CN103523233B - Based on many short distances stop over type electric airplane transport systems of intelligent grid - Google Patents
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- 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
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Abstract
The present invention relates to a kind of many short distances based on intelligent grid stop over type electric airplane transport systems, for solving quick traffic shortage problem between small and medium-sized cities, its be between adjacent small and medium-sized cities or and and adjacent center city satellite city between low altitude aircraft course line be set configure electric power storage electric airplane; Small and medium-sized cities and satellite city construction supply the airpark of landing, electric power storage electric airplane is configured with super capacitor storage power device, airpark is furnished with the super capacitor electric power storage station obtaining trough-electricity from intelligent grid, during each airpark of electric power storage electric airplane stop over, the super capacitor storage power device of electric power storage electric airplane all carries out fast charge by charge system from the super capacitor electric power storage station in stop over airpark.It has and can make full use of short distance stop over electric energy supplement advantage and electrical network trough-electricity and to have more than needed advantage, expand the new domestic demand of cleanliness without any pollution electric power energy, Optimization of Energy Structure, meet the urgent need to quick traffic between small and medium-sized cities and satellite city, key city, take up an area less, small investment, operating cost are low, can significantly promote most optimum distribution of resources between small and medium-sized cities economical integration process and small and medium-sized cities, excite the advantage of the small and medium-sized cities motive force of development.
Description
Technical field
The present invention relates to a kind of aircraft, particularly relate to a kind of many short distances based on intelligent grid stop over type electric airplane transport systems.
Background technology
At present, intercity fast public traffic system particularly between small and medium-sized cities remains the important force pulling economic development.Existing intercity bus can not meet the actual demand of the growing intercity quick circulation of people far away slowly due to speed, on the one hand, this kind of public transport is mostly that the pollution that the tail gas of emission of diesel engine causes to air is also anxious to be resolved, on the other hand, fuel oil belongs to the non-renewable rare energy, is badly in need of being substituted by other more clean energy more than needed or clean reproducible energy form improving in energy mix; Existing intercity light rail is high due to cost height operating cost, does not just have feasibility economically little medium and small intercity of passenger flow volume at all; Existing high ferro, motor-car, more owing to taking up an area, high cost, does not more have feasibility economically.So, be badly in need of a kind of less than novel medium and small intercity the quick public transport transportation system polluting, take up an area less, small investment, running velocity are fast, operating cost is low between all small and medium-sized cities of China.
Intelligent grid (smart power grids), it is exactly the intellectuality of electrical network, be also referred to as " electrical network 2.0 ", it is based upon integrated, on the basis of high-speed bidirectional communication network, by sensing and the measurement technique of advanced person, advanced equipment and technology, the application of advanced control method and the decision support system technology of advanced person, realize the reliable of electrical network, safety, economical, efficiently, the target of environmental friendliness and use safety, its principal character comprises self-healing, encourage and comprise user, resist attack, the quality of power supply meeting 21 century user's request is provided, allow the access of various different forms of electricity generation, start the optimization Effec-tive Function of electricity market and assets.Particularly intelligent grid can also provide cheap electrical network trough-electricity, for deep development electrical usage technology provides support and ensures in the mode of scientific and reasonable high efficient and reliable to user.
Summary of the invention
The object of the invention is the above-mentioned defect overcoming prior art, provide a kind of occupation of land less, low, the cleanliness without any pollution of small investment, operating cost, fast and easily based on many short distances stop over type electric airplane transport systems of intelligent grid.
