CN112009686A - Foldable flying wing formula unmanned aerial vehicle that has high continuation of journey function - Google Patents

Foldable flying wing formula unmanned aerial vehicle that has high continuation of journey function Download PDF

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Publication number
CN112009686A
CN112009686A CN202010940527.8A CN202010940527A CN112009686A CN 112009686 A CN112009686 A CN 112009686A CN 202010940527 A CN202010940527 A CN 202010940527A CN 112009686 A CN112009686 A CN 112009686A
Authority
CN
China
Prior art keywords
unmanned aerial
aerial vehicle
machine body
storage battery
power generation
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
Application number
CN202010940527.8A
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Chinese (zh)
Inventor
桂永斌
胡斌
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Jiangxi Zhongqing Intelligent Equipment Co ltd
Original Assignee
Jiangxi Zhongqing Intelligent Equipment Co ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Jiangxi Zhongqing Intelligent Equipment Co ltd filed Critical Jiangxi Zhongqing Intelligent Equipment Co ltd
Priority to CN202010940527.8A priority Critical patent/CN112009686A/en
Publication of CN112009686A publication Critical patent/CN112009686A/en
Pending legal-status Critical Current

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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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/24—Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
    • B64D27/353—
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00—Equipment not otherwise provided for
    • B64D47/08—Arrangements of cameras
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/19—Propulsion using electrically powered motors
    • 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
    • F03D9/10—Combinations of wind motors with apparatus storing energy
    • F03D9/11—Combinations of wind motors with apparatus storing energy storing electrical energy
    • 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
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/14—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries for charging batteries from dynamo-electric generators driven at varying speed, e.g. on vehicle
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
    • H02J7/34—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering
    • H02J7/35—Parallel operation in networks using both storage and other dc sources, e.g. providing buffering with light sensitive cells
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D2201/00—Airbags mounted in aircraft for any use
    • 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
    • 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
    • Y02E70/00—Other energy conversion or management systems reducing GHG emissions
    • Y02E70/30—Systems combining energy storage with energy generation of non-fossil origin
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Abstract

The invention discloses a folding flying wing type unmanned aerial vehicle with high endurance function, comprising: the device comprises a machine body, a rotary power generation device, a solar power generation plate, transparent glass, a rotary arm, a rotor motor, a rotating shaft, a rotor, an electromagnetic power generation device, an external storage battery, a reverse electric appliance and a storage battery; the unmanned aerial vehicle has stronger cruising ability, avoids damage caused by the fact that the unmanned aerial vehicle is impacted by external force, the inflatable bag can reduce the self weight of the unmanned aerial vehicle, thereby increasing the cruising ability of the unmanned aerial vehicle, in addition, the arrangement of the inflatable bag can protect the unmanned aerial vehicle from being influenced by external force, the unmanned aerial vehicle is prevented from being damaged by external impact, and meanwhile, the detachable connection of the unmanned aerial vehicle body and the inflatable bag increases the flexibility of the whole use of the unmanned aerial vehicle.

