CN206218218U - A kind of solar powered vertical lift unmanned plane - Google Patents
A kind of solar powered vertical lift unmanned plane Download PDFInfo
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- CN206218218U CN206218218U CN201621263018.1U CN201621263018U CN206218218U CN 206218218 U CN206218218 U CN 206218218U CN 201621263018 U CN201621263018 U CN 201621263018U CN 206218218 U CN206218218 U CN 206218218U
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- rotor
- organism frame
- unmanned plane
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- motor
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Abstract
The utility model is applied to unmanned plane field, there is provided a kind of solar powered vertical lift unmanned plane, including organism frame and fixed rotor, the fixed rotor is arranged on one end of the organism frame, and parallel to the organism frame, the unmanned plane also includes some solar battery sheets and regulation rotor, some solar battery sheets are arranged on the upper surface of the organism frame, the regulation rotor is arranged on the other end of the organism frame, and the rotationally switching between the state of the organism frame is parallel and perpendicular to, the regulation rotor is provided with the swaying direction regulating part for controlling the regulation rotor to be swung when perpendicular to the organism frame state.The unmanned plane, constantly for inside is powered and charges, improves the endurance of unmanned plane by self-contained solar battery sheet；Meanwhile, by adjusting rotor adjustment effect while realizing taking off, advance and turning to for unmanned plane, and then improve the convenience of unmanned plane operation.
Description
Technical field
The utility model belongs to unmanned plane field, more particularly to a kind of solar powered vertical lift unmanned plane.
Background technology
At present, rotary wind type unmanned plane has been widely used for agricultural, industrial circle, is used for ancillary staff and completes special
Fixed work.
Existing unmanned plane is mostly four rotors, six rotors or eight rotor wing unmanned aerial vehicles, and each rotor is in the flat of sustained height
On face, size is identical, and power is provided by the motor for being accordingly distributed in rotor bracket end.Cruising time is electric at 20-35 minutes
Machine is more, and cruising time is shorter, and the charging interval is long, reduces work limitation.Additionally, the rotor of existing unmanned plane is only used for
Unmanned plane takes off, and the steering of unmanned plane needs to be realized by mechanisms such as afterbody steering wheels that complex structure, production cost is high.
For example taken photo by plane for carrying out prospecting to photovoltaic plant, because photovoltaic plant floor space is big, at this stage to photovoltaic electric
The short circuit stood, the detection of solar energy hot spot are main by manually irregularly or periodically manually based on inspection, under manual inspection efficiency,
Unmanned plane can carry out some simple operations of taking photo by plane with ancillary staff, but due to endurance and facility without stabilization
Operability, made troubles to practical application.
Utility model content
Technical problem to be solved in the utility model is a kind of solar powered vertical lift unmanned plane of offer, it is intended to carried
The endurance of unmanned plane high, and improve the convenience of unmanned plane operation.
In order to solve the above technical problems, the utility model is achieved in that one kind is solar powered is vertically moved up or down nobody
Machine, including organism frame and fixed rotor, the fixed rotor are arranged on one end of the organism frame, and parallel to the machine
Body framework, the unmanned plane also includes some solar battery sheets and regulation rotor, and some solar battery sheets are arranged on
The upper surface of the organism frame, the regulation rotor is arranged on the other end of the organism frame, and rotationally parallel
And switch between the state of the organism frame, the regulation rotor is provided with for controlling the regulation rotor hanging down
The straight swaying direction regulating part swung when the organism frame state.
Further, the front end of the organism frame offers at least one through hole, and the rear end of the organism frame opens up
There is at least one through hole, the through hole of the through hole of the organism frame front end and the organism frame rear end is on the body frame
The center line of frame is symmetrical arranged, and the fixed rotor is contained in the through hole of the organism frame front end, and the regulation rotor can
Rotationally it is contained in the through hole of the organism frame rear end.
