CN101537777B

CN101537777B - Multi-functional water, land and space electric aerocar using wind and solar energy for generating electricity

Info

Publication number: CN101537777B
Application number: CN2009101388278A
Authority: CN
Inventors: 黄灿荣
Original assignee: Individual
Current assignee: Individual
Priority date: 2009-05-05
Filing date: 2009-05-05
Publication date: 2011-08-17
Anticipated expiration: 2029-05-05
Also published as: CN101537777A

Abstract

The invention relates to a transportation means, in particular to a multi-functional water, land and space electric aerocar using wind and solar energy for generating electricity. The invention aims at solving the technical problems of using no fuel, saving energy and automatically generating and charging electricity, and having multifunction in water, land and space for the electric aerocar. The multi-functional electric aerocar consists of four systems, namely a road system, a water navigation system, a wing horizontal expanding fight system and a helicopter flight system, and can be switched to two ways for fight: the wing horizontal expanding fight and the helicopter flight; and the electric motors arranged in the aerocar are all multi-functional electric motors. The subject of the aerocar adopts a streamlining shape in design; and the driving control room is internally provided with high-end technology equipment such as a driving joystick, a driving control switch system, an electronic computer automatic-control system, a global satellite positioning, navigation communication system, etc. The multi-functional electric aerocar is convenient to operate and control, and easy to drive, uses high-clean renewable energy, and is a comprehensive multi-purpose multi-functional transportation means in the future.

Description

Multi-functional water, land and space electric aerocar using wind and solar energy for generating electricity

One, technical field

The present invention relates to the vehicle, particularly a kind of have a multi-functional water, land and space electric aerocar using wind and solar energy for generating electricity.

Two, background technology

At present, the U.S. successfully makes first land and air double-used hovercar in the world on probation, in order further to save the energy, reduces the pollution of air ambient, slow down road traffic pressure, invention has wind energy, solar electrical energy generation and can be in the multiduty electronic carplane of water, land and air.

Three, summary of the invention

The technical problem to be solved in the present invention is without fuel oil, saves the energy, generating-charging and can be in the electronic carplane of water, land and air multi-purpose voluntarily.

In order to address the above problem, the technological means that the present invention adopts is:

Carplane is made up of four big systems: road traveling system, water boat system, wing horizontal development flight system and helicopter flight system, and changeable is that two kinds of modes are flown: wing horizontal development flight, helicopter flight, the motor of adapted all is multi-function motors on the carplane, can switch mutually by controlling switched system, i.e. both electrical generator, changeable again is electrical motor.

Its concrete structure comprises: the carplane main body adopts the streamline configuration design, help overall height speed and travel, in driving OPS, be furnished with: drive control lever and control high-end science and technology equipment such as switched system, automatic computer robot control system(RCS) and global positioning satellite navigation communication system, monitored meter system; The road traveling system: the front and rear wheel of car all adopts high-power wheel nave motor to drive and travels, the high-energy battery group is housed: (A) be the standby battery group for front-wheel battery pack commonly used, (C) in the car for trailing wheel battery pack commonly used, (B), (D) be storage battery dedicated group of helicopter, roof is equipped with wild goose shape arranges multi-functional wind power generation machine group, helping optimum air flows, reduce air resistance, save electric energy overall height speed is travelled, it can have the effect of quickening the run-up lift-off by switching to electrical motor the electrical generator of machine group; Water boat system: the lower front at headstock is equipped with the inflation air pump, being used for car spirit bed course puts on the air, the electric screw slurry of a tool telescopic folding formula is equipped with in the center, rear portion at the bottom of the car, being mainly used in driving under water travels and turns to, the bottom of car is provided with inflatable air cushion layer, can be used for the weight of bearing vehicle body on the water surface behind the top off; Four jiaos of dresses of car body bracing frame of triangular structure, the left and right sides, the place ahead is provided with the wind-force water conservancy diversion panel of outside one-tenth " eight " font on bracing frame, increase the flow velocity of air inlet area and quickening air for the wind power generation machine group of roof wild goose shape arrangement, to strengthen the electric energy generated that improves machine group, above bracing frame, be provided with frame surface layer platform, the wind power generating set of a multifunctional high-power is equipped with in frame surface layer dead ahead, it can be by controlling the electrical motor that switches to of switched system, become the propeller in dead ahead on the car, it is the active force of flying after the wing horizontal development, the front end of frame surface layer is provided with upwards air inlet curved panel, the rear end is that the arc impeller is controlled in activity, is provided with solar energy photovoltaic system on the top layer of frame surface layer; Wing horizontal development flight system: be installed in the frame surface layer left and right sides and be provided with folding extended position host wing, top layer at host wing is provided with solar energy photovoltaic system, be provided with movable aileron, in host wing, be provided with and stretch the lengthening wing, adopt steel cable to reinforce after the host wing horizontal development thereafter; Helicopter flight system: the flexible main shaft of helicopter is housed, on flexible main shaft, be provided with upper and lower blade screw slurry, the lower blade propeller is by the large power multifunctional direct motor drive that is contained in frame surface layer center, the lower blade propeller can be placed in the groove in the frame surface layer when driving a vehicle on the road surface, electronic blade is the helicopter main propeller, it is by the power supply of (D) battery pack, and it is the active force of helicopter airflight; In the afterbody left and right sides of frame surface layer revolving afterbody balance wing is housed, folding electric screw slurry is housed on its top, be mainly used in and control aerial turning to in-flight; Be furnished with electric energy-saving headlight and lighting system in the car, drive the OPS seat, take advantage of main structural components such as seat and external power charging inlet to form.

