CN113978693A - Solar unmanned aerial vehicle with drawable surface power generation skin and power supply method - Google Patents
Solar unmanned aerial vehicle with drawable surface power generation skin and power supply method Download PDFInfo
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- CN113978693A CN113978693A CN202111233325.0A CN202111233325A CN113978693A CN 113978693 A CN113978693 A CN 113978693A CN 202111233325 A CN202111233325 A CN 202111233325A CN 113978693 A CN113978693 A CN 113978693A
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- 238000010248 power generation Methods 0.000 title claims abstract description 81
- 238000000034 method Methods 0.000 title claims abstract description 17
- 238000004146 energy storage Methods 0.000 claims abstract description 26
- 230000001105 regulatory effect Effects 0.000 claims abstract description 7
- 230000001276 controlling effect Effects 0.000 claims abstract description 6
- 230000005540 biological transmission Effects 0.000 claims description 25
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims description 12
- 238000004891 communication Methods 0.000 claims description 10
- 230000005611 electricity Effects 0.000 claims description 5
- 230000008569 process Effects 0.000 claims description 5
- 238000005259 measurement Methods 0.000 claims description 3
- 238000010030 laminating Methods 0.000 claims description 2
- 239000013589 supplement Substances 0.000 claims description 2
- 239000002699 waste material Substances 0.000 abstract description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 12
- 239000004917 carbon fiber Substances 0.000 description 12
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 11
- 238000005286 illumination Methods 0.000 description 8
- 230000000007 visual effect Effects 0.000 description 4
- 238000011161 development Methods 0.000 description 2
- 241000463219 Epitheca Species 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000002457 bidirectional effect Effects 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 230000001066 destructive effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/12—Construction or attachment of skin panels
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/30—Aircraft characterised by electric power plants
- B64D27/35—Arrangements for on-board electric energy production, distribution, recovery or storage
- B64D27/353—Arrangements for on-board electric energy production, distribution, recovery or storage using solar cells
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Photovoltaic Devices (AREA)
Abstract
The invention provides a solar unmanned aerial vehicle with a drawable surface power generation skin and a power supply method, wherein the solar unmanned aerial vehicle comprises the following components: the intelligent power generation device comprises a fuselage module, a power generation skin, an energy storage battery and an intelligent driving module, wherein the power generation skin is arranged on the upper surface of at least one side wing of the fuselage module in a covering manner; the intelligent driving module is arranged in the machine body of the machine body module and used for regulating and controlling the power supply circuit; under the severe weather condition, the power generation skin is stored in the wing on at least one side, and the intelligent driving module drives an energy storage battery to supply power; under the normal weather condition, the power generation skin covers the wings on at least one side, and the intelligent driving module drives the power generation skin to supply power; the waste of the energy is greatly avoided, and the efficient cruising of the unmanned aerial vehicle is realized.
Description
Technical Field
The invention belongs to the field of design of solar unmanned aerial vehicles, and particularly relates to a solar unmanned aerial vehicle with a drawable surface power generation skin and a power supply method.
Background
In order to improve the endurance time of the fixed-wing unmanned aerial vehicle and expand the range of power sources of the fixed-wing unmanned aerial vehicle, a new solution is provided by using a solar cell as an auxiliary power source at present, and how to efficiently utilize the solar cell makes the fixed-wing unmanned aerial vehicle have the advantages of light overall structure weight, long cruising time and the like, so that the problem to be solved urgently in the unmanned aerial vehicle industry is solved. 5G technical development is faster and faster, provides probably for the super long-distance real-time transmission of data, and more trade gets into the era of 5G +, combines together 5G and unmanned aerial vehicle field, realizes that beyond visual range control also is a big direction of development in present unmanned aerial vehicle field.
To conventional solar energy unmanned aerial vehicle, when meetting bad weather, there is certain problem in its surperficial solar cell's protection, and in the sufficient weather of illumination, solar cell's cover is on the unmanned aerial vehicle surface, and how to alleviate whole weight also is a big problem.
