CN113525696A - Integrative new forms of energy unmanned aerial vehicle of scene - Google Patents
Integrative new forms of energy unmanned aerial vehicle of scene Download PDFInfo
- Publication number
- CN113525696A CN113525696A CN202110612180.9A CN202110612180A CN113525696A CN 113525696 A CN113525696 A CN 113525696A CN 202110612180 A CN202110612180 A CN 202110612180A CN 113525696 A CN113525696 A CN 113525696A
- Authority
- CN
- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- vehicle body
- wind
- body frame
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 7
- 229910052802 copper Inorganic materials 0.000 claims description 7
- 239000010949 copper Substances 0.000 claims description 7
- 238000010438 heat treatment Methods 0.000 claims description 5
- 238000010248 power generation Methods 0.000 abstract description 18
- 206010063385 Intellectualisation Diseases 0.000 abstract description 2
- 238000003763 carbonization Methods 0.000 abstract description 2
- 238000009434 installation Methods 0.000 description 11
- 239000000463 material Substances 0.000 description 6
- 239000000306 component Substances 0.000 description 5
- 238000005516 engineering process Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 230000002265 prevention Effects 0.000 description 3
- 239000002699 waste material Substances 0.000 description 3
- 238000004364 calculation method Methods 0.000 description 2
- 239000008358 core component Substances 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 230000008014 freezing Effects 0.000 description 2
- 238000007710 freezing Methods 0.000 description 2
- 238000012423 maintenance Methods 0.000 description 2
- 238000011084 recovery Methods 0.000 description 2
- 230000009466 transformation Effects 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910000976 Electrical steel Inorganic materials 0.000 description 1
- 235000017858 Laurus nobilis Nutrition 0.000 description 1
- 244000147568 Laurus nobilis Species 0.000 description 1
- 230000003044 adaptive effect Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
Images
Classifications
-
- 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
-
- 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
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
-
- 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
-
- 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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/02—Lightning protectors; Static dischargers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D9/00—Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
- F03D9/20—Wind motors characterised by the driven apparatus
- F03D9/25—Wind motors characterised by the driven apparatus the apparatus being an electrical generator
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03D—WIND MOTORS
- F03D9/00—Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
- F03D9/30—Wind motors specially adapted for installation in particular locations
- F03D9/32—Wind motors specially adapted for installation in particular locations on moving objects, e.g. vehicles
-
- 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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/72—Wind turbines with rotation axis in wind direction
-
- 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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/70—Wind energy
- Y02E10/728—Onshore wind turbines
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Power Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Wind Motors (AREA)
Abstract
The invention discloses a wind-solar integrated new energy unmanned aerial vehicle which comprises an unmanned aerial vehicle body, a wind-solar integrated generator module and an externally hung task tool module, wherein a power assembly is arranged on the unmanned aerial vehicle body and provides power for improving physical weight, flying and hovering for the unmanned aerial vehicle body; the wind-solar integrated generator module is connected with the unmanned aerial vehicle body and used for providing power required by the unmanned aerial vehicle body for hovering, cruising and flying in the air for a long time and the externally hung task tool module; the plug-in task tool module comprises a plug-in device and a plug-in task tool box body connected with the plug-in device. The wind-solar integrated new energy unmanned aerial vehicle is manufactured in a large scale, is low in price, mainly adopts wind power generation, adopts renewable energy of self-generation and self-power utilization with photovoltaic power generation as auxiliary power as unique power energy, can realize energy cleanness, low carbonization and intellectualization, and can hover or continue flight in the air for a long time and realize tasks required to be executed by the externally-hung task tool module.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to a wind-solar integrated new energy unmanned aerial vehicle.
Background
The existing unmanned aerial vehicle industry is mature in technology, various in types, prosperous in industry, wide in application and good in prospect. At present, the world energy scientific and technological revolution is different day by day, and the main country in the world all regards energy technological revolution as the important breach of scientific and technological revolution and economic transformation, and under the technological innovation drive, the energy is clean, and the low carbon is intelligent will further accelerate, and the unmanned aerial vehicle trade also need increase more diversified unmanned aerial vehicle.
Disclosure of Invention
Aiming at the defects of the prior art, the invention aims to provide a wind-solar integrated new energy unmanned aerial vehicle to solve the problems in the background technology.
