CN110217373A - A kind of solar energy floating airplane parking area and mating single blade unmanned plane - Google Patents
A kind of solar energy floating airplane parking area and mating single blade unmanned plane Download PDFInfo
- Publication number
- CN110217373A CN110217373A CN201910537047.4A CN201910537047A CN110217373A CN 110217373 A CN110217373 A CN 110217373A CN 201910537047 A CN201910537047 A CN 201910537047A CN 110217373 A CN110217373 A CN 110217373A
- Authority
- CN
- China
- Prior art keywords
- motor
- parking area
- plate
- airplane parking
- unmanned plane
- Prior art date
- 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.)
- Pending
Links
- 230000013011 mating Effects 0.000 title claims abstract description 14
- 239000007789 gas Substances 0.000 claims description 37
- 238000010943 off-gassing Methods 0.000 claims description 9
- 230000001105 regulatory effect Effects 0.000 claims description 7
- 230000005611 electricity Effects 0.000 claims description 5
- 230000000694 effects Effects 0.000 claims description 4
- 229910000838 Al alloy Inorganic materials 0.000 claims description 3
- 239000000956 alloy Substances 0.000 claims description 3
- 239000001307 helium Substances 0.000 claims description 3
- 229910052734 helium Inorganic materials 0.000 claims description 3
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims description 3
- 229920003023 plastic Polymers 0.000 claims description 2
- 239000004033 plastic Substances 0.000 claims description 2
- 238000010586 diagram Methods 0.000 description 6
- 230000006872 improvement Effects 0.000 description 3
- 230000007613 environmental effect Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000008901 benefit Effects 0.000 description 1
- 239000012141 concentrate Substances 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000007306 turnover Effects 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
- B64U70/30—Launching, take-off or landing arrangements for capturing UAVs in flight by ground or sea-based arresting gear, e.g. by a cable or a net
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/06—Rigid airships; Semi-rigid airships
- B64B1/24—Arrangement of propulsion plant
- B64B1/30—Arrangement of propellers
- B64B1/32—Arrangement of propellers surrounding hull
-
- 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
- B64D5/00—Aircraft transported by aircraft, e.g. for release or reberthing during flight
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/30—Lighter-than-air aircraft, e.g. aerostatic aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/13—Propulsion using external fans or propellers
- B64U50/14—Propulsion using external fans or propellers ducted or shrouded
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/30—Supply or distribution of electrical power
- B64U50/34—In-flight charging
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
- B64U70/20—Launching, take-off or landing arrangements for releasing or capturing UAVs in flight by another aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/60—UAVs characterised by the material
-
- 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
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
-
- 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
- B64U2101/60—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons
- B64U2101/64—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons for parcel delivery or retrieval
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Transportation (AREA)
- Toys (AREA)
- Photovoltaic Devices (AREA)
Abstract
A kind of solar energy floating airplane parking area and mating single blade unmanned plane; including airplane parking area and single blade unmanned plane; airplane parking area is suspended in the air by floating buoyancy; single blade unmanned plane is provided only with single main screw; power unit is few; compared with traditional multiple propeller unmanned plane, flies more steady, jolt and shake smaller.The present invention provides a kind of solar energy floating airplane parking area and mating single blade unmanned plane, airplane parking area and is suspended in the air, is not take up ground space and does not need special messenger and nurses, and unmanned plane runs smoothly, and guarantees that package can transport safely.
Description
Technical field
The present invention relates to unmanned planes to dispense field, more particularly to a kind of solar energy floating airplane parking area and mating single blade without
It is man-machine.
Background technique
Unmanned plane dispatching, i.e., it is unmanned by being manipulated using radio robot and the presetting apparatus provided for oneself
Low flyer deliver package, be sent to destination automatically, advantage essentially consists in the dispatching for solving the problems, such as remote districts, raising
Efficiency is dispensed, while reducing human cost.
Existing unmanned plane dispensing device is mostly to install additional to use on the basis of existing unmanned plane based on traditional unmanned aerial vehicle design
In the bracket for placing package, unmanned plane operational process moderately gusty air is larger, is easy to cause package to turn over and falls, and unmanned plane is collecting and distributing by wrapping up
It is longer that point is transported to destination distance, lacks suitable transfer platform, the residential quarter that resident concentrates lacks large stretch of vacant lot for building
If unmanned plane transfer break point, and ground break point needs special messenger to nurse, waste of manpower.