Further, the front end of the organism frame offers two through holes, and the rear end of the organism frame offers one
Individual through hole, the through hole of the organism frame rear end is located on the center line of through hole line of the organism frame front end two, described
Before fixed rotor includes that the first rotor and the second rotor, first rotor and the second rotor are respectively contained in the organism frame
In the through hole at end, the regulation rotor is rotationally contained in the through hole of the organism frame rear end.
Further, the unmanned plane also includes the first cover plate and the second cover plate, first cover plate and the second cover plate point
The side and symmetrically of first rotor and the second rotor, first cover plate and the second cover plate are not installed in rotation on
It is interlocked with the through hole where first rotor and the second rotor respectively or along the side expansion of respective rotor.
Further, the one side of fixed rotor is closed on after being interlocked with respective through hole on first cover plate and the second cover plate
Some solar battery sheets are provided with, its another side is provided with navigation lights.
Further, the first motor is installed, first motor passes through with the regulation rotor on the organism frame
Gear drive is connected, and first motor drives the regulation rotor to be rotated relative to the organism frame horizontal/vertical.
Further, the regulation rotor includes adjustment seat, rotor motor and rotating vane, the adjustment seat and described the
One motor is connected by gear drive, and is installed in rotation on institute's organism frame under the drive of first motor, institute
State rotor motor to be fixed in the adjustment seat, the rotating vane is arranged in the rotor motor.
Further, the swaying direction regulating part includes regulating part and the second motor, and the regulating part is arranged on described
On regulation rotor, second motor is fixed in the outer rim of the regulation rotor and is connected with the regulating part, described second
Motor drives the regulating part to swing.
Further, the rear end of the organism frame offers through hole, and the regulation rotor is rotationally contained in described
In through hole, the groove for placing second motor, the regulation rotor and the body are offered on the through-hole wall
Framework is under parastate, and second motor is correspondingly fastened in the groove.
Further, the unmanned plane also includes infrared thermovision camera and camera of taking photo by plane, the infrared thermovision shooting
Head and lower surface of the camera installed in the organism frame of taking photo by plane, and near the front end of the organism frame.
Further, the unmanned plane also includes the labelling apparatus for being marked to fault zone, the mark dress
Colored liquid is loaded with putting.
Compared with prior art, beneficial effect is the utility model：One kind of the present utility model is solar powered vertical
Lifting unmanned plane, it includes organism frame, some solar battery sheets, fixed rotor and regulation rotor.Due in organism frame
Upper surface be provided with some solar battery sheets, during unmanned plane during flying on daytime, by self-contained solar battery sheet not
Break as inside is powered and charges, during the non-flight of unmanned plane on daytime, also constantly charged to unmanned machine battery in the sun,
Until battery is full of, so as to improve the endurance of unmanned plane.Additionally, when unmanned plane takes off, by by the regulation rotor
The state parallel with fixed rotor is adjusted to, is rotated by the high speed of fixed rotor and regulation rotor and is produced lift to realize nobody
Machine takes off.It is perpendicular with fixed rotor by adjusting the regulation rotor when needing to advance after unmanned plane rising, then adjust
Rotor produces larger thrust forward with air-flow, realizes the flight of unmanned plane.When unmanned plane needs to turn to, by the tune
Swinging for the swaying direction regulating part on rotor is saved, changes the direction of unmanned plane tail wind, realize the steering of unmanned plane,
By adjusting the adjustment effect of rotor while realizing taking off, advance and turning to for unmanned plane, the convenient of unmanned plane operation is improve
Property.
Brief description of the drawings
Fig. 1 is the structural representation of a kind of solar powered vertical lift unmanned plane that the utility model embodiment is provided.
Fig. 2 is the structural representation of another state of Fig. 1.
Fig. 3 is the present invention looks up structural representation of Fig. 1.
Fig. 4 is the first motor and the structural representation for adjusting rotor in Fig. 1.