In order to achieve the purpose, the invention is realized by the following technical scheme:
a wind and solar integrated new energy unmanned aerial vehicle comprises an unmanned aerial vehicle body, a wind and solar integrated generator module and an externally hung task tool module, wherein a power assembly is arranged on the unmanned aerial vehicle body and provides power for lifting physical weight, flying and hovering in the air for the unmanned aerial vehicle body; the wind-solar integrated generator module is connected with the unmanned aerial vehicle body and is used for providing a power supply required by the unmanned aerial vehicle body for hovering, cruising and flying for a long time in the air and the externally-hung task tool module; the external task tool module comprises an exchangeable external hanging device arranged on the unmanned aerial vehicle body and external task tool boxes which are connected with the external hanging device and can execute different tasks and are independent of each other.
Preferably, the unmanned aerial vehicle body comprises an unmanned aerial vehicle body frame, an unmanned aerial vehicle body frame base pedestal platform and an unmanned aerial vehicle body frame bottom landing and collision prevention device;
the unmanned aerial vehicle frame comprises a frame body, a first upright post and a second upright post, wherein the frame body is of a rectangular structure; the first upright columns are vertically erected on the long side of the frame body at equal intervals, and a top surface cross beam is arranged between the top ends of two adjacent first upright columns; the second upright columns are vertically erected on the short side of the frame body at equal intervals, and a top surface cross beam is arranged between the top ends of every two adjacent second upright columns;
the unmanned aerial vehicle body frame base platform is of a rectangular structure and is arranged on the bottom surface of the frame body;
the unmanned aerial vehicle body frame bottom falls to the ground and buffer stop install in unmanned aerial vehicle body frame base platform bottom surface.
Preferably, power component is including installation pole and the rotatory flight wing in unmanned aerial vehicle body frame top, the installation pole is the cylinder structure, installation pole fixed connection in the top surface cross beam top, it is a plurality of the rotatory flight wing in unmanned aerial vehicle body frame top pass through installation pole evenly distributed in the top surface cross beam top.
Preferably, the wind-solar integrated generator module is composed of a generator main rotating shaft, motors connected and installed at the top ends of the two ends of the generator main rotating shaft, a transverse rotating main cross rod fixedly connected to the midpoint of the generator main rotating shaft, and force bearing pull rods connected to the top ends of the two ends of the transverse rotating main cross rod and arranged at the middle positions of photovoltaic generating wind blades, a track prime mover is installed between the top ends of the photovoltaic generating wind blades and the bottom end cross rod, wheels of the track prime mover installed at the top ends and the bottom ends respectively fall into respective circumferential tracks, the top circumferential tracks are installed in a downward direction, the bottom circumferential tracks are installed on respective generator stator supports in an upward direction, the generator is provided with four rotor supports and eight stator supports on the generator main rotating shaft in a manner that one rotor support is matched with two stator supports, wherein the midpoint positions of the four rotor supports are fixedly connected with the generator main rotating shaft, rotating the four rotor supports together with the main rotating shaft; eight bearings are arranged at the middle points of the eight stator supports and are sleeved on the main rotating shaft, so that the eight stator supports cannot rotate together with the main rotating shaft, four permanent magnet mounting frames are mounted on the four rotor supports, four sets of permanent magnets are mounted in the frames, eight stator yokes are mounted on the eight stator supports, and eight sets of copper coils are mounted on the eight stator supports.
Preferably, still be equipped with unmanned aerial vehicle body frame lightning protection device and unmanned aerial vehicle body frame self-heating device on the unmanned aerial vehicle body frame base platform.
Preferably, the plug-in device is integrally connected with the unmanned aerial vehicle body frame bottom landing and anti-collision device.
The invention has the beneficial effects that: the invention provides a wind-solar integrated new energy unmanned aerial vehicle which is low in price, mainly provided with wind power generation and assisted by photovoltaic power generation, takes renewable energy of self-power generation and self-power utilization as unique power energy, can realize energy cleaning, low carbonization and intellectualization, and can hover or continue flight in the air for a long time and realize tasks required to be executed by an externally hung task tool module; the invention selects and matches a proper lightning protection device and installs the device at a proper position, thereby ensuring the safety of the unmanned aerial vehicle; unmanned aerial vehicle holds to be other under the severe cold condition of freezing in the front of extreme weather, and it is necessary to take the intensive action to the unexpected bad weather, in order to ensure unmanned aerial vehicle's normal operating, sets up unmanned aerial vehicle frame from heat facility, can ensure that unmanned aerial vehicle can not cover ice.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the provided drawings without creative efforts.
