CN108279705A - Photovoltaic unmanned plane - Google Patents
Photovoltaic unmanned plane Download PDFInfo
- Publication number
- CN108279705A CN108279705A CN201810071358.1A CN201810071358A CN108279705A CN 108279705 A CN108279705 A CN 108279705A CN 201810071358 A CN201810071358 A CN 201810071358A CN 108279705 A CN108279705 A CN 108279705A
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- CN
- China
- Prior art keywords
- photovoltaic
- gondola
- unmanned plane
- connector
- drone body
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- 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.)
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D3/00—Control of position or direction
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Photovoltaic Devices (AREA)
Abstract
The present invention relates to a kind of photovoltaic unmanned planes, including drone body and ground controller, photovoltaic gondola is lifted with below the drone body, thermal imaging camera is installed in the photovoltaic gondola, locating module, wireless communication module, memory module and power-supply system, the photovoltaic gondola includes outline border, the top of the outline border has upwardly extended connector, it is extended with shaft on the downside of the ontology of the unmanned plane, the lower end of the shaft is equipped with clamp, the clamp coordinates with the connector, micromotor is installed in the drone body, shaft described in the minitype motor driving rotates.After drone body damage in the present invention, a new drone body is only needed to change, the photovoltaic gondola part so as to ensure intact can continue to use；Similarly, after damage occurs in photovoltaic gondola part, unmanned plane one's duty can be retained, new photovoltaic gondola is only needed to change, so as to ensure the service efficiency of entire photovoltaic unmanned plane.
Description
Technical field
The present invention relates to a kind of photovoltaic unmanned planes, belong to photovoltaic plant maintenance technology field.
Background technology
Photovoltaic plant is generally built up in that region is open, sun-drenched remote area, substantially unattended, it is difficult to which that it is fixed to accomplish
Phase makes an inspection tour.Over the past two years, unmanned plane was gradually applied in photovoltaic project, can be monitored to photovoltaic plant.
Equipment and unmanned plane are integrated together by its design of existing photovoltaic unmanned plane, can not be split, thus
Damaging occurs in unmanned plane and other equipment does not have under the premise of damaging, and can only be repaired to complete machine, to influence entire photovoltaic
The service efficiency of unmanned plane.
Invention content
It is of the existing technology in order to solve the problems, such as, the present invention provides a kind of photovoltaic unmanned plane, in drone body or
After there is damage in equipment in photovoltaic gondola, replaceable new drone body or photovoltaic gondola, to ensure the portion for damage
Divide and be continuing with, improves the service efficiency of entire photovoltaic unmanned plane.
The technical solution adopted in the present invention is：
A kind of photovoltaic unmanned plane, including drone body and ground controller are lifted with photovoltaic below the drone body
Gondola is equipped with thermal imaging camera, locating module, wireless communication module, memory module and power-supply system in the photovoltaic gondola,
Power-supply system is thermal imaging camera, locating module, wireless communication module and memory module power supply；
Thermal imaging camera and locating module are connected by wireless communication module and ground controller communication；
Memory module is recording the data of thermal imaging camera and locating module；
The photovoltaic gondola includes outline border, and the top of the outline border has upwardly extended connector, under the ontology of the unmanned plane
Side is extended with shaft, and the lower end of the shaft is equipped with clamp, and the clamp coordinates with the connector, in the drone body
Micromotor is installed, shaft rotates described in the minitype motor driving.
Preferably, the cross section of the connector is rectangle, and locking is equipped at least one side of the connector
Head offers lock hole corresponding with the elongated insertion part on the corresponding side wall of the clamp.
Preferably, mounting hole is offered on the side of the connector, and spring, the mounting hole are equipped in the mounting hole
Horizontally disposed, the mounting hole is provided with snap ring, the outer diameter of the snap ring and the mounting hole in the side-walls of the connector
Internal diameter match, the elongated insertion part includes disk and tapered end, and the diameter of the disk is matched with the internal diameter of the mounting hole,
The outer diameter of the tapered end is matched with the internal diameter of the snap ring, and the axis of the disk is with the axis of the tapered end same
On straight line, one end of the tapered end is plane, and one end of the tapered end is fixedly connected with the side of the disk.