Summary of the invention
In order to solve problem above, the present invention provides a kind of solar energy floating airplane parking area and mating single blade unmanned plane, stops
Machine level ground is suspended in the air, is not take up ground space and is not needed special messenger and nurses, and unmanned plane runs smoothly, and guarantees that package can pacify
It is for the national games defeated.
For this purpose, the present invention provides a kind of solar energy floating airplane parking area and mating single blade unmanned plane, including shut down
Level ground and single blade unmanned plane, the airplane parking area are the plate body of center symmetric shape, and plate body center is to shut down platform, are surrounded on plate body
It shuts down and is evenly arranged within platform one week solar panels, plate body edge is evenly arranged with floating ball for one week, is full of helium in floating ball, shuts down
Level ground can be floated under floating buoyancy effect it is aerial, plate body edge one week and also center symmetric setting have it is at least three horizontally disposed
Horizontal orientation motor, output end are connected with horizontal drive propeller, and each horizontal drive propeller central axes pass through plate body
Center line, plate body bottom are provided with support plate；The single blade unmanned plane includes the fuselage of hollow tube-shape, is provided with master in fuselage
Driving motor, main drive motor output end are main screw, and fuselage roof is provided with air inlet sieve plate, and main screw rotation makes fuselage
Outside air is entered in fuselage by air inlet sieve plate, is evenly arranged within side-of-body one week no less than three outgassing directions vertically downward
Power gas outlet, be evenly arranged within side-of-body one week no less than three outgassing direction levels torque offset gas outlet, turn round
Square counteracting gas outlet outgassing direction is identical as main screw direction of rotation, and fuselage bottom is provided with support frame, and support frame lower end is set
It is equipped with support foot, fixed plate is provided on support frame, master control borad and coupled battery and posture is provided in fixed plate
Sensor is additionally provided with camera in fixed plate, is connected to one output end of motor, and motor one is connected to two output end of motor, electricity
Machine one is vertical with two axis of motor, and motor two is vertically arranged, and camera can be achieved 360 ° under the drive of motor one and motor two
Rotation；The fixed plate bottom centre is additionally provided with vertical view camera, overlooks cam lens vertically downward, battery for pair
Main drive motor, motor one, motor two, attitude transducer and vertical view camera power supply.
The exit that further improvement of the present invention, the power gas outlet and torque offset gas outlet is provided with adjusting dress
It sets, the regulating device includes the adjustable plate at the central axes of gas outlet, and it is defeated that adjustable plate one end connects adjustable plate driving motor
Outlet can drive lower swing in motor, and adjustable plate driving motor is fixedly connected in gas outlet by adjustable plate motor fixing seat
Wall, adjustable plate other end connects hinge support, rocker bar bearing are fixedly connected on the inner wall of gas outlet.
Further improvement of the present invention, the torque are offset adjustable plate in gas outlet and are vertically arranged, the power gas outlet
Interior adjustable plate jante et perpendiculaire is in airplane parking area plate body centerline.
Further improvement of the present invention, the airplane parking area plate body and unmanned aerial vehicle body are all made of aluminum alloy materials or hard
Plastics are made.
A kind of the application solar energy floating airplane parking area and mating single blade unmanned plane, have the feature that
1) the application includes solar energy floating airplane parking area, and airplane parking area floats on control floating ball effect is small, and bottom can pass through drawing
Rope connection ground is not take up ground space, and airplane parking area has horizontally disposed horizontal drive propeller, and horizontal drive propeller turns
Dynamic certifiable airplane parking area is stablized in control position, and the consumed electric energy in airplane parking area is provided by solar panels, clean and environmental protection, the energy
It consumes low；
2) the application includes single blade unmanned plane, and the unmanned plane is only arranged independent blade for entering the wind, passes through power gas outlet
Unmanned plane during flying is realized in exhaust downwards, and since its power unit is few, compared with traditional multiple propeller unmanned plane, flight is more
Steadily, jolt and shake it is smaller, while be provided with torque offset gas outlet be used for offset main screw rotation generate torque, prevent
Only fuselage rotates in flight course, while power gas outlet and torque offset gas outlet and be additionally provided with regulating device progress outlet
Wind direction is adjusted, and realizes the adjusting in unmanned plane during flying direction.