Four, description of drawings

Concrete structure of the present invention is provided by the following drawings.

Fig. 1 is the synthesis structure scheme drawing of the multi-functional water, land and space electric aerocar using wind and solar energy for generating electricity of proposition according to the present invention.(explain among the figure: it is to stretch lengthening wing (21) in order to see to be provided with in it that the top layer solar energy photovoltaic system that is installed in frame surface layer left side host wing (19) in this Fig. 1 is not drawn, the lengthening wing (21) of right side host wing (19) is in the full extension state, but its horizontal development reinforcing steel cable (22) does not draw; Frame surface layer afterbody left side balance wing (28) is in the plumbness of Rotate 180 °, its top Foldable electric propeller (29) is launched, the general normality that afterbody right side balance wing (28) keeps when being the road surface driving, its top electric screw slurry (29) is in folding form, and it is requiredly when using to switch realization by controlling switched system that the change of the various states of carplane is cut.)

Sign in the accompanying drawing is represented respectively:

1, the electronic carplane main body 2 of streamline contour, drive OPS 3, drive control lever and control switched system 4, automatic computer robot control system(RCS) and global positioning satellite navigation communication system 5, monitored meter system 6, high-power wheel nave motor 7, high-energy battery group: A is a trailing wheel battery pack commonly used, B is a front-wheel battery pack commonly used, C is that standby battery group D is storage battery dedicated a group 8 in helicopter, wild goose shape is arranged multi-functional wind power generation machine group 9, inflation air pump 10, the electric screw that travels under water slurry 11, car bottom inflatable air cushion layer 12 triangular structure bracing frame 13, the left and right sides, the place ahead " eight " font wind-force water conservancy diversion panel 14 on the bracing frame, the frame surface layer platform 15 that the bracing frame top is set, frame surface layer dead ahead multifunctional high-power wind power generating set 16, the frame surface layer front end air inlet curved panel 17 that makes progress, arc impeller 18 is controlled in the rear end activity of frame surface layer, the solar energy photovoltaic system on frame surface layer top layer and host wing top layer solar energy photovoltaic system 19, be installed in the folding extended position host wing 20 in the frame surface layer left and right sides, movable aileron 21, stretching, extension lengthening wing 22 in the host wing, steel cable 23 is reinforced in the host wing horizontal development, the helicopter main shaft 24 that stretches, lower blade propeller 25, the driving motor 26 of lower blade propeller, the lower blade propeller is placed groove 27, electronic blade helicopter main propeller 28, the rotary afterbody balance wing 29 in the frame surface layer afterbody left and right sides, top Foldable electric propeller 30 on the balance wing, electric energy-saving headlight and lighting system 31, drive OPS seat 32, take advantage of seat 33, the external power charging inlet

Five, the specific embodiment

Electronic carplane main body profile serves as main the manufacturing with lightweight materials such as fiber reinforced composite (FRP) or carbon materials, and main support is made with high-strength light alloy material (as aluminum magnesium alloy), and is solid and light and handy to alleviate tare, saves electric energy.

