CN102616096A - Solar flying automobile with folding wings - Google Patents
Solar flying automobile with folding wings Download PDFInfo
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- CN102616096A CN102616096A CN2012101217859A CN201210121785A CN102616096A CN 102616096 A CN102616096 A CN 102616096A CN 2012101217859 A CN2012101217859 A CN 2012101217859A CN 201210121785 A CN201210121785 A CN 201210121785A CN 102616096 A CN102616096 A CN 102616096A
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Abstract
The invention discloses a flying automobile with front folding wings and rear folding wings are arranged in series. The front wings are arranged on two sides of the front part of an automobile body; the rear wings are arranged on two sides of the rear part of the automobile body; after being turned and folded, the front wings can be collected on two sides of the automobile body in parallel or collected in a front carriage in a vertical stacking manner; after being turned and folded, the rear wings can be collected on the rear upper side on the top of the automobile body; large-area solar battery panels are arranged on the surfaces of respective parts of the wings and the automobile body; when the wings are unfolded completely, the flying automobile is turned into a serially-arranged fixed wing airplane and becomes a giant solar charger, and the solar battery panels and batteries supply power; when the wings are folded, the appearance and the size of the flying automobile are the same as those of a common sedan; and an underwater propeller is arranged at the bottom of the automobile, so that the flying automobile can be landed on water and sails in the water. The flying automobile is well combined with functions of an airplane, an automobile and a ship and is environment-friendly and high in continuous voyage capacity and suitable for families.
Description
Technical field
The present invention relates to a kind of hovercar, but especially a kind of folded wing solar power hovercar of solar recharging.
Background technology
Automobile and two kinds of transportation meanss of aircraft are combined, and are human ideas that is of long duration.Up to the present; It is in kind with some products to occur many hovercar schemes both at home and abroad; Have various design defect, or there is the principle defective of Flight Vehicle Design in scheme, too small, wing aerodynamic center of ubiquity wing area and aircraft center of gravity hypertelorism can not be realized longitudinal moment balance or the like in the for example domestic patent family more; Aircraft pneumatic design principle be can satisfy, but still the profile and the structure of aircraft broken away from not.For example the Terrafugia hovercar and the More of the up-to-date appearance of the U.S. pause. and Taylor's hovercar can only be called the folded wing aircraft that can on highway, go.The several domestic and international patents the most close with the present invention; Like U.S. Patent number US6619584B11, name is called in the patent of " ROAD/AIR VEHICLE " and discloses a kind of hovercar, and one Chinese patent application number is CN201110047409.5; Open day is on July 27th, 2011; Name is called in the patent of " hovercar " and discloses a kind of hovercar, and these two kinds of hovercars have all adopted body forward structure that canard is installed, and body tail is installed the aerodynamic arrangement of main wing.In Flight Vehicle Design; Canard is a kind of auxiliary wing that is used for strengthening aircraft manipulative capability and manoevreability, and its area is much littler than main wing, does not bear main lift effect; Be used for modern combat aircraft (Song Wen piebald horse academician more; " development of canard configuration airplane ", the 6th seminar collection of thesis of the Chinese aeronautics overall professional branch of meeting, on 09 01st, 2003).More than two patents all adopted canard preceding, main wing after layout type; The pneumatic bearing area that produces main lift in-flight still is mounted in the main wing of body tail; And this aerodynamic arrangement mode will cause the center of gravity apart from each other of wing aerodynamic center and hovercar; It is stable to obtain pitching during flight, therefore adopt on the short and small automobile canard preceding, main wing after aerodynamic arrangement's mode and unreasonable.And one Chinese patent application number is CN201110047409.5, and name is called in the patent of " hovercar ", and the space of folding and unfolding wing is too little between two wheels of front and back, causes wing area too small, can't reach the required wing load of flight.
