CN106218849A - Aerial wind energy power station formula aircraft and aerial fixing aircraft device - Google Patents
Aerial wind energy power station formula aircraft and aerial fixing aircraft device Download PDFInfo
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- CN106218849A CN106218849A CN201610218029.6A CN201610218029A CN106218849A CN 106218849 A CN106218849 A CN 106218849A CN 201610218029 A CN201610218029 A CN 201610218029A CN 106218849 A CN106218849 A CN 106218849A
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/66—Mooring attachments
-
- 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
- B64C39/026—Aircraft not otherwise provided for characterised by special use for use as personal propulsion unit
-
- 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
-
- 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
-
- 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
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Power Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Wind Motors (AREA)
Abstract
Aerial wind energy power station formula aircraft relate to Electric aircraft manufacture, aerial wind-powered electricity generation and photoelectricity, ship in the air, the field of engineering technology such as military.It includes aircraft (1) or buoyance lift body (20), control system (4), advances propulsion system (5)；Feature is: aerial wind energy aircraft also includes aerial wind power generating system (2), the savings system (3) of dynamic power, ground connection collecting system of water (6)；Wherein power propulsion system (5) includes electric propulsion flight system (5.1).After ground connection collecting system of water (6) connection ground is easily connected object (12), fixes aircraft device (13), water body (14) in the air, it is at resting state, just can carry out aerial wind-power electricity generation.Aerial wind-powered electricity generation resupplies electric propulsion flight system (5.1) after being full of the savings system (3) of dynamic power and uses, and drives flight.It has reached to consume a fuel and utilize " aerial wind energy, wind-powered electricity generation " to realize air objective.Its cost is the lowest, and it is by the savings system (3) of dynamic power or fixes aircraft device (13) in the air, also aerial wind-powered electricity generation extremely low for cost can be transported to ground and use.
Description
Technical field
The present invention relates to Electric aircraft manufacture, aerial wind-power electricity generation, aerial photovoltaic generation, air traffic transport, aerial
The field of engineering technology such as mobile house, military airlift equipment, military field generating equipment.
Background technology
There is problems with in existing aircraft.1, existing aircraft major part is all dependent on airport landing, it is impossible to
Enough Vertical Free landings.2, the air mileage of the helicopter of existing VTOL is short, speed is the slowest.3, existing aircraft
Dangerous, as long as aloft having an accident, it is possible to cause and fall.4, existing aircraft cost is high, manipulate complexity again, limits
It commonly use in a large number；Easily family, private daily field is extensively entered not as automobile.5, existing aircraft
Only as vehicles one function, do not increase the function as aerial electric station.6, existing aircraft is merely able to stop
It is placed on ground, it is impossible to be enough parked in aerial.7, the superior structural of electric paramotor the most fully developed by existing aircraft.
There is problems with in existing electric airplane, the most fully develops high-altitude wind power generation.Existing electronic fly
Machine must rely on photovoltaic generation, ground charging, change these 3 kinds of modes of accumulator to obtain flight driving electric.Or must depend on
Lean against surface wind generating and supplement flight driving electric.The Helicopter Corporation AgustaWestland such as being anticipated joint by English sends out
Bright, entitled Project Zero's, the all-electric tilt rotor aircraft of the first in the world platform.Project Zero aircraft is merely capable of
Carry out wind-power electricity generation charging simple, on ground.When Project Zero aircraft rests in ground, it can be according to wind
To, adjust the angle of inclination of wing, utilize wind-power electricity generation.But high-altitude wind power generation amount is several times of surface wind generated energy,
Tens times, hundreds of times.Therefore electric airplane the most fully develops high-altitude wind power generation.
Existing electric airplane is only used as vehicles one function, does not increase as aerial wind power station, aerial
The function of photo-voltaic power generation station.When not flight, electric airplane can as aerial wind power station, aerial wind power station, to
Ground, the aerial clean electric power exporting unnecessary (after accumulator is fully charged).
There is problems with in existing propeller-parachuting.1, existing propeller-parachuting all relies solely on lifting flight, the most fully profit
Replace lift with buoyancy, in order to reduce lift power consumption, save fuel energy.2, existing propeller-parachuting is all consumable liquid fuel
, do not make full use of solar electric power.3, existing propeller-parachuting major part is all Horizontal Take-off and Landing, it is impossible to enough Vertical Frees rise
Fall.4, existing propeller-parachuting is dangerous, as long as aloft having an accident, it is possible to cause and fall.
Existing dirigible relies solely on huge floatage air bag flight, and the flight resistance of floatage air bag is the biggest；It does not set
Put wing, make full use of the lift of wing to replace part buoyancy, in order to reduce the volume of floatage air bag, reach to reduce flight resistance
The purpose of power；Reduce flight resistance and just decrease flight power consumption, save fuel energy.
There is problems with in existing aerial photovoltaic power generation apparatus.Do not increase and wind power generation plant is set.Due to
Skyborne wind power generation plant is not affected by any ground surface or terrain and is added wind-power electricity generation amount, therefore aerial wind-power electricity generation
The wind-power electricity generation amount that device is increased is more than 2-10 times of ground.Therefore, the wind-force that aerial wind power generation plant is increased
Generated energy likely equals to or more than the photovoltaic power generation quantity of the aerial photovoltaic power generation apparatus of several times to tens times, is equivalent to sky
In photovoltaic power generation apparatus additionally increase the photovoltaic power generation quantity of several times to more than tens times, its benefit is more considerable.
There is problems with in existing aerial wind power generating set.Do not increase and Airlift Flight device function is set.Existing
Aerial wind power generating set only as aerial wind power station one function, do not increase the aircraft as the vehicles
Function.
Existing aerial wind power generation plant there is problems.Do not increase and photovoltaic power generation apparatus is set.By
Do not affected by any Near Ground weather in skyborne photovoltaic power generation apparatus and added photovoltaic power generation quantity, simultaneously because empty
The extremely low photovoltaic power generation quantity that too increases of middle temperature, therefore the photovoltaic power generation quantity that aerial photovoltaic power generation apparatus is increased is the 1 of ground
More than Bei.Therefore, the photovoltaic power generation quantity that aerial photovoltaic power generation apparatus is increased likely equal to or more than 20% aerial
The wind-power electricity generation amount of wind power generation plant, be equivalent to aerial wind power generation plant and additionally increase by the wind-power electricity generation of more than 20%
Amount, its benefit is considerable.
Existing aerial photovoltaic and wind-power combined generating device, such as CN104806451A-float on the generating in high-altitude
, there is problems with in equipment patent.1, owing to not using aerial fixing aircraft device (13), self is entrained outer defeated
Electric wire, mooring line rope are canceled, cause aerial photovoltaic power generation apparatus from great, efficiency is low, cost is high, can not use flexibly.
2, owing to being not provided with hectare rotation mechanism of propulsion system, becoming pitch mechanism, make the aerial wind power generating system can not tuning, tune
Speed, efficiency is low, cost is high.3, owing to aerial wind power generating system not being arranged on two sides of buoyance lift system system, sky is made
Middle photovoltaic generating system space structure is unstable.4, owing to not using hoist cable group's system of adjustable in length that buoyance lift system is united
Separating with aerial wind power generating system, the center of gravity causing the generating equipment floating on high-altitude is the highest, and overall structure is unstable, easily
Being turned over by high wind, entirety is toppled.5, owing to not using hoist cable group's system of adjustable in length buoyance lift system system and aerial wind
Force generating system separates, and causes aerial photovoltaic power generation apparatus cannot adjust attitude, makes solar panel cannot follow the tracks of sunlight,
Photoelectric conversion rate cannot be improved.6, the least due to aerial wind power generating system diameter, cause generated output the least.
Summary of the invention
The purpose of the invention is contemplated to overcome above-mentioned existing shortcoming, it is provided that a kind of aerial wind energy power station formula aircraft
With aerial fixing aircraft device.The purpose of the present invention can reach by taking following measure.
Content 1.
Aerial wind energy power station formula aircraft includes aircraft (1), and its aircraft (1) includes buoyance lift body (20), controls
System (4), power propulsion system (5)；Or aerial wind energy power station formula aircraft include buoyance lift body (20), control system (4),
Power propulsion system (5)；It is characterized in that:
Aerial wind energy power station formula aircraft also includes aerial wind power generating system (2), the savings system of dynamic power
(3), ground connection collecting system of water (6)；
Power propulsion system therein (5) includes electric propulsion flight system (5.1)；
Wherein aerial wind power generating system (2) is arranged on following at least one of which kind alliance and is attached thereto,
Aircraft (1) or buoyance lift body (20), the savings system (3) of dynamic power, control system (4), power propulsion system (5), electricity push away
Enter flight system (5.1), ground connection collecting system of water (6)；The wherein following at least a part of which of circuit communication of aerial wind power generating system (2)
One of plant the circuit of system, aircraft (1) or buoyance lift body (20), the savings system (3) of dynamic power, control system (4), electricity push away
Enter flight system (5.1), ground connection collecting system of water (6)；
Wherein the savings system (3) of dynamic power is arranged on following at least one of which kind position and is attached thereto, and flies
Row device (1) or buoyance lift body (20), aerial wind power generating system (2), control system (4), power propulsion system (5), electric propulsion fly
Row system (5.1), ground connection collecting system of water (6)；Wherein the following at least a part of which of circuit communication of the savings system (3) of dynamic power it
The circuit of a kind of system, aircraft (1) or buoyance lift body (20), aerial wind power generating system (2), control system (4), electric propulsion fly
Row system (5.1), ground connection collecting system of water (6)；
Wherein ground connection collecting system of water (6) is arranged on following at least one of which kind alliance and ground connection collecting system of water
(6) one end is attached thereto, aircraft (1) or buoyance lift body (20), aerial wind power generating system (2), the savings system of dynamic power
System (3), control system (4), power propulsion system (5), electric propulsion flight system (5.1)；When needing, ground connection collecting system of water (6)
The other end can at any time with following at least one of which kind object dock after realize being connected, ground is easily connected object
(12) aircraft device (13), water body (14), are fixed in the air；Wherein ground connection collecting system of water (6) is the aerial fixing flight connected
Device device (13) connect sky mechanical splice system (41)；It can be trees, roofbolt body, hole that its ground is easily connected object (12)
The most connected object on body etc. ground.
Easily it is connected object (12) owing to ground connection collecting system of water (6) can connect ground after docking, consolidates in the air
Determine aircraft device (13)；Thus aerial wind energy power station formula aircraft can be fixed or mooring is easily connected thing to ground
Body (12), in the air fix aircraft device (13) upper time, make aerial wind energy power station formula aircraft not fly away, allow aerial wind-force send out
Electricity system (2) can enter aerial wind-power electricity generation state.
Or when its aerial wind energy power station formula aircraft flight is to position, water surface sea, connecing of its ground connection collecting system of water (6)
The other end of water mechanism (6.7) can discharge in water body (14)；Owing to water receiving mechanism (6.7) forms resistance in water body (14)
Water body, its resistance is very big, greatly reduces " aerial wind energy power station formula aircraft " downwind speed, makes " aerial wind energy electricity
Standing posture aircraft " downwind speed less than wind speed；Owing to wind speed is more than downwind speed, create " a wind speed
Difference "；This " wind speed is poor " can make the aerial wind power generating system (2) of " aerial wind energy power station formula aircraft " can enter generating
State；Therefore, the high altitude wind energy electric power on water surface sea also can be full of the savings system (3) of dynamic power, the most again to electricity
Flight system (5.1) is advanced to provide electric power for flying power；As marine sailing boat can be inverse by "the" shape route
The front course line of wind direction is the same, and " aerial wind energy power station formula aircraft " can also increase wind by "the" shape route flight forward against the wind
Speed, increases the generated energy of aerial wind power generating system (2).
This high altitude wind energy electric power can be full of the savings system (3) (such as accumulator) of dynamic power, then aerial wind
Power station formula aircraft flight can drop to ground.The savings system (3) of its dynamic power can use earthward as power supply source
Electricity facility, equipment provide electric power.One, savings system (3) directly electricity consumption facility, the equipment the most earthward of dynamic power provide electricity
Power.Two, unload the savings system (3) of the dynamic power of full electricity, load the savings system (3) without electric dynamic power, and empty
Middle wind energy power station formula aircraft again flies and returns to enter aerial wind-power electricity generation state in the air, and high altitude wind energy electric power is continued to be full of
Savings system (3) without the dynamic power of electricity.Meanwhile, the savings system (3) of dynamic power of full electricity is unloaded directly the most earthward
Electricity consumption facility, equipment provide electric power.At this moment, this aerial wind energy power station formula aircraft is exactly a small-sized " aerial wind-power electricity generation
Stand ".
Or after this high altitude wind energy electric power is full of the savings system (3) of dynamic power, fly to electric propulsion the most again
System (5.1) provides electric power as the main source of flying power.From this, reach to make aircraft just can consume one
Fuel, utilizes " aerial wind energy, wind-powered electricity generation " to realize the purpose of free flight transport.At this moment, this aerial wind energy power station formula flight
Device is exactly a frame " aerial wind energy aircraft ".
If being further added by the photovoltaic electric power supplementary source as flying power of aerial photovoltaic generating system (11), auxiliary
Source.Add under conditions of making full use of high-altitude radiated solar energy unobstructed, high, carry out the light at full capacity of large area buoyance lift body
Volt generating.Therefore, " aerial wind-powered electricity generation, aerial photoelectricity " just can fully meet the thrust power demand of aircraft, or the fullest
Foot heating ammonia (19), water etc. steam becomes the electricity needs (its vapours can be as buoyant gas) of the vapours of high temperature.
So aerial wind energy power station formula aircraft is achieved that: need not consume under fuel condition, is utilizing " aerial wind-powered electricity generation, aerial light
Electricity " just can carry out timeless flight, utilize solar energy just can carry out the VTOL limited without number of times.If
The aircraft of propeller-parachuting form, its performance more preferably, cost performance higher.
Content 2.
Supporting with the aerial wind energy power station formula aircraft described in content 1 dock the aerial fixing aircraft device share
(13), it is characterised in that:
Aerial fixing aircraft device (13) includes components described below, vertical mooring fixed system (30), earth anchor system
(36)；
Its vertical mooring fixed system (30) includes following at least one of which kind parts, vertical mooring mast (31), floating
Power system system (33)；Its vertical mooring fixed system (30) also includes following at least one of which kind parts, vertical mooring guy
Rope (34), vertical power transmission cable (37), location cable systems (44)；
Vertical mooring mast (31) therein can suspend or carry following at least one of which kind parts, buoyancy system in midair
System (33), vertical mooring guy rope (34), vertical power transmission cable (37), location cable systems (44)；And vertical mooring mast (31)
Upper end be connected to the upper end of following at least one of which kind parts, floatage body system (33), vertical mooring guy rope (34), vertical
Power transmission cable (37), location cable systems (44)；
Floatage body system (33) therein can suspend or carry following at least one of which kind parts, vertical mooring in midair
Bar (31), vertical mooring guy rope (34), vertical power transmission cable (37), location cable systems (44)；And floatage body system (33)
It is connected to the upper end of following at least one of which kind parts, vertical mooring mast (31), vertical mooring guy rope (34), vertical power transmission line
Cable (37), location cable systems (44)；Its vertical mooring mast (31) or vertically mooring guy rope (34) or vertical power transmission cable (37)
Or the upper end of location cable systems (44) is arranged on the following at least one of which kind position of floatage body system (33), top, on
Portion, middle part, bottom；
The upper end of vertical mooring guy rope (34) therein is connected to following at least one of which kind parts, floatage body system
(33), the top of vertical mooring mast (31), vertical power transmission cable (37)；The lower end of vertical mooring guy rope (34) therein connects ground
Anchor system (36)；
The upper end of vertical power transmission cable (37) therein is connected to following at least one of which kind parts, floatage body system
(33), the top of vertical mooring mast (31), the top of vertical mooring guy rope (34)；The circuit lower end of vertical power transmission cable (37) is even
Logical external electrical network or external electric energy savings device；Sky is connect electrically owing to the upper circuit of vertical power transmission cable (37) can connect
The circuit of docking system (40), connecing empty electrically docking system (40) just can be with the connecing of aerial aerial wind energy power station formula aircraft
Connect after ground connection plug mechanism (6.6) docking on ground collecting system of water (6) and realize circuit communication；
Location therein cable systems (44) includes at least 3 vertical mooring guy ropes (34) or vertical power transmission cable (37)
Composition, location cable systems (44) makes vertical mooring mast (31) or the floatage body system (33) can not occurred level displacement；Because
Vertical power transmission cable (37) can also be a kind of vertical mooring guy rope (34), thus vertical power transmission cable (37) also have mooring and
The function of fixing airborne aircraft；
Its earth anchor system (36) is connected to the lower end of following at least one of which kind parts, vertical mooring mast (31), vertical
Mooring guy rope (34), vertical power transmission cable (37), location cable systems (44).In the air fixing aircraft device (13) can be for it
Aerial wind energy power station formula aircraft is fixed or mooring, it is impossible to flies away, allows aerial wind power generating system (2) can enter generating shape
State；" aerial wind energy, wind-powered electricity generation " is utilized to be full of the savings system (3) of dynamic power.The most again to electric propulsion flight system (5.1)
There is provided electric power as the main source of flying power, reached to make aircraft just need not consume fuel and realized free flight transport
Purpose.