Disclosure of Invention
The invention aims to solve the problem of providing a solar unmanned aerial vehicle with a drawable surface power generation skin and a power supply method.
In order to solve the technical problems, the invention adopts the technical scheme that: a surface power generating skin drawable solar drone, comprising: the intelligent power generation device comprises a fuselage module, a power generation skin, an energy storage battery and an intelligent driving module, wherein the power generation skin is arranged on the upper surface of at least one side wing of the fuselage module in a covering manner;
the intelligent driving module is arranged in the machine body of the machine body module and used for regulating and controlling the power supply circuit;
under the severe weather condition, the power generation skin is stored in the wing on at least one side, and the intelligent driving module drives an energy storage battery to supply power;
under the normal weather condition, the power generation skin covers the wing on at least one side, and the intelligent driving module drives the power generation skin to supply power.
Further, the wing comprises a wing skin and a support arranged inside the wing, and the wing support is used for supporting the wing skin.
Furthermore, the upper surface of the wing shell on at least one side of the fuselage module is detachably provided with an upper shell, and the upper shell is arranged on the upper surface of the wing under the severe weather condition;
under normal weather conditions, the upper shell is removed from the upper surface of the wing.
Further, the power generation skin is wound on a drawing reel inside the wing on at least one side, and a drawing opening for drawing the power generation skin is formed in the lower surface of the wing;
under the normal weather condition, follow the pull-out of drawing mouth the electricity generation covering laminating the upper surface setting of wing, the electricity generation covering is kept away from one side of pull-out spool connect in the tail end of wing.
Further, still include communication transmission module, communication transmission module set up in the fuselage of fuselage module for realize that the data information of unmanned aerial vehicle flight control and the information between the ground equipment pass each other.
Further, the unmanned aerial vehicle is further provided with a sensor for measuring light irradiance, and the sensor feeds back measurement data to the intelligent driving module.
In order to achieve the purpose, the invention also provides a power supply method of the solar unmanned aerial vehicle with the drawable surface power generation skin, which comprises the following steps:
and judging the weather condition in the process of executing the flight task by the unmanned aerial vehicle, and regulating and controlling the power supply circuit according to the judgment result.
Further, in severe weather conditions, the upper surface of the wing is covered by an upper shell, and the power generation skin is arranged inside the wing; the intelligent driving module operates in a mode 1, and the unmanned aerial vehicle is directly powered by the energy storage battery;
and under normal weather, removing the upper shell from the upper surface of the wing, drawing out the power generation skin from the drawing opening, attaching the power generation skin to the upper surface of the wing, and judging the light irradiance.
Further, a sensor for measuring light irradiance is further installed on the unmanned aerial vehicle, the sensor feeds back measurement data to the intelligent driving module, and the intelligent driving module judges the light irradiance and adjusts the power control and supply circuit according to a judgment result.
Further, when the light irradiance is less than 500W/square meter, the intelligent driving module operates in a mode 2, and the power generation skin and the energy storage battery simultaneously supply power to the unmanned aerial vehicle;
when the light irradiance is 500 plus 750W per square meter, the intelligent driving module operates in a mode 3, the power generation skin supplies power to the unmanned aerial vehicle, and the energy storage battery plays an emergency supplement role when the light irradiance is suddenly insufficient;
when the light irradiance exceeds 750W/square meter, the intelligent driving module operates in a mode 4, and the power generation skin supplies power to the unmanned aerial vehicle and charges the energy storage battery.
Due to the adoption of the technical scheme, the method has the following beneficial effects:
1. detachable carbon fiber epitheca and flexible solar energy power generation covering use mutually in the cooperation under different weather, have improved unmanned aerial vehicle's energy supply and ability of cruising, have optimized unmanned aerial vehicle weight to the at utmost.