Further, the elongated insertion part can be installed on 2 sides of the connector, and is equipped with the two of elongated insertion part
A side is oppositely arranged.
Preferably, encoder is carried on the micromotor, and calibration zero-bit is equipped in the encoder.
In general, being also equipped with EL scanning detectors in the photovoltaic gondola.
Beneficial effects of the present invention：
Photovoltaic gondola and drone body in the present invention are split settings, after drone body damage, only need to change one
New drone body, the photovoltaic gondola part so as to ensure intact can continue to use；Similarly, in photovoltaic gondola
After damage occurs in part, unmanned plane one's duty can be retained, new photovoltaic gondola is only needed to change, so as to ensure entire photovoltaic
The service efficiency of unmanned plane.
The setting of clamp and adapter realizes the function of being connect soon with Quick Release between photovoltaic gondola and drone body,
It is convenient that the photovoltaic gondola part of damage or drone body are replaced.
The setting of micromotor and encoder can accurately control the rotational angle of micromotor, accurate to realize
The rotational angle of photovoltaic gondola is controlled, thus when the thermal imaging camera in photovoltaic gondola can not be rotated, using miniature
It controls motor and controls entire photovoltaic gondola rotation.
Description of the drawings
Fig. 1 is the structural schematic diagram of the present invention；
Fig. 2 is the sectional view that connector and clamp are in discrete state；
Fig. 3 is the enlarged drawing of part A in Fig. 2；
Fig. 4 is the enlarged drawing of part B in Fig. 2.
Wherein：1, drone body；2, photovoltaic gondola；3, shaft；4, connector；31, clamp；32, lock hole；42, bullet
Spring；43, disk；44, tapered end.
Specific implementation mode
Referring to Fig. 1-Fig. 4, the present invention provides a kind of photovoltaic unmanned plane, including drone body 1 and ground controller, nothings
The lower section of man-machine ontology 1 is lifted with photovoltaic gondola 2, is split settings between photovoltaic gondola 2 and drone body 1, referred to herein
Split settings to refer to photovoltaic gondola 2 can freely be mounted and dismounted with respect to drone body 1.
Specifically, the photovoltaic gondola 2 includes outline border, the top of the outline border has upwardly extended connector 4, the nothing
Shaft 3 is extended on the downside of man-machine ontology, the lower end of the shaft 3 is equipped with clamp 31, the clamp 31 and the connector 4
Coordinate, micromotor is installed in the drone body 1, shaft 3 rotates described in the minitype motor driving.
Photovoltaic gondola 2 is connect soon by the realization of clamp 31 of connector 4 and 1 downside of drone body above it and Quick Release；
In addition, being also equipped with micromotor in drone body 1, micromotor can drive shaft 3 to rotate, thus in photovoltaic gondola 2
It, can be by miniature if the equipment in photovoltaic gondola 2 can not carry out rotation shooting when mounted on the downside of drone body 1
Motor drives shaft 3 to rotate, and to drive photovoltaic gondola 2 to rotate, ensures the normal operation of photovoltaic gondola 2.
The cross section of the connector 4 is rectangle, is equipped with elongated insertion part at least one side of the connector 4, institute
It states and offers lock hole corresponding with the elongated insertion part 32 on the corresponding side wall of clamp 31.
The setting of elongated insertion part and lock hole 32 directly will even when photovoltaic gondola 2 is mounted on the downside of drone body 1
Connector 4 is inserted into clamp 31, and elongated insertion part pop-up snaps onto in lock hole 32, to realize photovoltaic gondola 2 and unmanned plane sheet
It is relatively fixed connection between body 1.