Fig. 1 is a schematic diagram of the overall structure of the wind-solar integrated new energy unmanned aerial vehicle provided by the invention.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1, the embodiment of the invention discloses a wind-solar integrated new energy unmanned aerial vehicle, which comprises an unmanned aerial vehicle body 1, a wind-solar integrated generator module 2 and an externally hung task tool module 3, wherein a power assembly 11 is arranged on the unmanned aerial vehicle body 1, and the power assembly 11 provides power for improving physical weight, flying and hovering of the unmanned aerial vehicle body 1; the wind-solar integrated generator module 2 is connected with the unmanned aerial vehicle body 1 and is used for providing power required by the unmanned aerial vehicle body 1 for long-time hovering, endurance flight and external task tool module 3 in the air; the external task tool module 3 comprises an exchangeable external hanging device 31 installed on the unmanned aerial vehicle body 1, and external task tool boxes 32 which are connected with the external hanging device 31 and can execute different tasks and are independent of each other.
In order to further optimize the technical scheme, the unmanned aerial vehicle body 1 comprises an unmanned aerial vehicle body frame 12, an unmanned aerial vehicle body frame base platform 13 and an unmanned aerial vehicle body frame bottom landing and collision prevention device 14;
the unmanned aerial vehicle body frame 12 comprises a frame body, a first upright post and a second upright post, wherein the frame body is of a rectangular structure; the first upright posts are vertically erected on the long side of the frame body at equal intervals, and a top surface cross beam is arranged between the top ends of two adjacent first upright posts; the second upright columns are vertically erected on the short side of the frame body at equal intervals, and a top surface cross beam is arranged between the top ends of two adjacent second upright columns;
the unmanned aerial vehicle body frame base platform 13 is of a rectangular structure and is arranged on the bottom surface of the frame body;
unmanned aerial vehicle body frame bottom is fallen to the ground and buffer stop 14 installs in unmanned aerial vehicle body frame base platform 13 bottom surface.
In order to further optimize above-mentioned technical scheme, power component 11 is including installation pole 112 and the rotatory flight wing 113 in unmanned aerial vehicle body frame top, and installation pole 112 is the cylinder structure, and installation pole 112 fixed connection is on top surface cross beam top, and a plurality of unmanned aerial vehicle body frame top rotatory flight wing 113 pass through installation pole 112 evenly distributed in top surface cross beam top.
In order to further optimize the technical scheme, the wind-solar integrated generator module 2 is composed of a generator main rotating shaft 21, motors 22 which are connected and installed at the top ends of the two ends of the generator main rotating shaft 21, a transverse rotating main cross rod 23 which is fixedly connected with the midpoint of the generator main rotating shaft 21, force bearing pull rods 25 which are connected with the top ends of the two ends of the transverse rotating main cross rod 23 and are arranged at the middle position of a photovoltaic generating wind blade 24, a track prime vehicle 26 is installed between the top end of the photovoltaic generating wind blade 24 and the bottom end cross rod, wheels of the track prime vehicle which are installed at the top end and the bottom end respectively fall into respective circumferential tracks 27, the circumferential tracks at the top end are installed in the downward direction, the circumferential tracks at the bottom end are installed on respective generator stator supports in the upward direction, a generator is provided with four rotor supports and eight stator supports on the generator main rotating shaft 21 in a mode that one rotor support is matched with two stator supports, the middle points of the four rotor supports are fixedly connected with a main rotating shaft 21 of the generator, so that the four rotor supports and the main rotating shaft rotate together; eight bearings are arranged at the middle points of the eight stator supports and are sleeved on the main rotating shaft, so that the eight stator supports cannot rotate together with the main rotating shaft, four permanent magnet mounting frames 28 are mounted on the four rotor supports, four sets of permanent magnets 29 are mounted in the frames, eight stator yokes are mounted on the eight stator supports, and eight sets of copper coils are mounted on the eight stator supports.
In order to further optimize the above technical solution, an unmanned aerial vehicle body frame lightning protection device 15 and an unmanned aerial vehicle body frame self-heating device 16 are further disposed on the unmanned aerial vehicle body frame base platform 13.
In order to further optimize the above technical solution, the plug-in device 31 is integrally connected with the unmanned aerial vehicle body frame bottom landing and collision avoidance device 14.
The unmanned aerial vehicle is manufactured into a final assembly product by modular design, and specifically comprises an unmanned aerial vehicle module, a wind-solar integrated generator module and an externally hung task tool module; the first embodiment is firstly applied to the military field, and provides a wind-solar integrated new energy unmanned aerial vehicle which is simple in structure, advanced in technology, wide in application, durable, light, miniaturized and high in maneuvering potential, and is used for sentry posts in frontier defense and severe cold regions;
the invention implements modular design and manufacture to the final assembly product, namely implements a module ratio system: the method is characterized in that a fixed scale is used as a basic module, and other components in the system are designed and manufactured to be an assembled product according to the proportion relation of the module; the specially designed wind-solar integrated new energy unmanned aerial vehicle product is suitable for meeting the field use requirements of on-site general assembly, transportation and storage, maintenance and the like under different environment conditions, and is specially designed.