Adopt the waste gas of the auto emission of combustion engine to cause serious atmospheric contamination.On the other hand, show that according to scientist's analysis existing oil resources will exhaust on the earth in 30 years, therefore oil price rises steadily in recent years.The great development direction in futures three of automobile is hybrid vehicle, pure electric automobile, fuel cell powered vehicle at present.Electronlmobil and electric airplane etc. itself do not pollute, but the employed electric energy that charges comes from fuel such as thermal powerplant burning petroleum and coal mostly, can cause increasing indirectly polluting.Solar power is reproducible clean energy resource, uses solar panel directly to change into electric energy to solar energy, can be used for driving the vehicle such as automobile and aircraft, and electric energy can also be stored in the storage battery subsequent use.Use the vehicle of solar power no longer to need combustion fuel, can realize zero-emission.But because fugitiveness, the dispersiveness of solar power and solar collecting device efficient is low, cost is high cause existing solar car and solar powered aircraft enormous size, load carrying ability is little, can't popularize practicability.Therefore, directly to use solar powers be to be difficult to the bottleneck that overcomes at present as power for the automobile of conventional size, aircraft, boats and ships etc.
[0004] in a word, above scheme and the perfect adaptation that all can't realize automobile and aircraft in kind also can't solve the difficult problem of direct use solar power as power source.
Summary of the invention
Defective to above-mentioned prior art existence; The technical matters that the present invention will solve provides a kind of hovercar; But the two function of perfect adaptation automobile and aircraft, and further combine the function of boats and ships, solve automobile, aircraft and boats and ships simultaneously and directly use the problem of solar power as power source.
In order to solve the problems of the technologies described above, the technical scheme that the present invention adopted is:
Adopted a kind of unconventional pneumatic layout of seldom usefulness in the airplane design---tandem wing aerodynamic arrangement; And wing-folding technology; Design hovercar, realized on the basis that is not increasing existing family-sized car size basically, the required big wing area that obtained to take off is (for single-shot or two s' propeller type dopey; One ton of take-off weight is wanted the wing area of 8～15 sq ms at least), solved this difficult problem for a long time of the two perfect adaptation of automobile and aircraft.Folded wing solar power hovercar disclosed by the invention; Comprise vehicle body, front vehicle wheel, rear wheel, driving engine, screw propeller; The body forward structure both sides are turning two folding secondary preceding wings, and the body tail both sides are turning two folding secondary back wings, and this fourth officer wing wing root separately all passes through head and body contact; Constitute front and back series type aerodynamic arrangement along vehicle body, common as the main pneumatic bearing area that produces lift.Compare with canard, the wing area between the forward and backward wing differs less, and the lift of generation is also big or small close, and front and back lift layout is even like this, and applied moment is reasonable, and two people ganged up in gambling before and after principle was similar to.Position after wherein preceding wing launches can the place ahead of front vehicle wheel, above or the rear.
Forward and backward wing becomes the aircraft of a tandem layout when launching; Can fly fast at a distance and on highway, take off and land; Simultaneously for fear of of the interference in air flow of preceding wing to the back wing; Preceding in-flight wing can suitably adopt inverted diherdral, back wing suitably to adopt the dihedral angle, has realized the forward and backward wing independence of aerodynamic characteristic separately.
The tailstock or headstock are installed at least one engine-driven screw propeller, and the screw propeller rotation is to produce the required power of flight during flight.When screw propeller was installed in the tailstock, car door can be installed in body forward structure or vehicle body both sides; When screw propeller was installed in headstock, car door can be installed in body tail or vehicle body both sides; Constitute when pulling in front and others push behind layout when screw propeller is installed in headstock and the tailstock simultaneously, car door is installed in both sides.
During as automotive use, left and right before wing close in vehicle body both sides or the stacked on top of one another income front compartment through the folding back of upset is parallel, left and right back wing closes at vehicle body top or the parallel vehicle body both sides that close at through upset after folding.
