CN108820197A - The unmanned hovering flight device of portable and collapsible aerating tourist line location - Google Patents
The unmanned hovering flight device of portable and collapsible aerating tourist line location Download PDFInfo
- Publication number
- CN108820197A CN108820197A CN201810740315.8A CN201810740315A CN108820197A CN 108820197 A CN108820197 A CN 108820197A CN 201810740315 A CN201810740315 A CN 201810740315A CN 108820197 A CN108820197 A CN 108820197A
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- China
- Prior art keywords
- unmanned plane
- unmanned
- body fuselage
- solar panels
- support bar
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- 230000001681 protective effect Effects 0.000 claims abstract description 41
- 239000005341 toughened glass Substances 0.000 claims abstract description 17
- 238000003466 welding Methods 0.000 claims abstract description 17
- 229920000297 Rayon Polymers 0.000 claims abstract description 4
- 239000007787 solid Substances 0.000 claims description 2
- 230000001771 impaired effect Effects 0.000 abstract description 4
- 238000000034 method Methods 0.000 description 8
- 238000010586 diagram Methods 0.000 description 3
- 230000003466 anti-cipated effect Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/16—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like specially adapted for mounting power plant
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/34—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising inflatable structural components
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Toys (AREA)
Abstract
The unmanned hovering flight device of portable and collapsible aerating tourist line location, including unmanned plane body fuselage, one corner of front surface of the unmanned plane body fuselage has been bolted to connection signal receiving antenna, the front surface middle position of the unmanned plane body fuselage is provided with solar panels, the corner of lower surface four of the solar panels is fixedly connected with solar panels connecting column A by viscous stick of viscous viscose, the two sides of the solar panels connecting column A are fixedly connected by welding and have elastic slice, the outer surface of the solar panels connecting column A is provided with solar panels connecting column B；By devising the tempered glass protective cover for being mounted on unmanned plane video camera outer surface convenient for protection unmanned plane video camera; if solving the unmanned hovering flight device of existing portable and collapsible aerating tourist line location, to occur the camera that accidental falling or collide with will lead to entrained by it in use impaired, thus the problem of causing unnecessary damage.
Description
Technical field
The invention belongs to air vehicle technique fields, and in particular to portable and collapsible aerating tourist line location is unmanned to suspend
Aircraft.
Background technique
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft, or fully or intermittently automatically operated by car-mounted computer.Unmanned plane presses application field, can be divided into
It is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane+industrial application are unmanned planes
Really just need；It taking photo by plane, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observation wild animal, monitoring at present
The application in infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, is greatly expanded
The purposes of unmanned plane itself, developed country also in actively extension industrial application and develop unmanned air vehicle technique.
If the existing unmanned hovering flight device of portable and collapsible aerating tourist line location is anticipated in use
It falls outside or the camera that will lead to entrained by it of colliding with is impaired, to cause unnecessary damage, and existing portable
Unmanned hovering flight device is reconnoitred since its long-time is in outdoor application in foldable inflating travelling route, takes off to not can guarantee it
Or level angle when landing, the problem of finally easily causing damage, thus it is proposed that portable and collapsible aerating tourist route
Reconnoitre unmanned hovering flight device.
Summary of the invention
The purpose of the present invention is to provide the unmanned hovering flight devices of portable and collapsible aerating tourist line location, to solve
It is proposed the unmanned hovering flight device of existing portable and collapsible aerating tourist line location in use process in above-mentioned background technique
If it is impaired to occur the camera that accidental falling or collide with will lead to entrained by it in, to cause unnecessary damage, and existing
Some unmanned hovering flight devices of portable and collapsible aerating tourist line location are since its long-time is in outdoor application, thus can not
The problem of guaranteeing level angle when it takes off or lands, finally easily causing damage.