The purpose of the invention can also reach by taking following measure.
Content 3.
According to the aerial wind energy power station formula aircraft described in content 1, also include following characteristics:
Its aircraft (1) or buoyance lift body (20) connect following at least one of which kind system, aerial wind power generating system
(2), the savings system (3) of dynamic power, control system (4), electric propulsion flight system (5.1), ground connection collecting system of water (6)；Its
Aircraft (1) includes buoyance lift body (20)；
The circuit of the circuit communication following at least one of which kind system of its control system (4), aircraft (1) or buoyance lift body
(20), aerial wind power generating system (2), the savings system (3) of dynamic power, power propulsion system (5), electric propulsion flight system
(5.1), ground connection collecting system of water (6)；
Its power propulsion system (5) or electric propulsion flight system (5.1) connect following at least one of which kind system, fly
Row device (1) or buoyance lift body (20), aerial wind power generating system (2), the savings system (3) of dynamic power, control system (4), connect
Ground collecting system of water (6)；The electricity of the circuit communication following at least one of which kind system of electric propulsion flight system (5.1) therein
Road, aerial wind power generating system (2), the savings system (3) of dynamic power, control system (4), ground connection collecting system of water (6).
Content 4.
According to the aerial wind energy power station formula aircraft described in content 1, also include following characteristics:
Its aerial wind power generating system (2) includes following at least one of which kind parts, blade (21), electromotor
(22)；Its aerial wind power generating system (2) also includes following at least one of which kind mechanism, speed adjusting gear (23), becomes pitch
Mechanism (24), blade fold mechanism (25), flight advance generating function changing-over mechanism (26), guard ring or duct mechanism (27), hectare
Transfer from one department to another to unite (9)；Wherein become pitch mechanism (24), blade fold mechanism (25) can change blade (21) towards or windward side
Long-pending, reduce flight resistance, improve wind-power electricity generation amount；
The savings system (3) of its dynamic power includes following at least one of which kind parts, accumulator (3.1), electric capacity
(3.2), fuel cell (3.3), point distribution system (3.4)；The savings system (3) of its dynamic power is arranged on following at least a part of which
One position and be attached thereto, aircraft (1) or buoyance lift body (20), aerial wind power generating system (2), control system (4),
Power propulsion system (5), electric propulsion flight system (5.1), ground connection collecting system of water (6)；
Its ground connection collecting system of water (6) includes following at least one of which kind parts, butt joint mechanism (6.1), water receiving machine
Structure (6.7)；One end of its butt joint mechanism (6.1) or water receiving mechanism (6.7) connects following at least one of which kind system, flies
Row device (1) or buoyance lift body (20), aerial wind power generating system (2), the savings system (3) of dynamic power, control system (4), dynamic
Power propulsion system (5), electric propulsion flight system (5.1)；
Its aerial wind energy power station formula aircraft flight is easily connected object (12), fixes aircraft device in the air to ground
(13) in when connecing sky mechanical splice system (41) position, the other end of butt joint mechanism (6.1) can dock and connect even afterwards
Logical ground is easily connected object (12), fixes aircraft device (13) in the air；Wherein the other end of butt joint mechanism (6.1) is permissible
Connect aerial fixing aircraft device (13) connects sky mechanical splice system (41)；So can be " aerial wind energy power station
Formula aircraft " fixing or mooring is easily connected object (12), fixes on aircraft device (13) in the air, make " in the air to ground
Wind energy power station formula aircraft " can not fly away, allow aerial wind power generating system (2) that generating state can be entered；This high altitude wind energy
Electric power can provide electric power to be used for flying to electric propulsion flight system (5.1) after the savings system (3) of full dynamic power
Power；
Or when its aerial wind energy power station formula aircraft flight is to position, water surface sea, another of its water receiving mechanism (6.7)
End can discharge in water body (14)；Owing to water receiving mechanism (6.7) forms the body that blocks water in water body (14), its resistance is very
Greatly, greatly reduce the downwind speed of " aerial wind energy power station formula aircraft ", make " aerial wind energy power station formula aircraft "
Downwind speed is less than wind speed；Owing to wind speed is more than downwind speed, create one " wind speed is poor "；This " wind speed is poor "
The aerial wind power generating system (2) that can make " aerial wind energy power station formula aircraft " can enter generating state；Therefore, at the water surface
High altitude wind energy electric power on sea can also be full of the savings system (3) of dynamic power, the most again to electric propulsion flight system
(5.1) provide electric power for flying power；As marine sailing boat can be by the upwind front course line one of "the" shape route
Sample, " aerial wind energy power station formula aircraft " can also be increased wind speed by "the" shape route flight forward against the wind, increased aerial wind
The generated energy of force generating system (2)；
Its butt joint mechanism (6.1) includes following at least one of which kind mechanism, staple joint mechanism (6.1.1), expands
Swollen joint mechanism (6.1.2), ejection joint mechanism (6.1.3), magetic indicator joint mechanism (6.1.4)；Its water receiving mechanism (6.7) includes
There is a following at least one of which kind mechanism, umbrella shape water receiving mechanism (6.7.1), barrel-shaped water receiving mechanism (6.7.2), Fan Xing water receiving mechanism
(6.7.3)；Water receiving mechanism (6.7) includes thin-film body (6.7.5)；Thin-film body (6.7.5) constitutes umbrella shape, barrel-shaped, sail form drag water
Body；
The circuit of its ground connection collecting system of water (6) circuit communication following at least one of which kind system, aircraft (1) or buoyance lift
Body (20), aerial wind power generating system (2), the savings system (3) of dynamic power, control system (4), power propulsion system (5),
Electric propulsion flight system (5.1).
Content 5.
According to the aerial wind energy power station formula aircraft described in content 1, also include following characteristics:
Aircraft (1) or buoyance lift body (20) also include following at least one of which kind system, and its buoyance lift body (20) wraps
Following at least one of which kind parts, floatage body (21), lifting body (22), rotor (23), buoyancy lift assembly (24) are included；Floating
The front end rising body (20) presents following at least one of which kind shape, close-shaped, opening shape；The front end of its buoyance lift body (20)
Presenting opening shape is lifting body (22)；
Floatage body (21) wherein includes following at least one of which kind portion body, buoyant gas (21.5), floatage air bag
(21.6), internal portioning layer (21.7), heat-insulation layer (21.8), balloonet system (21.9), air-pump inflating system (21.10)；Its buoyancy
Air bag (21.6) includes buoyant gas (21.5)；The density of buoyant gas (21.5) is less than aircraft outer air density；Floating
Power body (21) includes following at least one of which kind parts, rigidity floatage body (21.1), flexible buoyancy body (21.2), hard and soft group
Close floatage body (21.3)；Its internal portioning layer (21.7) is arranged on floatage body (21), the inside of floatage air bag (21.6)；Its internal portioning layer
(21.7) floatage body (21), floatage air bag (21.6) these part components can be isolated into multiple cavity；In order to improve them
Rigidity and leakage performance.There is seepage in the buoyant gas (21.5) of one cavity, does not results in the buoyancy gas of other cavity
There is seepage in body (21.5), the buoyant gas (21.5) also not interfering with other cavity normally works, i.e. the buoyancy of other cavity
Do not reduce.
Wherein lifting body (22) includes following at least one of which kind parts, rigidity lifting body (22.1), flexible lift
Body (22.2), hard and soft combination lifting body (22.3)；Lifting body (22) includes following at least one of which kind bodies, aerofoil profile liter
Power body (22.5), sail type lifting body (22.6), umbellate form lifting body (22.7), mixed type lifting body (22.8)；
Hard and soft combination floatage body (21.3) therein or hard and soft combination lifting body (22.3) include following at least a part of which it
A kind of combinative structure form: its top is rigidity floatage body (21.1) or rigidity lifting body (22.1), is rigidity buoyancy in the middle part of it
Body (21.1) or rigidity lifting body (22.1), its underpart are rigidity floatage body (21.1) or rigidity lifting body (22.1), its top
It is flexible buoyancy body (21.2) or flexible lifting body (22.2), is flexible buoyancy body (21.2) or flexible lifting body in the middle part of it
(22.2), its underpart is flexible buoyancy body (21.2) or flexible lifting body (22.2)；
Wherein buoyancy lift assembly (24) includes 2 kinds of parts of following at least a part of which, floatage body (21), lifting body
(22), rotor (23)；
Wherein heat-insulation layer (21.8) is arranged on floatage body (21) or the outside of floatage air bag (21.6) or inside；Insulation
Layer (21.8) reduces buoyant gas (21.5) temperature in floatage body (21) or floatage air bag (21.6) and reduces；
Wherein balloonet system (21.9) is arranged on floatage body (21) or the outside of floatage air bag (21.6) or inside；
Wherein air-pump inflating system (21.10) is for being full of buoyancy in floatage body (21) or floatage air bag (21.6)
The equipment of gas (21.5)；Also it is the equipment for being full of pressure-air to balloonet system (21.9), prevents from leaking buoyancy gas
Body (21.5)；Wherein air-pump inflating system (21.10) has pipeline to be connected in following at least one of which kind parts, floatage body
(21), floatage air bag (21.6), balloonet system (21.9).
Content 6.
According to the aerial wind energy power station formula aircraft described in content 1, also include following characteristics:
Aerial wind energy power station formula aircraft or aircraft (1) or buoyance lift body (20) also include following at least a part of which it
A kind of system, load Load System (7), hoist cable group's system (8) of adjustable in length, transfers from one department to another unite (9), photovoltaic generating system just
(11), cool down or compress storage gas system (15), electric heating system (16), manufacture freshwater system (17), airflight house
System (18)；
Aerial wind energy power station formula aircraft or aircraft (1) or buoyance lift body (20) also include following at least a part of which it
A kind of system, hoist cable group's system (8) of adjustable in length, just transfer from one department to another to unite (9), photovoltaic generating system (11), cools down or compresses and deposit
Storing gas system (15), electric heating system (16)；
Its buoyance lift body (20) and aerial wind power generating system (2) or the savings system (3) of dynamic power or control system (4)
Or hoist cable group's system of power propulsion system (5) or ground connection collecting system of water (6) or load Load System (7) or adjustable in length
(8) connection includes following at least one of which kind mode, is directly connected to, is indirectly connected with；Connection bag when buoyance lift body (20)
Include when being indirectly connected with, its buoyance lift body (20) and aerial wind power generating system (2) or the savings system (3) of dynamic power or control
System (4) or power propulsion system (5) or ground connection collecting system of water (6) or load Load System (7) or the hoist cable of adjustable in length
Include hoist cable group's system (8) of adjustable in length between group's system (8), constitute and be indirectly connected with；
Its control system (4) includes following at least one of which kind system, pilot steering control system (4.1), automatically
Ride Control System (4.2), mixing Ride Control System (4.3)；Its mixing Ride Control System (4.3) includes pilot steering
Control system (4.1) and automatic Pilot control system (4.2)；Its control system (4) is arranged on following at least one of which kind position
Put and be attached thereto, aircraft (1) or buoyance lift body (20), aerial wind power generating system (2), the savings system of dynamic power
(3), hoist cable group's system of power propulsion system (5), ground connection collecting system of water (6), load Load System (7), adjustable in length
(8)；
Its power propulsion system (5) is arranged on following at least one of which kind position, aircraft (1) or buoyance lift body (20),
Load Load System (7), hoist cable group's system (8) of adjustable in length, aerial wind power generating system (2)；Its power propulsion system
(5) also including following at least one of which kind, electric propulsion flight system (5.1), internal combustion engine propulsion system (5.2), jet push away
Enter system (5.4), manual feed system (5.5), hybrid propulsion system (5.6)；Its electric propulsion flight system (5.1) includes
There is a following at least one of which kind, electric propeller propulsion system (5.1.1), electric heating propulsion system (5.1.2), electrostatic push away
Enter system (5.1.3), electromagnetic type propulsion system (5.1.4), electric laser formula propulsion system (5.1.5), electricity microwave type propulsion system
(5.1.6), electric chemical formula propulsion system (5.1.7)；
Wherein hybrid propulsion system (5.6) includes 2 kinds of systems of following at least a part of which, electric propulsion flight system
(5.1), internal combustion engine propulsion system (5.2), jet propulsion system (5.4), manual feed system (5.5)；
Wherein electric propeller propulsion system (5.1.1) includes following at least one of which kind parts, blade (21), sends out
Motor (22)；Its electric propeller propulsion system (5.1.1) also includes following at least one of which kind mechanism, speed adjusting gear
(23), become pitch mechanism (24), blade fold mechanism (25), flight advance generating function changing-over mechanism (26), guard ring or duct
Mechanism (27), just transfer from one department to another unite (9)；Blade therein (21) connects at least one parts following: electromotor (22), become pitch mechanism
(24), blade fold mechanism (25), flight advance generating function changing-over mechanism (26)；
Its load Load System (7) is arranged on following at least one of which kind position and is attached thereto, aircraft (1) or
Buoyance lift body (20), aerial wind power generating system (2), the savings system (3) of dynamic power, control system (4), power propulsion system
(5), ground connection collecting system of water (6), hoist cable group's system (8) of adjustable in length, photovoltaic generating system (11)；Load Load System
(7) it is used for accommodating, loading personnel's goods；
Its load Load System (7) and aircraft (1) or buoyance lift body (20) or aerial wind power generating system (2) or power current
Can savings system (3) or control system (4) or power propulsion system (5) or ground connection collecting system of water (6) or load Load System
(7) or the connection of hoist cable group's system (8) of adjustable in length includes following at least one of which kind mode, be directly connected to,
Connect in succession；When the connection of load Load System (7) include be indirectly connected with time, its load Load System (7) is sent out with aerial wind-force
Electricity system (2) or the savings system (3) of dynamic power or control system (4) or power propulsion system (5) or ground connection collecting system of water
(6) or include hoist cable group's system (8) of adjustable in length between hoist cable group's system (8) of adjustable in length, constitute indirectly
Connect；
Hoist cable group's system (8) of its adjustable in length includes hoist cable (8.1), hoist cable group's system of its adjustable in length
(8) following at least one of which kind mechanism, electric rolling rope mechanism (8.2), manual Juan Suo mechanism (8.3) are also included；Part is hung
Rope (8.1) is wrapped in the wire drum of electric rolling rope mechanism (8.2) or manual Juan Suo mechanism (8.3), or the one of hoist cable (8.1)
It is partially around in the wire drum of electric rolling rope mechanism (8.2) or manual Juan Suo mechanism (8.3)；When load Load System (7) with
The savings system (3) of aircraft (1) or aerial wind power generating system (2) or dynamic power or power propulsion system (5) or ground connection
The connection of collecting system of water (6) includes when being indirectly connected with, and aerial wind energy power station formula aircraft also includes hanging of adjustable in length
Suo Qun system (8)；Its load Load System (7) and aircraft (1) or buoyance lift body (20) or aerial wind power generating system (2) or dynamic
Adjustable in length is included between the savings system (3) of power electric energy or power propulsion system (5) or ground connection collecting system of water (6)
Hoist cable group's system (8), constitutes and is indirectly connected with；
By regulation hoist cable length mode, hoist cable group's system (8) of adjustable in length can be with change of flight device (1) or buoyance lift
Body (20), aerial wind power generating system (2), the savings system (3) of dynamic power, power propulsion system (5), ground connection collecting system of water
(6), load Load System (7), photovoltaic generating system (11) etc. system towards, direction, be allowed to beneficially aircraft landing,
Reduce flight resistance, improve wind-force or photovoltaic power generation quantity etc. efficiency；Hoist cable group's system (8) of adjustable in length even can change
Become aircraft (1) or buoyance lift body (20) towards, direction, make aerial wind energy power station formula aircraft flight forward against the wind；This as
Marine sailing boat can be by the upwind front course line of "the" shape route, and " aerial wind energy power station formula aircraft " can also be by
"the" shape route flight forward against the wind, increases wind speed, increases the generated energy of aerial wind power generating system (2)；
Its hectare transfers from one department to another system (9) and is arranged on following at least one of which kind position and is attached thereto, aircraft (1) or buoyance lift
Body (20), aerial wind power generating system (2), the savings system (3) of dynamic power, power propulsion system (5), ground connection collecting system of water
(6), load Load System (7), hoist cable group's system (8) of adjustable in length, photovoltaic generating system (11)；By rotate or just
Turning mode, just transfering from one department to another to unite (9) can be with change of flight device (1) or buoyance lift body (20), aerial wind power generating system (2), dynamic power
Savings system (3), power propulsion system (5), ground connection collecting system of water (6), load Load System (7), the hanging of adjustable in length
Suo Qun system (8), photovoltaic generating system (11) etc. system towards, direction, be allowed to beneficially aircraft landing, reduce flight
Resistance, raising wind-force or photovoltaic power generation quantity etc. efficiency；Its hectare transfers from one department to another (9) following at least one of which kind system of uniting, and rotates just
Transfer from one department to another system (9.1), regulation hoist cable transfers from one department to another to unite (9.2) just；
Its photovoltaic generating system (11) includes photovoltaic cell (11.1)；Photovoltaic generating system (11) or photovoltaic cell
(11.1) upper surface or the side surface of following at least one of which kind position it are arranged on, aircraft (1) or buoyance lift body (20), aerial
Wind generator system (2), the savings system (3) of dynamic power, power propulsion system (5), electric propulsion flight system (5.1), connect
Ground collecting system of water (6), load Load System (7), hoist cable group's system (8) of adjustable in length, just transfer from one department to another unite (9)；Its photovoltaic is sent out
Electricity system (11) and following at least one of which kind system or the circuit communication of system, aircraft (1) or buoyance lift body (20), electricity push away
Enter flight system (5.1), aerial wind power generating system (2), the savings system (3) of dynamic power, ground connection collecting system of water (6).