Detailed description of the invention
Fig. 1 is airplane parking area of the present invention and mating single blade unmanned plane schematic diagram；
Fig. 2 is single blade unmanned plane schematic diagram of the present invention；
Fig. 3 is single blade unmanned plane partial schematic diagram one of the present invention；
Fig. 4 is single blade unmanned plane partial schematic diagram two of the present invention；
Fig. 5 is single blade unmanned plane partial schematic diagram three of the present invention；
Fig. 6 is single blade unmanned plane direction adjusting apparatus schematic diagram of the present invention；
Detailed description of the invention:
1, torque offsets gas outlet；2, air inlet sieve plate；3, power gas outlet；4, support frame；5, support foot；6, master control borad；7, it stores
Battery；8, camera；9, motor one；10, motor two；11, attitude transducer；12, camera is overlooked；13, main screw；14,
Main drive motor；15, adjustable plate motor fixing seat；16, adjustable plate driving motor；17, adjustable plate；18, rocker bar bearing；19, it floats
Ball；20, solar panels；21, platform is shut down；22, horizontal orientation motor；23, horizontal drive propeller；24, support plate.
Specific embodiment
Present invention is further described in detail with specific embodiment with reference to the accompanying drawing:
A kind of solar energy floating airplane parking area and mating single blade unmanned plane as shown in Figure 1, including airplane parking area and single blade nobody
Machine.Airplane parking area is the plate body of regular hexagon, and plate body center is to shut down platform 21, is uniformly set within platform 21 1 weeks on plate body around shutdown
Solar panels 20 are equipped with, plate body edge is uniformly arranged there are six floating ball 19 for one week, and each floating ball 19 is interior to be full of helium, and airplane parking area can
It is floated under 19 buoyancy of floating ball in the air, also there are three horizontally disposed horizontal fixed for center symmetric setting within one week at plate body edge
To motor 22, output end is connected with horizontal drive propeller 23, and each 23 central axes of horizontal drive propeller pass through plate body
Center line, plate body bottom are provided with support plate 24.Plate body can be connect by drawstring with ground, and plate body floats under the effect of floating ball 19
In aerial, floating ball 19 is greater than airplane parking area and unmanned plane carries the sum of package weight.
Airplane parking area has horizontally disposed horizontal drive propeller 23, and horizontal drive propeller 23, which rotates, can guarantee airplane parking area
Stablize in control position, the consumed electric energy in airplane parking area passes through solar panels 20 and provides, clean and environmental protection, low energy consumption.
The single blade unmanned plane as shown in Fig. 2,3,4 and 5 includes the fuselage of hollow tube-shape, and main driving electricity is provided in fuselage
Machine 14,14 output end of main drive motor are main screw 13, and fuselage roof is provided with air inlet sieve plate 2, and the rotation of main screw 13 makes
External fuselage air by air inlet sieve plate 2 enter fuselage in, be uniformly arranged within side-of-body one week there are three outgassing direction vertically downward
Power gas outlet 3, be uniformly arranged within side-of-body one week there are three outgassing direction level torque counteracting gas outlet 1, torque supports
1 outgassing direction of gas outlet that disappears is identical as 13 direction of rotation of main screw, and fuselage bottom is provided with support frame 4, and 4 lower end of support frame is set
It is equipped with support foot 5, fixed plate is provided on support frame 4, master control borad 6 and coupled 7 and of battery is provided in fixed plate
Attitude transducer 11 is additionally provided with camera 8 in fixed plate, is connected to one 9 output end of motor, motor 1 is connected to motor two
10 output ends, motor 1 is vertical with 2 10 axis of motor, and motor 2 10 is vertically arranged, and camera 8 is in motor 1 and motor two
360 ° of rotations can be achieved under 10 drive；Fixed plate bottom centre, which is additionally provided with, overlooks camera 12, overlooks 12 camera lens of camera
Vertically downward, battery 7 is used for main drive motor 14, motor 1, motor 2 10, attitude transducer 11 and overlooks camera
12 power supplies.
The exit that power gas outlet 3 and torque offset gas outlet 1 is provided with regulating device.Fig. 6 is with power gas outlet 3
Example, regulating device include the adjustable plate 17 at the central axes of gas outlet, and 17 one end of adjustable plate connection adjustable plate 17 drives electricity
16 output end of machine can drive lower swing in motor, and 17 driving motor 16 of adjustable plate is connected by 17 motor fixing seat 15 of adjustable plate is fixed
It is connected to the inner wall of gas outlet, 17 other end connects hinge support 18 of adjustable plate, rocker bar bearing 18 is fixedly connected on the interior of gas outlet
Wall.