Mounting hole is offered on the side of the connector 4, and spring 42, the installation hole horizontal are equipped in the mounting hole
Setting, the mounting hole are provided with snap ring in the side-walls of the connector 4, and the outer diameter of the snap ring is interior with the mounting hole
Diameter matches, and the elongated insertion part includes disk 43 and tapered end 44, and the diameter of the disk 43 and the internal diameter of the mounting hole match
It closes, the outer diameter of the tapered end 44 is matched with the internal diameter of the snap ring, axis and the tapered end 44 of the disk 43
Axis is on same straight line, and one end of the tapered end 44 is plane, and one end of the tapered end 44 and the side of the disk 43 are solid
Fixed connection.
Briefly, be exactly elongated insertion part by spring 42 under the action of, reach except mounting hole always, when elongated insertion part with lock
When determining the cooperation of hole 32, realizes drone body 1 and directly connect with photovoltaic gondola 2, and drone body 1 and light will be separated by working as
When lying prostrate gondola 2, elongated insertion part only need to be pressed, elongated insertion part is reduced in mounting hole, then pulls up connector 4, can realize drone body 1
With the separation of photovoltaic gondola 2.
The elongated insertion part is installed on 2 sides of the connector 4, and two sides for being equipped with elongated insertion part are set relatively
It sets.Encoder is carried on the micromotor, and calibration zero-bit is equipped in the encoder.
The setting of 2 elongated insertion parts opposite can ensure the stability after photovoltaic gondola 2 is installed with drone body 1.
Encoder can realize the amplitude of accurate 2 rotation of adjustment photovoltaic gondola.
Thermal imaging camera, locating module, wireless communication module, memory module, power supply system are installed in the photovoltaic gondola 2
System and EL scanning detectors.
Power-supply system is thermal imaging camera, locating module, wireless communication module and memory module power supply；
Thermal imaging camera and locating module are connected by wireless communication module and ground controller communication；
Memory module is recording the data of thermal imaging camera and locating module；
EL scanning detectors can carry out EL scannings to photovoltaic.
Claims (6)
1. a kind of photovoltaic unmanned plane, including drone body and ground controller, light is lifted with below the drone body
Gondola is lied prostrate, thermal imaging camera, locating module, wireless communication module, memory module and power supply system are installed in the photovoltaic gondola
System,
Power-supply system is thermal imaging camera, locating module, wireless communication module and memory module power supply；
Thermal imaging camera and locating module are connected by wireless communication module and ground controller communication；
Memory module is recording the data of thermal imaging camera and locating module；
It is characterized in that：The photovoltaic gondola includes outline border, and the top of the outline border has upwardly extended connector, the unmanned plane
Ontology on the downside of be extended with shaft, the lower end of the shaft is equipped with clamp, and the clamp coordinates with the connector, the nothing
Micromotor is installed, shaft rotates described in the minitype motor driving in man-machine ontology.
2. photovoltaic unmanned plane according to claim 1, it is characterised in that：The cross section of the connector is rectangle, described
Elongated insertion part is installed at least one side of connector, is offered on the corresponding side wall of the clamp and the elongated insertion part phase
Corresponding lock hole.
3. photovoltaic unmanned plane according to claim 2, it is characterised in that：Installation is offered on the side of the connector
Hole, the mounting hole is interior to be equipped with spring, and the mounting hole is horizontally disposed, and the mounting hole is arranged in the side-walls of the connector
There are snap ring, the outer diameter of the snap ring to be matched with the internal diameter of the mounting hole, the elongated insertion part includes disk and tapered end, the circle
The diameter of piece is matched with the internal diameter of the mounting hole, and the outer diameter of the tapered end is matched with the internal diameter of the snap ring, the institute
The axis of disk and the axis of the tapered end are stated on same straight line, one end of the tapered end is plane, one end of the tapered end
It is fixedly connected with the side of the disk.
4. photovoltaic unmanned plane according to claim 3, it is characterised in that：It is installed on 2 sides of the connector
Elongated insertion part is stated, and two sides for being equipped with elongated insertion part are oppositely arranged.
