CN205707386U - A kind of UAV Intelligent safe recovery device - Google Patents
A kind of UAV Intelligent safe recovery device Download PDFInfo
- Publication number
- CN205707386U CN205707386U CN201620455166.7U CN201620455166U CN205707386U CN 205707386 U CN205707386 U CN 205707386U CN 201620455166 U CN201620455166 U CN 201620455166U CN 205707386 U CN205707386 U CN 205707386U
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- recovery device
- uav intelligent
- intelligent safe
- pillar
- safe recovery
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- 238000011084 recovery Methods 0.000 title claims abstract description 38
- 238000004064 recycling Methods 0.000 claims abstract description 18
- 238000004891 communication Methods 0.000 claims abstract description 13
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 6
- 230000035807 sensation Effects 0.000 claims description 6
- 238000000034 method Methods 0.000 abstract description 5
- 230000002411 adverse Effects 0.000 abstract description 2
- 238000012856 packing Methods 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 230000003139 buffering effect Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 230000006870 function Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000003208 petroleum Substances 0.000 description 1
- 230000005622 photoelectricity Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
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- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The utility model discloses a kind of UAV Intelligent safe recovery device.Described UAV Intelligent safe recovery device includes: carriage assembly, for can be assembled into support in the way of being dismounted for multiple times；Recycling network, it is used for launching to support on the bracket, with safe retrieving unmanned plane；Communication device, for receiving the information of unmanned plane and/or sending the information of UAV Intelligent safe recovery device.This utility model UAV Intelligent safe recovery device has removable support assembly and the recycling network that can launch, thus volume is little when packing up, it is simple to transport, and can realize unmanned plane and reclaim in the case of without runway.It is particularly suited on Small Vessel, uses during field work, and even carry out reclaiming under adverse weather condition providing probability.Needing most proposition, light-duty unmanned plane can be accomplished to reclaim in traveling by the method completely.
Description
Technical field
This utility model relates to unmanned air vehicle technique field, particularly relates to a kind of UAV Intelligent safe recovery device.
Background technology
Along with the development of technology, unmanned plane will obtain utilizing the most widely.At present, big in terms of the recovery of unmanned plane
All use the mode that string hook-type reclaims, runway lands.On the one hand this mode needs point-device location, on the other hand needs
Bigger place.
Thus, it is desirable to have a kind of technical scheme overcomes or at least alleviates at least in the drawbacks described above of prior art
Individual.
Utility model content
The purpose of this utility model is provide a kind of UAV Intelligent safe recovery device to overcome or at least alleviate existing
There is at least one in the drawbacks described above of technology.
For achieving the above object, this utility model provides a kind of UAV Intelligent safe recovery device, described unmanned quick-witted
Can include by safe recovery device:
Carriage assembly, for can be assembled into support in the way of being dismounted for multiple times；
Recycling network, it is used for launching to support on the bracket, with safe retrieving unmanned plane；
Communication device, for receiving the information of unmanned plane and/or sending the information of UAV Intelligent safe recovery device.
Preferably, described support includes at least two pillars, and every described pillar is adjustable length pillar, wherein, described
Pillar is all identical.
Preferably, described support includes at least six roots of sensation pillar, to form a support providing regular hexagon fulcrum, and
It is horizontally disposed with recycling network at the top of support.
Preferably, described support includes at least six roots of sensation pillar, and each pillar at end with axially extending
Installing hole, installs the second end of another pillar with grafting, forms a double column support to assemble.
Preferably, the minimum of every pillar packs up length in the range of 1m to 1.5m, and maximum deployed length is at 1.5m extremely
In the range of 2.5m.
Preferably, described carriage assembly farther includes multiple connecting plate, for removably by described pillar even
Connecing and be fixed into self-supporting support, wherein said connecting plate is identical connecting plate, and is length-adjustable.
Preferably, at least some of in the plurality of connecting plate, just it is being adapted to into a rectangular susceptor or one
Hexagonal base.
Preferably, described UAV Intelligent safe recovery device farther includes charge and discharge air cushion.
Preferably, described air cushion after inflation, is placed on the lower section of the recycling network of expansion.
Preferably, described carriage assembly is provided with installing hole or interface, is used for arranging described communication device.
This utility model UAV Intelligent safe recovery device has removable support assembly and the recovery that can launch
Net, thus volume is little when packing up, it is simple to transport, and unmanned plane can be realized reclaim in the case of without runway.Especially
Be suitable on Small Vessel, use during field work, and even carry out reclaiming under adverse weather condition providing probability.
Needing most proposition, light-duty unmanned plane can be accomplished to reclaim in traveling by the method completely.