Description

Foldable flying wing formula unmanned aerial vehicle that has high continuation of journey function
Technical Field
The invention relates to the technical field of unmanned aerial vehicles, in particular to a foldable flying wing type unmanned aerial vehicle with a high endurance function.
Background
At present, along with the rapid development of communication technology and flight control technology, unmanned aerial vehicles are gradually and widely applied to many fields due to the advantages of small size and portability. Unmanned aerial vehicle mainly has three kinds of fixed wing unmanned aerial vehicle, unmanned helicopter and many rotor unmanned aerial vehicle, and wherein unmanned aerial vehicle still includes parachute wing unmanned aerial vehicle, flapping wing unmanned aerial vehicle and unmanned spacecraft etc.. Fixed wing drones are the most widely used. In the market, fixed wing unmanned aerial vehicle adopts the four-axis linkage, can realize the gesture of space optional position. But fixed wing unmanned aerial vehicle often leads to occupation space great because its huge structure, leads to unmanned aerial vehicle's duration to be relatively poor owing to adopt single battery drive moreover. In view of the above disadvantages, a foldable flying wing type unmanned aerial vehicle with high endurance function needs to be designed and developed, which can complement the above disadvantages.
Disclosure of Invention
The invention aims to provide a folding flying wing type unmanned aerial vehicle with a high endurance function.
In order to achieve the above object, the present invention employs the following:
a foldable flying wing formula unmanned aerial vehicle that has high continuation of journey function, includes: the device comprises a machine body, a rotary power generation device, a solar power generation plate, transparent glass, a rotary arm, a rotor motor, a rotating shaft, a rotor, an electromagnetic power generation device, an external storage battery, a reverse electric appliance and a storage battery; a rotary power generation device is arranged at the center of the interior of the machine body; a storage battery is arranged on the left side inside the machine body; an external storage battery is arranged on the right side of the machine body, the external storage battery is connected with the storage battery through a wire, and a reverse electric appliance is arranged at the position of the wire of the external storage battery; the rotary power generation device is connected with an external storage battery through a wire; a rotary arm is arranged at the upper end of the side surface of the machine body; a rotor motor is arranged at the bottom end of the spiral arm; a rotating shaft is arranged at the upper end of the rotor motor and penetrates through the swing arm; a rotor wing is arranged at the upper end of the rotating shaft; the solar power generation panel is arranged at the upper end of the machine body and is connected with the external storage battery through a wire; transparent glass is arranged at the upper end of the solar power generation panel; the electromagnetic power generation device is arranged around the rotating part of the device and is connected with an external storage battery through a wire.
Preferably, the rotary power generation device comprises a rotating shaft, a pinion, a gearwheel, a gear shaft, a generator, a connecting disc, a signal lamp, a supporting frame and blades; the rotating shaft is arranged at the longitudinal center inside the machine body, and the upper end of the rotating shaft penetrates through the machine body; a pinion is arranged at the middle lower end of the rotating shaft; a bull gear is arranged on one side of the pinion, and the bull gear is matched with the pinion for use; a gear shaft is arranged in the center of the large gear and is connected with a generator; a connecting disc is arranged at the top end of the rotating shaft; a signal lamp is arranged at the top end of the connecting disc; a support frame is arranged on the side surface of the connecting disc; and blades are arranged on the outer side of the support frame.
Preferably, the electromagnetic power generating device includes positive electrode iron and negative electrode iron; the positive electrode iron and the negative electrode iron are respectively arranged on two sides of the rotating shaft and the rotating shaft, the positive electrode and the negative electrode are respectively connected through wires, and the tail ends of the wires are connected to an external storage battery.
Preferably, the transparent glass is tempered glass.
Preferably, the radial arm is movably connected with the machine body through a bolt.
Preferably, the device further comprises an inflatable bag and a photographic device; the inflatable bag is arranged at the bottom end of the machine body and is connected with the machine body through threads; the photographic device is arranged between the machine body and the inflatable bag and is fixed in the middle of the bottom end of the machine body.
Preferably, the inflatable bag comprises an outer bag skin, an inner bag skin, an inflatable cavity photographing window, an inflation nozzle, a valve and a connecting part; the outer bag skin is spherical cambered surface form, and outer bag skin is connected with the inner bag skin, forms the inflation chamber between outer bag skin and the inner bag skin, and the inflation chamber is hollow structure, and the inflation chamber passes through the gas tube and inserts external gas, and the gas tube passes outer bag skin and is linked together with the inflation chamber, and the inflation tube tip sets up the valve, and the upper portion handing-over department of outer bag skin and inner bag skin sets up connecting portion, and threaded connection between connecting portion and the organism side bottom, sets up the photographic window in the bottom both sides of gas tube, and photographic window and photographic arrangement cooperate the application.