5. photovoltaic unmanned plane according to claim 1, it is characterised in that：Encoder is carried on the micromotor, it is described
Calibration zero-bit is equipped in encoder.
6. photovoltaic unmanned plane according to claim 1, it is characterised in that：EL scanning inspections are also equipped in the photovoltaic gondola
Survey instrument.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810071358.1A CN108279705A (en) | 2018-01-25 | 2018-01-25 | Photovoltaic unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810071358.1A CN108279705A (en) | 2018-01-25 | 2018-01-25 | Photovoltaic unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108279705A true CN108279705A (en) | 2018-07-13 |
Family
ID=62804967
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810071358.1A Pending CN108279705A (en) | 2018-01-25 | 2018-01-25 | Photovoltaic unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108279705A (en) |
Citations (9)
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|---|---|---|---|---|
| WO2010010420A1 (en) * | 2007-12-26 | 2010-01-28 | Tactical Systems Inc. | Suspended video imaging system |
| KR101050425B1 (en) * | 2010-02-25 | 2011-07-19 | 국방과학연구소 | Video pod system for testing the flying of an aircraft |
| CN104176265A (en) * | 2014-07-09 | 2014-12-03 | 中国人民解放军理工大学 | Overturnable bracket system for panoramic camera of unmanned aerial vehicle |
| CN104571140A (en) * | 2014-11-20 | 2015-04-29 | 中国建材检验认证集团股份有限公司 | Photovoltaic module routing inspection photographing control system |
| CN204992418U (en) * | 2015-09-22 | 2016-01-20 | 南方电网科学研究院有限责任公司 | Automatic device of patrolling and examining of unmanned aerial vehicle transmission line defect |
| CN105786017A (en) * | 2016-04-01 | 2016-07-20 | 常州天合光能有限公司 | Photovoltaic power station survey, operation and maintenance system based on unmanned aerial vehicle |
| CN205514228U (en) * | 2016-02-26 | 2016-08-31 | 中山市美斯特实业有限公司 | Removable blade of broken wall machine |
| CN106763062A (en) * | 2016-12-07 | 2017-05-31 | 上海宇航系统工程研究所 | A kind of forced locking device |
| CN206291264U (en) * | 2016-11-07 | 2017-06-30 | 佛山市顺德区合捷电器实业有限公司 | A kind of motor quickly positions Assembly And Disassembly structure with wind wheel |
-
2018
- 2018-01-25 CN CN201810071358.1A patent/CN108279705A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2010010420A1 (en) * | 2007-12-26 | 2010-01-28 | Tactical Systems Inc. | Suspended video imaging system |
| KR101050425B1 (en) * | 2010-02-25 | 2011-07-19 | 국방과학연구소 | Video pod system for testing the flying of an aircraft |
| CN104176265A (en) * | 2014-07-09 | 2014-12-03 | 中国人民解放军理工大学 | Overturnable bracket system for panoramic camera of unmanned aerial vehicle |
| CN104571140A (en) * | 2014-11-20 | 2015-04-29 | 中国建材检验认证集团股份有限公司 | Photovoltaic module routing inspection photographing control system |
| CN204992418U (en) * | 2015-09-22 | 2016-01-20 | 南方电网科学研究院有限责任公司 | Automatic device of patrolling and examining of unmanned aerial vehicle transmission line defect |
| CN205514228U (en) * | 2016-02-26 | 2016-08-31 | 中山市美斯特实业有限公司 | Removable blade of broken wall machine |
| CN105786017A (en) * | 2016-04-01 | 2016-07-20 | 常州天合光能有限公司 | Photovoltaic power station survey, operation and maintenance system based on unmanned aerial vehicle |
| CN206291264U (en) * | 2016-11-07 | 2017-06-30 | 佛山市顺德区合捷电器实业有限公司 | A kind of motor quickly positions Assembly And Disassembly structure with wind wheel |
| CN106763062A (en) * | 2016-12-07 | 2017-05-31 | 上海宇航系统工程研究所 | A kind of forced locking device |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180713 |