Fig. 5 is the close-up schematic view of part A in Fig. 4.
Specific embodiment
In order that the purpose of this utility model, technical scheme and advantage become more apparent, below in conjunction with accompanying drawing and implementation
Example, is further elaborated to the utility model.It should be appreciated that specific embodiment described herein is only used to explain
The utility model, is not used to limit the utility model.
As shown in Figure 1 to Figure 3, it is a kind of solar powered vertical lift unmanned plane that the utility model embodiment is provided
100, it includes organism frame 1, some solar battery sheets 2, fixed rotor 3 and regulation rotor 4.The fixed rotor 3 is set
In one end of the organism frame 1, and parallel to the organism frame 1, institute's some solar battery sheets 2 are arranged on described
The upper surface of organism frame 1, is charged for the internal cell endlessly to unmanned plane 100.The regulation rotor 4 sets
Put the other end in the organism frame 1, and rotationally cut between the state of the organism frame 1 is parallel and perpendicular to
Change, switched by the parallel and vertical mutual of regulation rotor 4, realize taking off and advancing for unmanned plane 100.The regulation rotation
The wing 4 is provided with swaying direction regulating part 41, and the swaying direction regulating part 41 controls the regulation rotor 4 perpendicular to the machine
Swung during the state of body framework 1, the airflow direction of the afterbody of unmanned plane 100 is changed with this, so as to realize turning for unmanned plane 100
To.
The front end of the organism frame 1 offers at least one through hole, and the rear end of the organism frame 1 offers at least one
Individual through hole, the through hole of the front end of the organism frame 1 and the through hole of the rear end of the organism frame 1 are on the organism frame 1
Center line is symmetrical arranged.The fixed rotor 3 is contained in the through hole of the organism frame front end 1, and the regulation rotor 4 can turn
It is contained in dynamicly in the through hole of the rear end of the organism frame 1, thereby protects the fixed rotor 3 and regulation rotor 4 is not damaged
Wound.
Specifically, in the utility model embodiment, the front end of the organism frame 1 offers two through holes and (does not mark
Note), the rear end of the organism frame 1 offers a through hole (mark), and the through hole of the organism frame rear end is positioned at described
On the center line of through hole line of organism frame front end two.The fixed rotor 3 includes the first rotor 31 and the second rotor 32, institute
State the first rotor 31 and the second rotor 32 is respectively contained in the through hole of the front end of the organism frame 1, the regulation rotor 4 can turn
It is contained in dynamicly in the through hole of the rear end of the organism frame 1, so as to form three rotor mechanisms of isosceles triangle.The utility model
In embodiment, the organism frame 1 is integrally formed, and holds by by first rotor 31, the second rotor 32 and regulation rotor 4
Put in the through hole of the organism frame 1, it is to avoid make the exposed outside in organism frame 1 of each rotor, will not in flight because
The rotation of rotor and accidentally injure staff, object etc.；Avoid simultaneously causes unmanned plane 100 to be broken after falling because of maloperation
Rotor, can play a part of to protect rotor, improve the security and economy of product.Additionally, three rotors of integral type
Mechanism is conducive to improving the stability of whole machine, strengthens wind resistance coefficient, it is ensured that the stationarity and reliability of the flight course of unmanned plane 100
Property.
The unmanned plane 100 also includes the first cover plate 5 and the second cover plate 6, and the cover plate 6 of first cover plate 5 and second is distinguished
The side for being installed in rotation on the rotor 32 of first rotor 31 and second is simultaneously symmetrical.First cover plate 5 and second
Cover plate 6 is interlocked or along the side expansion of respective rotor with the through hole where 31 and second rotor of the first rotor 32 respectively.
The one side that fixed rotor 3 is closed on after being interlocked with respective through hole on the cover plate 6 of first cover plate 5 and second is provided with some solar energy
Cell piece 2, its another side is provided with navigation lights 7.When the unmanned plane 100 is under non-working condition, by first cover plate 5
It is interlocked with the through hole where 31 and second rotor of the first rotor 32 with the second cover plate 6, so as to prevent first rotor
31 and second rotor 32 sustain damage.When the unmanned plane 100 begins to use, the cover plate 6 of first cover plate 5 and second is opened up
Open, now, if some solar battery sheets 2 on the cover plate 6 of first cover plate 5 and second coordinate on the organism frame 1
Dry solar battery sheet 2 is jointly for the unmanned plane 100 provides continuation of the journey.Additionally, when unmanned plane 100 is in night flight, can lead to
The highlighted LED navigation lights 7 crossed on the cover plate 6 of first cover plate 5 and second is for manipulator provides the visual field.
Reference picture 4 and Fig. 5, are provided with the first motor 8, first motor 8 and the regulation rotation on the organism frame 1
The wing 4 by gear drive connect, first motor 8 drive it is described regulation rotor 4 relative to the level of the organism frame 1/hang down
Direct rotary turns.
The regulation rotor 4 includes adjustment seat 42, rotor motor 43 and rotating vane 44, the adjustment seat 42 and described the
One motor 8 is connected by gear drive, and is installed in rotation on institute's organism frame 1 under the drive of first motor 8,
The rotor motor 43 is fixed in the adjustment seat 42, and the rotating vane 44 is arranged in the rotor motor 43.It is described
First motor 8 drives the adjustment seat 42 to be rotated relative to the horizontal vertical of the organism frame 1.When the adjustment seat 42 be in
During the parallel position of organism frame 1, the rotating vane 44 for controlling the regulation rotor 4 by hand-held control operation bar coordinates
Rotation forms lift to the rotating vane of the rotor 32 of first rotor 31 and second at a high speed jointly, when lift is more than unmanned plane 100
Main screw lift when, then unmanned plane 100 realize take off vertically, it is not necessary to runway and landing spatial domain, it is flexible and convenient to use.When described
When the vertical ascent of unmanned plane 100 needs to advance, the adjustment seat 42 is adjusted to and body frame by hand-held control operation bar
The perpendicular position of frame 1, now the rotating vane 44 and air-flow produce larger thrust forward, so as to realize unmanned plane
100 move ahead, compared to the flight of traditional unmanned plane, the traveling mode of unmanned plane of the present utility model 100 can possess higher
Forward flight speed.
The swaying direction regulating part 41 includes the motor 412 of regulating part 411 and second, and the regulating part 411 is arranged on institute
State regulation rotor 4 adjustment seat 42 on, second motor 412 be fixed in the outer rim of the adjustment seat 42 and with the regulation
Part 411 is connected.By hand-held control operation bar control second motor 412 drive the regulating part 411 it is described nobody
Swung under the state of flight of machine 100, so as to change the tail wind direction of unmanned plane 100, realize turning to, make the unmanned plane
100 steering flight more convenient quickly.Regulating part 411 in the utility model embodiment is semicircular rudder, but not
It is defined in the shape of the regulating part 411.
The groove 11 for placing second motor 412 is offered on the through-hole wall of the rear end of the organism frame 1.Institute
State adjustment seat 42 to be under parastate with the organism frame 1, second motor 412 is correspondingly fastened on the groove 11
It is interior, when unmanned plane 100 does not run, prevent second motor 412 from sustaining damage.
Reference picture 4, the first rotor 31 is identical with the structure of the second rotor 32 described in the utility model embodiment, and described first
Rotor 31 includes fixed seat 311, motor 312 and rotating vane 313, and the fixed seat 311 is fixed on the front end of the organism frame 1
Through hole in, the motor 312 is fixed in the fixed seat 311, the rotating vane 313 be arranged on the motor 312 on.
Reference picture 3, the unmanned plane 100 also includes infrared thermovision camera and camera 9 of taking photo by plane, and the infrared thermovision is taken the photograph
As head and lower surface of the camera 9 installed in the organism frame 1 of taking photo by plane, and near the front end of the organism frame 1.Double shootings
In the design that head is combined, infrared thermovision camera is used to shoot electrical property short circuit and hot spot undesired component in power station, and quickly adopts
Collection feedback；Camera of taking photo by plane then is used to gather traditional photo and video.Dual camera by photographed data common feedback to ground dough figurine
Member's collection center, finds and solve problem in time so as to staff.Unmanned plane 100 flies over space-time on photovoltaic plant, to photovoltaic
Apparatus assembly in power station carries out infrared thermal imaging shooting, when there is component to be short-circuited in photovoltaic plant, hot spot or has foreign matter to hide
During gear, power station component temperature can be raised therewith, and the infrared thermovision camera of the unmanned plane 100 and the scanning of camera 9 of taking photo by plane are arrived
During short-circuit component, temperature rising module can be rapidly found, and in the computer of image feedback to bottom surface staff, will allow ground handling people
The quick positioning of member, the operating efficiency that raising is patrolled and examined and short-circuit component is detected.
The unmanned plane 100 also includes being loaded with colored liquid in labelling apparatus 10, the labelling apparatus 10.When described red
Outer thermovision camera and take photo by plane camera 9 scanning to power station problem component when, can control the unmanned plane 100 drop to problem
Component top, and colored liquid is sprayed to problem component by the labelling apparatus 10, problem component is marked, convenient inspection
Personnel positioning maintenance is repaiied, the working time is saved.
The unmanned plane 100 also includes some landing gears 20, and some landing gears 20 are fixed on the nothing
The lower surface of people's machine frame 1, for when the unmanned plane 100 lands, supports the unmanned machine frame 1, prevent it is described nobody
Machine 100 directly falls on the ground and body is caused to damage.
During specific works, staff adjusts the regulation rotor 4 to parastate by hand-held control operation bar, this
When control unmanned plane 100 on rotor on the motor 312 of the first rotor, the motor (mark) of the second rotor and regulation rotor it is electric
Machine 43 starts jointly, and rotation forms lift at a high speed to drive each rotating vane, when gross weight of the lift more than unmanned plane 100, makes nothing
Man-machine 100 take off vertically.Fly to after certain altitude, staff controls the first motor 8 to open by hand-held control operation bar
It is dynamic, and drive adjustment seat 42 to rotate, so as to the regulation rotor 4 is converted into plumbness, after the regulation rotor 4 is vertical,
Larger thrust forward is produced with air-flow, makes the flight forward of unmanned plane 100.When needing to turn, controlled by the hand-held
Action bars controls the second motor 412 to start, and second motor 412 controls the regulating part 411 to swing, so as to change gas
The direction of stream, makes directional steering of the unmanned plane 100 to needs.In the flight course of unmanned plane 100, imaged by the infrared thermovision
Head and camera 9 of taking photo by plane are scanned to photovoltaic plant, after component of pinpointing the problems, image are back to the electricity of surface personnel
On brain, staff controls unmanned plane 100 to drop to the top of problem component by the hand-held control operation bar, and passes through
Labelling apparatus 10 are marked to problem component, are easy to later period maintenance to position.If when the unmanned plane 100 is used at night,
Can be by the highlighted LED navigation lights 7 on the cover plate 6 of first cover plate 5 and second for staff illuminates, there is provided the visual field.
In sum, a kind of solar powered vertical lift unmanned plane 100 that the utility model embodiment is provided, its bag
Include organism frame 1, some solar battery sheets 2, fixed rotor 3 and regulation rotor 4.Due to being set in the upper surface of organism frame 1
Some solar battery sheets 2 are put, has been constantly inside by self-contained solar battery sheet 2 during unmanned plane during flying on daytime
It is powered and charges, during the non-flight of unmanned plane on daytime, is also constantly charged to unmanned machine battery in the sun, until battery
It is full of, so as to improve the endurance of unmanned plane 100.Additionally, when unmanned plane 100 takes off, being adjusted by by the regulation rotor 4
It is whole to the state parallel with fixed rotor 3, rotated by the high speed of fixed rotor 3 and regulation rotor 4 and produce lift to realize nothing
Man-machine 100 take off.When needing to advance after the rising of unmanned plane 100, by adjusting the regulation rotor 4 with the fixed phase of rotor 3
Vertically, then regulation rotor 4 produces larger thrust forward with air-flow, realizes the flight of unmanned plane 100.When unmanned plane 100 is needed
When turning to, by swinging for the direction regulating part 41 on the regulation rotor 4, change the tail wind of unmanned plane 100
Direction, realizes the steering of unmanned plane 100, by adjusting the adjustment effect of rotor 4 while realizing taking off, advance and turning for unmanned plane
To, improve unmanned plane operation convenience.Infrared thermovision camera on unmanned plane 100 and take photo by plane camera 9 can be to light
The component of overhead utility carries out infrared detection, and when there is problem component, then the regional temperature is raised, and unmanned plane 100 is by image
Surface personnel is back to, staff can control unmanned plane 100 to drop to problem component top, be filled by the mark
Put 10 and spray colored liquid to problem component, problem component is marked, facilitate maintainer to position maintenance, when saving work
Between.
Preferred embodiment of the present utility model is the foregoing is only, is not used to limit the utility model, it is all at this
Any modification, equivalent and improvement made within the spirit and principle of utility model etc., should be included in the utility model
Protection domain within.
Claims (11)
1. a kind of solar powered vertical lift unmanned plane, including organism frame and fixed rotor, the fixed rotor are arranged on
One end of the organism frame, and parallel to the organism frame, it is characterised in that the unmanned plane also includes some solar energy
Cell piece and regulation rotor, some solar battery sheets are arranged on the upper surface of the organism frame, the regulation rotor
It is arranged on the other end of the organism frame, and rotationally cuts between the state of the organism frame is parallel and perpendicular to
Change, the regulation rotor is provided with for controlling what the regulation rotor swung when perpendicular to the organism frame state
Swaying direction regulating part.
2. solar powered vertical lift unmanned plane as claimed in claim 1, it is characterised in that the front end of the organism frame
Offer at least one through hole, the rear end of the organism frame offers at least one through hole, the organism frame front end it is logical
Center line of the through hole of hole and the organism frame rear end on the organism frame is symmetrical arranged, and the fixed rotor is housed
In the through hole of the organism frame front end, the regulation rotor is rotationally contained in the through hole of the organism frame rear end
It is interior.
3. solar powered vertical lift unmanned plane as claimed in claim 2, it is characterised in that the front end of the organism frame
Two through holes are offered, the rear end of the organism frame offers a through hole, and the through hole of the organism frame rear end is located at institute
State on the center line of through hole line of organism frame front end two, the fixed rotor includes the first rotor and the second rotor, described
First rotor and the second rotor are respectively contained in the through hole of the organism frame front end, and the regulation rotor is rotationally housed
In the through hole of the organism frame rear end.
4. solar powered vertical lift unmanned plane as claimed in claim 3, it is characterised in that the unmanned plane also includes the
One cover plate and the second cover plate, first cover plate and the second cover plate are installed in rotation on first rotor and the second rotation respectively
The side of the wing and symmetrically, first cover plate and the second cover plate respectively with it is logical where first rotor and the second rotor
Hole is interlocked or along the side expansion of respective rotor.
5. solar powered vertical lift unmanned plane as claimed in claim 4, it is characterised in that first cover plate and second
The one side that fixed rotor is closed on after being interlocked with respective through hole on cover plate is provided with some solar battery sheets, and its another side is provided with
Navigation lights.
6. solar powered vertical lift unmanned plane as claimed in claim 1, it is characterised in that installed on the organism frame
There is the first motor, first motor is connected with the regulation rotor by gear drive, and first motor drives the tune
Section rotor rotates relative to the organism frame horizontal/vertical.
7. solar powered vertical lift unmanned plane as claimed in claim 6, it is characterised in that the regulation rotor includes adjusting
Section seat, rotor motor and rotating vane, the adjustment seat are connected with first motor by gear drive, and described first
It is installed in rotation under the drive of motor on institute's organism frame, the rotor motor is fixed in the adjustment seat, the rotation
Rotating vane piece is arranged in the rotor motor.
8. solar powered vertical lift unmanned plane according to claim 1, it is characterised in that the swaying direction regulation
Part includes regulating part and the second motor, and the regulating part is arranged on the regulation rotor, and second motor is fixed on described
Adjust in the outer rim of rotor and be connected with the regulating part, second motor drives the regulating part to swing.
9. solar powered vertical lift unmanned plane as claimed in claim 8, it is characterised in that the rear end of the organism frame
Through hole is offered, the regulation rotor is rotationally contained in the through hole, is offered for placing on the through-hole wall
The groove of second motor, the regulation rotor is under parastate with the organism frame, and second motor is corresponding
Be fastened in the groove.
10. as in one of claimed in any of claims 1 to 9 solar powered vertical lift unmanned plane, it is characterised in that it is described
Unmanned plane also includes infrared thermovision camera and camera of taking photo by plane, and the infrared thermovision camera and camera of taking photo by plane are installed in institute
The lower surface of organism frame is stated, and near the front end of the organism frame.
11. solar powered vertical lift unmanned planes as in one of claimed in any of claims 1 to 9, it is characterised in that described
Unmanned plane also includes the labelling apparatus for being marked to fault zone, and colored liquid is loaded with the labelling apparatus.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621263018.1U CN206218218U (en) | 2016-11-21 | 2016-11-21 | A kind of solar powered vertical lift unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621263018.1U CN206218218U (en) | 2016-11-21 | 2016-11-21 | A kind of solar powered vertical lift unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206218218U true CN206218218U (en) | 2017-06-06 |
Family
ID=58790721
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621263018.1U Expired - Fee Related CN206218218U (en) | 2016-11-21 | 2016-11-21 | A kind of solar powered vertical lift unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206218218U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106628138A (en) * | 2016-11-21 | 2017-05-10 | 深圳市米思米自动化设备有限公司 | Solar-powered vertical lift unmanned aerial vehicle |
| CN107826244A (en) * | 2017-11-15 | 2018-03-23 | 安徽工程大学 | A kind of six shaft rotating devices of aircraft |
| CN109334947A (en) * | 2018-11-06 | 2019-02-15 | 西北农林科技大学 | A kind of helium balloon unmanned plane and its working method |
-
2016
- 2016-11-21 CN CN201621263018.1U patent/CN206218218U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106628138A (en) * | 2016-11-21 | 2017-05-10 | 深圳市米思米自动化设备有限公司 | Solar-powered vertical lift unmanned aerial vehicle |
| CN106628138B (en) * | 2016-11-21 | 2024-01-23 | 深圳市特研创新科技有限公司 | Solar power supply vertical lifting unmanned aerial vehicle |
| CN107826244A (en) * | 2017-11-15 | 2018-03-23 | 安徽工程大学 | A kind of six shaft rotating devices of aircraft |
| CN107826244B (en) * | 2017-11-15 | 2021-03-09 | 安徽工程大学 | Six rotary device of aircraft |
| CN109334947A (en) * | 2018-11-06 | 2019-02-15 | 西北农林科技大学 | A kind of helium balloon unmanned plane and its working method |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170606 Termination date: 20211121 |
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| CF01 | Termination of patent right due to non-payment of annual fee |