Unmanned aerial vehicle frame: according to a wind-solar integrated new energy unmanned aerial vehicle project plan task book (hereinafter referred to as project book for short, the standard size of the unmanned aerial vehicle body frame of the embodiment can be determined to be that the unmanned aerial vehicle body frame is 5mx in length, 4mx in width and 2.8m in height, determines the appearance shape of the unmanned aerial vehicle, is a bearing structure for executing takeoff, hovering or flying, is a mounting position and a peripheral protection structure for ensuring that a wind-solar integrated generator module realizes power supply, is a large grid structure with space permeable sunlight and a wind channel, and is also a bearing structure for hanging an external task tool module;
the frame body of the unmanned aerial vehicle frame is of a rectangular structure, the first upright posts which are upright on two long sides with the length of 5m are calculated according to the distance of 0.4m1, one side with the length is provided with 12 first upright posts, and the two sides are provided with 24 first upright posts; the height of each 24 first upright columns is 2.8 m; every 2 first columns are provided with 1 top cross beam, and 24 first columns are provided with 12 top cross floats in total; the second upright posts are erected on two wide sides with the width of 4m, and the number of the second upright posts is 8 on one side and 16 on the two sides according to the calculation of 1 with the distance of 0.5 m; the height of 16 second laurel trees is 2.75m (the actual height of the top surface of the long-side upright column needs to be subtracted from each other by 0.05 m); every 2 second columns are provided with 1 top surface cross beam, and 16 second columns are provided with 8 top surface cross beams; the first upright post, the second upright post and the top cross are all connected into an unmanned aerial vehicle body frame with a large grid structure by screw caps in a fastening way; the bottom ends of all the stand columns and the unmanned aerial vehicle body frame base platform are connected into a whole through right-angle connecting pieces and screw caps in a fastening mode.
The wind-solar integrated generator module and all related equipment are arranged on the unmanned aerial vehicle body frame base platform according to the project book; a lower plug-in task tool module; the total weight of the load bearing of the electric energy meter is 15 tons (including the sum of the load bearing weight of the electric energy meter and the movable load bearing weight of the electric energy meter), and the sum is used as a calculation reference number of the total demand of the electric energy; all power sources of the embodiment are from a wind-solar integrated generator module, and all power guarantee requirements of taking off to the rated maximum flying height by 15 tons must be met, so that the secret and safe power sources are ensured; therefore, the drone body mount base platform must provide adequate mounting area and a drone body mount base platform of adequate strength and rigidity; the standard size of the unmanned aerial vehicle body frame base platform is as follows: length 5mx and width 4 m. The chassis frame of the recovered waste automobile conforming to the length standard is widened at two sides to form an unmanned aerial vehicle body frame base platform; the widened transformation part is manufactured according to the module assembly part, so that the general assembly and the maintenance can be facilitated. When adopting the old and useless car chassis frame of recovery to repack into unmanned aerial vehicle body frame base platform, the good frame of embodiment selectivity ability is gone the performance and is kept complete recovery car to repack into pure electric motor car and drive the removal function in order to realize that scene an organic whole new forms of energy unmanned aerial vehicle ground someone, make things convenient for ground to use.
The unmanned aerial vehicle body frame top rotating flying wing and the mounting rod are combined to form a system, and power for lifting physical weight and flying or hovering the unmanned aerial vehicle is provided for the unmanned aerial vehicle. The prior unmanned aerial vehicle has mature technology, and the flying and control branches of the unmanned aerial vehicle are rich and colorful as armed unmanned aerial vehicles have been used to show hands on a battlefield. Although an adaptive flight wing product cannot be found, the method has a certain reference value, and has a technical support value for the type selection of the rotary flight wing and the mounting rod of the unmanned aerial vehicle; rotatory flight wing in unmanned aerial vehicle body frame top and installation pole, as shown in the attached drawing, install the suitable position on unmanned aerial vehicle body frame top, its key point lies in: firstly, the physical importance of the total load is required, including the total weight of the unmanned aerial vehicle and the total weight possibly required by the active load; calculating the lifting capacity and the flying or hovering capacity required by different heights, different distances and different times according to the flight height, flight distance and time requirements determined by the unmanned aerial vehicle task; then, calculating the number of the required flying wings according to the lifting force or flying and hovering capabilities provided by the selected flying wings; finally, reasonably and distributively installing flying wings according to the balance of the unmanned aerial vehicle in the air in flying or hovering; the total load of the exemplary embodiment is 15 tons, namely the takeoff lifting weight; assuming that each selected flight wing has 100kg lifting weight, 150 flight wings are required for rated 15-ton lifting weight, and safe takeoff can be realized only by one-key control and distribution balance; meanwhile, the total number of the flight wings is determined according to the number of the flight wings and the lifting force which are required to be increased until the rated height is 200m when the different heights are lifted, the total balanced distribution installation is carried out, and the safe and reliable operation state of the unmanned aerial vehicle is ensured.