Specifically; First kind of scheme of folding and retraction wing of the present invention is; The wing root of wing flexibly connects through the wing frame of preceding wing-folding device and body forward structure both sides respectively before two width of cloth; The wing root of wing flexibly connects through back wing draw off gear and both sides, vehicle body back upper place respectively behind two width of cloth, and the inner wing of back wing is connected through interplane folding device with outer wing; When packing up wing; Before horizontality left and right wing earlier around the wing exhibition to axis be turned to and the basic plumbness of the earth, rotate final folding close at vehicle body both sides and locking more backward around basic vertical axis greatly; At this moment preceding wing exhibition is to being parallel to the vehicle body longitudinal axis, and tangential is vertical; The outer wing of the left and right back wing of horizontality respectively upwards upset realize the wing doubling, wing integral body forwards horizontally rotates around the back wing draw off gear of wing root separately respectively behind two width of cloth then, closes at vehicle body top and locking.
Second kind of scheme of folding and retraction wing of the present invention is; The wing root of wing is connected with the body forward structure both sides through preceding wing draw off gear separately before two width of cloth; The outer wing of preceding wing, back wing is connected through interplane folding device with inner wing, and the wing root of wing flexibly connects through back wing draw off gear and both sides, vehicle body back upper place respectively behind two width of cloth; When packing up wing; Open front compartment lid earlier, before horizontality left and right the outer wing of wing respectively to above or below rotation, realize the wing doubling; Wing integral body is rotated to the top respectively again before left and right; Mode with stacked on top of one another closes in the front compartment, and the front compartment lid covers again, the upwards upset realization wing doubling respectively of the outer wing of the left and right back wing of horizontality; Wing integral body forwards horizontally rotates around the back wing draw off gear of wing root separately respectively behind two width of cloth then, closes at vehicle body top and locking.
In second kind of scheme; The wing folding and unfolding S. A. discord aerofoil profile string of a musical instrument coincidence of wing root portion separately before left and right; But the side on the upper side that lays respectively at the aerofoil profile string of a musical instrument is square with on the lower side, and the vertical dimension after wing launches fully before such two width of cloth on vehicle body is identical, guarantees that the both sides aerodynamic characteristic is identical.
Also have other wing-folding schemes, all open up to the parallel vehicle body both sides that close at after folding through upset like forward and backward wing, tangential is vertical state, and the forward and backward wing of each side is all overlapping at vehicle body one side equal altitudes.
Certainly, front and back fourth officer wing is not limited to hinge commonly used with connection mode between the vehicle body and is connected, and also can adopt other movable connection methods.
Oad was near the normal domestic use car when this sample hovercar was packed up wing, in conjunction with automobile and aircraft the two function and do not have open defect.
On the preceding wing of this hovercar elevating rudder is installed, back wing is equipped with aileron; Also on the wing aileron was installed in the past, back wing is installed elevating rudder.Also wing flap and winglet can be installed on preceding wing, the back wing, be used for the lift-rising drag reduction, improve flight usefulness.
In first kind of folding and retraction wing scheme, look the installation site of screw propeller, car door is installed in body forward structure or rear portion, during passenger getting on/off, and the upwardly-openable car door, the passenger comes into automobile from headstock.The car door of vehicle body both sides also keeps, but need open folding left front wing or right front wing, opens car door again, and the passenger can get on or off the bus.Also can suitably shorten preceding wing, a car door is set respectively in the body tail both sides, even during preceding like this wing collapsed state, also can not block the car door of rear side, passenger getting on/off is more convenient.
Vertical tail can be one, also can be a plurality of.Vertical tail is during more than one, and an available tailplane couples together the upper end or the lower end of a plurality of vertical tails, constitutes three aerofoil layouts.
As further improvement of the present invention; The body bottom profile of this hovercar is identical with the bottom of ship profile; Body bottom is equipped with at least one underwater scooter; Interior of body is designed to a plurality of water-proff packing cabin structures, landing and water sailing on the water, the land, water and air three that the become balancing performance hovercar of dwelling.Wherein underwater scooter can be propeller or waterjet propulsor, or the underwater scooter of other kinds.
