotor wing unmanned aerial vehicle, it is characterised in that the platform assembly Including multiple splice plates and the driving element being arranged between each splice plate and first telescopic component, Mei Gesuo State one end of splice plate to be rotatablely connected with first telescopic component, each driving element can drive corresponding described Splice plate rotates so that each splice plate folds or the horizontal development in same horizontal plane.
- 4. the vehicle according to claim 3 for being used to carry rotor wing unmanned aerial vehicle, it is characterised in that the driving element includes Second telescopic component, one end of second telescopic component are connected to first telescopic component, and the other end is connected to the spelling Fishplate bar, second telescopic component can stretching motion so that the splice plate around the splice plate and the described first flexible group One end of part connection is swung.
- 5. the vehicle according to claim 4 for being used to carry rotor wing unmanned aerial vehicle, it is characterised in that second telescopic component Including the second bearing, the second rod member and the second driver for driving second rod member movement, second bearing One end is rotatablely connected with first telescopic component, and one end and the splice plate of second rod member are rotatablely connected.
- 6. the vehicle according to claim 5 for being used to carry rotor wing unmanned aerial vehicle, it is characterised in that first telescopic component It is respectively the one or more in hydraulic cylinder, electric cylinder and pneumatic linear actuator with second telescopic component.
- 7. the vehicle according to claim 1 for being used to carry rotor wing unmanned aerial vehicle, it is characterised in that the vehicle body also wraps Include the lid of the opening for opening or closing the receiving storehouse.
- 8. the vehicle according to claim 7 for being used to carry rotor wing unmanned aerial vehicle, it is characterised in that the lid and the top Sealing gasket is provided between portion.
- 9. the vehicle according to claim 7 for being used to carry rotor wing unmanned aerial vehicle, it is characterised in that the vehicle body also wraps Horizontal slide rail is included, the lid passes through the horizontal slide rail and the top slidable connection.
- 10. the vehicle according to claim 1 for being used to carry rotor wing unmanned aerial vehicle, it is characterised in that in described contraction-like The height of the platform that rises and falls of state is less than the depth in the receiving storehouse.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720795169.XU CN206984419U (en) | 2017-07-03 | 2017-07-03 | For carrying the vehicle of rotor wing unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720795169.XU CN206984419U (en) | 2017-07-03 | 2017-07-03 | For carrying the vehicle of rotor wing unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206984419U true CN206984419U (en) | 2018-02-09 |
Family
ID=61400665
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720795169.XU Active CN206984419U (en) | 2017-07-03 | 2017-07-03 | For carrying the vehicle of rotor wing unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206984419U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108516080A (en) * | 2018-03-29 | 2018-09-11 | 南京理工大学 | Air-ground coordination dynamic docking facilities |
| WO2019171748A1 (en) * | 2018-03-09 | 2019-09-12 | ヤマハ発動機株式会社 | Aircraft platform |
| CN111959808A (en) * | 2019-05-20 | 2020-11-20 | 北京京东尚科信息技术有限公司 | Carrying structure |
-
2017
- 2017-07-03 CN CN201720795169.XU patent/CN206984419U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019171748A1 (en) * | 2018-03-09 | 2019-09-12 | ヤマハ発動機株式会社 | Aircraft platform |
| CN108516080A (en) * | 2018-03-29 | 2018-09-11 | 南京理工大学 | Air-ground coordination dynamic docking facilities |
| CN108516080B (en) * | 2018-03-29 | 2024-01-23 | 南京理工大学 | Ground-air cooperative dynamic docking device |
| CN111959808A (en) * | 2019-05-20 | 2020-11-20 | 北京京东尚科信息技术有限公司 | Carrying structure |
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