To achieve the above object, the present invention provides the following technical solutions：Portable and collapsible aerating tourist line location without
One corner of front surface of people's hovering flight device, including unmanned plane body fuselage, the unmanned plane body fuselage passes through bolt
It is fixedly connected with signal receiving antenna, the front surface middle position of the unmanned plane body fuselage is provided with solar panels, institute
State the corners of lower surface four of solar panels by viscous viscose it is viscous it is glutinous is fixedly connected with solar panels connecting column A, it is described too
The two sides of positive energy panel connecting column A are fixedly connected by welding and have elastic slice, and the outer surface of the solar panels connecting column A is provided with
Solar panels connecting column B, and solar panels connecting column B is fixedly connected by welding with unmanned plane body fuselage, the unmanned plane
The two sides of body fuselage are fixedly connected to gas tube, and front surface one end of the gas tube is rotatably connected to nobody by shaft
Machine propeller, the upper surface middle position of the unmanned plane body fuselage are provided with unmanned plane video camera, and the unmanned plane is taken the photograph
The rear surface of camera is rotatably connected to video camera connecting rod by shaft, and video camera connecting rod passes through with unmanned plane body fuselage
Shaft rotation connection, the outer surface of the unmanned plane video camera is provided with tempered glass protective cover, the tempered glass protective cover
Rear surface top and bottom be provided with protective cover fixed block, the inner upper end of the unmanned plane body fuselage is solid by welding
Surely it is connected with fixed link spring, one end of the fixed link spring, which is fixedly connected by welding, protective cover fixed link, and protects
Cover fixed link and protective cover fixed block are fixed company by groove, four corners of rear surface of the unmanned plane body fuselage
It is provided with second support bar, one end of the second support bar is provided with support rod base, and supports rod base and unmanned plane
Body fuselage is bolted to connection, and the front surface of the support rod base is fixed by thread groove is connected with support
Bar fixes handwheel, and one end of the second support bar is provided with first support bar, and the inside of the first support bar is enclosed with branch
Strut spring, and support rod spring is fixedly connected by welding with second support bar, one end of the first support bar passes through weldering
It connects and is fixedly connected with support baseboard.
Preferably, the upper surface of the unmanned plane body fuselage is provided with "U" shaped groove.
Preferably, the shape of the tempered glass protective cover is semi-hollow cuboid.
Preferably, the upper surface of the protective cover fixed block is provided with circular hole.
Preferably, the shape of the first support bar is hollow cylinder.
Preferably, the diameter of the second support bar is equal to eight times of zero point of first support bar internal diameter.
Preferably, it is triangular hill that one end of the protective cover fixed link, which is provided with section shape,.
Preferably, the width of the support baseboard is equal to the diameter of first support bar.
Compared with prior art, the beneficial effects of the invention are as follows：
（1）By devising the tempered glass protective cover for being mounted on unmanned plane video camera outer surface convenient for protection unmanned plane camera shooting
Machine is anticipated in use if solving the unmanned hovering flight device of existing portable and collapsible aerating tourist line location
It falls outside or the camera that will lead to entrained by it of colliding with is impaired, thus the problem of causing unnecessary damage.
（2）By devising the first support bar and the second support bar that are mounted on unmanned plane body fuselage rear surface convenient for guarantor
The steady of unmanned plane body fuselage is demonstrate,proved, solves the unmanned hovering flight device of existing portable and collapsible aerating tourist line location
Since its long-time is in outdoor application, to not can guarantee level angle when it takes off or lands, damage is finally easily caused
Problem.
（3）By devising the solar panels for being mounted on unmanned plane body fuselage front surface convenient for absorbing solar energy source, solve
The unmanned hovering flight device of existing portable and collapsible aerating tourist line location of having determined can not absorb solar energy source, thus compared with
The problem of for waste of resource.