The driving engine of this hovercar can be electrical motor, also can be combustion engine, turbojet, turbofan engine, propeller turbine, and the driving engine of other types, can also be hybrid power.Hovercar can also can be installed the multi-section driving engine and drive propelling units different separately under each state respectively through the shared driving engine of power output shifter in the land, when sky, water state.
When driving engine adopts electrical motor, will use powered battery, battery can be a storage battery, also can be fuel cell or other batteries, can also be the hybrid battery that comprises multiple battery.
Further improve again as of the present invention; It is the driving engine power supply that this hovercar not only is equipped with battery; And the upper surface, lower surface and the side that comprise preceding wing, back wing, vertical tail, each position of vehicle body all are equipped with large-area solar panel; Payload space can reach more than tens of sq ms, and wing launches the whole automobile in back like this becomes a huge solar charger.The solar panel at positions such as upper surface of the airfoil and vehicle body top is accepted the direct radiation of sunshine, wing lower surface and vehicle body other etc. the solar panel at position accept the indirec radiation of sunshine, utilized solar power to greatest extent.When charging on the ground, automobile can intelligence be adjusted the parking attitude, and the start point of forward and backward wing, makes aerofoil surface as far as possible perpendicular to sunray, improves the solar charging electrical efficiency.
Solar panel and battery are formed hybrid power system; When solar panel power shortage and dull thread absorption; Can switch to battery powered mode, the perhaps battery powered while is also utilized solar cell for supplying power, can prolong voyage or when boat of hovercar greatly.
According to present technology; The solar panel photoelectric transformation efficiency is near 20%; About 120～the 150W of every sq m solar panel maximum output power; Consider sunlight direct radiation and indirec radiation equiluminous problem, primary Calculation, this hovercar can obtain the most about 2000～5000 watts electric power at fine day.Typical energy consumption according to/hundred kilometers of 15～20 degree of in the market typical pure electric automobile is calculated; The solar panel of this hovercar can obtain at least 10 degree electric energy a daytime; Be enough to go nearly hundred kilometers, perhaps electric power can satisfy hovercar power demand with middle low speed driving in water or on the highway in real time.
The present invention has solved charge a difficult problem or the direct difficult problem that drives of applied solar energy of automobile, aircraft, boats and ships cleverly whenever and wherever possible, can also be fit to working clan and resident's use with the city in the land or the remote travelling waterborne that lack charging equipment.Along with technological advance, the solar panel conversion efficiency also can continue to improve, and vehicle body also adopts after the technology such as light-weight design, and the rideability of hovercar and endurance also can improve.Therefore in a single day this hovercar is popularized, and will become not consume fuel, zero-emission, complete environmental protection and the globaetrotting family expenses vehicle of ability.
For aircraft, lifesaving is the problem that can't avoid.According to statistics, " airplane crash " accident is to occur in to take off and the landing stage more than 70%, so complete life saving system also is installed on this hovercar, is made up of safety air bag at the bottom of safety air bag and the car in escape parachute, the car.When in-flight in case of emergency, the escape parachute and opening of dishing out is when emergency landing is landed; Safety air bag at the bottom of the car is full of gas immediately and ejects; Constitute the air bag buffer zone of body bottom section, alleviate the suffered impulsive force of car body colliding surface, the safe soft landing when realizing forced landing; Car in-to-in safety air bag is opened simultaneously, protection occupant safety.In order to improve the reliability of body bottom safety air bag; Can also airbag design be become multilayer; Even outer broken, internal layer does not also break, and makes vehicle body can directly not clash into ground all the time; Guarantee personal security to greatest extent, and reduced the related economic loss of crashing and causing owing to hovercar.
This programme does not adopt the VTOL technology that realizes that difficulty is bigger; But the prompting in advance of dependence land, water and air comprehensive traffic networking management system when finding the place ahead highway generation traffic congestion, is changed motoring condition in advance; Rolling start on highway is avoided land, the place ahead and is blocked up.