Carplane is charged to battery pack with the external power charging inlet before using, drive behind the full charge to travel, the main shaft of helicopter flight system (23) is in contraction state during driving, lower blade propeller (24) places in the groove (26), electric screw slurry (29) is folded on afterbody balance wing (28) top and places the left and right sides of frame surface layer afterbody, carplane road traveling: at first can enable battery pack (A) and the back wheels of vehicle wheel hub motor is driven travel, this moment car scooter 80～100km/h, enabling battery pack (B) again drives the front-wheel hub motor, the speed of a motor vehicle rises to 130～180km/h immediately, can control switched system for the speed of the lift-off that further steps on the juice or take off all multifunctional wind power generator groups (8) and (15) are switched to electrical motor, at this moment express scooter 200～300km/h.

Road traveling switches to wing horizontal development flight and the time presses and to control switched system (3) on the joystick, wing horizontal development flight system starts: the host wing (19) that is folded in the bracing frame left and right sides becomes horizontal development, the automatic full extension of lengthening wing (21) in it, afterbody left and right sides balance wing (28) outwards Rotate 180 ° is in vertical position and carries out the lift-off of taking off and prepare, balance wing top Foldable electric propeller (29) is organized work, raising along with the speed of a motor vehicle, the smooth operation lift-off, can be after the lift-off by automatic computer automatic control navigationsystem (4) flight at controls, aloft flight can be by frame surface layer dead ahead multifunctional high-power unit (15), it is powered by battery pack (C) becomes the active force of airflight, all the other wild goose shapes arrangement wind power generation machine groups (8) switch to the generating-charging state battery pack are charged at any time, simultaneously the electronic blade main propeller (27) of helicopter flight system being automatically switched to generating state charges to battery pack, solar energy photovoltaic system (18) also can increase electric energy generated battery pack is charged in the sun, flight arrives the destination can select the straight road surface of 300～500m stable landing, control switched system (3) then, lengthening wing (21) automatically retracts in the host wing (19), host wing is folded in the left and right sides of frame surface layer bracing frame (12), afterbody balance wing (28) is rotation automatically, and its top electric screw slurry (29) is folding to be resetted.If continue to travel on the road surface advances, then frame surface layer dead ahead multifunctional high-power wind power generating set (15) is switched to the generating-charging state battery pack is charged.Switch to operate when wing horizontal development flight the time need have the road surface of two-lane and front and back 1km with other vehicle ' of interior nothing by road traveling and switch the lift-off of taking off.

Use the helicopter flight system works: when electric energy is sufficient, carplane can be at the static state control switching system (3) of doing exercises of finishing drilling, start the equipment of helicopter flight system, the helicopter main shaft (23) that stretches upwards rises, afterbody left and right sides balance wing (28) outwards Rotate 180 ° is in plumbness, its top Foldable electric propeller (29) is organized work, enable go up (27) of helicopter main shaft, (24) blade screw slurry is worked simultaneously down, the mild lift-off of operation, can control flight at controls by automatic computer automatic control navigationsystem (4) after the lift-off, aloft flying, it can be flown for active force by electronic blade helicopter main propeller (27), the driving motor (25) of lower blade propeller (24), electrical generator cohort (8) and (15) all are cut to generating state, at any time battery pack is charged, solar energy photovoltaic system (18) also can increase electric energy generated battery pack is charged in the sun, also can be chosen on the lake surface behind the flight arrival destination and land, if at the lake surface water landing, should start earlier that inflation air pump (9) carries out behind the top off car bottom inflatable air cushion layer (11) can bearing vehicle body weight, switched system (3) is controlled in the landing back, afterbody left and right sides balance wing (28) is spinning reduction automatically, its top electric screw slurry (29) auto-folder is in its both sides, helicopter main shaft (23) retracted for clearance automatically arrives driving states, navigation then can maintain the original state in the water surface long period if need, and electronic blade main propeller (27) is reached (29) all can be cut to electrical generator and generate electricity battery pack is charged.