2. The intelligent driving module gives different power supply control modes to different weather conditions, greatly avoids energy waste, and realizes efficient cruising of the unmanned aerial vehicle
3.5G transmission module's carrying, rely on 5G powerful super long-distance transmission ability, realize unmanned aerial vehicle's beyond the visual range control.
Drawings
Fig. 1 is a schematic diagram of the overall structure of an unmanned aerial vehicle according to an embodiment of the present invention;
FIG. 2 is a schematic view of a wing under severe conditions in accordance with an embodiment of the invention;
FIG. 3 is a schematic view of a wing under normal conditions in accordance with an embodiment of the invention;
fig. 4 is a flow chart of the control of the intelligent driver module according to an embodiment of the present invention.
In the figure:
10. fuselage module 20, power generation skin 30, energy storage battery
40. Intelligent driving module 50, communication transmission module 60 and wing
61. Wing shell 62, support 63 and upper shell
64. Drawing reel
Detailed Description
The invention is further illustrated by the following examples and figures:
in one embodiment of the present invention, as shown in fig. 1, a surface power generation skin drawable solar drone includes: the intelligent power generation system comprises a fuselage module 10, a power generation skin 20, an energy storage battery 30, an intelligent driving module 40, a communication transmission module 50 and a sensor, wherein the power generation skin 20 is arranged on the upper surface of at least one side wing 60 of the fuselage module 10 in a covering mode; the intelligent driving module 40, the communication transmission module 50 and the sensor are all arranged in the body of the body module 10, wherein the intelligent driving module 40 is used for regulating and controlling the power supply circuit, the communication transmission module 50 is used for receiving flight control data information and outputting the flight control data information to ground equipment for control, and the sensor is used for measuring light radiation intensity.
In the working process, the sensor feeds back the measured light irradiance data to the intelligent driving module 40, judges the light irradiance data in the intelligent driving module 40, regulates and controls the power supply circuit, and performs bidirectional data information transmission with the ground equipment through the communication transmission module 50.
In severe weather conditions, the power generation skin 20 is stored in at least one side of the wing 60, and the intelligent driving module 40 drives the energy storage battery 30 to supply power; under normal weather conditions, the power generation skin 20 is coated on at least one side of the wing 60, and the intelligent driving module 40 drives the power generation skin 20 to supply power.
In the present embodiment, the severe weather is defined as a destructive thunderstorm weather, a strong wind weather, or the like, and the normal weather is a relatively calm weather other than the severe weather.
In the present embodiment, the power generation skin 20 is wrapped around both wings 60 of the fuselage module 10. As shown in fig. 2 to 3, the wing 60 includes a wing skin 61 and a wing support 62 disposed inside the wing 60, and the wing support 62 is used to support the wing skin 61. In this embodiment, the wing 60 has a streamline structure, so that the appearance is more attractive while the air resistance is reduced, the wing support 62 is a carbon fiber support, and the external shape structure of the wing support 62 conforms to the external shape structure of the wing skin 61, that is, the wing support is supported along the shape of the wing skin 61, as shown in fig. 2 to 3.
The fuselage airframe module 10 is a combination of a fixed wing, i.e., the wing 60 in this embodiment, and multiple rotors symmetrically disposed on both flanks, as shown in fig. 1. Wherein, the upper surface of the wing 60 at least one side of the fuselage module 10 is detachably provided with an upper shell 63, and under the severe weather condition, the upper shell 63 is arranged on the upper surface of the wing 60; in case of light weather, the upper case 63 is removed from the upper surface of the wing 60. The power generation skin 20 is wound on a drawing reel 64 in the wing 60 on at least one side, and a drawing opening 65 for drawing the power generation skin 20 is arranged on the lower surface of the wing 60; in the case of a light weather, the power generation skin 20 drawn out of the drawing opening 65 is arranged to be attached to the upper surface of the wing 60, and the side of the power generation skin 20 remote from the drawing reel 64 is connected to the tail end of the wing 60.