Torque offset gas outlet 1 in adjustable plate 17 be vertically arranged, in power gas outlet 3 17 jante et perpendiculaire of adjustable plate in
Airplane parking area plate body centerline.Power gas outlet 3 and torque offset gas outlet 1 and are additionally provided with regulating device progress outlet wind direction tune
Section realizes the adjusting in unmanned plane during flying direction.
Airplane parking area plate body and unmanned aerial vehicle body are all made of aluminum alloy materials, as far as possible reduction own wt.
In actual use, it can be seen in real time by the vertical view camera 12 of camera 8 and bottom above fixed plate
Unmanned plane during flying environment is examined, the equipment such as package basket can be set on the outside of support frame 4 for placing package.It airplane parking area can be every one end
Distance is arranged, also settable battery 7 and wireless charging device on airplane parking area, and solar panels 20 are continuously the charging of battery 7, nothing
It is man-machine when being parked in airplane parking area, it can also be charged by wireless charging device to itself.
The above described is only a preferred embodiment of the present invention, being not the limit for making any other form to the present invention
System, and made any modification or equivalent variations according to the technical essence of the invention, still fall within present invention model claimed
It encloses.
Claims (4)
1. a kind of solar energy floating airplane parking area and mating single blade unmanned plane, which is characterized in that including airplane parking area and single blade without
Man-machine, the airplane parking area is the plate body of center symmetric shape, and plate body center is to shut down platform, around shutdown platform one week on plate body
Solar panels are evenly arranged with, plate body edge is evenly arranged with floating ball for one week, and helium is full of in floating ball, and airplane parking area can be floating in floating ball
It is floated under power effect in the air, the one week also center symmetric setting in plate body edge has at least three horizontally disposed horizontal orientations electricity
Machine, output end are connected with horizontal drive propeller, and each horizontal drive propeller central axes pass through plate body center line, plate body
Bottom is provided with support plate；The single blade unmanned plane includes the fuselage of hollow tube-shape, and main drive motor is provided in fuselage, main
Driving motor output end is main screw, and fuselage roof is provided with air inlet sieve plate, main screw rotation make external fuselage air by
Air inlet sieve plate enters in fuselage, is evenly arranged within side-of-body one week the power outlet of no less than three outgassing directions vertically downward
Mouthful, the torque for being evenly arranged with no less than three outgassing direction levels for side-of-body one week offsets gas outlet, and torque offsets outlet
Mouth outgassing direction is identical as main screw direction of rotation, and fuselage bottom is provided with support frame, and support frame lower end is provided with support foot,
It is provided with fixed plate on support frame, master control borad and coupled battery and attitude transducer are provided in fixed plate, it is fixed
It is additionally provided with camera on plate, is connected to one output end of motor, motor one is connected to two output end of motor, motor one and motor two
Axis is vertical, and motor two is vertically arranged, and 360 ° of rotations can be achieved in camera under the drive of motor one and motor two；The fixation
Plate bottom centre is additionally provided with vertical view camera, overlooks cam lens vertically downward, and battery is used for main drive motor, electricity
Machine one, motor two, attitude transducer and vertical view camera power supply.
2. a kind of solar energy floating airplane parking area according to claim 1 and mating single blade unmanned plane, it is characterised in that: institute
The exit for stating power gas outlet and torque counteracting gas outlet is provided with regulating device, and the regulating device includes being located at gas outlet
Adjustable plate at central axes, adjustable plate one end connect adjustable plate driving motor output end, can drive lower swing, adjustable plate in motor
Driving motor is fixedly connected on the inner wall of gas outlet, adjustable plate other end connects hinge support, hinge by adjustable plate motor fixing seat
Chain support is fixedly connected on the inner wall of gas outlet.
3. a kind of solar energy floating airplane parking area according to claim 2 and mating single blade unmanned plane, it is characterised in that: institute
It states adjustable plate in torque counteracting gas outlet to be vertically arranged, adjustable plate jante et perpendiculaire is in airplane parking area plate in the power gas outlet
Body centerline.