For achieving the above object, the many short distances stop over type electric airplane transport systems that the present invention is based on intelligent grid be between adjacent small and medium-sized cities or and and adjacent center city satellite city between low altitude aircraft course line be set, configure electric power storage electric airplane along described airline operation; Described small and medium-sized cities and satellite city construction have the airpark for the landing of described electric power storage electric airplane, described electric power storage electric airplane is configured with super capacitor storage power device, described airpark is furnished with the super capacitor electric power storage station obtaining trough-electricity from intelligent grid, during described each airpark of electric power storage electric airplane stop over, the super capacitor storage power device of described electric power storage electric airplane all carries out fast charge by charge system from the described super capacitor electric power storage station in stop over airpark.Although it is aircraft but non-oil consumption, greenhouse gases can not be produced, more can not produce the tail gas of atmosphere pollution; It utilizes the trough-electricity of intelligent grid as power, not only cleans, and can also save a large amount of operating cost; It builds railway or highway without the need to investment, can reduce investment outlay in a large number, and greater amount saves land used; It is aerial through, does not affect, arrive fast secure by ground speed limit or other load conditions; Particularly it belongs to short range stop over, and stop over must carry out fast charge by charge system, so power autonomous can the guarantee of aircraft is supplemented in time, there will not be electric energy deficiency to affect the situation of normal/cruise.Described aircraft is specifically electronic revolves oar fixed wing aircraft.It has occupation of land less, low, the cleanliness without any pollution of small investment, operating cost, efficient and convenient, the advantage of quick public trip needs between small and medium-sized cities can be met completely.
As optimization, described airpark is furnished with the boost installation or take-off-helping device that promote or pull described electric airplane to take off.What namely promote is boost installation, and what pull is take-off-helping device.Because the flight of this aircraft belongs to the low-latitude flying of short distance stop over, from last airport to next airport, aircraft only must take off, flat to fly, land, and when only taking off in these three links, power drain intensity is maximum.After boost installation described in adapted or take-off-helping device, not only can save a large amount of electric energy, more relatively can reduce the power configuration of aircraft, reduce cost and alleviate deadweight, improve load-carrying capacity and the flight support ability of aircraft.
As optimization, described boost installation is the electric boosted automobile of electric power storage or air assisted automobile or the fuel power automobile carrying compressed air tank; When described boost installation is the air assisted automobile carrying compressed air tank, described airpark is furnished with compressed air reservoir and the Air compressor to compressed air reservoir air feed, described Air compressor utilizes the trough-electricity of intelligent grid to storing compressed air in described compressed air reservoir, and described compressed air tank obtains pressurized air from described compressed air reservoir.The described boost installation pushed away forward compared with the described take-off-helping device drawn forward, more convenient configuration, safer.The air assisted automobile of compressed air-driven, can with the simplest structure, minimum cost compared with the automobile of other two kinds of power form, minimum energy storage cost, meets the help-fly needs exporting maximum driving force at short notice.
As optimization, described compressed air tank and compressed air reservoir are the thermally insulated tank of band insulating, described airpark terminal and other building are fitted with solar thermal collector, described solar thermal collector is by thermal medium delivery duct to the H Exch transfer heat be configured in described adiabatic compression air accumulator, and the heat from described thermal medium is passed to the pressurized air in adiabatic compression air accumulator by described H Exch; Described compressed air reservoir is by the insulated piping of easy disassembly or carry pressurized air with adiabatic valve to described adiabatic compression air holder; In a straightforward manner the solar power that solar thermal collector collects can be changed into pressurized air energy like this, significantly save help-fly cost.
The electric boosted automobile of described electric power storage is furnished with described super capacitor electrical storage device, and described super capacitor electrical storage device obtains trough-electricity from described intelligent grid; Or described super capacitor electrical storage device is put for convenience of the work of replacing is equipped, and described super capacitor electric power storage station is furnished with the described super capacitor electrical storage device of Gong the replacement of several times.Directly or indirectly obtain trough-electricity from intelligent grid also can reduce help-fly cost to the electric boosted automobile of electric power storage.Certainly can also be that the electric boosted automobile of described electric power storage was connected with the power supply of aircraft with the convenient automatic cable connection system automatically disconnected by convenient connection, boost phase is accepted at aircraft, there is provided to aircraft the electric energy that takes off by the cable of lashup, the power consumption burden reducing takeoff phase, strengthen ability of taking off, limited for preciousness is carried electric power for normally taking off and landing.After boosting terminates, the cable of described interim docking also disconnects thereupon, and after disconnecting, aircraft only uses the super capacitor electrical storage device carried to power.