Preferably, the outer bag skin and the inner bag skin are made of PU plastic materials.
Preferably, the photographing apparatus includes a connection rod, a joint part, an auxiliary link, and a camera; a connecting rod is arranged in the middle of the bottom end of the machine body; the bottom end of the connecting rod is provided with a joint part; the auxiliary connecting rod is connected with the joint part; and a camera is arranged at the rear end of the auxiliary connecting rod.
Preferably, the joint part comprises a joint groove and a rotary ball, the joint groove is in a hollow spherical shape, the joint groove is arranged at the bottom end of the connecting rod, the rotary ball is arranged in the joint groove in a matched mode and is in a spherical shape, and one side of the bottom end of the rotary ball is fixedly connected with the auxiliary connecting rod.
The invention has the following advantages:
the unmanned aerial vehicle has stronger cruising ability, avoids damage caused by the fact that the unmanned aerial vehicle is impacted by external force, the inflatable bag can reduce the self weight of the unmanned aerial vehicle, thereby increasing the cruising ability of the unmanned aerial vehicle, in addition, the arrangement of the inflatable bag can protect the unmanned aerial vehicle from being influenced by external force, the unmanned aerial vehicle is prevented from being damaged by external impact, and meanwhile, the detachable connection of the unmanned aerial vehicle body and the inflatable bag increases the flexibility of the whole use of the unmanned aerial vehicle.
Drawings
The following describes embodiments of the present invention in further detail with reference to the accompanying drawings.
Fig. 1 is a schematic structural diagram of a foldable flying wing type unmanned aerial vehicle with high endurance function according to the present invention.
Fig. 2 is a schematic structural view of the inflatable bag.
In the figures, the various reference numbers are:
1-body, 2-inflatable bag, 21-outer airbag, 22-inner airbag, 23-inflatable cavity, 24-photographic window, 25-inflatable tube, 26-valve, 27-connecting part, 3-photographic device, 31-connecting rod, 32-joint part, 321-joint groove, 322-rotary ball, 33-auxiliary connecting rod, 34-camera, 4-rotary generating device, 41-rotary shaft, 42-small gear, 43-big gear, 44-gear shaft, 45-generator, 46-connecting disc, 47-signal lamp, 48-supporting frame, 49-blade, 5-solar generating plate, 6-transparent glass, 7-rotary arm, 8-rotary motor, 9-rotary shaft, 10-rotary wing, 11-an electromagnetic generating device, 111-positive electrode iron, 112-negative electrode iron, 12-an external storage battery, 13-an inverter and 14-a storage battery.
Detailed Description
In order to more clearly illustrate the invention, the invention is further described below in connection with preferred embodiments. It is to be understood by persons skilled in the art that the following detailed description is illustrative and not restrictive, and is not to be taken as limiting the scope of the invention.
As shown in fig. 1, a foldable flying-wing drone with high endurance function includes: the solar energy power generation device comprises a machine body 1, a rotary power generation device 4, a solar power generation panel 5, transparent glass 6, a rotary arm 7, a rotary wing motor 8, a rotary shaft 9, a rotary wing 10, an electromagnetic power generation device 11, an external storage battery 12, a reverse power device 13 and a storage battery 14; a rotary power generation device 4 is arranged at the center of the interior of the machine body 1; a storage battery 14 is arranged at the left side in the machine body 1; an external storage battery 12 is arranged on the right side of the machine body 1, the external storage battery 12 is connected with a storage battery 14 through a wire, a reverse electric appliance 13 is arranged at the position of the wire of the external storage battery 12, and the reverse electric appliance 13 is arranged to prevent the current in the storage battery 14 from being connected with the storage battery 12; the rotary power generation device 4 is connected with the external storage battery 12 through an electric wire, so that the generated electricity can be conveniently transmitted to the external storage battery 12; the upper end of the side surface of the machine body 1 is provided with a rotating arm 7; a rotor motor 8 is arranged at the bottom end of the rotary arm 7; a rotating shaft 9 is arranged at the upper end of the rotor motor 8, and the rotating shaft 9 penetrates through the rotary arm 7; the upper end of the rotating shaft 9 is provided with a rotor wing 10, and the rotor wing 10 can be driven to rotate when the rotor wing motor 8 is started; the solar power generation panel 5 is arranged at the upper end of the machine body 1, and the solar power generation panel 5 is connected with the external storage battery 12 through an electric wire, so that the generated electricity can be conveniently transmitted to the external storage battery 12; the transparent glass 6 is arranged at the upper end of the solar power generation panel 5, so that sunlight can penetrate through the glass and can be incident on the solar power generation panel 5 conveniently; the electromagnetic generating device 11 is arranged around the rotating part of the device and is connected with the external storage battery 12 through wires, so that the generated electricity can be conveniently transmitted to the external storage battery 12.