4. a kind of solar energy floating airplane parking area according to claim 1 to 3 and mating single blade unmanned plane, feature
It is: the airplane parking area plate body and unmanned aerial vehicle body is all made of aluminum alloy materials or rigid plastics is made.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910537047.4A CN110217373A (en) | 2019-06-20 | 2019-06-20 | A kind of solar energy floating airplane parking area and mating single blade unmanned plane |
| PCT/CN2020/095624 WO2020253614A1 (en) | 2019-06-20 | 2020-06-11 | Solar floating parking apron and matching single-blade unmanned aerial vehicle |
| BE20205444A BE1027331B1 (en) | 2019-06-20 | 2020-06-18 | Hovering solar aircraft parking area and associated single-blade unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910537047.4A CN110217373A (en) | 2019-06-20 | 2019-06-20 | A kind of solar energy floating airplane parking area and mating single blade unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110217373A true CN110217373A (en) | 2019-09-10 |
Family
ID=67813973
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910537047.4A Pending CN110217373A (en) | 2019-06-20 | 2019-06-20 | A kind of solar energy floating airplane parking area and mating single blade unmanned plane |
Country Status (3)
| Country | Link |
|---|---|
| CN (1) | CN110217373A (en) |
| BE (1) | BE1027331B1 (en) |
| WO (1) | WO2020253614A1 (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20200009989A1 (en) * | 2018-07-04 | 2020-01-09 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | Aircraft |
| WO2020253614A1 (en) * | 2019-06-20 | 2020-12-24 | 金陵科技学院 | Solar floating parking apron and matching single-blade unmanned aerial vehicle |
| CN114919741A (en) * | 2022-05-17 | 2022-08-19 | 西安电子科技大学 | Tiltable four-rotor aerostat array |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114847064B (en) * | 2022-05-26 | 2023-07-14 | 安徽科技学院 | Noctuid black egg bee field bee-releasing positioning system |
| WO2024056195A1 (en) * | 2022-09-16 | 2024-03-21 | Kji Dronelab Bv | Propulsion system for multicopters and related aircrafts |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2296851Y (en) * | 1997-01-08 | 1998-11-11 | 邱刚 | Single rotor craft groove air passage antitorque device |
| US20180093766A1 (en) * | 2016-09-30 | 2018-04-05 | Youngsub Ahn | Propeller-Enclosed Airlifting Air Tube Apparatus |
| CN107953995A (en) * | 2017-12-01 | 2018-04-24 | 雷安静 | A kind of combined system of aerostatics unmanned plane |
| JP2018144539A (en) * | 2017-03-02 | 2018-09-20 | 株式会社プロドローン | Unmanned aircraft |
| CN109178313A (en) * | 2018-10-17 | 2019-01-11 | 江苏铨铨信息科技有限公司 | Cooperate satellite navigation long continuation of the journey unmanned plane and mating long-range photovoltaic laser battery charger cradle |
| CN109398734A (en) * | 2018-10-31 | 2019-03-01 | 送飞实业集团有限公司 | A kind of solar energy radio charging unmanned plane airplane parking area |
| CN109733598A (en) * | 2018-11-26 | 2019-05-10 | 顺丰科技有限公司 | Aircraft duct and culvert type aircraft |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6616094B2 (en) * | 1999-05-21 | 2003-09-09 | Vortex Holding Company | Lifting platform |
| US20060284002A1 (en) * | 2005-02-08 | 2006-12-21 | Kurt Stephens | Unmanned Urban Aerial Vehicle |
| KR101217804B1 (en) * | 2010-06-01 | 2013-01-22 | (주)선택이앤티 | Bottom propeller control type vehicle |
| US8596571B2 (en) * | 2011-03-31 | 2013-12-03 | Lta Corporation | Airship including aerodynamic, floatation, and deployable structures |
| JP5875093B1 (en) * | 2015-06-17 | 2016-03-02 | 浩平 中村 | Levitation aircraft |
| US20190176986A1 (en) * | 2016-08-03 | 2019-06-13 | Stealth Air Corp | Multi-craft uav carrier system and airframe |
| CN107117316B (en) * | 2017-04-27 | 2019-06-11 | 上海电力学院 | A kind of detachable unmanned plane assisting in flying device |
| CN206826924U (en) * | 2017-06-08 | 2018-01-02 | 北京化工大学 | A kind of two-stage balanced control device of multi-rotor unmanned aerial vehicle aircraft carrier |
| CN208284090U (en) * | 2018-04-13 | 2018-12-25 | 北京中科遥数信息技术有限公司 | A kind of unmanned plane low battery emergency set |
| CN110217373A (en) * | 2019-06-20 | 2019-09-10 | 金陵科技学院 | A kind of solar energy floating airplane parking area and mating single blade unmanned plane |