In this embodiment, as shown in fig. 2 to 3, the upper surfaces of the wings 60 on both sides of the unmanned aerial vehicle are detachably provided with upper shells 63, the upper shells 63 are also carbon fiber shells, the flexible solar power generation skin 20 can be drawn out from the lower sides of the front edges of the wings 60 on both sides of the unmanned aerial vehicle, the power generation skin 20 covers the surfaces of the wings 60, and the drawn out side of the power generation skin 20 extends into the wings 60 through an opening and is locked with the tail end inside the wings 60 by means of a lock catch.
Under severe weather conditions, the upper shell 63 made of carbon fiber is covered above the wings 60 on two sides, so that the flight task of the unmanned aerial vehicle is completed, and the unmanned aerial vehicle is further protected; under normal weather conditions, the upper shells 63 of the carbon fibers of the wings 60 on the two sides can be removed, the flexible solar power generation skin 20 is pulled out from the lower side of the front edge of the wing 60 and laid on the upper surface of the wing 60, the carbon fiber supports in the wing 60 support the flexible solar power generation skin, the surface of the solar power generation skin is kept in a good wing shape state, and the solar power generation skin 60 is tensioned and fixed by means of the lock catches.
As shown in fig. 1, an intelligent driving module 40 is installed inside the fuselage, and the power supply loop of the unmanned aerial vehicle can be switched according to whether a flexible solar power generation skin is laid or not and whether the illumination is sufficient or not. In this embodiment, the intelligent driver module 40 includes 4 modes as shown in fig. 4:
mode 1: when the flexible solar power generation skin 20 is not laid, the unmanned aerial vehicle system is powered by the energy storage battery 30;
when the flexible solar power generation skin 20 is laid, the intelligent driving module 40 can start the mode 2, mode 3 or mode 4 operation according to whether the illumination is sufficient.
Mode 2: the solar power generation skin and the energy storage battery 30 simultaneously supply power to the unmanned aerial vehicle system;
mode 3: the solar power generation skin independently supplies power to the unmanned aerial vehicle system, and the energy storage battery 30 is in an emergency power supply state;
mode 4: the solar power skin supplies power to the unmanned aerial vehicle system and charges the energy storage battery 30.
In this embodiment, the communication transmission module 50 is a 5G transmission module, and the unmanned aerial vehicle flight control information can be transmitted to the fixed IP address by means of the 5G transmission module, so as to realize over-the-horizon control. Specifically, the unmanned aerial vehicle has an independent flight control module to control the takeoff, landing, fixed-point navigation and the like of the unmanned aerial vehicle. Unmanned aerial vehicle flight control and 5G transmission module lug connection, unmanned aerial vehicle control and state data directly convey to 5G transmission module without decoding, and unmanned aerial vehicle control and state data will be transmitted to fixed IP address through the 5G link, receive unmanned aerial vehicle control and state data on ground equipment to accomplish the work of decoding in the ground station. Meanwhile, after the control data sent by the ground station is internally coded, the control data are fed back to the 5G transmission module through the 5G transmission link and then transmitted to the unmanned aerial vehicle flight control, decoding is completed in the flight control, and corresponding control is performed.
The working process of one embodiment of the invention is as follows:
in the process of executing the flight task by the unmanned aerial vehicle, the weather condition is directly judged artificially, and the power supply circuit is regulated and controlled according to the judgment result.
In the case of damaging inclement weather, the upper shell 63 covers the upper surface of the wing 60; the wing 60 upside adopts the carbon fiber casing to cover, and intelligent drive module 20 is in mode 1 operation, and unmanned aerial vehicle is direct to be supplied power by energy storage battery 30, and flexible solar power generation covering 20 is located the fuselage inside.