Detailed description of the invention
Fig. 1 is the structural diagram of the present invention；
Fig. 2 is tempered glass protective cover surface schematic cross-sectional view of the invention；
Fig. 3 is unmanned plane body fuselage surface structural schematic diagram of the invention；
Fig. 4 is first support bar partial cross-sectional structural diagram of the invention；
Fig. 5 is solar panels surface schematic cross-sectional view of the invention；
In figure：1- unmanned plane body fuselage, 2- tempered glass protective cover, 3- video camera connecting rod, 4- unmanned plane video camera, 5- fill
Tracheae, 6- signal receiving antenna, 7- fixed link spring, 8- protective cover fixed block, 9- protective cover fixed link, 10- support rod base,
11- support rod fix handwheel, 12- first support bar, 13- second support bar, 14- support baseboard, 15- support rod spring, 16- without
Man-machine propeller, 17- solar panels, 18- solar panels connecting column A, 19- elastic slice, 20- solar panels connecting column B.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Fig. 1-5 is please referred to, the present invention provides a kind of technical solution：Nobody is outstanding for portable and collapsible aerating tourist line location
Floating aircraft, including unmanned plane body fuselage 1, one corner of front surface of unmanned plane body fuselage 1 are bolted company
It is connected to signal receiving antenna 6, the front surface middle position of unmanned plane body fuselage 1 is provided with solar panels 17, solar panels
17 corner of lower surface four is fixedly connected with solar panels connecting column A18 by viscous stick of viscous viscose, solar panels connection
The two sides of column A18, which are fixedly connected by welding, elastic slice 19, and the outer surface of solar panels connecting column A18 is provided with solar panels
Connecting column B20, and solar panels connecting column B20 is fixedly connected by welding with unmanned plane body fuselage 1, unmanned plane body fuselage
1 two sides are fixedly connected to gas tube 5, and front surface one end of gas tube 5 is rotatably connected to unmanned plane propeller by shaft
16, the upper surface middle position of unmanned plane body fuselage 1 is provided with unmanned plane video camera 4, the rear surface of unmanned plane video camera 4
It is rotatably connected to video camera connecting rod 3 by shaft, and video camera connecting rod 3 and unmanned plane body fuselage 1 are rotated by shaft
Connection, the outer surface of unmanned plane video camera 4 are provided with tempered glass protective cover 2, the rear surface upper end of tempered glass protective cover 2 and
Lower end is provided with protective cover fixed block 8, and the inner upper end of unmanned plane body fuselage 1, which is fixedly connected by welding, fixed link bullet
Spring 7, one end of fixed link spring 7, which is fixedly connected by welding, protective cover fixed link 9, and protective cover fixed link 9 and protective cover
Fixed block 8 is fixed company by groove, and four corners of rear surface of unmanned plane body fuselage 1 are provided with second support bar
13, one end of second support bar 13 is provided with support rod base 10, and rod base 10 and unmanned plane body fuselage 1 is supported to pass through spiral shell
Bolt is fixedly connected, and the front surface of support rod base 10 is fixed by thread groove is connected with the fixed handwheel 11 of support rod, the
One end of two support rods 13 is provided with first support bar 12, and the inside of first support bar 12 is enclosed with support rod spring 15, and props up
Strut spring 15 is fixedly connected by welding with second support bar 13, and one end of first support bar 12 is fixedly connected by welding and has
Support baseboard 14.
It is inserted into for the ease of protective cover fixed block 8 and tempered glass protective cover 2, in the present embodiment, it is preferred that unmanned plane machine
The upper surface of body case 1 is provided with "U" shaped groove.
For the ease of package video camera connecting rod 3 and unmanned plane video camera 4, in the present embodiment, it is preferred that tempered glass is protected
The shape of shield 2 is semi-hollow cuboid.
It is inserted into for the ease of protective cover fixed link 9, in the present embodiment, it is preferred that the upper surface of protective cover fixed block 8 is arranged
There is circular hole.
For the ease of installation support rod spring 15 and second support bar 13, in the present embodiment, it is preferred that first support bar 12
Shape be hollow cylinder.
For the ease of being placed on the inside of first support bar 12, in the present embodiment, it is preferred that the diameter of second support bar 13
It is octuple equal to the zero point of 12 internal diameter of first support bar.
For the ease of fixed protective cover fixed block 8, in the present embodiment, it is preferred that one end of protective cover fixed link 9 is provided with
Section shape is triangular hill.
For the ease of folding, in the present embodiment, it is preferred that the width of support baseboard 14 is equal to the straight of first support bar 12
Diameter.
The working principle of the invention and process for using：After the device is installed, tempered glass protective cover 2 is linked in nothing
The outer surface of man-machine video camera 4, and guarantee that protective cover fixed block 8 is inserted into the inside of unmanned plane body fuselage 1, then firmly press
Tempered glass protective cover 2 so that protective cover fixed link 9 is fastened among the hole on protective cover fixed block 8, then rotates vertical
One support rod 12 and second support bar 13, and locked using the fixed handwheel 11 of support rod, it then can normally let the dress fly away
It sets, due to the presence of support rod spring 15, lands in the device with before letting fly away, can still be protected ground is not stable enough
It is horizontal to demonstrate,prove unmanned plane body fuselage 1, and when needing to dismantle unmanned plane video camera 4, firmly extracting tempered glass protective cover 2 is
Can, due to the presence of solar panels 17, the i.e. absorbable solar energy source of solar panels 17 in the device use process, to increase
It is continued a journey, and when needing to dismantle lower solar panels 17, to the both ends of 18 extrusion elastic 19 of solar panels connecting column A, simultaneously will
Solar panels connecting column A 18 is extracted inside solar panels connecting column B20.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (8)
1. the unmanned hovering flight device of portable and collapsible aerating tourist line location, including unmanned plane body fuselage（1）, feature
It is：The unmanned plane body fuselage（1）One corner of front surface be bolted to connection signal receiving antenna
（6）, the unmanned plane body fuselage（1）Front surface middle position be provided with solar panels（17）, the solar panels
（17）The corner of lower surface four glutinous be fixedly connected with solar panels connecting column A by the way that viscous viscose is viscous（18）, the sun
It can panel connecting column A（18）Two sides be fixedly connected by welding and have elastic slice（19）, the solar panels connecting column A（18）It is outer
Surface is provided with solar panels connecting column B（20）, and solar panels connecting column B（20）With unmanned plane body fuselage（1）Pass through weldering
It connects and is fixedly connected, the unmanned plane body fuselage（1）Two sides be fixedly connected to gas tube（5）, the gas tube（5）Before
Surface one end is rotatably connected to unmanned plane propeller by shaft（16）, the unmanned plane body fuselage（1）Upper surface among
Unmanned plane video camera is provided at position（4）, the unmanned plane video camera（4）Rear surface camera shooting is rotatably connected to by shaft
Machine connecting rod（3）, and video camera connecting rod（3）With unmanned plane body fuselage（1）It is rotatablely connected by shaft, the unmanned plane is taken the photograph
Camera（4）Outer surface be provided with tempered glass protective cover（2）, the tempered glass protective cover（2）Rear surface upper end and under
End is provided with protective cover fixed block（8）, the unmanned plane body fuselage（1）Inner upper end be fixedly connected by welding have it is solid
Fixed pole spring（7）, the fixed link spring（7）One end be fixedly connected by welding and have protective cover fixed link（9）, and protective cover
Fixed link（9）With protective cover fixed block（8）It is fixed company by groove, the unmanned plane body fuselage（1）Rear surface four
A corner is provided with second support bar（13）, the second support bar（13）One end be provided with support rod base（10）,
And support rod base（10）With unmanned plane body fuselage（1）It is bolted to connection, the support rod base（10）Preceding table
Face is fixed by thread groove is connected with the fixed handwheel of support rod（11）, the second support bar（13）One end be provided with
First support bar（12）, the first support bar（12）Inside be enclosed with support rod spring（15）, and support rod spring（15）
With second support bar（13）It is fixedly connected by welding, the first support bar（12）One end be fixedly connected by welding and have branch
Support bottom plate（14）.