Beneficial effect
The present invention contrasts prior art and has following beneficial effect:
1. adopt forward and backward wing along vehicle body tandem layout, jointly as main pneumatic bearing area, the moment equal and opposite in direction that forward and backward lifting force of wings produces hovercar, in the opposite direction, the lift layout is even, and fore-and-aft stability is good;
2. the collapsible folding and unfolding of forward and backward wing, pack up wing after hovercar close with the family-sized car size, the landing of can on highway, going and take off, the two function of perfect adaptation automobile and aircraft;
3. anti-on anti-down, the back wing of wing before adopting in-flight, realized that the aerodynamic characteristic of forward and backward wing is independent;
4. the upper and lower surface at the wing of hovercar and each position of vehicle body and side are equipped with large-area solar panel; Wing launches the whole automobile in back becomes a huge solar charger; And can self adaptation the angle of adjustment parking attitude and wing expansion; The direct radiation and the indirec radiation of sunlight have been utilized to greatest extent; Self-sustaining and the green non-pollution of power self-support, duration performance is good, and the automobile, aircraft, the boats and ships that have solved stock size directly utilize the difficult problem of solar power as power;
5. profile is identical with the bottom of ship profile and underwater scooter is installed at the bottom of the car, and interior of body is designed to a plurality of water-proff packing cabin structures, and having realized can be on highway and the landing of going and take off waterborne; Perfect adaptation automobile, aircraft and boats and ships three's function;
6. complete life saving system is installed on the hovercar, has solved the safety problem of family expenses aircraft, family expenses are popularized on a large scale, also can be used for other fields such as military affairs;
7. technology is simple, realizability is high, does not adopt the high VTOL technology of technical sophistication and energy consumption.
The specific embodiment
Do further detailed explanation below in conjunction with the accompanying drawing specific embodiments of the invention.
Fig. 1 is the block diagram of tandem wing hovercar of the present invention;
Fig. 2 is first kind of wing-folding mode folding and unfolding schematic diagram of the present invention;
Fig. 3 is the block diagram after first kind of wing-folding mode of the present invention packed up;
Fig. 4 is the schematic diagram of second kind of wing-folding mode of the present invention folding and unfolding;
Fig. 5 is the block diagram after second kind of wing-folding mode of the present invention packed up;
Fig. 6 is that preceding wing stacked on top of one another is received in the local schematic diagram in the front compartment in second kind of wing-folding mode of the present invention;
Fig. 7 is the scheme drawing that each position of the present invention adds solar panel;
Fig. 8 is the scheme drawing that the present invention adds the top wing hound, and is anti-on down anti-, the back wing of wing before wherein;
Fig. 9 is that the present invention adds three of landing function waterborne, two side-by-side helix oars of the tail hovercar birds-eye view of dwelling;
Figure 10 is that the present invention adopts jet engine, afterwards wing is the back view of not collapsible wing;
Figure 11 is a life saving system work scheme drawing of the present invention;
The dihedral angle and the inverted diherdral of intelligence adjustment parking attitude and forward and backward wing when Figure 12 is a solar recharging of the present invention improve solar energy power generating usefulness scheme drawing.
Among the figure: 1. vehicle body, 2. front vehicle wheel, 3. rear wheel, 4. front compartment lid, 5. screw propeller, 6. before wing; 7. preceding wing frame, 8. preceding wing-folding device, 9. back wing, 10. back wing draw off gear, 11. interplane folding devices, 12. preceding wing draw off gears; 13. the front open type car door, 14. car doors, 15. wing root S. A.s, 16. solar panels, 17. underwater scooters, 18. vertical tails; 19. tailplane, 20. elevating rudders, 21. ailerons, 22. yaw rudders, 23. escape parachutes; 24. safety air bag in the car, safety air bag at the bottom of 25. cars, 26. hounds, 27. jet engine propelling units, 28. mangers.