Wherein manufacture freshwater system (17) and include following at least one of which kind, condensing water vapor system (17.1), sea water
Desalination system (17.2)；Manufacture freshwater system (17) to be arranged in load Load System (7)；Manufacture the circuit of freshwater system (17)
Connect the circuit of following at least one of which kind system, aircraft (1) or buoyance lift body (20), aerial wind power generating system (2), dynamic
The savings system (3) of power electric energy, control system (4), photovoltaic generating system (11)；Due to have free and sufficient wind energy wind-powered electricity generation,
Luminous energy photovoltaic electric power, utilizes wind energy wind-powered electricity generation, luminous energy photovoltaic electric power just can manufacture substantial amounts of fresh water to meet passenger, driver
Eat and drink；
Wherein airflight Housing system (18) is arranged on load Load System (7) position and is attached thereto；Fly in the air
The circuit of the circuit communication following at least one of which kind system of having sexual intercourse house system (18), aircraft (1) or buoyance lift body (20), sky
Middle wind generator system (2), the savings system (3) of dynamic power, control system (4), photovoltaic generating system (11).
Content 7.
According to the aerial wind energy power station formula aircraft described in content 4 or content 6, also include following characteristics:
Its aerial wind power generating system (2) and electric propeller propulsion system (5.1.1) are one or consubstantiality；Logical
Crossing flight advance generating function changing-over mechanism (26), make propelling, generating both functions can mutually change, switch operating；
Its ground connection collecting system of water (6) also includes following at least one of which kind mechanism, ground connection rope (6.2), unmanned plane machine
Structure (6.3), ground connection mechanism of twisting rope (6.4), earth conductor cable (6.5), ground connection plug mechanism (6.6)；
Wherein ground connection mechanism of twisting rope (6.4) connects following at least one of which kind mechanism, aircraft (1) or buoyance lift body
(20), aerial wind power generating system (2), the savings system (3) of dynamic power, control system (4), power propulsion system (5), connect
Ground collecting system of water (6), load Load System (7)；
Wherein ground connection rope (6.2) or earth conductor cable (6.6) are wrapped on ground connection mechanism of twisting rope (6.4)；
Wherein the lower end of ground connection rope (6.2) or earth conductor cable (6.6) connects following at least one of which kind mechanism, docking
Head mechanism (6.1), unmanned plane mechanism (6.3), ground connection plug mechanism (6.6)；Butt joint mechanism (6.1) or ground connection plug
Mechanism (6.6) connects unmanned plane mechanism (6.3)；Fly by remotely pilotless machine mechanism (6.3) drive butt joint mechanism (6.1) is controlled
OK, butt joint mechanism (6.1) flight so can be made easily to be connected object (12) to ground, fix aircraft device (13) in the air
Position, and be easily connected with ground object (12), in the air fix aircraft device (13) docking after be connected.So rely on
Ground connection is restricted (6.2) or earth conductor cable (6.6) " aerial wind energy power station formula aircraft " can be fixed or mooring is easy to ground
It is connected object (12), fixes on aircraft device (13) in the air, make aerial wind energy power station formula aircraft not fly away, allow aerial
Wind generator system (2) can enter generating state；This high altitude wind energy electric power can be full of the savings system of dynamic power
(3), provide electric power for flying power to electric propulsion flight system (5.1) the most again；
The wherein circuit of the upper end circuit communication following at least one of which kind system of earth conductor cable (6.5), aircraft (1)
Or the savings system (3) of buoyance lift body (20), aerial wind power generating system (2), dynamic power, control system (4), electric propulsion flight
System (5.1), photovoltaic generating system (11)；Lower end circuit communication ground connection plug mechanism (6.6) of earth conductor cable (6.5)；Connect
Ground plug mechanism (6.6) connects following at least one of which kind mechanism, butt joint mechanism (6.1), unmanned plane mechanism (6.3)；
Drive ground connection plug mechanism (6.6) controlled flight by remotely pilotless machine mechanism (6.3), so can make ground connection plug machine
Structure (6.6) flight is easily connected object (12), fixes the position of aircraft device (13) in the air to ground, and with ground easily quilt
Attached article (12), fix in the air aircraft device (13) insertion docking after connection circuit；So, one can rely on and connect
Ground electric wire (6.6) reaches the purpose of fixing aerial wind energy power station formula aircraft, its two can pass through earth conductor cable (6.5) reach to
The formula aircraft input of aerial wind energy power station or the purpose of output power；
Wherein butt joint mechanism (6.1) or ground connection plug mechanism (6.6) can be one or consubstantiality；Wherein
Ground connection rope (6.2) or earth conductor cable (6.6) can be one or consubstantiality；So can reduce weight.
Content 8.
According to the aerial wind energy power station formula aircraft described in content 5 or content 6, also include following characteristics:
The cross sectional shape of its floatage body (21) or floatage air bag (21.6) includes following at least one of which kind, wing body
Shape, fairing shape, spindle shape, ellipsoidal shape, shuttle shape, rugby ball shape, cylindrical shape, rectangle
Shape, square shape；Floatage body (21) or floatage air bag (21.6) include single or multiple；Its floatage body (21) or buoyancy
The utricule structure of air bag (21.6) includes following at least one of which kind, determines volume main gasbag system (21.11) structure, " determines
Volume main gasbag system (21.10)+balloonet system (21.9) " structure, variable volume main gasbag system (21.12) structure, " variant
Long-pending main gasbag system (21.12)+balloonet system (21.9) "；
Wherein variable volume main gasbag system (21.12) structure, " variable volume main gasbag system (21.12)+balloonet system
(21.9) " " variable volume main gasbag system (the 21.12) " structural volume among structure can change, and structural volume can greatly may be used
Little, structural volume is changeable；" variant type sky airship " therein version includes following at least one of which
Kind, radially variable volume version (21.13), longitudinal variable volume version (21.14)；Be respectively directed to different application purpose and
Range of application；" variable volume main gasbag (21.12) " version can make to rise to a few myriametre and fly to tens meters altitudes；Example
As, " variant type sky airship " version of Chinese invention people Li Xiaoyang design is exactly a kind of " variable volume main gasbag system
(21.12)”；
Internal combustion engine propulsion system (5.2) or the jet propulsion system (5.4) of its power propulsion system (5) can use buoyancy
Gas (1) is as fuel；Internal combustion engine propulsion system (5.2) or jet propulsion system (5.4) and following at least one of which kind portion
Buoyant gas (21.5) in part has pipeline to connect, floatage body (21), floatage air bag (21.6)；
Its load Load System (7) includes following at least one of which kind, manned or drive pedestal (7.1), manned or
Drive nacelle (7.2), loading nacelle (7.3), loading support body (7.4), loading pedestal (7.5), house or office room house body
(7.6)；
Hoist cable group's system (8) of its adjustable in length can also be directly connected to floatage air bag (21.6)；
Its photovoltaic generating system (11) also includes following at least one of which kind parts, inverter, load governor, with
Track sunlight system；Its photovoltaic generating system (11) or photovoltaic cell (11.1) can also be arranged on following at least one of which kind
The upper surface of position or side surface；Hoist cable group's system (8) of adjustable in length, just transfer from one department to another to unite (9)；Its photovoltaic cell (11.1) wraps
Include and following included a following type: crystal silicon type battery, amorphous silicon type battery, film type battery, flexible thin film type electricity
Pond, light-focusing type battery, multi-element compounds type battery, dye sensitization type battery, CaAs type battery, CIGS type battery, CdTe type electricity
Pond, InGaP/A type battery；
Buoyant gas (21.5) includes following at least one of which kind, hydrogen, helium, ammonia, steam, combustion gas；
Wherein cooling down or compress storage gas system (15) can be by cooling, compression etc. method buoyant gas
(21.5) volume-diminished, even becomes liquid, is stored in high-pressure bottle or in pressure pan；Thus avoid when high-altitude
There is volumetric expansion in buoyant gas (21.5), causes increase flight resistance, or damage floatage body (21) or flexible floating
Power body (21.2) or floatage air bag (21.6) situation；During in particular by ammonia as buoyant gas (21.5), effect is notable；
Cooling or compression storage gas system (15) have pipeline even with the buoyant gas (21.5) in following at least one of which kind parts
Connect, floatage body (21), flexible buoyancy body (21.2), floatage air bag (21.6)；
Wherein electric heating system (16) makes full use of the unobstructed advantage in high-altitude and carries out the electric power of photovoltaic generation at full capacity
Heat ammonia (19), water, air etc. aqueous vapor and form the vapours of high temperature, hot-air.Its vapours, hot-air can conducts
Buoyant gas (1) among floatage body (21) or floatage air bag (21.6), in order to improve floatage body (21) or floatage air bag
(21.6) buoyancy；Electric heating system (16) is arranged in floatage body (21) or floatage air bag (21.6), electric heating system
(16) circuit of circuit communication following at least one of which kind system, aircraft (1) or buoyance lift body (20), aerial wind-power electricity generation
System (2), the savings system (3) of dynamic power, control system (4), photovoltaic generating system (11).
Content 9.
According to content 2 aerial fixing aircraft device (13) according to claim 2；It is characterized in that:
Aerial fixing aircraft device (13) also includes following at least one of which kind parts, connects sky mechanical splice system
(41), empty electrically docking system (40) is connect:
Its vertical mooring fixed system (30) is connected with following at least one of which kind parts, connects sky mechanical splice system
(41), empty electrically docking system (40) is connect；
Sky mechanical splice system (41) that connects therein can be with the ground connection water receiving of aerial aerial wind energy power station formula aircraft
Realize connecting after system (6) docking；
The upper circuit connecing the empty electrically vertical power transmission cable of the circuit communication (37) of docking system (40) therein, connects empty electricity
Gas docking system (40) can be with the ground connection plug mechanism of the ground connection collecting system of water (6) of aerial aerial wind energy power station formula aircraft
(6.6) after docking, connection realizes circuit communication.
Content 10.
According to the aerial fixing aircraft device (13) described in content 1, it is characterised in that:
Aerial fixing aircraft device also includes following at least one of which kind parts, aerial laterally bands system
(32), lightning protection system (42), ice melting system (43)；
Vertical mooring guy rope (34) can be combined into one with vertical power transmission cable (37), and they employings are following the most extremely
Few one combining form, consubstantiality combines, allosome combines, binary combines；
Floatage body system (33) can also suspend or carry aerial laterally bands system (32) in midair；
Aerial laterally bands system (32) includes following at least one of which kind parts, aerial laterally rope rope (35), sky
In horizontal power transmission cable (38)；Owing to aerial laterally power transmission cable (38) also has mooring and the function of fixing airborne aircraft,
Therefore aerial laterally power transmission cable (38) is also a kind of aerial laterally rope rope (35)；Its aerial laterally rope rope (35) is horizontal with aerial
Power transmission cable (38) can be combined into one, and they use following at least one of which kind combining form, and consubstantiality combines, allosome
Combine in conjunction with, binary；
Aerial laterally bands system (32) is connected with following at least one of which kind parts, vertical mooring fixed system
(30), lightning protection system (42), ice melting system (43)；Aerial laterally bands system (32) includes wall scroll or a plurality of, and it is a plurality of
Aerial laterally bands system (32) can intersect connection, forms aerial antilift wire net (45)；Wherein aerial antilift wire net
(45) monolayer or multilamellar are included；
Aerial laterally power transmission cable (38) therein and the circuit communication of following at least one of which kind parts, vertically transmit electricity
Cable (37), connect empty electrically docking system (40), ice melting system (43)；Aerial laterally power transmission cable (38) therein includes list
Bar or a plurality of, its a plurality of aerial laterally power transmission cable (38) can intersect connection, forms aerial electrical grid (46)；Its
In aerial electrical grid (46) include monolayer or multilamellar；Following at least one of which kind parts also include insulating barrier, perpendicular
To power transmission line (37, the most laterally power transmission cable (38)；
Connect empty electrically docking system (40) and be arranged on following at least one of which kind component locations and the circuit company with it
Connect, vertical power transmission cable (37), aerial laterally power transmission cable (38)；Connect empty electrically docking system (40) include following the most extremely
Few one parts, manual electrical connector socket system (40.1), automatic electrical connector socket system (40.2)；
Connect sky mechanical splice system (41) aerial laterally bands system (32) position to be arranged on and be connected with it；
Wherein connect sky mechanical splice system (41) to dock with the ground connection collecting system of water (6) of aerial aerial wind energy power station formula aircraft
Realize afterwards connecting；Wherein connecing sky mechanical splice system (41) and include following at least one of which kind parts, manual locking is opened
Pass system (41.1), automatic locking switch system (41.2)；
Lightning protection system (42) and following at least one of which kind component locations, floatage body system (33), vertical mooring are fixed
System (30), aerial laterally bands system (32)；
Ice melting system (43) is arranged on following at least one of which kind component locations and is connected with its circuit, floatage body
System (33), vertical power transmission cable (37), aerial laterally power transmission cable (38)；
The following at least one of which kind parts height away from ground is between 100-10000 rice, floatage body system (33), perpendicular
To mooring fixed system (30), aerial laterally bands system (32).
Compared with prior art, the invention has a following outstanding advantages:
1, take full advantage of than ground be up to several times, Shi Jibei, hundreds of times high altitude wind energy wind-powered electricity generation to replace fuel to fly
OK, it is achieved that without the flight of fuel, saved fuel energy, decreased pollution.2, take full advantage of than ground be up to several times,
Sufficient, high-altitude solar photovoltaic electric power replaces fuel fly, overcome high altitude wind energy wind-powered electricity generation need to charge and between producing
Disconnected property flight problem.Thoroughly achieving aviation aircraft from this can be without company fuel, timeless, that limit without voyage
Continuous flight.3, straight owing to increasing the blade (21) of electric propeller propulsion system (5.1.1) and aerial wind power generating system (2)
Footpath, causes aerial wind power generating system (2) generated output to be greatly improved.4, owing to using hoist cable group's system of adjustable in length
(8), cause aerial photovoltaic generating system (11) that attitude can be adjusted, enable solar panel to follow the tracks of sunlight, significantly
Improve photoelectric conversion rate.5, owing to using hoist cable group's system (8) of adjustable in length that buoyance lift body (20) is loaded system with load
System (7), the savings system (3) of dynamic power separate, and cause the center of gravity of this aerial wind energy power station formula aircraft to be substantially reduced, overall
Structure is highly stable, it is not easy to be turned over by high wind, and entirety is toppled.6, make full use of buoyancy and replace lift, in order to reduce lift consumption
Can, save fuel energy.7, the buoyance lift body (20) of umbrella wing-like makes full use of lift to replace part buoyancy, in order to reduce buoyancy
The volume of air bag, reaches to reduce the purpose of flight resistance；Reduce flight resistance and just decrease flight power consumption, save fuel energy.