The unmanned aerial vehicle body frame bottom landing and collision avoidance device can be determined according to project books, and the requirements of two landing and collision avoidance devices of the wind-solar integrated new energy unmanned aerial vehicle need to be met; secondly, when the external task tool module is available, the external task tool module integrally falls to the ground and the anti-collision device from the air; therefore, a set of floor falling devices and anti-collision devices which are compatible with two different types are designed and manufactured according to modularization and practical requirements, and the specific floor falling and anti-collision devices of the embodiment have the following examples: the embodiment adopts a recycled waste automobile chassis frame as the unmanned body frame, and retains the embodiment of recycling waste automobiles, so that the recycled automobiles with good frame driving performance and complete integrity are required to be selected and refitted into pure electric vehicles to realize the function of driving and moving the unmanned aerial vehicle by a person on the ground, and the unmanned body frame bottom landing and collision avoidance device is convenient to use on the ground, so that the unmanned body frame bottom landing and collision avoidance device has to be freely installed and released, and meets the requirements of independent system landing and collision avoidance devices; unmanned aerial vehicle body frame end falls to ground and buffer stop is the load structure that main unmanned aerial vehicle rises and falls, and when the design preparation, it should be noted that, selects the bracing piece and receive and release articular rationality, maneuverability and security.
The unmanned aerial vehicle is necessary to be equipped with the lightning protection device no matter the unmanned aerial vehicle is positioned on the ground or in the air, and the appropriate lightning protection device is selected and matched and is installed at an appropriate position, so that the necessary measures for ensuring the safety of the unmanned aerial vehicle are provided; the unmanned aerial vehicle is necessary to take reinforcement measures aiming at predictable severe weather under the conditions of severe cold and freezing in the front of extreme weather, and the unmanned aerial vehicle body frame self-heating device is arranged to ensure that the unmanned aerial vehicle cannot be covered with ice in order to ensure the normal operation of the unmanned aerial vehicle; the self-heating device of the embodiment belongs to unmanned aerial vehicle self-service secondary equipment, and is easy to obtain, install and use.
Generator owner rotation axis, this technical characterstic owner rotation axis, its characterized in that: the wind-solar integrated generator module consists of eight generators and is a core structural member for synchronous power generation by a vertical main rotating shaft; the material performance requirement is very high, and the material has excellent rigidity and strength, and also has excellent deformation resistance and tension-torsion resistance, so that the four rotor supports of eight generators can synchronously rotate, and the deviation speed are not asynchronous. Therefore, the main rotating shaft of the embodiment must strictly select materials according to design requirements, and can not be replaced by common shaft materials, and the top ends of the two ends of the main rotating shaft of the generator are connected with the installed motors, and the generator is characterized in that: the top ends of the two ends of the main rotating shaft are connected with two motors, one motor is fixedly arranged at the central point position of the top stator support in a downward direction, the rotating shafts of the motors are connected with the main rotating shaft, and the rotating directions of the two rotating shafts are ensured to be the same; the other motor is fixedly arranged at the central point of the bottom stator bracket in the upward direction, the motor shaft is connected with the main rotating shaft, and the rotating directions of the two rotating shafts are ensured to be the same; the two motors can be independently switched on or off, and can also be simultaneously switched on or off; when the two motors are closed, the normal rotation operation of the main rotating shaft is not influenced.
Generator owner rotation axis mid point goes up fixed connection's horizontal rotation owner horizontal pole, its characterized in that: the transverse rotating main cross rod component fixedly connected with the midpoint of the vertical main rotating shaft is a core component of the generator; the wind power transmission of the photovoltaic power generation wind blade is a power source of a generator main rotating shaft, so that a core component which rotates together with the vertical main rotating shaft and the transverse rotating main cross rod group is formed, a rotor support of the generator is driven to rotate together, and magnetic lines of force are cut to realize power generation.
The embodiment uses only one transverse rotary main transverse rod, and the material requirement of the transverse rotary main transverse rod is basically the same as that of the main rotary shaft, if the difference is the material shape.