2. the unmanned hovering flight device of portable and collapsible aerating tourist line location according to claim 1, feature exist
In：The unmanned plane body fuselage（1）Upper surface be provided with "U" shaped groove.
3. the unmanned hovering flight device of portable and collapsible aerating tourist line location according to claim 1, feature exist
In：The tempered glass protective cover（2）Shape be semi-hollow cuboid.
4. the unmanned hovering flight device of portable and collapsible aerating tourist line location according to claim 1, feature exist
In：The protective cover fixed block（8）Upper surface be provided with circular hole.
5. the unmanned hovering flight device of portable and collapsible aerating tourist line location according to claim 1, feature exist
In：The first support bar（12）Shape be hollow cylinder.
6. the unmanned hovering flight device of portable and collapsible aerating tourist line location according to claim 1, feature exist
In：The second support bar（13）Diameter be equal to first support bar（12）The zero point of internal diameter is octuple.
7. the unmanned hovering flight device of portable and collapsible aerating tourist line location according to claim 1, feature exist
In：The protective cover fixed link（9）One end be provided with section shape be triangular hill.
8. the unmanned hovering flight device of portable and collapsible aerating tourist line location according to claim 1, feature exist
In：The support baseboard（14）Width be equal to first support bar（12）Diameter.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2018103130518 | 2018-04-09 | ||
| CN201810313051 | 2018-04-09 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108820197A true CN108820197A (en) | 2018-11-16 |
Family
ID=64135562
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810740315.8A Pending CN108820197A (en) | 2018-04-09 | 2018-07-07 | The unmanned hovering flight device of portable and collapsible aerating tourist line location |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108820197A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110481778A (en) * | 2019-08-28 | 2019-11-22 | 清远市巨劲科技有限公司 | A kind of monitoring unmanned plane being tethered at long endurance |
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| CN104787335A (en) * | 2015-04-18 | 2015-07-22 | 南昌航空大学 | 3D printed solar unmanned aerial vehicle |
| CN105752332A (en) * | 2016-04-11 | 2016-07-13 | 徐州蓝翼航空科技有限公司 | Portable foldable four-rotor aircraft |
| US20170217562A1 (en) * | 2016-02-02 | 2017-08-03 | James Schalla | Unmanned inflatable aircraft |
| CN206664919U (en) * | 2017-04-14 | 2017-11-24 | 中博宇图信息科技有限公司 | A kind of unmanned plane |
| CN206782059U (en) * | 2017-06-05 | 2017-12-22 | 新疆飞诺植保科技有限公司 | Plant protection unmanned plane rack leg buffer unit |
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2018
- 2018-07-07 CN CN201810740315.8A patent/CN108820197A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104787335A (en) * | 2015-04-18 | 2015-07-22 | 南昌航空大学 | 3D printed solar unmanned aerial vehicle |
| US20170217562A1 (en) * | 2016-02-02 | 2017-08-03 | James Schalla | Unmanned inflatable aircraft |
| CN105752332A (en) * | 2016-04-11 | 2016-07-13 | 徐州蓝翼航空科技有限公司 | Portable foldable four-rotor aircraft |
| CN206664919U (en) * | 2017-04-14 | 2017-11-24 | 中博宇图信息科技有限公司 | A kind of unmanned plane |
| CN206782059U (en) * | 2017-06-05 | 2017-12-22 | 新疆飞诺植保科技有限公司 | Plant protection unmanned plane rack leg buffer unit |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110481778A (en) * | 2019-08-28 | 2019-11-22 | 清远市巨劲科技有限公司 | A kind of monitoring unmanned plane being tethered at long endurance |
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