8, the buoyance lift body (20) of umbrella wing-like also has the buoyancy of buoyant gas, and it combines electric propeller propulsion system of can verting
(5.1.1), it is achieved that this aerial wind energy power station formula aircraft forever can be with the safe landing of Vertical Free；If aloft occurred
Accident (such as collide, stop, meteorological sudden change etc. accident), this aerial wind energy power station formula aircraft also can be slowly declined to ground
Face, will not occur crash accident, the safest.9, owing to being provided with servomechanism and autopilot, manipulation becomes
Extremely simple, the simplest easier than driving a car.10, owing to taking full advantage of floating technology, this aerial wind energy power station formula is made to fly
The deadweight reduction of row device, efficiency raising, performance are enriched, are used flexibly, make low cost cost be substantially reduced；The same intermediate vehicle of its cost
Relatively easy extensively enter family, private daily field.11, due to aerial wind energy power station formula aircraft, " aerial fixing flight
Device device (13) ", can be at high-altitude prolonged stay, it can provide a kind of high-altitude value-added service cheap, cleaning, safety and put down
Platform, such as high altitude communication platform, high-altitude monitor supervision platform, be equivalent to additionally increase New function of more than two kinds.12 if unmanned
Aerial wind energy power station formula aircraft, its performance more preferably, cost performance higher.13, the most aerial wind energy power station formula aircraft is permissible
As physical culture instrument, the apparatus of propeller-parachuting, a thing three is used.
14, due to when aircraft does not uses, aircraft can be placed on high-altitude and combine as aerial wind-force and photovoltaic and send out
Power station carries the electric power exporting unnecessary (after accumulator is fully charged), dual-use material earthward.Owing to aerial wind-force and photovoltaic join
Its cogeneration benefit of conjunction electric station, investment cost performance are the highest, and degree electricity cost, less than 0.3 yuan/kws, can substitute for fossil
The energy, thoroughly solves the global problem of regenerative resource.
15, propose " the fixing aircraft device (13) in the air " of originality, make this aerial wind energy power station formula aircraft can
With at high-altitude prolonged stay；Therefore create a kind of airport aloft and deposit " aerial aviation " pattern of aircraft, should " navigate in the air
Empty " pattern is different from present, deposit aircraft on airport, ground " field aerial " pattern.
16, first as the air transportation vehicles, its cost is extremely low, the aerial wind energy power station formula flight of its 2 people seat type
Device cost is less than 1,300,000 yuan；Secondly as aerial wind-force and photovoltaic cogeneration station, its investment cost performance is high, depends on
By selling the clean electric power of output, 2-3 is just recoverable to its cost of 1,300,000 yuan.So, aerial wind energy power station formula flies
Row device is the generally the least expensive individual air transportation vehicles that the poor can also afford, afford to support, afford to use.17, it is created
Go out a kind of cheap, cleaning, safety, at a high speed, point-to-point, door-to-door, quick and brand-new whole people's green air traffic mode.
18, just can carry out timeless, without boat owing to aerial wind energy power station formula aircraft need not carry fuel
Degree, safe, quiet low noise, the non-stop flight of low cost expense, so it is particularly suitable as military airlift
Equipment.19, just can carry out timeless, round-the-clock owing to aerial wind energy power station formula aircraft need not carry fuel
, high intensity, powerful wind-power electricity generation or photovoltaic generation, so it is particularly suitable as military field generating equipment.
20, aerial wind energy power station formula aircraft can move freely on the ground that the mankind are pursued as " flight house "
Life and work enjoy to improve and be upgraded to the life and work that freedom of the air moves and enjoy.Started a kind of brand-new, aerial simultaneously
Living and working method of flight movement.Be equivalent to ground huge pillar industry in national economy---" premises
Produce " industry, transfer raising is upgraded to a huger pillar industry in national economy brand-new, that fly movement---" room sky
Produce " industry.
21, thus, aerial wind energy power station formula aircraft propulsion human society from " ground civilization " social transformation, upgrading, across
Enter brand-new " civilization in the air " society.
Accompanying drawing explanation
Digital labelling in following accompanying drawing " " represent the "or" meaning.Such as (1) (2), represent (1) or (2).
Fig. 1, Fig. 1 .1 is the aerial wind energy power station formula of a kind of suspension using the flexible umbrella wing-buoyancy lift assembly (24)
The side elevational cross-section schematic diagram of aircraft, face generalized section (not including ground connection collecting system of water (6)).
Fig. 1 .2, Fig. 1 .3, Fig. 1 .4 are that 3 kinds of side elevational cross-section sketches of the aerial wind energy power station formula aircraft of Fig. 1 (are wherein schemed
1.3, Fig. 1 .4 does not include ground connection collecting system of water (6)).
Fig. 2, Fig. 2 .1, Fig. 2 .2 is a kind of employing flexible umbrella wing---suspension of column type buoyancy lift assembly (24)
Side elevational cross-section sketch, the top cross-sectional view of aerial wind energy power station formula aircraft, face generalized section (wherein Fig. 2 .1, figure
2.2 only include buoyancy lift assembly (24)).
Fig. 3, Fig. 3 .1, Fig. 3 .2 is a kind of employing flexible umbrella wing---suspension of streamlined buoyancy lift assembly (24)
Side elevational cross-section sketch, the top cross-sectional view of aerial wind energy power station formula aircraft, face generalized section (wherein Fig. 3 .1, figure
3.2 only include buoyancy lift assembly (24)).
Fig. 4, Fig. 4 .1 is a kind of employing flexible umbrella wing---aerial wind energy power station of the suspension of buoyancy lift assembly (24)
The side elevational cross-section sketch of formula aircraft, elevational diagrammatic view.
Fig. 5, Fig. 5 .1 is a kind of employing flexible umbrella wing---aerial wind energy power station of the suspension of buoyancy lift assembly (24)
The side elevational cross-section sketch of formula aircraft, elevational diagrammatic view.
Fig. 6 is the side of the aerial wind energy power station formula aircraft of a kind of suspension using streamlined flexible buoyancy body (21.2)
Depending on sketch.
Fig. 7, Fig. 7 .1, Fig. 7 .2 is the aerial wind energy power station of a kind of suspension using barrel shape flexible buoyancy body (21.2)
The schematic side view of formula aircraft, face generalized section, (wherein Fig. 7 .2 does not include ground connection water receiving system to local photo figure in kind
System (6)).
Fig. 8, Fig. 8 .1, Fig. 8 .2, Fig. 8 .3 is the aerial wind of a kind of suspension using cylinder flexible floatage body (21.2)
Can the side elevational cross-section schematic diagram of power station formula aircraft, partial perspective schematic view, local photo figure (wherein Fig. 8 .2, Fig. 8 .3 in kind
Do not include ground connection collecting system of water (6)).
Fig. 9 is the aerial wind energy electricity of the suspension of a kind of flexible buoyancy body (21.2) using fairshaped, opening shape
The side elevational cross-section sketch of standing posture aircraft.
Figure 10, Figure 10 .1, Figure 10 .2, Figure 10 .3 is the aerial wind energy power station formula of the suspension using profile lift body (22)
The side elevational cross-section sketch of aircraft, elevational diagrammatic view, local photo figure in kind, local photo figure (wherein Figure 10 .2, Figure 10 .3 in kind
Do not include ground connection collecting system of water (6)).
Figure 11, Figure 11 .2 is the aerial wind energy power station formula aircraft of the suspension of a kind of lifting body (22) using airfoil body
Side elevational cross-section sketch, side elevational cross-section sketch (wherein Figure 11 .2 does not include ground connection collecting system of water (6)).
Figure 11 .1, Figure 11 .2 are the side-lookings of the aerial wind energy power station formula aircraft of a kind of lifting body (22) using airfoil body
Diagrammatic sectional view, side elevational cross-section sketch (wherein Figure 11 .2 does not include ground connection collecting system of water (6)).
Figure 12, Figure 12 .1, Figure 12 .2 is the aerial wind energy power station formula aircraft of a kind of lifting body (22) using airfoil body
Diagrammatic side views, side elevational cross-section sketch, photo figure in kind (wherein Figure 12 .1, Figure 12 .2 do not include ground connection collecting system of water (6)).
Figure 13, Figure 13 .1 is that the side-looking of the aerial wind energy power station formula aircraft of a kind of lifting body (22) using airfoil body is cutd open
Face sketch, look up sketch (not including ground connection collecting system of water (6)).
Figure 14, Figure 14 .1 is that the side-looking of the aerial wind energy power station formula aircraft of a kind of lifting body (22) using airfoil body is cutd open
Face sketch, look up sketch (not including ground connection collecting system of water (6)).
Figure 15, Figure 15 .1, Figure 15 .2 is the streamlined flexible buoyancy body (21.2) of a kind of employing and profile lift body (22)
The side elevational cross-section sketch of the aerial wind energy power station formula aircraft of suspension, look up sketch, elevational diagrammatic view (wherein Figure 15, Figure 15 .1
Do not include ground connection collecting system of water (6)).
Figure 16 is that the side-looking of the aerial wind energy power station formula aircraft of a kind of suspension using helicopter rotor (23) is cutd open
Face sketch.
Figure 17 is the bowing of ground connection collecting system of water (6) that one includes butt joint mechanism (6.1), unmanned plane mechanism (6.3)
Depending on simplified schematic diagram.
Figure 18 is that a kind of heat-insulation layer (21.8) is arranged on facing of the inside of floatage body (21) or floatage air bag (21.6)
Diagrammatic sectional view.
Figure 19, Figure 19 .1 is 2 kinds is provided with the sky of 2 layers of Mesh air antilift wire net (45) or aerial electrical grid (46)
In fix the side-looking simplified schematic diagram of aircraft device (13).
Figure 20 is the vertical view simplified schematic diagram of the aerial fixing aircraft device (13) of Figure 19.
Figure 21, Figure 21 .1, Figure 21 .2 is that vertical mooring guy rope (34) is combined into consubstantiality knot with vertical power transmission cable (37)
Close, allosome combine, binary combine 3 kinds of combining forms face diagrammatic sectional view.
Figure 22, Figure 22 .1 is a kind of floatage body (21) or floatage air bag (21.6) includes variable volume main gasbag system
(21.12) the side-looking simplified schematic diagram of the aerial wind energy power station formula aircraft of structure.
Figure 23 be umbrella shape water receiving mechanism (6.7.1), barrel-shaped water receiving mechanism (6.7.2), Fan Xing water receiving mechanism (6.7.3) this 3
Plant the water receiving mechanism (6.7) side-looking perspective simplified schematic diagram in water body (14).
Detailed description of the invention.
Embodiment 1.From Fig. 1, Fig. 1 .1, Fig. 1 .2, Fig. 1 .3, Fig. 1 .4, Fig. 2, Fig. 2 .1, Fig. 2 .2, Fig. 2, Fig. 2 .1, figure
2.2, Figure 17 understands, and is that the flexible umbrella wing---the aerial wind energy power station formula of the suspension of buoyancy lift assembly (24) flies in a kind of employing
Row device.
It is characterized in that: it includes aircraft (1), aerial wind power generating system (2), the savings system of dynamic power
(3), control system (4), power propulsion system (5), ground connection collecting system of water (6), load Load System (7), adjustable in length
Hoist cable group's system (8), just transfer from one department to another unite (9)；
Its aircraft (1) connects following 2 kinds of systems, aerial wind power generating system (2), load Load System (7)；Its load
Hoist cable group's system of adjustable in length is included between Load System (7) and aircraft (1) or aerial wind power generating system (2)
(8), constitute and be indirectly connected with；
Its aircraft (1) includes buoyance lift body (20), and the front end of its buoyance lift body (20) presents close-shaped；Its buoyance lift body
(20) it being the flexible umbrella wing---buoyancy lift assembly (24), its buoyancy lift assembly (24) includes components described below, floatage body
(21), lifting body (22)；Its floatage body (21), lifting body (22) use flexible buoyancy body (21.2), flexible lifting body (22.2),
They unite two into one and constitute buoyancy lift assembly (24)---the flexible umbrella wing with buoyancy and lift；Buoyancy lift assembly (24)
Front end present close-shaped；Its buoyancy lift assembly (24) includes floatage air bag (21.6), in floatage air bag (21.6)
Include buoyant gas (21.5)；The density of buoyant gas (21.5) is less than aircraft outer air density；Buoyancy lift assembly
(24) following 2 kinds of bodies are included, profile lift body (22.5), umbellate form lifting body (22.7)；
Wherein floatage air bag (21.6) presents cylinder aerofoil profile；Arrange in the inside of floatage body (21), floatage air bag (21.6)
Internal portioning layer (21.7), is provided with internal portioning layer (21.7) between multiple floatage air bags (21.6)；Its internal portioning layer (21.7) can be
Floatage body (21), floatage air bag (21.6) these part components are isolated into multiple cavity；In order to improve they rigidity and antiseep
Performance.There is seepage in one cavity buoyant gas (21.5), does not results in other cavity buoyant gas (21.5) and seepage occurs, also
Do not interfere with other cavity buoyant gas (21.5) normally to work, i.e. the buoyancy of other cavity does not reduces；
Due at the flexible umbrella wing---in buoyancy lift assembly (24) under the effect of buoyant gas (21.5), make aerial wind energy
Power station formula aircraft not only has single " lift " function of umbrella wing body, also has " buoyancy " function of wing body.At " lift "
" buoyancy " is added under folded effect, and result greatly reduces the deadweight of aerial wind energy power station formula aircraft.The most both decreased
Flight energy consumes, and makes again aircraft vertical lifting be possibly realized.Further, since be provided with buoyant gas (21.5), aloft
Even if the accident of there occurs (such as collide, stop, meteorological sudden change etc. accident), the propeller-parachuting of this photovoltaic electric also can slowly decline
To ground, crash accident will not occur.Again due to the flexible umbrella wing---buoyancy lift assembly (24) is the flexible air-bag of large volume,
Aloft there occurs collision accident, also do not result in personnel and the injury in cabin and damage.If it occur that air bag gas leakage, buoyancy
Gas (21.5) revealed, without this accident of buoyancy, aerial wind energy power station formula aircraft has reformed into aerodone, glide
Umbrella, relies on glide to drop to ground.Therefore, aerial wind energy power station formula aircraft is the safest, substantially without personnel's casualties occur
Accident.If unmanned propeller-parachuting, its performance more preferably, cost performance higher.Additionally, there is wing body shape, fairing shape, spin
Hammer body shape, the flexible umbrella wing of ellipsoidal shape---buoyancy lift assembly (24) can greatly reduce wind resistance during flight, greatly
Improve greatly flight speed.
Its aerial wind power generating system (2) connects following 3 kinds of systems, aircraft (1), control system (4), electric propulsion flight
System (5.1), load Load System (7)；The electricity of the following 5 kinds of systems of circuit communication of aerial wind power generating system therein (2)
Road, aircraft (1), the savings system (3) of dynamic power, control system (4), electric propulsion flight system (5.1), ground connection water receiving system
System (6)；Its aerial wind power generating system (2) includes following 7 kinds of parts, blade (21), electromotor (22), speed adjusting gear
(23), become pitch mechanism (24), blade fold mechanism (25), flight advance generating function changing-over mechanism (26), guard ring or duct
Mechanism (27), just transfer from one department to another unite (9)；Blade (21) connects following 3 kinds of parts: electromotor (22), change pitch mechanism (24), blade are rolled over
Folded mechanism (25), flight advance generating function changing-over mechanism (26)；
Savings system (3) the connected load Load System (7) of its dynamic power, and it is arranged on load Load System (7)
Bottom, is convenient for changing accumulator；The circuit of the following system of circuit communication of the savings system (3) of its dynamic power, aircraft
(1), aerial wind power generating system (2), control system (4), electric propulsion flight system (5.1), ground connection collecting system of water (6)；It moves
The savings system (3) of power electric energy includes following 2 kinds of parts, accumulator (3.1) or electric capacity (3.2), point distribution system (3.4)；
Its control system (4) is arranged on following position and is attached thereto, buoyancy lift assembly (24), aerial wind-power electricity generation
System (2), the savings system (3) of dynamic power, power propulsion system (5), ground connection collecting system of water (6), load Load System
(7), hoist cable group's system (8) of adjustable in length；The circuit of the following system of circuit communication of its control system (4), aircraft
(1), aerial wind power generating system (2), the savings system (3) of dynamic power, electric propulsion flight system (5.1), ground connection water receiving system
System (6), load Load System (7)；Its control system (4) includes mixing Ride Control System (4.3)；It mixes Driving control
System (4.3) includes pilot steering control system (4.1) and automatic Pilot control system (4.2)；
Its power propulsion system (5) uses hybrid propulsion system (5.6), and it includes electric propulsion flight system
(5.1), manual feed system (5.5)；The wherein circuit of the following system of circuit communication of electric propulsion flight system (5.1), in the air
Wind generator system (2), the savings system (3) of dynamic power, control system (4), ground connection collecting system of water (6)；Its electric propulsion flies
Row system (5.1) includes electric propeller propulsion system (5.1.1)；Aerial wind power generating system (2) and electric propeller push away
Entering system (5.1.1) is one or consubstantiality, constitutes aerial wind power generating system (2)/electric propeller propulsion system
(5.1.1) system；By flight advance generating function changing-over mechanism (26), make propelling, generating both functions mutually change,
Switch operating；
Its ground connection collecting system of water (6) upper end connected load Load System (7)；When needing, ground connection collecting system of water (6) lower end can
To connect following at least one of which kind system at any time, ground is easily connected object (12), fixes aircraft device (13) in the air；
Its ground connection collecting system of water (6) be used for docking connect aerial fixing aircraft device (13) connect sky mechanical splice system (41), this
Sample can be fixed fixing to " aerial wind energy power station formula aircraft " or mooring on aircraft device (13) to aerial, and being in can not
Fly away state；Ground connection collecting system of water (6) is arranged on load Load System (7) position and is attached thereto；Ground connection collecting system of water (6)
Including butt joint mechanism (6.1), its butt joint mechanism (6.1) includes following 2 kinds of mechanisms, staple joint mechanism (6.1.1),
Eject joint mechanism (6.1.3)；Ground connection collecting system of water (6) also includes following at least one of which kind mechanism, and ground connection is restricted
(6.2), unmanned plane mechanism (6.3), ground connection mechanism of twisting rope (6.4)；
Wherein ground connection mechanism of twisting rope (6.4) connected load Load System (7)；Wherein ground connection rope (6.2) is wrapped in ground connection volume
On rope mechanism (6.4)；The lower end of ground connection rope (6.2) connects following at least one of which kind mechanism, butt joint mechanism (6.1), nothing
People's machine mechanism (6.3)；Butt joint mechanism (6.1) connects unmanned plane mechanism (6.3)；Driven by remotely pilotless machine mechanism (6.3)
Butt joint mechanism (6.1) controlled flight, so can make butt joint mechanism (6.1) flight be easily connected to ground object (12),
The position of aerial fixing aircraft device (13), and be easily connected object (12) with ground, fix aircraft device in the air
(13) docking connects, and relies on ground connection rope (6.2) to reach the purpose of fixing aerial wind energy power station formula aircraft；
Its load Load System (7) connects following at least one of which kind system, buoyance lift body (20) or buoyancy lift assembly
(24), aerial wind power generating system (2), the savings system (3) of dynamic power, power propulsion system (5), ground connection collecting system of water
(6)；Its load Load System (7) includes manned or drives nacelle (7.2) or loading nacelle (7.3) or house or office house
Body (7.6)；
Hoist cable group's system (8) of its adjustable in length includes hoist cable (8.1), hoist cable group's system of its adjustable in length
(8) 2 kinds of mechanisms, electric rolling rope mechanism (8.2), manual Juan Suo mechanism (8.3) are also included；Part hoist cable (8.1) is wrapped in electricity
In the wire drum of Dong Juan rope mechanism (8.2) or manually Juan Suo mechanism (8.3), or a part for hoist cable (8.1) is wrapped in electronic
In the wire drum of Juan Suo mechanism (8.2) or manually Juan Suo mechanism (8.3)；When load Load System (7) and aircraft (1) or aerial
The savings system (3) of wind generator system (2) or dynamic power or power propulsion system (5) or the company of ground connection collecting system of water (6)
Connecing and include when being indirectly connected with, aerial wind energy power station formula aircraft also includes hoist cable group's system (8) of adjustable in length, and it is born
Lotus Load System (7) pushes away with savings system (3) or the power of aircraft (1) or aerial wind power generating system (2) or dynamic power
Enter hoist cable group's system (8) including adjustable in length between system (5) or ground connection collecting system of water (6), between constituting in succession
Connect；Reach to adjust the flexible umbrella wing by the length of hoist cable group's system (8) of adjustable in length---buoyancy lift assembly (24)
Attitude, buoyance lift body (20) just can follow the tracks of alignment sunlight；Thus can make the photovoltaic electric power that output is maximum, about improve
The photovoltaic electric power output of 35%；
Its hectare transfers from one department to another system (9) and is arranged on following at least one of which kind position and is attached thereto, aerial wind-power electricity generation system
System (2), power propulsion system (5), hoist cable group's system (8) of adjustable in length；By rotating or just turning or regulate hoist cable
Length mode, just transfers from one department to another system (9) and can change buoyancy lift assembly (24), aerial wind power generating system (2), power propulsion system
(5), ground connection collecting system of water (6), hoist cable group's system (8) of adjustable in length, photovoltaic generating system (11) etc. system towards,
Direction, is allowed to beneficially aircraft landing, reduces flight resistance, raising wind-force or photovoltaic power generation quantity etc. efficiency；Its hectare transfers from one department to another
System (9) following at least one of which kind system, system (9.1) is transfered from one department to another in rotation just, regulation hoist cable transfers from one department to another to unite (9.2) just；Just system is transfered from one department to another
(9) drive change power propulsion system (5) direction of propulsion, can before, can afterwards, can go up, can descend rotate advance；
The buoyancy of this aerial wind energy power station formula aircraft is more than deadweight, less than full load take-off weight；Or buoyancy is more than
Full load take-off weight.When taking off vertically, just transfer from one department to another system (9) rotation aerial wind power generating system (2)/electric propeller and advance system
System (5.1.1) system becomes flat shape, and whole thrusts advance for upward direction.After entering in the air, just transfer from one department to another (9) rotation of uniting
Aerial wind power generating system (2)/electric propeller propulsion system (5.1.1) system becomes vertical shape；Because the flexible umbrella wing---
Buoyancy lift assembly (24) creates lift, decreases the thrust of upward direction when forward direction flight.Later by aerial
It is complete that whole thrusts of wind generator system (2)/electric propeller propulsion system (5.1.1) system are just used for overcoming horizontal resistance
Speed flight.During landing, reversal procedure operates.
When existing accumulator (3.1) power drain, more renew after aerial wind energy power station formula aircraft is dropped to ground
, be full of electric power relay accumulator (3.1) continue flight.In future, the accumulator (3.1) being full of electric power is as conventional replacing
Commodity selling, be equivalent to change LPG cyoinders business method.
Owing to buoyancy is more than deadweight, this aerial wind energy power station formula aircraft, when not carrying people to fly, can load more
Accumulator (3.1) swims in aerial for aerial wind power generating system (2)/electric propeller propulsion system (5.1.1) system, photovoltaic
Electricity generation system (11) uses.Its aerial wind power generating system (2)/electric propeller propulsion system (5.1.1) system, photovoltaic generation
System (11) works on, and provides power charge to accumulator (3.1).After accumulator (3.1) is full of electric power, photovoltaic generation system
System (11) continues to provide electric power earthward, is equivalent to an aerial micro generation station.Or ground of landing back, unloads full electric power
Accumulator (3.1), then the accumulator (3.1) changing unregulated power into returns to go in the air continue charging.When needs use aerial wind energy
During the formula aircraft of power station, use tractive manner or rely on automatic Pilot control system (4.2) to make the formula flight of aerial wind energy power station
Device drops to ground, allows personnel enter aerial wind energy power station formula aircraft, again takes off vertically.
Thus, aerial wind energy power station formula aircraft does not use fuel, it is possible to the wind-power electricity generation amount fully relying on self is complete
Become aerial mission.At this moment, this aerial wind energy power station formula aircraft is exactly a frame " aerial wind energy aircraft ".
Embodiment 2.Knowable to Fig. 4, Fig. 4 .1, it it is a kind of employing flexible umbrella wing---suspension of buoyancy lift assembly (24)
Aerial wind energy power station formula aircraft.
It is characterized in that: aerial wind power generating system (2)/electric propeller propulsion system (5.1.1) system is arranged on length
Spend the middle part of adjustable hoist cable group's system (8)；Remaining feature is with embodiment 1.
Embodiment 3.Knowable to Fig. 5, Fig. 5 .1, it it is a kind of employing flexible umbrella wing---suspension of buoyancy lift assembly (24)
Aerial wind energy power station formula aircraft.
It is characterized in that: 2 sets aerial wind power generating system (2)/electric propeller propulsion system (5.1.1) system is arranged on
Buoyance lift body (20) or buoyancy lift assembly (24) front and rear part；Remaining feature is with embodiment 1.
Embodiment 4.As can be seen from Figure 6, it is the aerial wind energy of a kind of suspension using streamlined flexible buoyancy body (21.2)
Power station formula aircraft.
It is characterized in that: buoyance lift body (20) uses streamlined flexible buoyancy body (21.2)；Remaining feature is with embodiment 1.
Embodiment 5.Knowable to Fig. 7, Fig. 7 .1, Fig. 7 .2, it it is a kind of suspention using barrel shape flexible buoyancy body (21.2)
The aerial wind energy power station formula aircraft of formula.
It is characterized in that: its buoyance lift body (20) uses flexible buoyancy body (21.2), flexible buoyancy body (21.2) shape cylindrical in shape；
Aerial wind power generating system (2)/electric propeller propulsion system (5.1.1) system is arranged on cylindrical flexible floatage body (21.2)
In cylinder；Remaining feature is with embodiment 1.
Embodiment 6.Knowable to Fig. 8, Fig. 8 .1, Fig. 8 .2, Fig. 8 .3, it it is a kind of employing cylinder flexible floatage body (21.2)
The aerial wind energy power station formula aircraft of suspension.
It is characterized in that: its buoyance lift body (20) uses flexible buoyancy body (21.2), and flexible buoyancy body (21.2) is in cylinder
Shape；Aerial wind power generating system (2)/electric propeller propulsion system (5.1.1) system is arranged on cylinder flexible floatage body
(21.2) two ends；Remaining feature is with embodiment 1.
Embodiment 7.As can be seen from Figure 9, it is the suspention of a kind of flexible buoyancy body (21.2) using fairshaped, opening shape
The aerial wind energy power station formula aircraft of formula.
It is characterized in that: it is lifting body (22) that the front end of its buoyance lift body (20) presents opening shape；Its buoyance lift body (20) is adopted
With aerofoil profile, opening shape flexible lifting body (22.2), remaining feature is with embodiment 1.
Embodiment 8.Knowable to Figure 10, Figure 10 .1, Figure 10 .2, Figure 10 .3, it it is a kind of lifting body (22) using airfoil body
The aerial wind energy power station formula aircraft of suspension.
It is characterized in that: aerial wind energy power station formula aircraft includes aircraft (1)；Aircraft (1) includes airfoil body
Lifting body (22), the lifting body (22) of airfoil body uses firm lifting body (22.1)；4 sets aerial wind power generating system (2)/electronic
Propeller propulsion system (5.1.1) system is arranged on the upper-lower position in firm lifting body (22.1) front portion；Remaining feature is with implementing
Example 1.
Embodiment 9.Knowable to Figure 11, Figure 11 .2, it it is a kind of suspension aerial wind energy electricity using profile lift body (22)
Standing posture aircraft.
It is characterized in that: aerial wind energy power station formula aircraft includes aircraft (1)；Aircraft (1) includes airfoil body
Lifting body (22), the lifting body (22) of airfoil body uses firm lifting body (22.1)；Aerial wind power generating system (2)/electronic spiral shell
Rotation oar propulsion system (5.1.1) system is arranged at firm lifting body (22.1) anterior；Just lifting body (22.1) includes transfering from one department to another after a little while
System (9), firm lifting body (22.1) dependence is just transfered from one department to another system (9) and can be rotated；Load Load System (7) is hung by adjustable in length
Suo Qun system (8) is indirectly connected with aircraft (1)；Remaining feature is with embodiment 1.
Embodiment 10.Knowable to figure Figure 11 .1, Figure 11 .2, it it is a kind of aerial wind energy power station using profile lift body (22)
Formula aircraft.
It is characterized in that: aerial wind energy power station formula aircraft includes aircraft (1)；Aircraft (1) includes airfoil body
Lifting body (22), the lifting body (22) of airfoil body uses firm lifting body (22.1)；Aerial wind power generating system (2)/electronic spiral shell
Rotation oar propulsion system (5.1.1) system is arranged at firm lifting body (22.1) anterior；Just lifting body (22.1) includes transfering from one department to another after a little while
System (9), firm lifting body (22.1) dependence is just transfered from one department to another system (9) and can be rotated；Load Load System (7) is directly connected to aircraft (1)；
Remaining feature is with embodiment 1.
Embodiment 11.Knowable to Figure 12, Figure 12 .1, Figure 12 .2, it it is the aerial wind energy power station using profile lift body (22)
Formula aircraft.
It is characterized in that: aerial wind energy power station formula aircraft includes aircraft (1)；Aircraft (1) includes airfoil body
Lifting body (22), the lifting body (22) of airfoil body uses firm lifting body (22.1)；Aerial wind power generating system (2)/electronic spiral shell
Rotation oar propulsion system (5.1.1) system is arranged at firm lifting body (22.1) middle part；Aerial wind power generating system (2) includes after a little while
Transfering from one department to another to unite (9), firm lifting body (22.1) dependence is just transfered from one department to another system (9) and can be rotated；Remaining feature is with embodiment 1.Wherein Figure 12 .1,
Electric aircraft in Figure 12 .2 is exactly this Helicopter Corporation AgustaWestland being anticipated joint by English invention, entitled
Project Zero's, the all-electric tilt rotor aircraft of the first in the world platform.
Embodiment 12.Knowable to Figure 13, Figure 13 .1, it it is the aerial wind energy power station of a kind of lifting body (22) using airfoil body
Formula aircraft.
It is characterized in that: aerial wind energy power station formula aircraft includes aircraft (1)；Aircraft (1) includes airfoil body
Lifting body (22), the lifting body (22) of airfoil body uses firm lifting body (22.1)；Aerial wind power generating system (2)/electronic spiral shell
It is anterior that rotation oar propulsion system (5.1.1) is arranged on firm lifting body (22.1)；Just lifting body (22.1) has been directly connected to load loading
System (7)；2 small-sized aerial wind power generating system (2)/electric propellers it are additionally provided with in load Load System (7) both sides
Propulsion system (5.1.1) system；Wherein ground connection collecting system of water (6) is not drawn into；Remaining feature is with embodiment 1.
Embodiment 12.Knowable to Figure 14, Figure 14 .1, it it is the aerial wind energy power station of a kind of lifting body (22) using airfoil body
Formula aircraft.
It is characterized in that: aerial wind energy power station formula aircraft includes aircraft (1)；Aircraft (1) includes one greatly
The lifting body (22) of the airfoil body of plane；The lifting body (22) of airfoil body uses firm lifting body (22.1)；At firm lifting body
(22.1) inside includes buoyant gas (21.5) or floatage air bag (21.6)；Its aerial wind power generating system (2)/electronic
Propeller propulsion system (5.1.1) system is arranged on the front portion of firm lifting body (22.1)；In the both sides of load Load System (7) also
It is provided with 2 small-sized aerial wind power generating system (2)/electric propeller propulsion system (5.1.1) system；Remaining feature is with real
Execute example 1.
Embodiment 13.Knowable to Figure 15, Figure 15 .1, Figure 15 .2, be a kind of use streamlined flexible buoyancy body (21.2) and
The aerial wind energy power station formula aircraft of the suspension of the lifting body (22) of airfoil body.
It is characterized in that: aerial wind energy power station formula aircraft includes aircraft (1)；Aircraft (1) includes streamlined
The lifting body (22) of flexible buoyancy body (21.2) and airfoil body；2 streamlined flexible buoyancy body (21.2) tops connect one greatly
The lifting body (22) of the airfoil body of plane；The lifting body (22) of airfoil body uses firm lifting body (22.1) or flexible lifting body
(22.2)；Aerial wind power generating system (2)/electric propeller propulsion system (5.1.1) system is arranged on 2 streamlined flexible floatings
The centre of power body (21.2)；Be additionally provided with in the both sides of load Load System (7) 2 small-sized aerial wind power generating system (2)/
Electric propeller propulsion system (5.1.1) system；Remaining feature is with embodiment 1.
Embodiment 14.As can be seen from Figure 9, it is the streamlined flexible buoyancy body (21.2) of a kind of employing and the lifting body of airfoil body
(22) the aerial wind energy power station formula aircraft of suspension.
It is characterized in that: aerial wind energy power station formula aircraft includes aircraft (1)；Aircraft (1) includes streamlined
The lifting body (22) of flexible buoyancy body (21.2) and airfoil body；2 streamlined flexible buoyancy body (21.2) tops connect one greatly
The lifting body (22) of the airfoil body of plane；The lifting body (22) of airfoil body uses firm lifting body (22.1) or flexible lifting body
(22.2)；Aerial wind power generating system (2)/electric propeller propulsion system (5.1.1) system is arranged on 2 streamlined flexible floatings
The centre of power body (21.2)；Be additionally provided with in the both sides of load Load System (7) 2 small-sized aerial wind power generating system (2)/
Electric propeller propulsion system (5.1.1) system；Remaining feature is with embodiment 1.
Embodiment 15.As can be seen from Figure 16, it is the aerial wind energy power station of a kind of suspension using helicopter rotor (23)
Formula aircraft.
It is characterized in that: aerial wind energy power station formula aircraft includes the aircraft (1) of helicopter；Aircraft (1)
Buoyance lift body (20) is coaxial DCB Specimen (23)；DCB Specimen (23) is main aerial wind power generating system (2)/electric screw
Oar propulsion system (5.1.1) system；The afterbody of aircraft (1) also sets up aerial wind power generating system (2)/electric propeller
Propulsion system (5.1.1) system；Remaining feature is with embodiment 1.
Embodiment 16.Knowable to Fig. 2 .2, Fig. 3 .2, Fig. 6, Figure 13, Figure 14, Figure 15, Figure 15 .2, it is that one is provided with photovoltaic
The aerial wind energy power station formula aircraft of electricity generation system (11).
It is characterized in that: aerial wind energy power station formula aircraft also includes photovoltaic generating system (11)；Photovoltaic generating system
(11) photovoltaic cell (11.1) is included；Photovoltaic generating system (11) or photovoltaic cell (11.1) be arranged on following at least a part of which it
The upper surface of a kind of position or side surface, aircraft (1), aerial wind power generating system (2), the savings system (3) of dynamic power,
Power propulsion system (5), electric propulsion flight system (5.1), ground connection collecting system of water (6), load Load System (7), adjustable length
Joint hoist cable group's system (8), just transfer from one department to another unite (9)；Its photovoltaic generating system (11) and following at least one of which kind system or be
The circuit communication of system, aircraft (1), electric propulsion flight system (5.1), aerial wind power generating system (2), the savings of dynamic power
System (3), ground connection collecting system of water (6)；Remaining feature is with embodiment 1-embodiment 15.
Utilize aircraft (1), aerial wind power generating system (2), the savings system (3) of dynamic power, power propulsion system
(5), the hoist cable group system of electric propulsion flight system (5.1), ground connection collecting system of water (6), load Load System (7), adjustable in length
System (8), the photovoltaic generating system (11) on (9) that just transfers from one department to another to unite photovoltaic electric power can be as the supplementary source of flying power.
Under conditions of making full use of high-altitude radiated solar energy unobstructed, high, carrying out photovoltaic generation at full capacity, photovoltaic electric power is possible to energy
Enough fully meet the thrust power demand of aircraft, or fully meet heating ammonia (19), water, air etc. aqueous vapor and become high
The vapours of temperature, the electricity needs of hot-air.Its vapours, hot-air can be as buoyant gas (21.5).So aerial wind energy
Power station formula aircraft is achieved that: under need not consumption fuel condition, utilize solar energy just can carry out timeless
Fly, utilize solar energy just can carry out the VTOL limited without number of times.If unmanned Airlift Flight device, its performance is more
Good, cost performance is higher.
Embodiment 17.From Fig. 1 .2, Fig. 4, Fig. 4 .1, Fig. 5, Fig. 5 .1, Fig. 6, Fig. 7, Fig. 7 .1, Fig. 8, Fig. 8 .1, Fig. 9, figure
10, Figure 10 .1, Figure 11, Figure 11 .1, Figure 12, Figure 15, Figure 15 .2 understands, and is the one aerial wind that is provided with earth conductor cable (6.5)
Can power station formula aircraft.
It is characterized in that: the ground connection collecting system of water (6) of aerial wind energy power station formula aircraft also includes following at least a part of which
One mechanism, earth conductor cable (6.5), ground connection plug mechanism (6.6)；Wherein butt joint mechanism (6.1) or ground connection electric mortiser
Head mechanism (6.6) can be one or consubstantiality；Wherein ground connection rope (6.2) or earth conductor cable (6.6) can be one
Or consubstantiality；So can reduce weight；
Wherein earth conductor cable (6.6) is wrapped on ground connection mechanism of twisting rope (6.4)；
Wherein the lower end of earth conductor cable (6.6) connects following at least one of which kind mechanism, ground connection plug mechanism
(6.6), unmanned plane mechanism (6.3)；Ground connection plug mechanism (6.6) connects butt joint mechanism (6.1), unmanned plane mechanism (6.3)；
The wherein circuit of the upper end circuit communication following at least one of which kind system of earth conductor cable (6.5), aircraft (1) or buoyance lift body
(20), aerial wind power generating system (2), the savings system (3) of dynamic power, control system (4), electric propulsion flight system
(5.1)；Lower end circuit communication ground connection plug mechanism (6.6) of earth conductor cable (6.5)；By remotely pilotless machine mechanism (6.3)
Drive ground connection plug mechanism (6.6) controlled flight, ground connection plug mechanism (6.6) flight so can be made easily to be connected to ground
Connect object (12), fix the position of aircraft device (13) in the air, and be easily connected object (12) with ground, aerial fixing fly
The circuit of row device device (13) is docked and connected；One can rely on earth conductor cable (6.6) to reach fixing aerial wind energy power station formula to fly
The purpose of row device, its two can pass through earth conductor cable (6.5) reach to aerial wind energy power station formula aircraft input or output electricity
The purpose of power；
Remaining feature is with embodiment 1-embodiment 16.
Embodiment 18.Figure 18 is that one includes heat-insulation layer (21.8) and is arranged on floatage body (21) or floatage air bag
(21.6) internal aerial wind energy power station formula aircraft.
It is characterized in that: heat-insulation layer (21.8) that aerial wind energy power station formula aircraft also includes, cool down or compress storage
Gas system (15), electric heating system (16)；Wherein heat-insulation layer (21.8) is arranged on floatage body (21) or floatage air bag
(21.6) inside；Heat-insulation layer (21.8) reduces buoyant gas (21.5) temperature in floatage body (21) or floatage air bag (21.6)
Degree reduces；
In wherein electric heating system (16) is arranged on floatage body (21) or floatage air bag (21.6), electric heating system (16)
The circuit of circuit communication following at least one of which kind system, aerial wind power generating system (2), the savings system of dynamic power
(3), photovoltaic generating system (11)；Floatage body (21) also includes following portion body, heat-insulation layer (21.8), balloonet system
(21.9), air-pump inflating system (21.10)；Wherein balloonet system (21.9), air-pump inflating system (21.10) are not drawn into；Floating
Strength body (21.5) uses ammonia or steam；Wherein electric heating system (16) makes full use of high altitude wind, photovoltaic generation
Electric power heats ammonia (19), water, air etc. aqueous vapor and forms the hot ammonia vapour of high temperature, vapours, hot-air.Its hot ammonia vapour, heat
Steam, hot-air can be as the buoyant gas (1) among floatage body (21) or floatage air bag (21.6), in order to improve buoyancy
Body (21) or the buoyancy of floatage air bag (21.6)；The method can become cheap, safe, practical the floating in above example
Power body (21)；Both hydrogen explosion can have been avoided, it is also possible to avoid the high cost of helium.
Wherein cooling down or compress storage gas system (15) can be by cooling, compression etc. method buoyant gas
(21.5) volume-diminished of hot ammonia vapour, even becomes liq ammonia (19), is stored in high-pressure bottle or in pressure pan；So
Avoid the hot ammonia vapour generation volumetric expansion as buoyant gas (21.5) when high-altitude, cause increase flight resistance, or
Damage floatage body (21) or flexible buoyancy body (21.2) or floatage air bag (21.6) situation；Make in particular by ammonia
During for buoyant gas (21.5), effect is notable；Cooling or compression store gas system (15) and following at least one of which kind portion
Buoyant gas (21.5) in part has pipeline to connect, floatage body (21), flexible buoyancy body (21.2), floatage air bag (21.6)；Its
Remaining feature is with embodiment 1-embodiment 17.
Embodiment 19.As can be seen from Figure 23, be provided with umbrella shape water receiving mechanism (6.7.1), barrel-shaped water receiving mechanism (6.7.2),
The aerial wind energy power station formula aircraft of these 3 kinds of water receiving mechanisms (6.7) of Fan Xing water receiving mechanism (6.7.3).
It is characterized in that: the ground connection collecting system of water (6) of aerial wind energy power station formula aircraft uses water receiving mechanism (6.7) to replace
Butt joint mechanism (6.1)；Its water receiving mechanism (6.7) following at least one of which kind mechanism, umbrella shape water receiving mechanism (6.7.1), bucket
Shape water receiving mechanism (6.7.2), Fan Xing water receiving mechanism (6.7.3)；Water receiving mechanism (6.7) includes thin-film body (6.7.5)；At water body
(14) in, umbrella shape water receiving mechanism (6.7.1), barrel-shaped water receiving mechanism (6.7.2), these 3 kinds of water receiving machines of Fan Xing water receiving mechanism (6.7.3)
The thin-film body (6.7.5) of structure (6.7) constitutes umbrella shape, barrel-shaped, sail form drag water body；
Remaining feature is with embodiment 1-embodiment 18.
Embodiment 20.It is provided with manufacturing freshwater system (17), the aerial wind energy power station of airflight Housing system (18)
Formula aircraft.
It is characterized in that: aerial wind energy power station formula aircraft is additionally provided with manufacture freshwater system (17), airflight house
System (18)；Wherein airflight Housing system (18) is arranged on load Load System (7) position and is attached thereto；Wherein make
Make freshwater system (17) and include following at least one of which kind, condensing water vapor system (17.1), seawater desalination system (17.2)；
Manufacture freshwater system (17) to be arranged in load Load System (7)；Manufacture freshwater system (17), airflight Housing system (18)
The circuit of circuit communication following at least one of which kind system, aircraft (1) or buoyance lift body (20), aerial wind power generating system
(2), the savings system (3) of dynamic power, control system (4), photovoltaic generating system (11).Remaining feature is implemented with embodiment 1-
Example 19.
Embodiment 21.Knowable to Figure 22, Figure 21 .1, it is a kind of floatage body (21) or floatage air bag (21.6) includes change
The aerial wind energy power station formula aircraft of volume main gasbag system (21.12) structure.
It is characterized in that: floatage body (21) or floatage air bag (21.6) include flexible buoyancy body (21.2)；Flexible floating
The cross sectional shape of power body (21.2) uses cylindrical shape；Cylindrical shape flexible buoyancy body (21.2) uses variable volume main gasbag
Longitudinal variable volume version (21.14) of system (21.12) structure.Wherein Figure 22 on ground, volume is when diminishing
State diagram, wherein Figure 22 .1 is the state diagram after high-altitude, volume have diminished.Remaining feature is with embodiment 1-embodiment 18.
The longitudinal variable volume version (21.14) using this strip cylindrical shape can produce 2 good effects.One, carries
High flying height.Flying height can rise to more than 5000m.Its two, improve flight speed.Owing to substantially reducing
The diameter of cylindrical shape flexible buoyancy body (21.2), cross-sectional area, and then greatly reduce the air drag of flight, thus have
Improve to effect the flight speed of several times.Remaining feature is with embodiment 1-embodiment 20.
Embodiment 22.This is the aerial wind energy power station formula aircraft that one is not provided with load Load System (7).
It is characterized in that: it is not provided with load Load System (7)；Savings system (3) (the such as electric power storage of its dynamic power
Pond) it is arranged on bottom, directly it is connected with hoist cable group's system (8) of aircraft (1) or buoyance lift body (20) or adjustable in length；Remaining
Feature is with embodiment 1-embodiment 21.
This high altitude wind energy electric power can be full of the savings system (3) (such as accumulator) of dynamic power, then aerial wind
Power station formula aircraft flight can drop to ground.The savings system (3) of its dynamic power can use earthward as power supply source
Electricity facility, equipment provide electric power.One, savings system (3) directly electricity consumption facility, the equipment the most earthward of dynamic power provide electricity
Power.Two, unload the savings system (3) of the dynamic power of full electricity, load the savings system (3) without electric dynamic power, and empty
Middle wind energy power station formula aircraft again flies and returns to enter aerial wind-power electricity generation state in the air, and high altitude wind energy electric power is continued to be full of
Savings system (3) without the dynamic power of electricity.Meanwhile, the savings system (3) of dynamic power of full electricity is unloaded directly the most earthward
Electricity consumption facility, equipment provide electric power.At this moment, this aerial wind energy power station formula aircraft is exactly a small-sized " aerial wind-power electricity generation
Stand ".
Embodiment 23.Knowable to Figure 19, Figure 20, it it is that one is provided with 2 layers of Mesh air antilift wire net (45) and content
The aerial fixing aircraft device (13) that the supporting docking of aerial wind energy power station formula aircraft (0) described in 1 is share.
It is characterized in that: it includes components described below, vertical mooring fixed system (30), aerial laterally bands system
(32), floatage body system (33), earth anchor system (36), connect sky mechanical splice system (41), lightning protection system (42), ice melting system
(43), location cable systems (44)；
Wherein vertical mooring fixed system (30) includes vertical mooring guy rope (34)；Wherein aerial laterally bands system
(32) including aerial laterally rope rope (35), its aerial laterally bands system (32) is with following at least one of which kind parts even
Connect, vertical mooring fixed system (30), lightning protection system (42), ice melting system (43)；Aerial laterally rope rope (35) includes a plurality of,
Its a plurality of aerial laterally rope rope (35) can intersect connection, forms aerial antilift wire net (45)；Wherein aerial antilift wire net
(45) 2 layers are included；Vertical mooring guy rope (34), aerial laterally rope rope are suspended or carry to its floatage body system (33) in midair
(35)；The upper end of its vertical mooring fixed system (30) connects floatage body system (33), under vertical mooring fixed system (30)
End connects earth anchor system (36)；The upper end of vertical mooring guy rope (34) be arranged on floatage body system (33) following at least a part of which it
A kind of position, top, top；The following at least one of which kind parts height away from ground between 300--25000 rice, buoyancy
System system (33), vertical mooring fixed system (30), aerial laterally bands system (32)；
Sky mechanical splice system (41) that connects therein can be arranged on vertical mooring guy rope (34), aerial laterally rope rope (35)
Position and being connected with it；Wherein connect sky mechanical splice system (41) and include following at least one of which kind parts, manual lock
Determine switching system (41.1), automatic locking switch system (41.2)；Wherein connecing sky mechanical splice system (41) can be with aerial
Realize connecting after ground connection collecting system of water (6) docking in aerial wind energy power station formula aircraft (0)；
Lightning protection system therein (42) and following at least one of which kind component locations, floatage body system (33), be vertically
Stay fixed system (30), aerial laterally bands system (32)；Wherein ice melting system (43) is arranged on following at least one of which kind
Component locations and being connected with its circuit, floatage body system (33), vertical power transmission cable (37), aerial laterally power transmission cable
(38)；Wherein position cable systems (44) to be made up of vertical mooring guy rope (34) or the vertical power transmission cable (37) of more than 3,
Make the floatage body system (33) can not horizontal displacement；
Embodiment 24.Knowable to Figure 19, Figure 20, Figure 21, Figure 21 ..1 Figure 21 .2, it is defeated to be that one is provided with 2 layers of Mesh air
Wire mesh (46) dock the aerial fixing flight share with aerial wind energy power station formula aircraft (0) described in content 1 supporting
Device device (13).
It is characterized in that: it also includes components described below, vertical power transmission cable (37), aerial laterally power transmission cable (38),
Connect empty electrically docking system (40)；Owing to vertical power transmission cable (37) also has mooring and the function of fixing airborne aircraft, because of
This vertical power transmission cable (37) is also a kind of vertical mooring guy rope (34)；Its vertical mooring guy rope (34) and vertical power transmission cable
(37) can be combined into one, they use following at least one of which kind combining form, and consubstantiality combines, allosome combines, double
Body combines；The circuit lower end connection external electrical network of vertical power transmission cable (37) therein or external electric energy savings device；At sky
In, owing to aerial laterally rope rope (35), vertical mooring guy rope (34) are connected to aerial laterally power transmission cable (38), vertical power transmission line
Cable (37), connect empty electrically docking system (40), thus can be avoided vertical power transmission cable (37), aerial laterally power transmission line
Cable (38), connecing that empty electrically docking system (40) is by powerful pulling force, cause damage power transmission lines installations and facilities；A plurality of,
Aerial laterally power transmission cable (38) intersects connection, forms aerial electrical grid (46)；
The circuit communication of aerial laterally power transmission cable (38) therein and following system, vertical power transmission cable (37), connects sky
Electrically docking system (40), ice melting system (43)；Aerial laterally power transmission cable (38) therein includes a plurality of, and it is a plurality of in the air
Laterally power transmission cable (38) can intersect connection, forms aerial electrical grid (46)；Wherein aerial electrical grid (46) bag
2 layers are included；Following at least one of which kind parts also include insulating barrier, vertical power transmission line (37, the most laterally power transmission cable
(38)；
The sky electrically docking system (40) that connects therein is connected with vertical mooring guy rope (34), aerial laterally rope rope (35)；Its
In the empty electrically docking system (40) that connects be arranged on following at least one of which kind component locations and be connected with its circuit, erect
To power transmission cable (37), aerial laterally power transmission cable (38)；The circuit communication connecing empty electrically docking system (40) therein is vertical
The upper circuit of power transmission cable (37), connects empty electrically docking system (40) and includes following at least one of which kind parts, manually
Electrical connector socket system (40.1), automatic electrical connector socket system (40.2)；Connecing empty electric docking system (40) can be with aerial sky
Ground connection plug mechanism (6.6) of the ground connection collecting system of water (6) of middle wind energy power station formula aircraft (0) realizes after being inserted into connection
Circuit communication；Remaining feature is with embodiment 23.
Embodiment 25.Knowable to Figure 19 .1, it it is that one is provided with 2 layers of Mesh air antilift wire net (45) and content 1 institute
The aerial fixing aircraft device (13) that the supporting docking of aerial wind energy power station formula aircraft (0) stated is share.
It is characterized in that: it includes components described below, in vertical mooring fixed system (30), use vertical mooring mast
(31) floatage body system (33) is replaced；Article 3, vertical mooring guy rope (34) or vertical power transmission cable (37) connect vertical mooring mast
(31) top, middle part composition location cable systems (44), make the vertical mooring mast (31) can not horizontal displacement；Remaining feature is same
Embodiment 23 or embodiment 24.
Claims (10)
1. aerial wind energy power station formula aircraft includes aircraft (1), and its aircraft (1) includes buoyance lift body (20), controls system
System (4), power propulsion system (5)；Or aerial wind energy power station formula aircraft includes buoyance lift body (20), control system (4), moves
Power propulsion system (5)；It is characterized in that:
Aerial wind energy power station formula aircraft also includes aerial wind power generating system (2), the savings system (3) of dynamic power, connects
Ground collecting system of water (6)；
Wherein power propulsion system (5) includes electric propulsion flight system (5.1)；
Wherein aerial wind power generating system (2) is arranged on following at least one of which kind alliance and is attached thereto, flight
Device (1) or buoyance lift body (20), the savings system (3) of dynamic power, control system (4), power propulsion system (5), electric propulsion fly
Row system (5.1), ground connection collecting system of water (6)；The wherein following at least one of which of circuit communication of aerial wind power generating system (2)
The circuit of kind of system, aircraft (1) or buoyance lift body (20), the savings system (3) of dynamic power, control system (4), electric propulsion fly
Row system (5.1), ground connection collecting system of water (6)；
Wherein the savings system (3) of dynamic power is arranged on following at least one of which kind position and is attached thereto, aircraft
(1) or buoyance lift body (20), aerial wind power generating system (2), control system (4), power propulsion system (5), electric propulsion flight system
System (5.1), ground connection collecting system of water (6)；The wherein circuit communication following at least one of which kind of the savings system (3) of dynamic power
The circuit of system, aircraft (1) or buoyance lift body (20), aerial wind power generating system (2), control system (4), electric propulsion flight system
System (5.1), ground connection collecting system of water (6)；
Wherein ground connection collecting system of water (6) is arranged on following at least one of which kind alliance and ground connection collecting system of water (6)
One end is attached thereto, aircraft (1) or buoyance lift body (20), aerial wind power generating system (2), the savings system (3) of dynamic power,
Control system (4), power propulsion system (5), electric propulsion flight system (5.1)；When needing, another of ground connection collecting system of water (6)
End can realize being connected after docking with following at least one of which kind object at any time, and ground is easily connected object (12), in the air
Fixing aircraft device (13), water body (14)；Wherein ground connection collecting system of water (6) is the aerial fixing aircraft device (13) connected
Connect sky mechanical splice system (41).
2. dock, with the supporting of the aerial wind energy power station formula aircraft described in claim 1, the aerial fixing aircraft device share
(13), it is characterised in that:
Aerial fixing aircraft device (13) includes components described below, vertical mooring fixed system (30), earth anchor system (36)；
Its vertical mooring fixed system (30) includes following at least one of which kind parts, vertical mooring mast (31), floatage body
System (33)；Its vertical mooring fixed system (30) also includes following at least one of which kind parts, vertical mooring guy rope
(34), vertical power transmission cable (37), location cable systems (44)；
Vertical mooring mast (31) therein can suspend or carry following at least one of which kind parts, floatage body system in midair
(33), vertical mooring guy rope (34), vertical power transmission cable (37), location cable systems (44)；And vertical mooring mast (31)
Upper end is connected to the upper end of following at least one of which kind parts, floatage body system (33), vertical mooring guy rope (34), the most defeated
Electric wire cable (37), location cable systems (44)；
Floatage body system (33) therein can suspend or carry following at least one of which kind parts, vertical mooring mast in midair
(31), vertical mooring guy rope (34), vertical power transmission cable (37), location cable systems (44)；And floatage body system (33) is even
The upper end of the most following at least one of which kind parts, vertical mooring mast (31), vertical mooring guy rope (34), vertical power transmission cable
(37), location cable systems (44)；Its vertical mooring mast (31) or vertical mooring guy rope (34) or vertical power transmission cable (37) or
The upper end of location cable systems (44) is arranged on the following at least one of which kind position of floatage body system (33), top, top,
Middle part, bottom；
The upper end of vertical mooring guy rope (34) therein is connected to following at least one of which kind parts, floatage body system (33),
The vertical top of mooring mast (31), vertical power transmission cable (37)；The lower end of vertical mooring guy rope (34) therein connects earth anchor system
System (36)；
The upper end of vertical power transmission cable (37) therein is connected to following at least one of which kind parts, floatage body system (33),
The vertical top of mooring mast (31), the top of vertical mooring guy rope (34)；Outside the circuit lower end connection of vertical power transmission cable (37)
Portion's electrical network or external electric energy savings device；
Location therein cable systems (44) includes at least 3 vertical mooring guy ropes (34) or vertical power transmission cable (37) group
Become；Vertical power transmission cable (37) can also be a kind of vertical mooring guy rope (34)；
Its earth anchor system (36) is connected to the lower end of following at least one of which kind parts, vertical mooring mast (31), vertical mooring
Rope rope (34), vertical power transmission cable (37), location cable systems (44).
Aerial wind energy power station the most according to claim 1 formula aircraft, it is characterised in that:
Its aircraft (1) or buoyance lift body (20) connect following at least one of which kind system, aerial wind power generating system (2), dynamic
The savings system (3) of power electric energy, control system (4), power propulsion system (5), electric propulsion flight system (5.1), ground connection water receiving
System (6)；Its aircraft (1) includes buoyance lift body (20)；
The circuit of the circuit communication following at least one of which kind system of its control system (4), aircraft (1) or buoyance lift body
(20), aerial wind power generating system (2), the savings system (3) of dynamic power, power propulsion system (5), electric propulsion flight system
(5.1), ground connection collecting system of water (6)；
Its power propulsion system (5) or electric propulsion flight system (5.1) connect following at least one of which kind system, aircraft
Or buoyance lift body (20), aerial wind power generating system (2), the savings system (3) of dynamic power, control system (4), ground connection connect (1)
Water system (6)；The circuit of the circuit communication following at least one of which kind system of electric propulsion flight system (5.1) therein, empty
Middle wind generator system (2), the savings system (3) of dynamic power, control system (4), ground connection collecting system of water (6).
Aerial wind energy power station the most according to claim 1 formula aircraft；It is characterized in that:
Its aerial wind power generating system (2) includes following at least one of which kind parts, blade (21), electromotor (22)；Its
Aerial wind power generating system (2) also includes following at least one of which kind mechanism, speed adjusting gear (23), becomes pitch mechanism
(24), blade fold mechanism (25), flight advance generating function changing-over mechanism (26), guard ring or duct mechanism (27), just transfer from one department to another
System (9)；
The savings system (3) of its dynamic power includes following at least one of which kind parts, accumulator (3.1), electric capacity
(3.2), fuel cell (3.3), point distribution system (3.4)；The savings system (3) of its dynamic power is arranged on following at least a part of which
One position and be attached thereto, aircraft (1) or buoyance lift body (20), aerial wind power generating system (2), control system (4),
Power propulsion system (5), electric propulsion flight system (5.1), ground connection collecting system of water (6), control system (4)；
Its ground connection collecting system of water (6) includes following at least one of which kind parts, butt joint mechanism (6.1), water receiving mechanism
(6.7)；One end of its butt joint mechanism (6.1) or water receiving mechanism (6.7) connects following at least one of which kind system, flight
Device (1) or buoyance lift body (20), aerial wind power generating system (2), the savings system (3) of dynamic power, control system (4), power
Propulsion system (5), electric propulsion flight system (5.1)；
Its aerial wind energy power station formula aircraft flight is easily connected object (12), fixes in aircraft device (13) in the air to ground
When connecing sky mechanical splice system (41) position, the other end of butt joint mechanism (6.1) can dock and connect ground afterwards
Easily connected object (12), fix aircraft device (13) in the air；Wherein the other end of butt joint mechanism (6.1) can connect
Lead to aerial fixing aircraft device (13) connects sky mechanical splice system (41)；
Or when its aerial wind energy power station formula aircraft flight is to position, water surface sea, the other end of its water receiving mechanism (6.7) can
To discharge in water body (14)；
Its butt joint mechanism (6.1) includes following at least one of which kind mechanism, staple joint mechanism (6.1.1), dilates and connects
Head mechanism (6.1.2), ejection joint mechanism (6.1.3), magetic indicator joint mechanism (6.1.4)；Its water receiving mechanism (6.7) includes down
State at least one of which kind mechanism, umbrella shape water receiving mechanism (6.7.1), barrel-shaped water receiving mechanism (6.7.2), Fan Xing water receiving mechanism
(6.7.3)；Water receiving mechanism (6.7) includes thin-film body (6.7.5)；Thin-film body (6.7.5) constitutes umbrella shape, barrel-shaped, sail form drag water
Body；
The circuit of its ground connection collecting system of water (6) circuit communication following at least one of which kind system, aircraft (1) or buoyance lift body
(20), aerial wind power generating system (2), the savings system (3) of dynamic power, control system (4), electric propulsion flight system
(5.1)。
Aerial wind energy power station the most according to claim 1 formula aircraft；It is characterized in that:
Aircraft (1) or buoyance lift body (20) also include following at least one of which kind system, and its buoyance lift body (20) includes
Following at least one of which kind parts, floatage body (21), lifting body (22), rotor (23), buoyancy lift assembly (24)；Buoyance lift body
(20) front end presents following at least one of which kind shape, close-shaped, opening shape；The front end of its buoyance lift body (20) presents
Opening shape is lifting body (22)；
Floatage body (21) wherein includes following at least one of which kind portion body, buoyant gas (21.5), floatage air bag
(21.6), internal portioning layer (21.7), heat-insulation layer (21.8), balloonet system (21.9), air-pump inflating system (21.10)；Its buoyancy
Air bag (21.6) includes buoyant gas (21.5)；The density of buoyant gas (21.5) is less than aircraft outer air density；Floating
Power body (21) includes following at least one of which kind parts, rigidity floatage body (21.1), flexible buoyancy body (21.2), hard and soft group
Close floatage body (21.3)；Its internal portioning layer (21.7) is arranged on floatage body (21), the inside of floatage air bag (21.6)；Its internal portioning layer
(21.7) floatage body (21), floatage air bag (21.6) these part components can be isolated into multiple cavity；
Wherein lifting body (22) includes following at least one of which kind parts, rigidity lifting body (22.1), flexible lifting body
(22.2), hard and soft combination lifting body (22.3)；Lifting body (22) includes following at least one of which kind bodies, profile lift
Body (22.5), sail type lifting body (22.6), umbellate form lifting body (22.7), mixed type lifting body (22.8)；
Hard and soft combination floatage body (21.3) therein or hard and soft combination lifting body (22.3) include following at least one of which kind
Combinative structure form: its top is rigidity floatage body (21.1) or rigidity lifting body (22.1), is rigidity floatage body in the middle part of it
Or rigidity lifting body (22.1), its underpart are that rigidity floatage body (21.1) or rigidity lifting body (22.1), its top are (21.1)
Flexible buoyancy body (21.2) or flexible lifting body (22.2), it is flexible buoyancy body (21.2) or flexible lifting body in the middle part of it
(22.2), its underpart is flexible buoyancy body (21.2) or flexible lifting body (22.2)；
Wherein buoyancy lift assembly (24) includes 2 kinds of parts of following at least a part of which, floatage body (21), lifting body (22), rotation
The wing (23)；
Wherein heat-insulation layer (21.8) is arranged on floatage body (21) or the outside of floatage air bag (21.6) or inside；
Wherein balloonet system (21.9) is arranged on floatage body (21) or the outside of floatage air bag (21.6) or inside；
Wherein air-pump inflating system (21.10) has pipeline to be connected in following at least one of which kind parts, floatage body
(21), floatage air bag (21.6), balloonet system (21.9).