Accompanying drawing explanation
Fig. 1 is the first arrangement of the UAV Intelligent safe recovery device according to this utility model one embodiment
Schematic elevational view.
Fig. 2 is the schematic perspective view of the first arrangement shown in Fig. 1.
Fig. 3 and Fig. 4 a-4c is the schematic diagram illustrating the first arrangement step when reclaiming unmanned plane shown in Fig. 1.
Fig. 5 is the second arrangement of the UAV Intelligent safe recovery device according to this utility model one embodiment
Schematic elevational view.
Fig. 6 is the schematic perspective view of the second arrangement shown in Fig. 5.
Fig. 7 and Fig. 8 a-8c is the schematic diagram of the step illustrating the second arrangement shown in Fig. 5 when reclaiming unmanned plane.
Reference:
Detailed description of the invention
In the accompanying drawings, same or similar label is used to represent same or similar element or have same or like function
Element.Below in conjunction with the accompanying drawings embodiment of the present utility model is described in detail.
In description of the present utility model, term is " " center ", " longitudinally ", " laterally ", "front", "rear", "left", "right", " perpendicular
Directly ", orientation or the position relationship of the instruction such as " level ", " top ", " end " " interior ", " outward " is based on orientation shown in the drawings or position
Relation, is for only for ease of description this utility model and simplifies description rather than instruction or imply that the device of indication or element must
Must have specific orientation, with specific azimuth configuration and operation, therefore it is not intended that to this utility model protection domain
Limit.
Unmanned plane can be divided into fixed-wing unmanned plane, many rotor wing unmanned aerial vehicles according to profile and go straight up to unmanned plane.No matter its power
Being that battery provides, petroleum-based energy provides, or solar energy provides, and is intended to the time that unmanned plane aloft runs the longest
For a long time, steady safety is wanted in landing.Unmanned plane, takeoff and landing when, can expend the substantial amounts of energy, directly affects it aloft
The operation time.
Therefore, currently for the fixed-wing unmanned plane in unmanned plane, have employed catapult-launching gear and fixed-wing unmanned plane is launched
To aerial, help it to save its energy consumption in taking off, meanwhile, save the time of lift-off.As for landing or recalling receipts.
The range that the present invention relates to can contain fixed-wing unmanned plane, many rotor wing unmanned aerial vehicles and go straight up to unmanned plane machine
The recovery of type, is not limited only to fixed-wing unmanned plane, and the version of the safest catching net is different, and matched electronics is fixed
Position and piloting system really can be general.
The UAV Intelligent safe recovery device of the present invention has two kinds of arrangement forms.Fig. 1 to Fig. 4 c is that the first is arranged
Form: vertically arrangement form.Fig. 5-Fig. 8 c is the second arrangement form: horizontally disposed form.Wherein the first arrangement form is more
Add the safe retrieving being applicable to fixed-wing unmanned plane.
Communication device 3 in the UAV Intelligent safe recovery device of the present invention includes radio receiver,
For receiving the information for receiving unmanned plane.The information of unmanned plane such as include the position of unmanned plane, course line, when
Front speed, loading capacity, model, the information such as article of carrying.The information of unmanned plane can be that unmanned plane self sends, it is also possible to
Sent by control centre, communication center or other devices.
Communication device 3 in the UAV Intelligent safe recovery device of the present invention also includes that wireless base station apparatus is for sending
The information of UAV Intelligent safe recovery device.The information of UAV Intelligent safe recovery device such as includes positional information, shape
State information (whether being in receptive phase), arrangement form information (vertically or horizontally arrange), receive time window information, be suitable to
Information of unmanned plane specification received etc..
Advantageously, the communication device 3 in the UAV Intelligent safe recovery device of the present invention also includes main frame 3a, is used for
Carry out the operations such as data process or storage.
It is understood that communication device 3 includes the composition of electronic location and piloting system.Electronic positioning system includes electricity
Pond or solar energy, portable power plants, as energy offer, carry out accurate gps signal offer.Launch accurate safety to catch
The installation geographical position of net, with safe catching net as target position, formed one virtual and have the solid space of boundary limit, as
One pipeline is the same, after unmanned plane flies into this pipeline, gives piloting system, and unmanned plane pulls to safe catching net virtually,
Until touching net.