Further, the rotary power generating device 4 comprises a rotating shaft 41, a pinion 42, a gearwheel 43, a gear shaft 44, a generator 45, a connecting disc 46, a signal lamp 47, a supporting frame 48 and blades 49; the rotating shaft 41 is arranged at the longitudinal center inside the machine body 1, and the upper end of the rotating shaft 41 penetrates through the machine body 1; a pinion gear 42 is arranged at the middle lower end of the rotating shaft 41; a large gear 43 is arranged on one side of the small gear 42, and the large gear 43 is matched with the small gear 42 for use; a gear shaft 44 is arranged at the center of the large gear 43, and the gear shaft 44 is connected with a generator 45; a connecting disc 46 is arranged at the top end of the rotating shaft 41; a signal lamp 47 is arranged at the top end of the connecting disc 46; a support frame 48 is arranged on the side surface of the connecting disc 46; the blades 49 are arranged on the outer side of the support frame 48, when the blades 49 are driven by outside wind to rotate, the rotating shaft 41 can be driven to rotate, at the moment, the rotating shaft 41 drives the small gear 42 to rotate, the small gear 42 drives the large gear 43 to rotate, and finally the generator 45 is driven to rotate to generate electricity.
Further, the electromagnetic power generating device 11 includes a positive electrode iron 111 and a negative electrode iron 112; the positive electrode iron 111 and the negative electrode iron 112 are respectively arranged at two sides of the rotating shaft 9 and the rotating shaft 41, and when the rotating shaft 9 and the rotating shaft 41 rotate, the cutting magnetic induction line motion is performed, and electricity can be generated at the moment; and the positive electrode 111 and the negative electrode 112 are connected by wires, respectively, and the ends of the wires are connected to the external storage battery 12, so that the generated points are transferred to the external storage battery for storage.
Further, the transparent glass 6 is tempered glass, so that the solar power generation panel 5 is protected conveniently.
Further, the radial arm 7 is movably connected with the machine body 1 through a bolt.
Further, the device also comprises an inflatable bag 2 and a photographic device 3; the inflatable bag 2 is arranged at the bottom end of the machine body 1 and is connected with the machine body 1 through threads; the photographic device 3 is arranged between the machine body 1 and the inflatable bag 2, and the photographic device 3 is fixed in the middle of the bottom end of the machine body 1.
Further, the inflatable bag 2 comprises an outer bag skin 21, an inner bag skin 22, an inflatable cavity 23, a photographing window 24, an inflating nozzle 25, a valve 26 and a connecting part 27; the outer bag skin 21 is spherical cambered surface shape, the outer bag skin 21 is connected with the inner bag skin 22, an inflation cavity 23 is formed between the outer bag skin 21 and the inner bag skin 22, the inflation cavity 23 is of a hollow structure, the inflation cavity 23 is connected with external air through an inflation tube 25, the inflation tube 25 penetrates through the outer bag skin 21 and is communicated with the inflation cavity 23, the end part of the inflation tube 25 is provided with a valve 26, the upper joint of the outer bag skin 21 and the inner bag skin 22 is provided with a connecting part 27, the connecting part 27 is in threaded connection with the bottom end of the side face of the machine body 1, the two sides of the bottom end of the inflation bag 2 are provided with the photographing windows 24, and the photographing windows 24 are matched with the photographing device 3. The method simplifies the connecting and fixing steps of the inflatable bag 2 and the machine body 1, and the inflatable bag 2 and the machine body 1 are not easy to fall off after being fixed.
Further, the outer bag skin 21 and the inner bag skin 22 are made of PU plastic materials.
Further, the photographing device 3 includes a connecting rod 31, a joint 32, an auxiliary link 33, and a camera 34; a connecting rod 31 is arranged in the middle of the bottom end of the machine body 1; a joint part 32 is provided at the bottom end of the connecting rod 31, an auxiliary link 33 is connected to the joint part 32, and a camera 34 is provided at the rear end of the auxiliary link 33.
Further, the joint part 32 includes a joint groove 321 and a rotary ball 322, the joint groove 321 is a hollow spherical shape, the joint groove 321 is opened at the bottom end of the connecting rod 31, the rotary ball 322 is arranged in the joint groove 321 in a matching manner, the rotary ball 322 is a spherical shape, and one side of the bottom end of the rotary ball 322 is fixedly connected with the auxiliary connecting rod 33.
The unmanned aerial vehicle has stronger cruising ability, avoids damage caused by external impact on the unmanned aerial vehicle, the inflatable bag 2 can reduce the self weight of the unmanned aerial vehicle, thereby increasing the cruising ability of the unmanned aerial vehicle, in addition, the arrangement of the inflatable bag 2 can protect the unmanned aerial vehicle from being influenced by external force, the unmanned aerial vehicle is prevented from being damaged by external impact, and meanwhile, the detachable connection of the unmanned aerial vehicle body and the inflatable bag 2 increases the flexibility of the whole use of the unmanned aerial vehicle.
It should be understood that the above-mentioned embodiments of the present invention are only examples for clearly illustrating the present invention, and are not intended to limit the embodiments of the present invention, and it will be obvious to those skilled in the art that other variations or modifications may be made on the basis of the above description, and all embodiments may not be exhaustive, and all obvious variations or modifications may be included within the scope of the present invention.

Claims (10)

1. The utility model provides a foldable all-wing aircraft formula unmanned aerial vehicle that has high continuation of the journey function which characterized in that includes: the device comprises a machine body, a rotary power generation device, a solar power generation plate, transparent glass, a rotary arm, a rotor motor, a rotating shaft, a rotor, an electromagnetic power generation device, an external storage battery, a reverse electric appliance and a storage battery; a rotary power generation device is arranged at the center of the interior of the machine body; a storage battery is arranged on the left side inside the machine body; an external storage battery is arranged on the right side of the machine body, the external storage battery is connected with the storage battery through a wire, and a reverse electric appliance is arranged at the position of the wire of the external storage battery; the rotary power generation device is connected with an external storage battery through a wire; a rotary arm is arranged at the upper end of the side surface of the machine body; a rotor motor is arranged at the bottom end of the spiral arm; a rotating shaft is arranged at the upper end of the rotor motor and penetrates through the swing arm; a rotor wing is arranged at the upper end of the rotating shaft; the solar power generation panel is arranged at the upper end of the machine body and is connected with the external storage battery through a wire; transparent glass is arranged at the upper end of the solar power generation panel; the electromagnetic power generation device is arranged around the rotating part of the device and is connected with an external storage battery through a wire.
2. The folding flying-wing unmanned aerial vehicle with high endurance function of claim 1, wherein the rotary power generation device comprises a rotating shaft, a pinion, a gearwheel, a gear shaft, a generator, a connecting disc, a signal lamp, a supporting frame and a blade; the rotating shaft is arranged at the longitudinal center inside the machine body, and the upper end of the rotating shaft penetrates through the machine body; a pinion is arranged at the middle lower end of the rotating shaft; a bull gear is arranged on one side of the pinion, and the bull gear is matched with the pinion for use; a gear shaft is arranged in the center of the large gear and is connected with a generator; a connecting disc is arranged at the top end of the rotating shaft; a signal lamp is arranged at the top end of the connecting disc; a support frame is arranged on the side surface of the connecting disc; and blades are arranged on the outer side of the support frame.
3. The foldable flying wing type unmanned aerial vehicle with high endurance function of claim 1, wherein the electromagnetic power generation device comprises a positive electrode iron and a negative electrode iron; the positive electrode iron and the negative electrode iron are respectively arranged on two sides of the rotating shaft and the rotating shaft, the positive electrode and the negative electrode are respectively connected through wires, and the tail ends of the wires are connected to an external storage battery.
4. The foldable flying wing type unmanned aerial vehicle with high cruising ability according to claim 1, wherein the transparent glass is tempered glass.
5. The foldable flying wing type unmanned aerial vehicle with high endurance function of claim 1, wherein the swing arm is movably connected with the body through a bolt.
6. The foldable flying wing type unmanned aerial vehicle with high endurance function of claim 1, further comprising an inflatable bag and a camera device; the inflatable bag is arranged at the bottom end of the machine body and is connected with the machine body through threads; the photographic device is arranged between the machine body and the inflatable bag and is fixed in the middle of the bottom end of the machine body.
7. The foldable flying wing type unmanned aerial vehicle with high endurance function of claim 6, wherein the inflatable bag comprises an outer bag skin, an inner bag skin, an inflatable cavity photography window, an inflation nozzle, a valve and a connecting part; the outer bag skin is spherical cambered surface form, and outer bag skin is connected with the inner bag skin, forms the inflation chamber between outer bag skin and the inner bag skin, and the inflation chamber is hollow structure, and the inflation chamber passes through the gas tube and inserts external gas, and the gas tube passes outer bag skin and is linked together with the inflation chamber, and the inflation tube tip sets up the valve, and the upper portion handing-over department of outer bag skin and inner bag skin sets up connecting portion, and threaded connection between connecting portion and the organism side bottom, sets up the photographic window in the bottom both sides of gas tube, and photographic window and photographic arrangement cooperate the application.
8. The foldable flying wing type unmanned aerial vehicle with high endurance function of claim 7, wherein the outer bag skin and the inner bag skin are made of PU plastic material.
9. The foldable flying wing drone with high endurance function according to claim 6, wherein said camera device comprises a connecting rod, a joint, an auxiliary connecting rod and a camera; a connecting rod is arranged in the middle of the bottom end of the machine body; the bottom end of the connecting rod is provided with a joint part; the auxiliary connecting rod is connected with the joint part; and a camera is arranged at the rear end of the auxiliary connecting rod.
10. The foldable flying wing type unmanned aerial vehicle with high endurance function of claim 9, wherein the joint portion comprises a joint groove and a rotary ball, the joint groove is hollow and spherical, the joint groove is opened at the bottom end of the connecting rod, the rotary ball is arranged in the joint groove in a matching manner, the rotary ball is spherical, and one side of the bottom end of the rotary ball is fixedly connected with the auxiliary connecting rod.
CN202010940527.8A 2020-09-09 2020-09-09 Foldable flying wing formula unmanned aerial vehicle that has high continuation of journey function Pending CN112009686A (en)

Priority Applications (1)

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CN202010940527.8A CN112009686A (en) 2020-09-09 2020-09-09 Foldable flying wing formula unmanned aerial vehicle that has high continuation of journey function

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20120068131A (en) * 2010-12-17 2012-06-27 한국항공우주연구원 Long endurance wind aircraft
KR20130054805A (en) * 2011-11-17 2013-05-27 재단법인대구경북과학기술원 Flying robots with flight angle control function based on solar cells
CN108839793A (en) * 2018-05-31 2018-11-20 智飞智能装备科技东台有限公司 A kind of continue a journey for unmanned plane increases the generating equipment of journey
CN110884657A (en) * 2018-12-21 2020-03-17 苏州律点信息科技有限公司 Unmanned aerial vehicle power control system
CN111056027A (en) * 2019-12-28 2020-04-24 河南省科宇信息技术有限公司 High-endurance anti-collision monitoring inspection unmanned aerial vehicle

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20120068131A (en) * 2010-12-17 2012-06-27 한국항공우주연구원 Long endurance wind aircraft
KR20130054805A (en) * 2011-11-17 2013-05-27 재단법인대구경북과학기술원 Flying robots with flight angle control function based on solar cells
CN108839793A (en) * 2018-05-31 2018-11-20 智飞智能装备科技东台有限公司 A kind of continue a journey for unmanned plane increases the generating equipment of journey
CN110884657A (en) * 2018-12-21 2020-03-17 苏州律点信息科技有限公司 Unmanned aerial vehicle power control system
CN111056027A (en) * 2019-12-28 2020-04-24 河南省科宇信息技术有限公司 High-endurance anti-collision monitoring inspection unmanned aerial vehicle

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