Aerial wind energy power station the most according to claim 1 formula aircraft, it is characterised in that:
Aerial wind energy power station formula aircraft or aircraft (1) or buoyance lift body (20) also include following at least one of which kind
System, load Load System (7), hoist cable group's system (8) of adjustable in length, just transfer from one department to another unite (9), photovoltaic generating system (11),
Cooling or compression storage gas system (15), electric heating system (16), manufacture freshwater system (17), airflight Housing system
(18)；
Its buoyance lift body (20) and aerial wind power generating system (2) or the savings system (3) of dynamic power or control system (4) or dynamic
Hoist cable group's system (8) of power propulsion system (5) or ground connection collecting system of water (6) or load Load System (7) or adjustable in length
Connect and include following at least one of which kind mode, be directly connected to, be indirectly connected with；Between the connection of buoyance lift body (20) includes
When connecing in succession, its buoyance lift body (20) and aerial wind power generating system (2) or the savings system (3) of dynamic power or control system
(4) or power propulsion system (5) or ground connection collecting system of water (6) or load Load System (7) or adjustable in length hoist cable group system
Include hoist cable group's system (8) of adjustable in length between system (8), constitute and be indirectly connected with；
Its control system (4) includes following at least one of which kind system, pilot steering control system (4.1), automatic Pilot
Control system (4.2), mixing Ride Control System (4.3)；Its mixing Ride Control System (4.3) includes pilot steering control
System (4.1) and automatic Pilot control system (4.2)；Its control system (4) is arranged on following at least one of which kind position also
And be attached thereto, aircraft (1) or buoyance lift body (20), aerial wind power generating system (2), the savings system (3) of dynamic power, dynamic
Power propulsion system (5), ground connection collecting system of water (6), load Load System (7), hoist cable group's system (8) of adjustable in length；
Its power propulsion system (5) is arranged on following at least one of which kind position, aircraft (1) or buoyance lift body (20), load
Load System (7), hoist cable group's system (8) of adjustable in length, aerial wind power generating system (2)；Its power propulsion system (5) is also
Include following at least one of which kind, electric propulsion flight system (5.1), internal combustion engine propulsion system (5.2), jet propulsion system
(5.4), manual feed system (5.5), hybrid propulsion system (5.6)；Its electric propulsion flight system (5.1) includes following
At least one of which kind, electric propeller propulsion system (5.1.1), electric heating propulsion system (5.1.2), electrostatic propulsion system
(5.1.3), electromagnetic type propulsion system (5.1.4), electric laser formula propulsion system (5.1.5), electricity microwave type propulsion system
(5.1.6), electric chemical formula propulsion system (5.1.7)；
Wherein hybrid propulsion system (5.6) includes 2 kinds of systems of following at least a part of which, electric propulsion flight system (5.1),
Internal combustion engine propulsion system (5.2), jet propulsion system (5.4), manual feed system (5.5)；
Wherein electric propeller propulsion system (5.1.1) includes following at least one of which kind parts, blade (21), electromotor
(22)；Its electric propeller propulsion system (5.1.1) also includes following at least one of which kind mechanism, speed adjusting gear (23),
Become pitch mechanism (24), blade fold mechanism (25), flight advance generating function changing-over mechanism (26), guard ring or duct mechanism
(27), just transfer from one department to another to unite (9)；Blade therein (21) connects at least one parts following: electromotor (22), become pitch mechanism
(24), blade fold mechanism (25), flight advance generating function changing-over mechanism (26)；
Its load Load System (7) is arranged on following at least one of which kind position and is attached thereto, aircraft (1) or buoyance lift
Body (20), aerial wind power generating system (2), the savings system (3) of dynamic power, control system (4), power propulsion system (5),
Ground connection collecting system of water (6), hoist cable group's system (8) of adjustable in length, photovoltaic generating system (11)；Load Load System (7) is used
In accommodating, loading personnel's goods；
Its load Load System (7) and aircraft (1) or buoyance lift body (20) or aerial wind power generating system (2) or dynamic power
Savings system (3) or control system (4) or power propulsion system (5) or ground connection collecting system of water (6) or load Load System (7) or
The connection of hoist cable group's system (8) of adjustable in length includes following at least one of which kind mode, is directly connected to, in succession
Connect；When the connection of load Load System (7) include be indirectly connected with time, its load Load System (7) and aerial wind-power electricity generation system
System (2) or the savings system (3) of dynamic power or control system (4) or power propulsion system (5) or ground connection collecting system of water (6) or
Include hoist cable group's system (8) of adjustable in length between hoist cable group's system (8) of adjustable in length, constitute and be indirectly connected with；
Hoist cable group's system (8) of its adjustable in length includes hoist cable (8.1), and hoist cable group's system (8) of its adjustable in length is also
Include following at least one of which kind mechanism, electric rolling rope mechanism (8.2), manual Juan Suo mechanism (8.3)；Part hoist cable
(8.1) it is wrapped in the wire drum of electric rolling rope mechanism (8.2) or manual Juan Suo mechanism (8.3), or one of hoist cable (8.1)
Divide in the wire drum being wrapped in electric rolling rope mechanism (8.2) or manual Juan Suo mechanism (83)；When load Load System (7) and flight
The savings system (3) of device (1) or aerial wind power generating system (2) or dynamic power or power propulsion system (5) or ground connection water receiving
The connection of system (6) includes when being indirectly connected with, and aerial wind energy power station formula aircraft also includes the hoist cable group of adjustable in length
System (8)；Its load Load System (7) and aircraft (1) or buoyance lift body (20) or aerial wind power generating system (2) or power current
The hoist cable of adjustable in length is included between savings system (3) or power propulsion system (5) or the ground connection collecting system of water (6) of energy
Group's system (8), constitutes and is indirectly connected with；
Its hectare transfers from one department to another system (9) and is arranged on following at least one of which kind position and is attached thereto, aircraft (1) or buoyance lift body
(20), aerial wind power generating system (2), the savings system (3) of dynamic power, power propulsion system (5), ground connection collecting system of water
(6), load Load System (7), hoist cable group's system (8) of adjustable in length, photovoltaic generating system (11)；Its hectare transfers from one department to another to unite (9)
Following at least one of which kind system, system (9.1) is transfered from one department to another in rotation just, regulation hoist cable transfers from one department to another to unite (9.2) just；
Its photovoltaic generating system (11) includes photovoltaic cell (11.1)；Photovoltaic generating system (11) or photovoltaic cell (11.1) set
Put the upper surface in following at least one of which kind position or side surface, aircraft (1) or buoyance lift body (20), aerial wind-power electricity generation
System (2), the savings system (3) of dynamic power, power propulsion system (5), electric propulsion flight system (5.1), ground connection water receiving system
System (6), load Load System (7), hoist cable group's system (8) of adjustable in length, just transfer from one department to another unite (9)；Its photovoltaic generating system
(11) with following at least one of which kind system or the circuit communication of system, aircraft (1) or buoyance lift body (20), electric propulsion flight
System (5.1), aerial wind power generating system (2), the savings system (3) of dynamic power, ground connection collecting system of water (6).
Wherein manufacture freshwater system (17) and include following at least one of which kind, condensing water vapor system (17.1), desalinization
System (17.2)；Manufacture freshwater system (17) to be arranged in load Load System (7)；Manufacture the circuit communication of freshwater system (17)
The circuit of following at least one of which kind system, aircraft (1) or buoyance lift body (20), aerial wind power generating system (2), power current
The savings system (3) of energy, control system (4), photovoltaic generating system (11)；
Wherein airflight Housing system (18) is arranged on load Load System (7) position and is attached thereto；Airflight room
The circuit of the circuit communication following at least one of which kind system of house system (18), aircraft (1) or buoyance lift body (20), aerial wind
Force generating system (2), the savings system (3) of dynamic power, control system (4), photovoltaic generating system (11).
7. according to the aerial wind energy power station formula aircraft described in claim 4 or claim 6；It is characterized in that:
Its aerial wind power generating system (2) and electric propeller propulsion system (5.1.1) are one or consubstantiality；By flying
Row advance generating function changing-over mechanism (26), make propelling, generating both functions can mutually change, switch operating；
Its ground connection collecting system of water (6) also includes following at least one of which kind mechanism, ground connection rope (6.2), unmanned plane mechanism
(6.3), ground connection mechanism of twisting rope (6.4), earth conductor cable (6.5), ground connection plug mechanism (6.6)；
Wherein ground connection mechanism of twisting rope (6.4) connects following at least one of which kind mechanism, aircraft (1) or buoyance lift body (20), empty
Middle wind generator system (2), the savings system (3) of dynamic power, control system (4), power propulsion system (5), ground connection water receiving
System (6), load Load System (7)；
Wherein ground connection rope (6.2) or earth conductor cable (6.6) are wrapped on ground connection mechanism of twisting rope (6.4)；
Wherein the lower end of ground connection rope (6.2) or earth conductor cable (6.6) connects following at least one of which kind mechanism, butt joint machine
Structure (6.1), unmanned plane mechanism (6.3), ground connection plug mechanism (6.6)；Butt joint mechanism (6.1) or ground connection plug mechanism
(6.6) unmanned plane mechanism (6.3) is connected；
The wherein circuit of the upper end circuit communication following at least one of which kind system of earth conductor cable (6.5), aircraft (1) or floating
Rise body (20), aerial wind power generating system (2), the savings system (3) of dynamic power, control system (4), electric propulsion flight system
(5.1), photovoltaic generating system (11)；Lower end circuit communication ground connection plug mechanism (6.6) of earth conductor cable (6.5)；Ground connection electricity
Plug mechanism (6.6) connects following at least one of which kind mechanism, butt joint mechanism (6.1), unmanned plane mechanism (6.3)；
Wherein butt joint mechanism (6.1) or ground connection plug mechanism (6.6) can be one or consubstantiality；Wherein ground connection
Rope (6.2) or earth conductor cable (6.6) can be one or consubstantiality；So can reduce weight.
8. according to the aerial wind energy power station formula aircraft described in claim 5 or claim 6；It is characterized in that:
The cross sectional shape of its floatage body (21) or floatage air bag (21.6) includes following at least one of which kind, wing body shape
Shape, fairing shape, spindle shape, ellipsoidal shape, cylindrical shape, shuttle shape, rugby ball shape, oblong-shaped,
Square shape；Floatage body (21) or floatage air bag (21.6) include single or multiple；Its floatage body (21) or buoyancy gas
The utricule structure of capsule (21.6) includes following at least one of which kind, determines volume main gasbag system (21.11) structure, " determines body
Long-pending main gasbag system (21.10)+balloonet system (21.9) " structure, variable volume main gasbag system (21.12) structure, " variable volume
Main gasbag system (21.12)+balloonet system (21.9) "；
" variant type sky airship " therein version includes following at least one of which kind, radially variable volume version
(21.13), longitudinal variable volume version (21.14)；
Internal combustion engine propulsion system (5.2) or the jet propulsion system (5.4) of its power propulsion system (5) can use buoyant gas
(1) as fuel；Internal combustion engine propulsion system (5.2) or jet propulsion system (5.4) with in following at least one of which kind parts
Buoyant gas (21.5) have pipeline to connect, floatage body (21), floatage air bag (21.6)；
Its load Load System (7) includes following at least one of which kind, manned or driving pedestal (7.1), manned or driving
Nacelle (7.2), loading nacelle (7.3), loading support body (7.4), loading pedestal (7.5), house or office room house body (7.6)；
Hoist cable group's system (8) of its adjustable in length can also be directly connected to floatage air bag (21.6)；
Its photovoltaic generating system (11) also includes following at least one of which kind parts, and inverter, load governor, tracking are too
Sunlight system；Its photovoltaic generating system (11) or photovoltaic cell (11.1) can also be arranged on following at least one of which kind position
Upper surface or side surface；Hoist cable group's system (8) of adjustable in length, just transfer from one department to another to unite (9)；Its photovoltaic cell (11.1) includes
Following include a following type: crystal silicon type battery, amorphous silicon type battery, film type battery, flexible thin film type battery, poly-
Light type battery, multi-element compounds type battery, dye sensitization type battery, CaAs type battery, CIGS type battery, CdTe type battery,
InGaP/A type battery.
Buoyant gas (21.5) includes following at least one of which kind, hydrogen, helium, ammonia, steam, combustion gas；
Wherein cool down or compress storage gas system (15) and the buoyant gas (21.5) in following at least one of which kind parts
Pipeline is had to connect, floatage body (21), flexible buoyancy body (21.2), floatage air bag (21.6)；
In wherein electric heating system (16) is arranged on floatage body (21) or floatage air bag (21.6), the electricity of electric heating system (16)
Road connects the circuit of following at least one of which kind system, aircraft (1) or buoyance lift body (20), aerial wind power generating system
(2), the savings system (3) of dynamic power, control system (4), photovoltaic generating system (11).
Aerial fixing aircraft device (13) the most according to claim 2；It is characterized in that:
Aerial fixing aircraft device (13) also includes following at least one of which kind parts, connects sky mechanical splice system
(41), empty electrically docking system (40) is connect；
Its vertical mooring fixed system (30) is connected with following at least one of which kind parts, connect sky mechanical splice system (41),
Connect empty electrically docking system (40)；
Sky mechanical splice system (41) that connects therein can be with the ground connection collecting system of water of aerial aerial wind energy power station formula aircraft
(6) realize after docking connecting；
The upper circuit connecing the empty electrically vertical power transmission cable of the circuit communication (37) of docking system (40) therein, connects sky the most right
Welding system (40) can be with the ground connection plug mechanism of the ground connection collecting system of water (6) of aerial aerial wind energy power station formula aircraft
(6.6) after docking, connection realizes circuit communication.
10. according to the aerial fixing aircraft device (13) described in claim 2 or claim 9, it is characterised in that:
Aerial fixing aircraft device also includes following at least one of which kind parts, aerial laterally bands system (32), keeps away
Thunder system (42), ice melting system (43)；
Vertical mooring guy rope (34) can be combined into one with vertical power transmission cable (37), they following at least a part of which of employing it
A kind of combining form, consubstantiality combines, allosome combines, binary combines；
Floatage body system (33) can also suspend or carry aerial laterally bands system (32) in midair；
Aerial laterally bands system (32) includes following at least one of which kind parts, aerial laterally rope rope (35), in the air horizontal stroke
To power transmission cable (38)；Aerial laterally power transmission cable (38) is also a kind of aerial laterally rope rope (35)；Its aerial laterally rope rope
(35) can be combined into one with aerial laterally power transmission cable (38), they use following at least one of which kind to combine shape
Formula, consubstantiality combines, allosome combines, binary combines；
Aerial laterally bands system (32) is connected with following at least one of which kind parts, vertical mooring fixed system (30), keeps away
Thunder system (42), ice melting system (43)；Aerial laterally bands system (32) includes wall scroll or a plurality of, its a plurality of aerial laterally
Bands system (32) can intersect connection, forms aerial antilift wire net (45)；Wherein aerial antilift wire net (45) includes
Monolayer or multilamellar；
Aerial laterally power transmission cable (38) therein and the circuit communication of following at least one of which kind parts, vertical power transmission cable
(37), empty electrically docking system (40), ice melting system (43) are connect；Aerial laterally power transmission cable (38) therein include wall scroll or
Person is a plurality of, and its a plurality of aerial laterally power transmission cable (38) can intersect connection, forms aerial electrical grid (46)；Its hollow
Middle electrical grid (46) includes monolayer or multilamellar；Following at least one of which kind parts also include insulating barrier, the most defeated
Electric wire (37, the most laterally power transmission cable (38)；
Connect empty electrically docking system (40) be arranged on following at least one of which kind component locations and be connected with its circuit, perpendicular
To power transmission cable (37), aerial laterally power transmission cable (38)；Connect empty electrically docking system (40) include following at least a part of which it
A kind of parts, manual electrical connector socket system (40.1), automatic electrical connector socket system (40.2)；
Connect sky mechanical splice system (41) aerial laterally bands system (32) position to be arranged on and be connected with it；Wherein
Connect sky mechanical splice system (41) and include following at least one of which kind parts, manual locking switching system (41.1), automatically
Locking switch system (41.2)；
Lightning protection system (42) and following at least one of which kind component locations, floatage body system (33), vertical mooring fixed system
(30), aerial laterally bands system (32)；
Ice melting system (43) is arranged on following at least one of which kind component locations and is connected with its circuit, floatage body system
(33), vertical power transmission cable (37), aerial laterally power transmission cable (38)；
The following at least one of which kind parts height away from ground, between 100-10000 rice, floatage body system (33), is vertically
Stay fixed system (30), aerial laterally bands system (32).
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| CN201610218029.6A CN106218849A (en) | 2016-04-02 | 2016-04-02 | Aerial wind energy power station formula aircraft and aerial fixing aircraft device |
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|---|---|---|---|
| CN201610218029.6A CN106218849A (en) | 2016-04-02 | 2016-04-02 | Aerial wind energy power station formula aircraft and aerial fixing aircraft device |
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| CN106218849A true CN106218849A (en) | 2016-12-14 |
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| CN (1) | CN106218849A (en) |
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| CN107352023A (en) * | 2017-05-24 | 2017-11-17 | 深圳大学 | Aircraft |
| CN108583913A (en) * | 2018-04-13 | 2018-09-28 | 合肥凯石投资咨询有限公司 | Towed solar powered aircraft and its take-off and landing device |
| CN109398674A (en) * | 2018-09-11 | 2019-03-01 | 中国科学院光电研究院 | Tandem is tethered at aerostatics and its distribution method |
| CN110285016A (en) * | 2019-05-14 | 2019-09-27 | 曾庆福 | A kind of float-type aerial wind power generating system |
| CN110573727A (en) * | 2017-04-13 | 2019-12-13 | 圣弗里奇有限公司 | High-altitude wind power station tied on ground |
| CN110621876A (en) * | 2017-05-11 | 2019-12-27 | 维斯塔斯风力系统有限公司 | Wind turbine and onboard wind energy system sharing yaw system |
| CN110740932A (en) * | 2017-04-27 | 2020-01-31 | R·I·米勒 | Systems, methods, and apparatus to improve safety and functionality of aircraft having or more rotors |
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