Meanwhile, piloting system is by including battery or solar energy, and portable power plants provides as the energy, can launch electronics
Signal, laser, microwave, far infrared or photoelectricity are freeed device, are bundled on the border of safe catching net as depicted, form one
Individual unmanned plane can be allowed to receive, virtual visual, the three-dimensional course line as pipeline and border, course line, and, on ground
Piloting system in, be provided with local wind speed, wind direction, the sensor acquisition of weather is to necessary to navigation system automatic to unmanned plane
Related data, in order to be adjusted flight in the course line that unmanned plane can accurately provide according to piloting system, and remain minimum
Biased error.
Unmanned plane also to have a set of automatic Pilot system that with the border interaction of virtual course line, can revise course line in time
System, so, unmanned plane just can be precisely targeted safe catching net, revises off-line action at any time, until it touches
Safe catching net, completes perfect postflight recycling step.
The UAV Intelligent safe recovery device of diagram embodiment includes:
Carriage assembly, for can be assembled into support in the way of being dismounted for multiple times；
Recycling network 2, it is used for launching to support on the bracket, with safe retrieving unmanned plane 6；
Communication device 3, for receiving the information of unmanned plane and/or sending the information of UAV Intelligent safe recovery device.
Advantageously, recycling network 2 has certain elasticity.For vertical arrangement and horizontal arranging mode, Ke Yishe
Put and use identical recycling network, it would however also be possible to employ different recycling networks.Seeing Fig. 1 and Fig. 5, recycling network 2 is passed through logical in corner portion
Cross the elastic devices such as spring and be connected to support or pillar 1.Thus, it is possible to the buffering unmanned plane impact to recycling network well
Advantageously, described support or carriage assembly include at least two pillars 1, and every described pillar 1 is adjustable length
Pillar.Preferably, pillar 1 is all identical.This advantageously reduces manufacturing cost, and beneficially O&M.Every pillar 1 wraps
Include inner tube and the outer tube of mutually socket, regulate length by stretching.It is of course also possible to use other adjustable length forms.Have
Profit, the minimum of every pillar 1 packs up length in the range of 1m to 1.5m, and maximum deployed length is at the model of 1.5m to 2.5m
In enclosing.Thus be conducive to using, transport and storing.
In order to lay orthohexagonal support to be horizontally disposed with recycling network 2, described support includes at least six roots of sensation pillar 1, with
Form a support that regular hexagon fulcrum is provided, and at the top of support, be horizontally disposed with recycling network 2.Advantageously, at water
In the case of plain cloth sets, the height of whole support is relatively low, for example, 2m, is generally arranged in the range of 1.5m-3m.
Advantageously, described pillar can be set to be mutually butted.Such as, in one embodiment, described
Frame includes at least six roots of sensation pillar 1, and each pillar at end with the installing hole axially extended, with grafting, another is installed
Second end of pillar, forms a double column support to assemble.Two, three, four, five or the most can be used
Pillar docks and is combined into a long struts.Thus build the height shown in Fig. 1 and reach the recovery structure of 10m.
Seeing Fig. 2 and Fig. 6, carriage assembly farther includes multiple connecting plate 8, for removably by described pillar
1 is connected into self-supporting support, and wherein said connecting plate is identical connecting plate 8, and is length-adjustable.Advantageously,
First connect a pedestal 7 with connecting plate 8.
In a preferred embodiment, at least some of in multiple connecting plates 8, it is adapted to into the pedestal of a rectangle
7 or an orthohexagonal pedestal 7.
In order to the unmanned plane reclaimed further is buffered, it is further provided with the air cushion 4 of charge-discharge type.Using
After, air cushion can be packed up.Described air cushion 4 after inflation, is placed on the lower section of the recycling network 2 of expansion.
Advantageously, described carriage assembly is provided with installing hole or interface, is used for arranging described communication device 3.From
And so that communication device is in higher height, it is simple to carry out communication.
Last it is noted that above example is only in order to illustrate the technical solution of the utility model, rather than it is limited
System.It will be understood by those within the art that: the technical scheme described in foregoing embodiments can be modified, or
Person carries out equivalent to wherein portion of techniques feature；These amendments or replacement, do not make the essence of appropriate technical solution take off
Spirit and scope from this utility model each embodiment technical scheme.
Claims (10)
1. a UAV Intelligent safe recovery device, it is characterised in that including:
Carriage assembly, for can be assembled into support in the way of being dismounted for multiple times；
Recycling network (2), it is used for launching to support on the bracket, with safe retrieving unmanned plane (6)；
Communication device (3), for receiving the information of unmanned plane and/or sending the information of UAV Intelligent safe recovery device.
2. UAV Intelligent safe recovery device as claimed in claim 1, it is characterised in that described support includes at least two
Pillar (1), every described pillar (1) is adjustable length pillar, and wherein, described pillar (1) is all identical.