-
2019
- 2019-06-20 CN CN201910537047.4A patent/CN110217373A/en active Pending
-
2020
- 2020-06-11 WO PCT/CN2020/095624 patent/WO2020253614A1/en active Application Filing
- 2020-06-18 BE BE20205444A patent/BE1027331B1/en active IP Right Grant
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2296851Y (en) * | 1997-01-08 | 1998-11-11 | 邱刚 | Single rotor craft groove air passage antitorque device |
| US20180093766A1 (en) * | 2016-09-30 | 2018-04-05 | Youngsub Ahn | Propeller-Enclosed Airlifting Air Tube Apparatus |
| JP2018144539A (en) * | 2017-03-02 | 2018-09-20 | 株式会社プロドローン | Unmanned aircraft |
| CN107953995A (en) * | 2017-12-01 | 2018-04-24 | 雷安静 | A kind of combined system of aerostatics unmanned plane |
| CN109178313A (en) * | 2018-10-17 | 2019-01-11 | 江苏铨铨信息科技有限公司 | Cooperate satellite navigation long continuation of the journey unmanned plane and mating long-range photovoltaic laser battery charger cradle |
| CN109398734A (en) * | 2018-10-31 | 2019-03-01 | 送飞实业集团有限公司 | A kind of solar energy radio charging unmanned plane airplane parking area |
| CN109733598A (en) * | 2018-11-26 | 2019-05-10 | 顺丰科技有限公司 | Aircraft duct and culvert type aircraft |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20200009989A1 (en) * | 2018-07-04 | 2020-01-09 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | Aircraft |
| US11505087B2 (en) * | 2018-07-04 | 2022-11-22 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | Aircraft |
| WO2020253614A1 (en) * | 2019-06-20 | 2020-12-24 | 金陵科技学院 | Solar floating parking apron and matching single-blade unmanned aerial vehicle |
| CN114919741A (en) * | 2022-05-17 | 2022-08-19 | 西安电子科技大学 | Tiltable four-rotor aerostat array |
| CN114919741B (en) * | 2022-05-17 | 2024-03-12 | 西安电子科技大学 | Tilting four-rotor aerostat array |
Also Published As
| Publication number | Publication date |
|---|---|
| BE1027331B1 (en) | 2021-03-12 |
| BE1027331A1 (en) | 2021-01-06 |
| WO2020253614A1 (en) | 2020-12-24 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN110217373A (en) | A kind of solar energy floating airplane parking area and mating single blade unmanned plane | |
| US10076763B2 (en) | Propeller lift suspension boom truss spray combination module system | |
| CN103944236B (en) | wireless charging platform based on natural energy electric power storage | |
| CN108162795A (en) | A kind of airborne aircraft aerial power supply unit of mating solar energy | |
| CN110037004A (en) | Bird damage prevention device and man-made nest integral system for transmission line of electricity | |
| CN206954522U (en) | A kind of hanging type loading unmanned plane | |
| CN108820229A (en) | Hybrid power unmanned plane based on computer mode control | |
| CN205667717U (en) | A kind of balloon flighter | |
| CN111976973A (en) | Vision-assisted cleaning unmanned aerial vehicle system | |
| CN107276185A (en) | Solar energy unmanned plane base station | |
| CN108316167B (en) | A kind of rotary unmanned plane airplane parking area | |
| CN106941246B (en) | A kind of electrical power distribution electric network Bird's Nest removing unmanned plane | |
| CN110979628A (en) | Intelligent aerostat and control terminal | |
| CN205921296U (en) | Flight system for clearing away hanging objects on power transmission line | |
| CN203318682U (en) | Solar parafoil aerocraft | |
| CN216070561U (en) | Portable unmanned aerial vehicle berths platform | |
| CN213200125U (en) | Unmanned aerial vehicle with balanced lifting | |
| CN204979221U (en) | There is asynchronous multiaxis aircraft of rope | |
| CN109866929A (en) | A kind of unmanned plane with long cruising ability | |
| CN208979094U (en) | A kind of water quality sampling unmanned plane | |
| CN209270816U (en) | A kind of small-sized solar aeromodelling airplane | |
| CN205098465U (en) | That takes transformer has a rope asynchronous machine multiaxis aircraft | |
| CN208947595U (en) | A kind of power supply station's intelligent fault inspection device | |
| CN209600800U (en) | A kind of VTOL is verted three rotor wing unmanned aerial vehicles | |
| CN111332471A (en) | Self-rotating single-wing seed aircraft |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination |