CN208947605U - Cooperate satellite navigation long continuation of the journey unmanned plane and mating long-range photovoltaic laser battery charger cradle - Google Patents
Cooperate satellite navigation long continuation of the journey unmanned plane and mating long-range photovoltaic laser battery charger cradle Download PDFInfo
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- CN208947605U CN208947605U CN201821680721.1U CN201821680721U CN208947605U CN 208947605 U CN208947605 U CN 208947605U CN 201821680721 U CN201821680721 U CN 201821680721U CN 208947605 U CN208947605 U CN 208947605U
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- unmanned plane
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- 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
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/70—Energy storage systems for electromobility, e.g. batteries
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- 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
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/7072—Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
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- 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
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/10—Technologies relating to charging of electric vehicles
- Y02T90/14—Plug-in electric vehicles
Abstract
Cooperate satellite navigation with long continuation of the journey unmanned plane, mainboard chip has GPS navigation chip in unmanned plane main body, respectively there is a support rod at four angles of the unmanned plane main body, there is propeller motor in the end of support rod, the shaft of propeller motor is equipped with propeller, there is signal projector above the middle part of unmanned plane main body, there is hydrogen gas storage device above unmanned plane main body, a solenoid valve is provided with above each hydrogen gas storage device, the gas nozzle of solenoid valve is connected with corresponding hydrogen balloon, unmanned plane bottom part body has control panel and battery, two middle side part of focalization plate is mounted on unmanned plane bottom part body by focalization plate grip block.The utility model continuation of the journey uav bottom is provided with adjustable angle focalization plate and can carry out filling energy by remote laser, to guarantee to continue a journey, aerating ballon is provided at the top of unmanned plane, after unmanned plane rises to corresponding height, use of the buoyancy reduction to rotor is provided using balloon, the corresponding long-range photovoltaic laser battery charger cradle of ground configuration setting, charges for unmanned plane.
Description
Technical field
The utility model relates to satellite remote sensing field, more particularly to the long continuation of the journey unmanned plane of cooperation satellite navigation and mating
Long-range photovoltaic laser battery charger cradle.
Background technique
It is influenced to will affect the transmission of navigation signal, and often situation by factors such as cloud covers during satellite navigation
It is changeable, in order to cope with problem above, corresponding ancillary equipment is often required to use, wherein since unmanned plane there are the spies such as flexibility ratio height
Property, therefore be adapted as navigation intermediary and use, it is provided to fixed area and reinforces signal or flight as needed to correspondence
Region carries out increase signal, but uses Navigation of Pilotless Aircraft there are the following problems, continuation of the journey is required as navigation intermediary it is high, and
Traditional unmanned plane is limited due to being limited cruise duration by overall structure, not can guarantee and continues a journey for a long time, more than solving
It is contemplated that remotely charged using superlaser charging modes, thus guarantee cruise duration as far as possible, in addition to this due to
Navigational state is to be in stratosphere, therefore wind-force is limited on unmanned plane influence, if still guaranteeing to suspend using larger power rotor,
It will cause very big waste of energy, it can be considered to be substituted by other suspending powers, the high speed rotation of reduction rotor in this way
Turn to reduce waste of energy, then the mating ground laser battery charger cradle according to unmanned aerial vehicle design, so as to guarantee unmanned plane as far as possible
Continuation of the journey, energy supplement can also be carried out by photovoltaic power generation plate by supplementing electricity condition battery charger cradle usually, and the application designs one kind thus
Cooperate satellite navigation long continuation of the journey unmanned plane and mating long-range photovoltaic laser battery charger cradle, to solve problem above.
Utility model content
In order to solve problem above, the utility model provides cooperation satellite navigation long continuation of the journey unmanned plane and mating long-range light
Laser battery charger cradle is lied prostrate, which is provided with adjustable angle focalization plate and can carry out filling energy by remote laser, from
And guarantee continuation of the journey, it is provided with aerating ballon at the top of unmanned plane, after unmanned plane rises to corresponding height, is provided using balloon floating
Power reduces the use to rotor, and configuration setting corresponding long-range photovoltaic laser battery charger cradle in ground charges for unmanned plane, so as to
To greatly improve the cruise duration of unmanned plane, guarantee its stability as navigation intermediary, for this purpose, the utility model mentions
For a kind of long continuation of the journey unmanned plane of cooperation satellite navigation, including hydrogen balloon, solenoid valve, hydrogen gas storage device, propeller, support
Bar, unmanned plane main body, signal projector, control panel, battery, focalization plate, focalization plate grip block and focalization plate adjust motor, institute
Stating mainboard chip in unmanned plane main body has GPS navigation chip, and respectively there is a support rod at four angles of the unmanned plane main body, described
There is a propeller motor in the end of support rod, and the shaft of the propeller motor is equipped with propeller, in the unmanned plane main body
There is signal projector above portion, there is the hydrogen gas storage device being arranged in pairs, each hydrogen storage above the unmanned plane main body
It is provided with a solenoid valve above device, the gas nozzle of the solenoid valve is connected with corresponding hydrogen balloon, the unmanned plane bottom part body
There are control panel and battery, is charging panel in the middle part of the focalization plate and respectively has a photo resistance, the focalization plate up and down
Two middle side parts are mounted on unmanned plane bottom part body by focalization plate grip block, and the shaft that the focalization plate adjusts motor passes through side
Focalization plate grip block be connected with focalization plate side, the battery connects each electrical equipment by connecting line.
The further improvement of the utility model unmanned plane, the hydrogen balloon have two pairs the left up and down of signal projector is arranged in
The right side, in order to guarantee that steady lift is preferably provided two pairs of hydrogen balloons.
The further improvement of the utility model unmanned plane, four angles of the unmanned plane bottom part body are respectively equipped with a remote sensing
Camera, the back seat of the remote sensing camera be mounted in camera grip block by shaft and on the outside of camera grip block
The shaft of motor two is connected, and the camera grip block is mounted in the shaft of motor one, and the pedestal of the motor one is mounted on
Below four angles of corresponding unmanned plane bottom part body, the remote sensing camera is infrared remote sensing camera, is provided with remote sensing camera shooting
It is the most frequently used to can be used for completing tasks, the mid infrared range remote sensing camera such as landform exploration and heat sensitivity processing for head.
The utility model provides a kind of mating long-range photovoltaic laser battery charger cradle of long continuation of the journey unmanned plane of cooperation satellite navigation,
Including support plate, solar panel, interior empty triangular support bracket, charging station battery, bottom plate, laser emitter, carriage motor
One, transmitter grip block and carriage motor two, there is laser emitter on the bottom plate, in the middle part of the transmitting terminal of the laser emitter
For the Laser emission mouth that charges, the charging Laser emission mouth of the transmitting terminal of the laser emitter respectively has an auxiliary up and down
Laser emission mouth, the laser emitter on both sides of the middle are mounted in transmitter grip block by shaft, the carriage motor one
In transmitter grip block side, the shaft of the carriage motor one passes through carriage motor one and laser emitter side shaft phase
Even, transmitter grip block bottom is mounted in the shaft of carriage motor two, and the pedestal of the carriage motor two is fixed on bottom
On plate, the floor rear has interior empty triangular support bracket, has support plate, the support on the inclined-plane of the interior empty triangular support bracket
It is equipped with solar panel in plate, is placed with charging station battery, the charging station electric power storage in the interior empty triangular support bracket
Pond connects each electrical equipment by connecting line.
The further improvement of the utility model charging station, the laser emitter have 1-4, can basis in practice
Charging station size designs corresponding transmitter.
The further improvement of the utility model charging station is additionally provided with airplane parking area frame, the airplane parking area frame on the bottom plate
There are 4 locating racks, there is cross alignment mark on the bottom plate in the airplane parking area frame, the airplane parking area frame there are 1-4, and design is shut down
Level ground can stop for unmanned plane and safeguard, generally according to charging station size and can need that respective number is arranged.
The utility model cooperates satellite navigation long continuation of the journey unmanned plane and mating long-range photovoltaic laser battery charger cradle, and advantage is such as
Under；
1, there is GPS navigation chip in the utility model unmanned plane main body, used to cooperate as navigation unmanned plane, in nothing
It is provided with aerating ballon in man-machine main body, after unmanned plane rises to corresponding height, buoyancy is kept using balloon, thus indirectly
The use for reducing rotor motor improves whole cruising ability；
2, the utility model bottom is provided with adjustable focalization plate, and contraposition can be carried out with laser and carries out contraposition adjustment, from
And convenient long-range charging；
3, the utility model bottom is provided with remote sensing camera, can be used for completing landform exploration and heat sensitivity processing etc.
Task；
4, the utility model Aided design has corresponding long-range photovoltaic laser battery charger cradle, which is provided with rotary laser
Charger, unmanned plane can charge automatically after flying to specified region；
5, the utility model charging station is provided with landing gear, and unmanned plane can also drop to be safeguarded above；
6, the also mating solar panel of the utility model charging station, normal condition can carry out electric energy by photovoltaic power generation
Supplement.
Detailed description of the invention
Fig. 1 is the utility model unmanned plane and mating battery charger cradle schematic diagram one；
Fig. 2 is the utility model unmanned plane and mating battery charger cradle schematic diagram two；
Fig. 3 is the utility model battery charger cradle laser charger schematic diagram；
Fig. 4 is the utility model unmanned plane overall schematic；
Fig. 5 is the utility model unmanned plane partial schematic diagram；
Wherein, 1, support plate；2, airplane parking area frame；3, cross alignment mark；4, solar panel；5, interior empty gusseted
Frame；6, charging station battery；7, bottom plate；8, auxiliary laser emission port；9, charge Laser emission mouth；10, laser emitter；11,
Carriage motor one；12, transmitter grip block；13, carriage motor two；14, hydrogen balloon；15, solenoid valve；16, hydrogen gas storage device；
17, propeller；18, propeller motor；19, support rod；20, unmanned plane main body；21, signal projector；22, control panel 23, electricity
Pond；24, motor one；25, camera grip block；26, motor two；27, remote sensing camera；28, focalization plate；29, focalization plate clamps
Plate；30, focalization plate adjusts motor.
Specific embodiment
The utility model is described in further detail with specific embodiment with reference to the accompanying drawing:
The utility model provides cooperation satellite navigation long continuation of the journey unmanned plane and mating long-range photovoltaic laser battery charger cradle, this is continuous
Endurance unmanned plane bottom, which is provided with adjustable angle, which fills energy solar panel, can carry out filling energy by remote laser, thus guarantee to continue a journey, nothing
Man-machine top is provided with aerating ballon, after unmanned plane rises to corresponding height, provides buoyancy using balloon and reduces to rotor
Use, configuration setting corresponding long-range photovoltaic laser battery charger cradle in ground charges for unmanned plane, so as to greatly improve nothing
Guarantee its stability as navigation intermediary man-machine cruise duration.
As a kind of embodiment of the utility model unmanned plane, the utility model provides a kind of long continuation of the journey of cooperation satellite navigation
Unmanned plane, including hydrogen balloon 14, solenoid valve 15, hydrogen gas storage device 16, propeller motor 17, propeller 18, support rod 19, nothing
Man-machine main body 20, signal projector 21, control panel 22, battery 23, focalization plate 28, focalization plate grip block 29 and focalization plate are adjusted
Motor 30, mainboard chip has GPS navigation chip in the unmanned plane main body 20, and four angles of the unmanned plane main body 20 respectively have one
There are propeller motor 17 in a support rod 19, the end of the support rod 19, and the shaft of the propeller motor 17 is equipped with spiral
There is signal projector 21 in the middle part top of paddle 18, the unmanned plane main body 20, and the top of the unmanned plane main body 20 has to be set in pairs
The hydrogen gas storage device 16 set is provided with a solenoid valve 15 above each hydrogen gas storage device 16, the solenoid valve 15
Gas nozzle is connected with corresponding hydrogen balloon 14, and control panel 22 and battery 23 arranged at 20 bottom of unmanned plane main body, in the focalization plate 28
Portion is charging panel and respectively has a photo resistance up and down, and 28 liang of middle side parts of the focalization plate are pacified by focalization plate grip block 29
Mounted in 20 bottom of unmanned plane main body, the shaft that the focalization plate adjusts motor 30 passes through the focalization plate grip block 29 of side and to light
28 side of plate is connected, and the battery 23 connects each electrical equipment by connecting line.
As a kind of specific embodiment of the utility model unmanned plane, the utility model provides one kind as shown in Figures 4 and 5 and matches
Close satellite navigation long continuation of the journey unmanned plane, including hydrogen balloon 14, solenoid valve 15, hydrogen gas storage device 16, propeller motor 17, spiral shell
Revolve paddle 18, support rod 19, unmanned plane main body 20, signal projector 21, control panel 22, battery 23, focalization plate 28, focalization plate folder
It holds plate 29 and focalization plate adjusts motor 30, mainboard chip has GPS navigation chip, the unmanned owner in the unmanned plane main body 20
Respectively there is a support rod 19 at four angles of body 20, and there are propeller motor 17, the propeller motor in the end of the support rod 19
17 shaft is equipped with propeller 18, has signal projector 21, the unmanned owner above the middle part of the unmanned plane main body 20
There is the hydrogen gas storage device 16 being arranged in pairs in the top of body 20, and a solenoid valve is provided with above each hydrogen gas storage device 16
15, the gas nozzle of the solenoid valve 15 is connected with corresponding hydrogen balloon 14, and the hydrogen balloon 14 has two pairs signal projector 21 is arranged in
Up and down, in order to guarantee that steady lift is preferably provided two pairs of hydrogen balloons, 22 He of control panel is arranged at 20 bottom of unmanned plane main body
Battery 23 has for charging panel and respectively a photo resistance, 28 two sides of focalization plate in the middle part of the focalization plate 28 up and down
Middle part is mounted on 20 bottom of unmanned plane main body by focalization plate grip block 29, and the shaft that the focalization plate adjusts motor 30 passes through one
The focalization plate grip block 29 of side is connected with 28 side of focalization plate, and the battery 23 connects each electrical equipment by connecting line, described
The back seat that unmanned plane main body 20 bottom four angle is respectively equipped with remote sensing camera 27 described in a remote sensing camera 27 passes through shaft
It is mounted in camera grip block 25 and is connected with the shaft of the motor 2 26 in 25 outside of camera grip block, the camera clamp
It holds plate 25 to be mounted in the shaft of motor 1, the pedestal of the motor 1 is mounted on the four of corresponding 20 bottom of unmanned plane main body
Below a angle, the remote sensing camera, 27 be infrared remote sensing camera, is provided with remote sensing camera, can be used for completing landform
The tasks such as exploration and heat sensitivity processing, mid infrared range remote sensing camera is the most frequently used,
As a kind of embodiment of the utility model charging station, the utility model provides a kind of long continuation of the journey of cooperation satellite navigation
The mating long-range photovoltaic laser battery charger cradle of unmanned plane, including support plate 1, solar panel 4, interior empty triangular support bracket 5, charging
It stands battery 6, bottom plate 7, laser emitter 10, carriage motor 1, transmitter grip block 12 and carriage motor 2 13, the bottom
There is laser emitter 10 on plate 7, is charging Laser emission mouth 9 in the middle part of the transmitting terminal of the laser emitter 10, the laser hair
The charging Laser emission mouth 9 of the transmitting terminal of emitter 10 respectively has an auxiliary laser emission port 8, the Laser emission up and down
10 on both sides of the middle of device is mounted in transmitter grip block 12 by shaft, and the carriage motor 1 is in transmitter grip block 12 1
Side, the shaft of the carriage motor 1 pass through carriage motor 1 and are connected with 10 side shaft of laser emitter, the transmitting
12 bottom of device grip block is mounted in the shaft of carriage motor 2 13, and the pedestal of the carriage motor 2 13 is fixed on bottom plate 7,
There is interior empty triangular support bracket 5 on rear side of the bottom plate 7, has support plate 1, the support on the inclined-plane of the interior empty triangular support bracket 5
It is equipped with solar panel 4 in plate 1, is placed with charging station battery 6, the charging station in the interior empty triangular support bracket 5
Battery 6 connects each electrical equipment by connecting line.
As a kind of specific embodiment of the utility model charging station, the utility model provides one kind as shown in Figs. 1-3 and matches
Close the satellite navigation mating long-range photovoltaic laser battery charger cradle of long continuation of the journey unmanned plane, including support plate 1, solar panel 4, interior
Empty triangular support bracket 5, charging station battery 6, bottom plate 7, laser emitter 10, carriage motor 1,12 and of transmitter grip block
Carriage motor 2 13 has laser emitter 10 on the bottom plate 7, and the laser emitter 10 has 1-4, can be in practice
Corresponding transmitter is designed according to charging station size, is charging Laser emission mouth 9 in the middle part of the transmitting terminal of the laser emitter 10,
The charging Laser emission mouth 9 of the transmitting terminal of the laser emitter 10 respectively has an auxiliary laser emission port 8, institute up and down
It states 10 on both sides of the middle of laser emitter to be mounted in transmitter grip block 12 by shaft, the carriage motor 1 is in transmitter
The shaft of 12 side of grip block, the carriage motor 1 passes through carriage motor 1 and 10 side shaft phase of laser emitter
Even, 12 bottom of transmitter grip block is mounted in the shaft of carriage motor 2 13, and the pedestal of the carriage motor 2 13 is solid
It is scheduled on bottom plate 7, has interior empty triangular support bracket 5 on rear side of the bottom plate 7, have support on the inclined-plane of the interior empty triangular support bracket 5
Plate 1 is equipped with solar panel 4 in the support plate 1, is placed with charging station battery in the interior empty triangular support bracket 5
6, the charging station battery 6 connects each electrical equipment by connecting line, and airplane parking area frame 2 is additionally provided on the bottom plate 7, described to stop
Machine level ground frame 2 has 4 locating racks, has cross alignment mark 3 on the bottom plate 7 in the airplane parking area frame 2, the airplane parking area frame 3 has 1-4
A, design airplane parking area can be stopped for unmanned plane and be safeguarded, generally according to charging station size and can need that respective number is arranged.
Utility model works process is as follows: solar panel power supply has battery electric power storage.Unmanned plane during flying electricity is not
When sufficient, unmanned plane emits positioning signal and gives charging base station, and focalization plate adjusts motor work to adjust focalization plate, carriage motor one,
So that laser emitter is to firmly focalization plate, auxiliary laser first emits for two work, is divided into four areas on focalization plate other than charged area
Domain has photo resistance in region, and only when auxiliary laser is experienced in four regions simultaneously, charging Laser emission is filled for unmanned plane
Electricity.
The above descriptions are merely preferred embodiments of the present invention, is not to make any other to the utility model
The limitation of form, and according to any modification or equivalent variations made by the technical essence of the utility model, it is practical new to still fall within this
Type range claimed.
Claims (8)
1. cooperate the long continuation of the journey unmanned plane of satellite navigation, including hydrogen balloon (14), solenoid valve (15), hydrogen gas storage device (16),
Propeller motor (17), propeller (18), support rod (19), unmanned plane main body (20), signal projector (21), control panel
(22), battery (23), focalization plate (28), focalization plate grip block (29) and focalization plate adjust motor (30), the unmanned owner
Body (20) interior mainboard chip has GPS navigation chip, which is characterized in that respectively there is a branch at four angles of the unmanned plane main body (20)
The end of strut (19), the support rod (19) has propeller motor (17), and the shaft of the propeller motor (17) is equipped with
The middle part top of propeller (18), the unmanned plane main body (20) has signal projector (21), the unmanned plane main body (20)
There is the hydrogen gas storage device (16) being arranged in pairs in top, and is provided with a solenoid valve above each hydrogen gas storage device (16)
(15), the gas nozzle of the solenoid valve (15) is connected with corresponding hydrogen balloon (14), and control panel is arranged at unmanned plane main body (20) bottom
(22) and battery (23) it is, charging panel in the middle part of the focalization plate (28) and respectively has a photo resistance up and down, it is described right
(28) two middle side part of tabula rasa is mounted on unmanned plane main body (20) bottom by focalization plate grip block (29), and the focalization plate adjusts electricity
The focalization plate grip block (29) that the shaft of machine (30) passes through side is connected with focalization plate (28) side, and the battery (23) passes through
Connecting line connects each electrical equipment.
2. the long continuation of the journey unmanned plane of cooperation satellite navigation according to claim 1, it is characterised in that: the hydrogen balloon (14)
Have two pairs setting signal projector (21) up and down.
3. the long continuation of the journey unmanned plane of cooperation satellite navigation according to claim 1, it is characterised in that: the unmanned plane main body
(20) angle of bottom four is respectively equipped with a remote sensing camera (27), and the back seat of the remote sensing camera (27) is installed by shaft
It is connected in camera grip block (25) and with the shaft of the motor two (26) on the outside of camera grip block (25), the camera
Grip block (25) is mounted in the shaft of motor one (24), and the pedestal of the motor one (24) is mounted on corresponding unmanned plane main body
(20) below four angles of bottom.
4. the long continuation of the journey unmanned plane of cooperation satellite navigation according to claim 3, it is characterised in that: the remote sensing camera
It (27) is infrared remote sensing camera.
5. cooperating the mating long-range photovoltaic laser of long continuation of the journey unmanned plane of cooperation satellite navigation described in claim 1-4 any one
Battery charger cradle, including support plate (1), solar panel (4), interior empty triangular support bracket (5), charging station battery (6), bottom plate
(7), laser emitter (10), carriage motor one (11), transmitter grip block (12) and carriage motor two (13), feature exist
In: have laser emitter (10) on the bottom plate (7), is charging Laser emission in the middle part of the transmitting terminal of the laser emitter (10)
Mouth (9), the charging Laser emission mouth (9) of the transmitting terminal of the laser emitter (10) respectively have an auxiliary laser up and down
Emission port (8), laser emitter (10) on both sides of the middle are mounted in transmitter grip block (12) by shaft, the bracket
Motor one (11) in transmitter grip block (12) side, the shaft of the carriage motor one (11) pass through carriage motor one (11) with
Laser emitter (10) side shaft is connected, and transmitter grip block (12) bottom is mounted on the shaft of carriage motor two (13)
On, the pedestal of the carriage motor two (13) is fixed on bottom plate (7), there is interior empty triangular support bracket on rear side of the bottom plate (7)
(5), have support plate (1) on the inclined-plane of the interior empty triangular support bracket (5), be equipped with solar battery in the support plate (1)
Plate (4), the interior empty triangular support bracket (5) is interior to be placed with charging station battery (6), and the charging station battery (6) passes through company
Wiring connects each electrical equipment.
6. the mating long-range photovoltaic laser battery charger cradle of the long continuation of the journey unmanned plane of cooperation satellite navigation according to claim 5,
Be characterized in that: the laser emitter (10) has 1-4.
7. the mating long-range photovoltaic laser battery charger cradle of the long continuation of the journey unmanned plane of cooperation satellite navigation according to claim 5,
It is characterized in that: being additionally provided with airplane parking area frame (2) on the bottom plate (7), the airplane parking area frame (2) has 4 locating racks, the shutdown
There is cross alignment mark (3) on bottom plate (7) in level ground frame (2).
8. the mating long-range photovoltaic laser battery charger cradle of the long continuation of the journey unmanned plane of cooperation satellite navigation according to claim 7,
Be characterized in that: the airplane parking area frame (2) has 1-4.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821680721.1U CN208947605U (en) | 2018-10-17 | 2018-10-17 | Cooperate satellite navigation long continuation of the journey unmanned plane and mating long-range photovoltaic laser battery charger cradle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821680721.1U CN208947605U (en) | 2018-10-17 | 2018-10-17 | Cooperate satellite navigation long continuation of the journey unmanned plane and mating long-range photovoltaic laser battery charger cradle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208947605U true CN208947605U (en) | 2019-06-07 |
Family
ID=66741732
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821680721.1U Active CN208947605U (en) | 2018-10-17 | 2018-10-17 | Cooperate satellite navigation long continuation of the journey unmanned plane and mating long-range photovoltaic laser battery charger cradle |
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| Country | Link |
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| CN (1) | CN208947605U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115300828A (en) * | 2022-07-11 | 2022-11-08 | 天立泰科技股份有限公司 | Forest fire rescue extinguishing device |
-
2018
- 2018-10-17 CN CN201821680721.1U patent/CN208947605U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115300828A (en) * | 2022-07-11 | 2022-11-08 | 天立泰科技股份有限公司 | Forest fire rescue extinguishing device |
| CN115300828B (en) * | 2022-07-11 | 2023-04-07 | 天立泰科技股份有限公司 | Forest fire rescue extinguishing device |
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