3. UAV Intelligent safe recovery device as claimed in claim 2, it is characterised in that described support includes at least six roots of sensation
Pillar (1), to form a support providing regular hexagon fulcrum, and is horizontally disposed with recycling network (2) at the top of support.
4. UAV Intelligent safe recovery device as claimed in claim 2, it is characterised in that described support includes at least six roots of sensation
Pillar (1), and each pillar at end with the installing hole axially extended, install the second of another pillar with grafting
End, forms a double column support to assemble.
5. UAV Intelligent safe recovery device as claimed in claim 4, it is characterised in that the minimum receipts of every pillar (1)
Rise length in the range of 1m to 1.5m, maximum deployed length is in the range of 1.5m to 2.5m.
6. the UAV Intelligent safe recovery device as according to any one of claim 2-5, it is characterised in that described support group
Part farther includes multiple connecting plate (8), for removably described pillar (1) being connected into self-supporting support,
Wherein said connecting plate is identical connecting plate (8), and is length-adjustable.
7. UAV Intelligent safe recovery device as claimed in claim 6, it is characterised in that in the plurality of connecting plate (8)
At least some of, be adapted to into the pedestal (7) of a rectangle or an orthohexagonal pedestal (7).
8. the UAV Intelligent safe recovery device as according to any one of claim 1-5, it is characterised in that farther include
The air cushion (4) of charge-discharge type.
9. UAV Intelligent safe recovery device as claimed in claim 8, it is characterised in that described air cushion (4) after inflation,
It is placed on the lower section of the recycling network (2) of expansion.
10. UAV Intelligent safe recovery device as claimed in claim 1, it is characterised in that arrange on described carriage assembly
There are installing hole or interface, are used for arranging described communication device (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620455166.7U CN205707386U (en) | 2016-05-18 | 2016-05-18 | A kind of UAV Intelligent safe recovery device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620455166.7U CN205707386U (en) | 2016-05-18 | 2016-05-18 | A kind of UAV Intelligent safe recovery device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205707386U true CN205707386U (en) | 2016-11-23 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620455166.7U Expired - Fee Related CN205707386U (en) | 2016-05-18 | 2016-05-18 | A kind of UAV Intelligent safe recovery device |
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| CN (1) | CN205707386U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106494631A (en) * | 2016-12-06 | 2017-03-15 | 中国工程物理研究院总体工程研究所 | A kind of SUAV hits net energy-absorbing retracting device and its method for designing |
| CN107264735A (en) * | 2017-06-16 | 2017-10-20 | 上海复亚通信科技有限公司 | It is a kind of to offset the unmanned plane recycle bin of natural wind |
| CN107697303A (en) * | 2017-09-27 | 2018-02-16 | 北京航空航天大学 | A kind of unmanned plane space base retracting device and method based on the stable target system of aviation pull-type |
| CN108945328A (en) * | 2018-07-24 | 2018-12-07 | 西安天博机电科技有限公司 | A kind of recyclable device waterborne for unmanned plane |
| CN109144096A (en) * | 2018-08-15 | 2019-01-04 | 东汉太阳能无人机技术有限公司 | A kind of control method and unmanned plane of UAV Landing |
-
2016
- 2016-05-18 CN CN201620455166.7U patent/CN205707386U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106494631A (en) * | 2016-12-06 | 2017-03-15 | 中国工程物理研究院总体工程研究所 | A kind of SUAV hits net energy-absorbing retracting device and its method for designing |
| CN106494631B (en) * | 2016-12-06 | 2019-05-14 | 中国工程物理研究院总体工程研究所 | A kind of small drone hits the design method of net energy-absorbing recyclable device |
| CN107264735A (en) * | 2017-06-16 | 2017-10-20 | 上海复亚通信科技有限公司 | It is a kind of to offset the unmanned plane recycle bin of natural wind |
| CN107697303A (en) * | 2017-09-27 | 2018-02-16 | 北京航空航天大学 | A kind of unmanned plane space base retracting device and method based on the stable target system of aviation pull-type |
| CN108945328A (en) * | 2018-07-24 | 2018-12-07 | 西安天博机电科技有限公司 | A kind of recyclable device waterborne for unmanned plane |
| CN108945328B (en) * | 2018-07-24 | 2020-10-30 | 西安天博机电科技有限公司 | A recovery unit on water for unmanned aerial vehicle |
| CN109144096A (en) * | 2018-08-15 | 2019-01-04 | 东汉太阳能无人机技术有限公司 | A kind of control method and unmanned plane of UAV Landing |
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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: 20161123 |