As optimization, the wedge shape that described power-assisted car is flat short, the thick height in rear end in front end, middle part is increased by progressive additive after forward direction.Like this in help-fly process, the front of described power-assisted car and above can produce the up current of one upwards lifting, described power-assisted car, while pushing away forward, also promotes aircraft by described up current and upwards takes off.
As optimization, described wedge shape power-assisted car top is the ramp extended to the back-end from front end, the front end ground proximity of described ramp, and described ramp has the clear glass front window observing front situation for chaufeur.While described like this up current strengthens further, also can produce the positice ground effect and ground effect effect that contribute to taking off further.
As optimization, described electric power storage electric airplane is the rotary propeller type low latitude fixed wing aircraft being furnished with multilayer wing, the super capacitor of described super capacitor storage power device or described super capacitor storage power device is configured on described wing or on the afterbody of aircraft and described wing, such fuselage does not configure super capacitor, the fuselage of original design need not change, and only need redesign wing; Described aircraft is low speed or middle dopey.Described aircraft F-Zero below 400 kilometers/hour, such as, can be 200-360 kilometer/hour, preferred 260-300 kilometer/hour.On above-mentioned configuration mode basis, can also adopt further: described fuselage comprises the keel lattice plate intersected in length and breadth, the super capacitor of described super capacitor storage power device is configured in the grid that described keel lattice plate surrounds, can significantly increase super capacitor Disposing rate like this, be conducive to realizing under the prerequisite not reducing aircraft bearing space, increase considerably the object of described super capacitor storage power device power reservoir capacity.
Alternatives as arranged side by side with technique scheme: can also be that described fuselage comprises the keel lattice plate intersected in length and breadth, configure the super capacitor of described super capacitor storage power device in the grid that described keel lattice plate surrounds.Original like this wing design does not make any change, and only needing increases configuration super capacitor at original keel lattice plate, and configuration super capacitor also can not produce large impact to airframe structure, only needs to increase in original design basis to join.On this basis, described electric power storage electric airplane can be taked further to be the low latitude fixed wing aircraft being furnished with multilayer wing, and the super capacitor of described super capacitor storage power device or described super capacitor storage power device is configured on described wing or on the afterbody of aircraft and described wing.Very many capacitance of storage can be obtained like this.
As optimization, described wing comprises the lower floor's host wing and the upper strata slave wing extended to both sides from airframe top or the upper strata slave wing extended to both sides from airframe top and the top layer random wing be positioned at above the slave wing that extend to both sides in the middle part of airframe; Be fixed together by vertical or oblique or the vertical and oblique reinforcement that windage is little between adjacent described wing.Preferred: the described top layer random wing is fixed on the little support of windage that fuselage protrudes upward, together with also being reinforced with the slave wing below by described vertical or oblique or vertical and oblique reinforcement.
The wing of described fuselage both sides configures electric propeller side by side, and electric propeller is little relative to fuel power oar lightweight, is more conveniently configured on wing; Or each self-configuring side electric propeller and described fuselage roof configure two overhead electric propellers on the wing of described fuselage both sides, such four type drive paddles are compared with two type drive paddles, and power is stronger, and reliability is higher, and safety is better.During use, four screw propellers can be enabled when taking off and land, only using wherein two screw propellers when flat flying, preferably only with two screw propellers on the wing of both sides.
As optimization, between the base portion of between the middle part of neighbouring described wing or middle part and close fuselage, is furnished with described reinforcement.Also can increase between described wing and fuselage side and be furnished with oblique pull reinforcement.Described wing and fuselage configure solar panel, and described solar panel is charged to described super capacitor storage power device by charge circuit.Relatively can alleviate the self-powered load of aircraft like this, improve safe flight supportability.