The top ends of the two ends of the transverse rotary main cross rod are connected with a bearing pull rod on the middle position of the photovoltaic power generation wind blade: the technical support is that the transverse rotating main cross rod group is a main component for transmitting a power source of wind power generation to the main rotating shaft to operate; the photovoltaic power generation wind blade is a structural member received and transmitted by a wind power source, a force bearing pull rod is arranged in the middle of the photovoltaic power generation wind blade, and every two photovoltaic power generation blades form a group and are effectively connected with the top ends of two ends of each main transverse rod of the transverse rotating main transverse rod group.
A track prime mover is arranged between the cross rods at the top end and the bottom end of the photovoltaic power generation wind blades, and the number of the photovoltaic power generation wind blades is determined by the number of the transversely-rotating main cross rods; and a track prime mover is arranged between the cross bars at the top end and the bottom end of each photovoltaic power generation wind blade.
The wheels of the track prime mover arranged at the top end and the bottom end respectively fall into respective circumferential tracks, and the wheels of the track prime mover arranged at the top of the photovoltaic power generation wind blades are upward; the wheels of the track prime mover mounted at the bottom end are downward, and the wheels of the track prime mover mounted at the top end and the bottom end of all the photovoltaic power generation wind blades are required to fall into respective circumferential tracks.
The top end circumferential track is installed in a downward direction, the bottom end circumferential track is installed on respective generator stator supports in an upward direction, the top end circumferential track is installed on a top end stator support of the generator set in a downward direction, and the bottom end circumferential track is installed on the generator set bottom end stator support in an upward direction; the well ensures that the prime mover wheels of the top and bottom tracks normally run in their respective circumferential tracks.
The generator is provided with four rotor supports and eight stator supports on a main rotating shaft of the generator in a mode that one rotor support is matched with two stator supports, wherein the middle points of the four rotor supports are fixedly connected with the main rotating shaft, so that the four rotor supports and the main rotating shaft rotate together; eight bearings of eight stator support mid point installations and suit are on main rotation axis, make eight stator supports can not rotate its characterized in that with main rotation axis together: the structure mode that one rotor bracket is matched with two stators is that two generators are obtained; the four rotor supports are matched with eight stator supports, namely eight generators; each rotor support is provided with a set of permanent magnet mounting frame, and a set of permanent magnets is arranged in the frame; each stator bracket is provided with a set of magnetic yokes, and a set of copper picture is arranged on each magnetic yoke; eight generators of the embodiment form a wind-light integrated generator set which is divided into an upper part and a lower part by the transverse rotary main transverse rods, wherein the upper part is provided with four generators, and the lower part is provided with four generators; eight generators are driven by a main rotating shaft to generate electricity together, and the center points of four rotor supports are fixedly connected with the main rotating shaft and rotate together with the main rotating shaft; eight bearings are arranged on the central points of the eight stator supports, are sleeved on the main rotating shaft and cannot rotate together with the main rotating shaft.
Four permanent magnet mounting frames are mounted on the four rotor supports, four sets of permanent magnets are mounted in the frames, and the H/s two pole faces of the permanent magnet are used in the embodiment; and a space is arranged in the permanent magnet mounting frame between the S poles of the permanent magnet H pole machine to keep a magnetic force line channel.
Eight stator magnetic yokes are arranged on the eight stator supports, eight sets of copper coils are arranged on the eight stator magnetic yokes, and the eight stator magnetic yokes are wound by oriented silicon steel strips; eight sets of copper coils are wound by thick insulated copper wires;
an alternative external hanging device is installed below the base platform of the unmanned aerial vehicle body frame, and the alternative external hanging device is integrally designed, manufactured, installed and used with the unmanned aerial vehicle body frame bottom landing and collision prevention device; different tasks and independent external task tool boxes can be executed, and the external task tool boxes are manufactured and used by users or manufactured according to requirements.
The embodiments in the present description are described in a progressive manner, each embodiment focuses on differences from other embodiments, and the same and similar parts among the embodiments are referred to each other. The device disclosed by the embodiment corresponds to the method disclosed by the embodiment, so that the description is simple, and the relevant points can be referred to the method part for description.
The previous description of the disclosed embodiments is provided to enable any person skilled in the art to make or use the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other embodiments without departing from the spirit or scope of the invention. Thus, the present invention is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
Claims (6)
1. The wind-solar integrated new energy unmanned aerial vehicle is characterized by comprising an unmanned aerial vehicle body (1), a wind-solar integrated generator module (2) and an externally hung task tool module (3), wherein a power assembly (11) is arranged on the unmanned aerial vehicle body (1), and the power assembly (11) provides power for lifting physical weight, flying and hovering in the air for the unmanned aerial vehicle body (1); the wind-solar integrated generator module (2) is connected with the unmanned aerial vehicle body (1) and is used for providing a power supply required by the unmanned aerial vehicle body (1) for long-time hovering, endurance flight and plug-in task tool module (3); the external task tool module (3) comprises an exchangeable external hanging device (31) arranged on the unmanned aerial vehicle body (1) and external task tool boxes (32) which are connected with the external hanging device (31) and can execute different tasks and are independent of each other.
2. The wind-solar integrated new energy unmanned aerial vehicle of claim 1, wherein the unmanned aerial vehicle body (1) comprises an unmanned aerial vehicle body frame (12), an unmanned aerial vehicle body frame base platform (13) and an unmanned aerial vehicle body frame bottom landing and collision avoidance device (14);
the unmanned aerial vehicle frame (12) comprises a frame body, a first upright post and a second upright post, wherein the frame body is of a rectangular structure; the first upright columns are vertically erected on the long side of the frame body at equal intervals, and a top surface cross beam is arranged between the top ends of two adjacent first upright columns; the second upright columns are vertically erected on the short side of the frame body at equal intervals, and a top surface cross beam is arranged between the top ends of every two adjacent second upright columns;
the unmanned aerial vehicle body frame base platform (13) is of a rectangular structure and is arranged on the bottom surface of the frame body;
the unmanned aerial vehicle body frame bottom landing and anti-collision device (14) is installed on the bottom surface of the unmanned aerial vehicle body frame base platform (13).
3. The wind-solar integrated new energy unmanned aerial vehicle of claim 2, wherein the power assembly (11) comprises a mounting rod (112) and an unmanned aerial vehicle body frame top rotary flight wing (113), the mounting rod (112) is of a cylindrical structure, the mounting rod (112) is fixedly connected to the top surface cross beam top end, and the plurality of unmanned aerial vehicle body frame top rotary flight wings (113) are uniformly distributed on the top surface cross beam top end through the mounting rod (112).
4. The wind-solar integrated new energy unmanned aerial vehicle as claimed in claim 1, wherein the wind-solar integrated generator module (2) is composed of a generator main rotating shaft (21), motors (22) connected and mounted at the top ends of the two ends of the generator main rotating shaft (21), a transverse rotating main cross rod (23) fixedly connected to the midpoint of the generator main rotating shaft (21), force bearing pull rods (25) connected to the top ends of the two ends of the transverse rotating main cross rod (23) and connected to the middle positions of photovoltaic generation wind blades (24), a track prime mover (26) mounted between the top ends of the photovoltaic generation wind blades (24) and the bottom end cross rod, wheels of the track prime movers mounted at the top ends and the bottom ends respectively fall into respective circumferential tracks (27), the top circumferential tracks are mounted in a downward direction, the bottom circumferential tracks are mounted on respective generator stator supports in an upward direction, and the generator is characterized in that one rotor support is matched with two stator supports to mount four rotor supports and eight stators The bracket is arranged on a main rotating shaft (21) of the generator, wherein the midpoint positions of the four rotor brackets are fixedly connected with the main rotating shaft (21) of the generator, so that the four rotor brackets and the main rotating shaft rotate together; eight bearings are arranged at the middle points of the eight stator supports and are sleeved on the main rotating shaft, so that the eight stator supports cannot rotate together with the main rotating shaft, four permanent magnet mounting frames (28) are mounted on the four rotor supports, four sets of permanent magnets (29) are mounted in the frames, eight stator yokes are mounted on the eight stator supports, and eight sets of copper coils are mounted on the eight stator supports.
5. The wind-solar integrated new energy unmanned aerial vehicle of claim 2, wherein an unmanned aerial vehicle body frame lightning protection device (15) and an unmanned aerial vehicle body frame self-heating device (16) are further arranged on the unmanned aerial vehicle body frame base platform (13).
6. The wind-solar integrated new energy unmanned aerial vehicle of claim 1, wherein the plug-in device (31) is integrally connected with the unmanned aerial vehicle body frame bottom landing and collision avoidance device (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110612180.9A CN113525696A (en) | 2021-06-02 | 2021-06-02 | Integrative new forms of energy unmanned aerial vehicle of scene |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110612180.9A CN113525696A (en) | 2021-06-02 | 2021-06-02 | Integrative new forms of energy unmanned aerial vehicle of scene |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN113525696A true CN113525696A (en) | 2021-10-22 |
Family
ID=78094949
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202110612180.9A Pending CN113525696A (en) | 2021-06-02 | 2021-06-02 | Integrative new forms of energy unmanned aerial vehicle of scene |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN113525696A (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2005003554A1 (en) * | 2003-07-08 | 2005-01-13 | Cosmo Plant Co., Ltd | Wind power generation system, arrangement structure of permanent magnets, and electricity/force conversion system |
| CN205142077U (en) * | 2015-10-08 | 2016-04-06 | 李�杰 | Complementary intelligent power generation system of vertical axis scene |
| CN106314806A (en) * | 2016-10-19 | 2017-01-11 | 黄河交通学院 | Wind-solar complementary generation system of UAV (unmanned aerial vehicle) and operation method of system |
| CN106533325A (en) * | 2015-09-11 | 2017-03-22 | 特科芯有限公司 | Mechanism for realizing duration distance increase of unmanned aerial vehicle through power generation by means of solar energy and mechanical energy |
| CN109866929A (en) * | 2017-12-04 | 2019-06-11 | 西安知点信息科技有限公司 | A kind of unmanned plane with long cruising ability |
| CN110171295A (en) * | 2018-02-20 | 2019-08-27 | 南昌市周静新能源有限公司 | A kind of wind and solar integrated new energy pure electric automobile |
| CN110174025A (en) * | 2018-02-20 | 2019-08-27 | 南昌市周静新能源有限公司 | A kind of wind and solar integrated new energy guided missile vertical air flat pad |
-
2021
- 2021-06-02 CN CN202110612180.9A patent/CN113525696A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2005003554A1 (en) * | 2003-07-08 | 2005-01-13 | Cosmo Plant Co., Ltd | Wind power generation system, arrangement structure of permanent magnets, and electricity/force conversion system |
| CN106533325A (en) * | 2015-09-11 | 2017-03-22 | 特科芯有限公司 | Mechanism for realizing duration distance increase of unmanned aerial vehicle through power generation by means of solar energy and mechanical energy |
| CN205142077U (en) * | 2015-10-08 | 2016-04-06 | 李�杰 | Complementary intelligent power generation system of vertical axis scene |
| CN106314806A (en) * | 2016-10-19 | 2017-01-11 | 黄河交通学院 | Wind-solar complementary generation system of UAV (unmanned aerial vehicle) and operation method of system |
| CN109866929A (en) * | 2017-12-04 | 2019-06-11 | 西安知点信息科技有限公司 | A kind of unmanned plane with long cruising ability |
| CN110171295A (en) * | 2018-02-20 | 2019-08-27 | 南昌市周静新能源有限公司 | A kind of wind and solar integrated new energy pure electric automobile |
| CN110174025A (en) * | 2018-02-20 | 2019-08-27 | 南昌市周静新能源有限公司 | A kind of wind and solar integrated new energy guided missile vertical air flat pad |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP0022635B1 (en) | Fluid powered tracked vehicle for generating electricity | |
| CN102345557B (en) | Variable windmill wing wind power generator having power generation efficiency increasing means | |
| JP5684264B2 (en) | Wind power generator | |
| CN101383569A (en) | Solar energy linkage rod sun-following electricity generation plant | |
| EP2894097B1 (en) | Electrodynamic dish-shaped flying generator | |
| CN113525696A (en) | Integrative new forms of energy unmanned aerial vehicle of scene | |
| CN112065660B (en) | Yaw mechanism of wind driven generator | |
| CN211116719U (en) | Modularized solar direct-drive ventilation fan based on permanent magnet repulsion force | |
| CN110748458A (en) | Road magnetic suspension wind driven generator and power generation device | |
| CN102996333A (en) | Wind energy conversion mechanism and upper-air wind power generation device | |
| CN102979676A (en) | Luminous energy and wind energy gradient power system applying magnetic suspension technique | |
| CN102723837A (en) | Electrically-controlled magnetic motor | |
| CN102011707A (en) | Large-sized magnetically levitated circular track wind driven generator | |
| CN204124363U (en) | A kind of multi-rotor aerocraft | |
| CN202997900U (en) | Two-phase switched reluctance motor | |
| CN210405192U (en) | Photovoltaic energy storage container | |
| CN202946309U (en) | Wind energy converting mechanism and high altitude wind power generation device | |
| CN206590057U (en) | New type electric bicycle | |
| CN220043259U (en) | Wind-solar complementary integrated power generation device | |
| CN204741385U (en) | Many drive unit's of distributing type switched reluctance motor | |
| CN217629505U (en) | Novel highway anti-dazzle guardrail with wind energy utilization function | |
| CN215420147U (en) | Wind-solar integrated power generation vehicle refitted by recycling chassis frame | |
| CN204312251U (en) | A kind of wind power generation system | |
| CN218235343U (en) | Tandem type multi-impeller wind generating set | |
| CN102979670A (en) | Wind power conversion mechanism and high altitude wind power generator |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20211022 |
|
| RJ01 | Rejection of invention patent application after publication |