Water sailing: after using inflatable air cushion layer (11) top off of inflation air pump (9) to bottom at the bottom of the car, stretch out the propeller of Foldable electric under water (10) that is contained in center, rear portion at the bottom of the car and drive waterborne travelling, can switch to electrical motor to (15) and become roof dead ahead propeller it is advanced at utmost speed in order to accelerate moving velocity waterborne.Control lift-off mode waterborne and have two kinds: utilize the helicopter flight system rolling takeoff lift-off, utilize wing horizontal development flight system host wing to become the lift-off of taking off of the limit of travelling waterborne, horizontal development limit, can use the inflation air pump that the air in the air cushion layer of car bottom is drained after the lift-off flight, the Foldable electric propeller (10) that drives travelling is under water shunk automatically to be folded in the car body and is restored to the original state.

The present invention is solid and light and handy, is furnished with high-end science and technology equipment, control conveniently, drive easily, the landing of can taking off of road surface with two-lane, need not to build private track, the landing of also can travelling on river, lake water face is taken off, both without fuel oil, reduce the pollution of air ambient, himself electric energy abundance, stroke is long, speed is fast and can slow down the pressure of road traffic, and it is employed to be the abrasive renewable sources of energy, it has great importance to national energy-saving and emission-reduction, is the vehicle of comprehensive multi-purpose in a kind of future.

Claims

1. one kind has multi-functional water, land and space electric aerocar using wind and solar energy for generating electricity, its structural attitude is that it comprises: carplane main body (1) adopts the streamline configuration design, helping overall height speed travels, high-end science and technology equipment is housed: drive control lever and control switched system (3) in driving OPS (2), automatic computer robot control system(RCS) and global positioning satellite navigation communication system (4), monitored meter system (5), road traveling system: before the car, trailing wheel all adopts high-power wheel nave motor (6) to drive and travels, high-energy battery group (7) is housed in the car: trailing wheel is used battery pack (A) always, front-wheel is used battery pack (B) always, standby battery group (C), storage battery dedicated group of helicopter (D), roof is equipped with wild goose shape arranges multi-functional wind power generation machine group (8), helping optimum air flows, reduce air resistance, save electric energy overall height speed is travelled, machine group can quicken the run-up lift-off by switching to electrical motor; Water boat system: the lower front at car is equipped with inflation air pump (9), be used for the inflation of car spirit bed course, the center, bottom is equipped with the scalable Foldable electric propeller (10) that turns to of travelling under water behind the car, be used for driving under water travelling, the bottom of car is provided with inflatable air cushion layer (11), is used for bearing vehicle body weight waterborne; Four jiaos of dresses of car body bracing frame (12) of triangular structure, the place ahead, the left and right sides is provided with the wind-force water conservancy diversion panel (13) of outside one-tenth " eight " font, in the dead ahead of bracing frame surface layer (14) a multifunctional high-power wind power generating set (15) is housed, it is changeable to be electrical motor, become the active force of the propeller lift-off flight in roof dead ahead, the front end of bracing frame surface layer is provided with upwards air inlet curved panel (16), the rear end is a controlled adjustable arc impeller (17), and solar energy photovoltaic system (18) is housed in the middle of the frame face; Flight system: the frame surface layer left and right sides is equipped with and can be rolled over extended position host wing (19), solar energy photovoltaic system (18) is equipped with on the top layer, after establish movable aileron (20), in have and stretch lengthening wing (21), the host wing horizontal development is reinforced with steel cable (22), the flexible main shaft (23) of Helicopter System, it is provided with lower blade propeller (24), drive by the large power multifunctional electrical motor (25) that is contained in frame surface layer center, lower blade is placed groove (26), blade is helicopter main propeller (27), by storage battery dedicated group of (D) power supply of helicopter, it is the active force of helicopter airflight, and rotary balance wing (28) is equipped with in the afterbody left and right sides, and Foldable electric propeller (29) is equipped with on its top, being used to control airflight turns to, electric energy-saving headlight and lighting system (30) are driven OPS seat (31), take advantage of seat (32) and external power charging inlet (33) to form.