As optimization, described lower floor host wing, the upper strata slave wing or and top layer random wing configuration straggly forward successively from the bottom to top.The air bolus of upwards support aircraft can be formed like this below described multilayer wing, the lift of aircraft and stagnant empty ability can be significantly improved, improve the ability of the complicated weather condition of reply.Lower floor's host wing, the upper strata slave wing can be 1/2,1/3,2/3,3/4,1/4,2/5,3/5,1/5 of relative misalignment wing width with the relative distance by means of opening before and after the top layer random wing.
Certainly on this basis, can adopt further and described electric propeller is arranged on the slave wing of upper strata or the technical scheme be arranged between lower floor's host wing and the upper strata slave wing, ground effect effect can be produced further like this, enlarge markedly aircraft load-carrying capacity.
After adopting technique scheme, the many short distances stop over type electric airplane transport systems that the present invention is based on intelligent grid has the advantage that can make full use of short distance stop over electric energy supplement and electrical network trough-electricity and to have more than needed advantage, expand the new domestic demand of cleanliness without any pollution electric power energy, Optimization of Energy Structure, meet the eager needs to quick transport between small and medium-sized cities and satellite city, key city, take up an area few, small investment, operating cost is low, efficient and convenient, greatly can promote small and medium-sized cities economical integration process and contribute to very much most optimum distribution of resources between small and medium-sized cities, improve small and medium-sized cities operational efficiency of the economy and the advantage exciting small and medium-sized cities economic development power.
Detailed description of the invention
The many short distances stop over type electric airplane transport systems that the present invention is based on intelligent grid be between adjacent small and medium-sized cities or and and adjacent center city satellite city between low altitude aircraft course line be set, configure rotary propeller type fixed-wing electric power storage electric airplane along described airline operation; Described small and medium-sized cities and satellite city construction have the airpark for the landing of described electric power storage electric airplane, described electric power storage electric airplane is configured with super capacitor storage power device, described airpark is furnished with the super capacitor electric power storage station obtaining trough-electricity from intelligent grid, during described each airpark of electric power storage electric airplane stop over, the super capacitor storage power device of described electric power storage electric airplane all carries out fast charge by charge system from the described super capacitor electric power storage station in stop over airpark.
Described airpark is furnished with the boost installation or take-off-helping device that promote or pull described electric airplane to take off.Preferred described boost installation is the electric boosted automobile of electric power storage or air assisted automobile or the fuel power automobile carrying compressed air tank; When described boost installation is the air assisted automobile carrying compressed air tank, described airpark is furnished with compressed air reservoir and the Air compressor to compressed air reservoir air feed, described Air compressor utilizes the trough-electricity of intelligent grid to storing compressed air in described compressed air reservoir, and described compressed air tank obtains pressurized air from described compressed air reservoir.More preferably described compressed air tank and compressed air reservoir are the thermally insulated tank of peripheral zone insulating, described airpark terminal and other building are fitted with solar thermal collector, described solar thermal collector is by thermal medium delivery duct to the H Exch transfer heat be configured in described adiabatic compression air accumulator, and the heat from described thermal medium is passed to the pressurized air in adiabatic compression air accumulator by described H Exch; Described compressed air reservoir by the insulated piping of easy disassembly or adiabatic valve to described adiabatic compression air holder conveying pressurized air; The electric boosted automobile of described electric power storage is furnished with described super capacitor electrical storage device, and described super capacitor electrical storage device obtains trough-electricity from described storage intelligent grid; Or described super capacitor electrical storage device is put for convenience of the work of replacing is equipped, and described super capacitor electric power storage station is furnished with the described super capacitor electrical storage device of Gong the replacement of several times.Certainly can also be that the electric boosted automobile of described electric power storage was connected with the power supply of aircraft with the convenient automatic cable connection system automatically disconnected by convenient connection, boost phase is accepted at aircraft, there is provided to aircraft the electric energy that takes off by the cable of lashup, the power consumption burden reducing takeoff phase, strengthen ability of taking off, limited for preciousness is carried electric power for normally taking off and landing.After boosting terminates, the cable of described interim docking also disconnects thereupon, and after disconnecting, aircraft only uses the super capacitor electrical storage device carried to power.
The wedge shape that described power-assisted car is flat short, the thick height in rear end in front end, middle part is increased by progressive additive after forward direction.Preferred described wedge shape power-assisted car top is the ramp extended to the back-end from front end, the front end ground proximity of described ramp, and described ramp has the clear glass front window observing front situation for chaufeur.
Described electric power storage electric airplane is the low latitude fixed wing aircraft being furnished with multilayer wing, the super capacitor of described super capacitor storage power device or described super capacitor storage power device is configured on described wing or on the afterbody of aircraft and described wing, on above-mentioned configuration mode basis, can also adopt further: described fuselage comprises the keel lattice plate intersected in length and breadth, in the grid that described keel lattice plate surrounds, configure the super capacitor of described super capacitor storage power device; Described aircraft is low speed or middle dopey; Described aircraft F-Zero below 400 kilometers/hour, such as, can be 200-360 kilometer/hour, preferred 260-300 kilometer/hour.
Or described fuselage comprises the keel lattice plate intersected in length and breadth, the super capacitor of described super capacitor storage power device is configured in the grid that described keel lattice plate surrounds, on this basis, described electric power storage electric airplane can be taked further to be the low latitude fixed wing aircraft being furnished with multilayer wing, and the super capacitor of described super capacitor storage power device or described super capacitor storage power device is configured on described wing or on the afterbody of aircraft and described wing.Described aircraft is low speed or middle dopey; Described aircraft F-Zero below 400 kilometers/hour, such as, can be 200-360 kilometer/hour, preferred 260-300 kilometer/hour.
Preferred described wing comprises the lower floor's host wing and the upper strata slave wing extended to both sides from airframe top or the upper strata slave wing extended to both sides from airframe top and the top layer random wing be positioned at above the slave wing that extend to both sides in the middle part of airframe; Be fixed together by vertical or oblique or the vertical and oblique reinforcement that windage is little between adjacent described wing;
On the wing of described fuselage both sides, on the wing configuring electric propeller or described fuselage both sides arranged side by side, each self-configuring side electric propeller and described fuselage roof configure two overhead electric propellers.During use, four screw propellers can be enabled when taking off and land, only using wherein two screw propellers when flat flying, preferably only with two screw propellers on the wing of both sides.
More preferably described reinforcement is furnished with between the middle part of neighbouring described wing or the base portion of middle part and close fuselage.Also can increase between described wing and fuselage side and be furnished with oblique pull reinforcement.Described wing and fuselage configure solar panel, and described solar panel is charged to described super capacitor storage power device by charge circuit.
More preferably described lower floor host wing, the upper strata slave wing or and top layer random wing configuration straggly forward successively from the bottom to top.Lower floor's host wing, the upper strata slave wing can be 1/2,1/3,2/3,3/4,1/4,2/5,3/5,1/5 of relative misalignment wing width with the relative distance by means of opening before and after the top layer random wing.Certainly on this basis, can adopt further and described electric propeller is arranged on the slave wing of upper strata or the technical scheme be arranged between lower floor's host wing and the upper strata slave wing, ground effect effect can be produced further like this, enlarge markedly aircraft load-carrying capacity.
Claims (10)
1., based on many short distances stop over type electric airplane transport systems of intelligent grid, it is characterized in that, low altitude aircraft course line is set between adjacent small and medium-sized cities or between the satellite city in small and medium-sized cities and adjacent center city, configures electric power storage electric airplane along described airline operation; Described small and medium-sized cities and satellite city construction have the airpark for the landing of described electric power storage electric airplane, described electric power storage electric airplane is configured with super capacitor storage power device, described airpark is furnished with the super capacitor electric power storage station obtaining trough-electricity from intelligent grid, during described each airpark of electric power storage electric airplane stop over, the super capacitor storage power device of described electric power storage electric airplane all carries out fast charge by charge system from the described super capacitor electric power storage station in stop over airpark.