In normal weather, the carbon fiber upper shell 63 on the upper side of the wing 60 is removed, the power generation skin 20 is extracted from the extraction opening 65 on the lower side of the front edge of the wing 60, the power generation skin 20 is attached to the upper surface of the wing 60, the tightening locking is completed by utilizing the lock catch, and meanwhile, the light irradiance is continuously judged:
the sensor feeds back the measured light irradiance data to the intelligent driving module 40, and the intelligent driving module 40 judges the light irradiance and regulates and controls the power supply circuit according to the judgment result.
When the light irradiation is less than 500W/square meter, the condition of insufficient light irradiation is determined. When the illumination is insufficient, the intelligent driving module 40 is in the mode 2, and the solar power generation skin 20 and the energy storage battery 30 simultaneously supply power to the equipment on the unmanned aerial vehicle system in a cooperative manner;
when the light irradiation is 500-750W/square meter, the condition is sufficient. When illumination is more sufficient, intelligent drive module 40 is in mode 3, and the last equipment of unmanned aerial vehicle is supplied power by flexible solar energy power generation covering 20, and energy storage battery 30 is in the emergency power source state this moment, when illumination is not enough suddenly, plays the complementary action. The solar power generation skin independently supplies power to the unmanned aerial vehicle system, and the energy storage battery is in an emergency power supply state;
when the light irradiation is more than 750W/square meter, the condition of sufficient irradiation is obtained. When the illumination is very strong, the intelligent drive module is in mode 4, the equipment on the unmanned aerial vehicle is powered by the flexible solar power generation skin 20, and the solar power generation skin 20 also has part of the surplus electricity to charge the energy storage battery 30.
On the basis of above-mentioned step, unmanned aerial vehicle flight control directly links to each other with 5G transmission module, unmanned aerial vehicle control and status data do not decode direct transfer to 5G transmission module, 5G transmission module transmits received flight control data information (unmanned aerial vehicle control and status data) to the ground equipment of appointed IP through the 5G link, ground station on the ground equipment receives unmanned aerial vehicle control and status data, decode reading this information, and then produce new control information, rely on the 5G link to feed back to unmanned aerial vehicle flight control again, it carries out the information interaction task with ground equipment to accomplish unmanned aerial vehicle through 5G transmission module, realize unmanned aerial vehicle's beyond visual range control.
According to the invention, the carbon fiber upper shell is arranged on the surface of the detachable carbon fiber wing upper shell in severe weather, the structural strength of the unmanned aerial vehicle is enhanced, the carbon fiber upper shell is detached in normal weather, the flexible solar power generation skin is drawn out from the lower side of the front edge of the wing to cover the upper side of the wing, and the carbon fiber support inside the wing plays a supporting role, so that the unmanned aerial vehicle has a better wing shape, and the intelligent driving module inside the body can regulate and control the power supply loop of the unmanned aerial vehicle in real time according to the existence of the solar power generation skin and the illumination strength, so that the high-efficiency utilization of energy is achieved; the 5G transmission module in the fuselage directly receives the data information who flies the accuse, transmits ground equipment through the 5G link, relies on 5G technique to realize unmanned aerial vehicle's beyond visual range control.
The embodiments of the present invention have been described in detail, but the description is only for the preferred embodiments of the present invention and should not be construed as limiting the scope of the present invention. All equivalent changes and modifications made within the scope of the present invention shall fall within the scope of the present invention.
Claims (10)
1. The utility model provides a solar energy unmanned aerial vehicle that surface power generation covering can pull which characterized in that includes: the intelligent power generation device comprises a fuselage module, a power generation skin, an energy storage battery and an intelligent driving module, wherein the power generation skin is arranged on the upper surface of at least one side wing of the fuselage module in a covering manner;
the intelligent driving module is arranged in the machine body of the machine body module and used for regulating and controlling the power supply circuit;
under the severe weather condition, the power generation skin is stored in the wing on at least one side, and the intelligent driving module drives an energy storage battery to supply power;
under the normal weather condition, the power generation skin covers the wing on at least one side, and the intelligent driving module drives the power generation skin to supply power.
2. The surface power generation skin drawable solar drone of claim 1, characterized in that: the wing comprises a wing shell and a support arranged inside the wing, and the wing support is used for supporting the wing shell.
3. The surface power generation skin drawable solar drone of claim 2, characterized in that: the upper surface of the wing shell on at least one side of the fuselage module is detachably provided with an upper shell, and the upper shell is arranged on the upper surface of the wing under the severe weather condition;
under normal weather conditions, the upper shell is removed from the upper surface of the wing.
4. The surface power generation skin drawable solar drone of claim 3, characterized in that: the power generation skin is wound on a drawing reel inside the wing on at least one side, and a drawing opening for drawing the power generation skin is formed in the lower surface of the wing;
under the normal weather condition, follow the pull-out of drawing mouth the electricity generation covering laminating the upper surface setting of wing, the electricity generation covering is kept away from one side of pull-out spool connect in the tail end of wing.
5. The surface power generation skin drawable solar drone of claim 1, characterized in that: still include communication transmission module, communication transmission module set up in the fuselage of fuselage module for realize that the data information of unmanned aerial vehicle flight control and the information between the ground equipment pass each other.
6. The surface power-generating skin drawable solar drone of any one of claims 1 to 5, characterized in that: and a sensor for measuring light irradiance is further installed on the unmanned aerial vehicle, and the sensor feeds back measurement data to the intelligent driving module.
7. A method of powering the solar drone of claim 1 with a drawable surface power-generating skin, characterized by the steps of:
and judging the weather condition in the process of executing the flight task by the unmanned aerial vehicle, and regulating and controlling the power supply circuit according to the judgment result.
8. The method of claim 7, wherein the method of powering the solar drone with the drawable surface power-generating skin comprises,
in severe weather conditions, the upper surface of the wing is covered by an upper shell, the power generating skin being disposed inside the wing; the intelligent driving module operates in a mode 1, and the unmanned aerial vehicle is directly powered by the energy storage battery;
and under normal weather, removing the upper shell from the upper surface of the wing, drawing out the power generation skin from the drawing opening, attaching the power generation skin to the upper surface of the wing, and judging the light irradiance.
9. The method as claimed in claim 8, wherein the drone further has a sensor for measuring the light irradiance, the sensor feeds back the measured data to the intelligent driving module, and the intelligent driving module determines the light irradiance and adjusts the power control circuit according to the determination result.
10. The power supply circuit of a surface power generation skin drawable solar drone of claim 9,
when the light irradiance is less than 500W/square meter, the intelligent driving module operates in a mode 2, and the power generation skin and the energy storage battery simultaneously supply power to the unmanned aerial vehicle;
when the light irradiance is 500 plus 750W per square meter, the intelligent driving module operates in a mode 3, the power generation skin supplies power to the unmanned aerial vehicle, and the energy storage battery plays an emergency supplement role when the light irradiance is suddenly insufficient;
when the light irradiance exceeds 750W/square meter, the intelligent driving module operates in a mode 4, and the power generation skin supplies power to the unmanned aerial vehicle and charges the energy storage battery.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111233325.0A CN113978693A (en) | 2021-10-22 | 2021-10-22 | Solar unmanned aerial vehicle with drawable surface power generation skin and power supply method |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202111233325.0A CN113978693A (en) | 2021-10-22 | 2021-10-22 | Solar unmanned aerial vehicle with drawable surface power generation skin and power supply method |
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2021
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Effective date of registration: 20221130 Address after: 300384 No. 6 Huake No. 7 Road, Binhai New Area, Tianjin Binhai High-tech Industrial Development Zone Applicant after: The 18th Research Institute of China Electronics Technology Group Corporation Address before: 300384 No. 6 Huake No. 7 Road, Binhai New Area, Tianjin Binhai High-tech Industrial Development Zone Applicant before: The 18th Research Institute of China Electronics Technology Group Corporation Applicant before: CETC Energy Co.,Ltd. |