2. aircraft dispatch system according to claim 1, is characterized in that described airpark is furnished with the boost installation or take-off-helping device promoted or pull described electric airplane to take off.
3. aircraft dispatch system according to claim 2, is characterized in that described boost installation is the electric boosted automobile of electric power storage or air assisted automobile or the fuel power automobile carrying compressed air tank; When described boost installation is the air assisted automobile carrying compressed air tank, described airpark is furnished with compressed air reservoir and the Air compressor to compressed air reservoir air feed, described Air compressor utilizes the trough-electricity of intelligent grid to storing compressed air in described compressed air reservoir, and described compressed air tank obtains pressurized air from described compressed air reservoir.
4. aircraft dispatch system according to claim 3, it is characterized in that described compressed air tank and compressed air reservoir are the thermally insulated tank of band insulating, described airpark terminal and other airport ancillary building are fitted with solar thermal collector, described solar thermal collector is by thermal medium delivery duct to the H Exch transfer heat be configured in described adiabatic compression air accumulator, and the heat from described thermal medium is passed to the pressurized air in adiabatic compression air accumulator by described H Exch; Described compressed air reservoir is by the insulated piping of easy disassembly or carry pressurized air with adiabatic valve to described adiabatic compression air holder;
The electric boosted automobile of described electric power storage is furnished with described super capacitor electrical storage device, and described super capacitor electrical storage device obtains trough-electricity from described intelligent grid; Or described super capacitor electrical storage device is put for convenience of the work of replacing is equipped, and described super capacitor electric power storage station is furnished with the described super capacitor electrical storage device of Gong the replacement of several times.
5. aircraft dispatch system according to claim 3 or 4, is characterized in that the wedge shape that described power-assisted car is flat short, the thick height in rear end in front end, middle part is increased by progressive additive after forward direction.
6. aircraft dispatch system according to claim 5, it is characterized in that described wedge shape power-assisted car top is the ramp extended to the back-end from front end, the front end ground proximity of described ramp, described ramp has the clear glass front window observing front situation for chaufeur.
7. aircraft dispatch system according to claims 1 or 2 or 3 or 4, it is characterized in that described electric power storage electric airplane is the rotary propeller type low latitude fixed wing aircraft being furnished with multilayer wing, the super capacitor of described super capacitor storage power device or described super capacitor storage power device is configured on described wing or on the afterbody of aircraft and described wing; Described aircraft is low speed or middle dopey;
Or the fuselage of described aircraft comprises the keel lattice plate intersected in length and breadth, in the grid that described keel lattice plate surrounds, configure the super capacitor of described super capacitor storage power device.
8. aircraft dispatch system according to claim 7, is characterized in that described wing comprises the lower floor's host wing and the upper strata slave wing extended to both sides from airframe top or the upper strata slave wing extended to both sides from airframe top and the top layer random wing be positioned at above the slave wing extended to both sides in the middle part of airframe; Be fixed together by vertical or oblique or the vertical and oblique reinforcement that windage is little between adjacent described wing;
On the wing of described fuselage both sides, on the wing configuring electric propeller or described fuselage both sides arranged side by side, each self-configuring side electric propeller and described fuselage roof configure two overhead electric propellers.
9. aircraft dispatch system according to claim 8, between the middle part that it is characterized in that neighbouring described wing or middle part and be furnished with described reinforcement between the base portion of fuselage; Described wing and fuselage configure solar panel, and described solar panel is charged to described super capacitor storage power device by charge circuit.
10. aircraft dispatch system according to claim 8, is characterized in that described lower floor host wing, the upper strata slave wing or and top layer random wing configuration straggly forward successively from the bottom to top.
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