Embodiment one:
Referring to accompanying drawing 1,2,3,650 kilograms of this hovercar deadweights, according to 4 designs, 75 kilograms of each passengers respectively carry 10 kilograms of luggage, and four passengers' gross load is 340 kilograms, so about one ton of this hovercar maximum take-off weight.Be lower than 400 kilometers/hour single-shot and two dopeies of sending out for flying speed; Every sq m wing area can carry 80～150 kilograms load; After this hovercar has adopted unconventional tandem wing design; Can obtain the gross wing area of 8～15 sq ms, be enough to let this hovercar take off smoothly.The hovercar principle of design of other seating capacities is identical therewith.
The tailstock is installed an engine-driven screw propeller 5, and screw propeller 5 rotations are to produce the required power of flight during flight.
Two vertical tails 18 about the tailstock has; Tailplane 19 connects the upper end of two vertical tails 18; Constitute three aerofoil layouts; So both strengthened structural strength, and tailplane 19 is used to strengthen aloft stability and road-holding property as an auxiliary pneumatic bearing area of hovercar.
During as aircraft utilization, forward and backward fourth officer wing all opens and locking position, and at this moment hovercar becomes a tandem wing aircraft, can on highway, take off and land.
Can slide race on the ground for hovercar and take off smoothly, preceding wing 6 is equipped with enlargement devices such as wing flap, puts down wing flap front wing lift is strengthened, and headstock is lifted smoothly take off.
Referring to accompanying drawing 8, for weaken or eliminate before the interference in air flow of wing 9 behind 6 pairs on the wing, in-flight before wing 6 can adopt suitable inverted diherdral, back wing 9 adopts the suitable dihedral angle, back wing 9 is staggered before the following gas washing that produces of wing 6 flow.And for the structure stress of wing before improving 6 with back wing 9, also can increase hound 26, one ends and be connected with the lower aerofoil of wing, an end is connected with vehicle body 1.
During as automotive use; Wing 6 and back wing 9 before need packing up; Before horizontality left and right wing 6 earlier around the wing exhibition to axis be turned to and the basic plumbness of the earth, rotate final folding close at vehicle body 1 both sides and locking more backward around basic vertical axis greatly; At this moment preceding wing 6 exhibitions are to being parallel to the vehicle body longitudinal axis, and tangential is vertical; The outer wing of the left and right back wing 9 of horizontality respectively upwards upset realize the wing doubling, wing 9 forwards horizontally rotates around back wing draw off gear 10 integral body of wing root separately respectively behind two width of cloth then, closes at vehicle body top and locking.
At this moment hovercar is close with a normal domestic use car size, can on highway, go smoothly.Car door 14 is installed in vehicle body 1 front portion and is front open type car door 13, during passenger getting on/off, and upwardly-openable car door 14, the passenger comes into automobile from headstock.The car door 14 of vehicle body 1 both sides also keeps, and need open folding left front wing 6 or right front wing 6 earlier but get on or off the bus, and opens car door 14 again.
Referring to accompanying drawing 11, complete life saving system is installed on this hovercar, form by safety air bag 25 at the bottom of safety air bag 24 and the car in escape parachute 23, the car.In case of emergency, escape parachute 23 is dished out and is opened, when emergency landing is landed when flight; Safety air bag 25 is full of gas and ejection immediately at the bottom of the car; Constitute the air bag buffer zone of vehicle body 1 bottom, alleviate the suffered impulsive force of car body colliding surface, the safe soft landing when realizing the hovercar forced landing; Safety air bag 24 is opened in the car simultaneously, protection occupant safety.
Embodiment two:
Referring to accompanying drawing 4,5; The wing root of wing 6 is connected with vehicle body 1 front part sides through preceding wing draw off gear 12 separately before two width of cloth; The outer wing of preceding wing 6 and back wing 9 is connected through interplane folding device 11 with inner wing, and the wing root of wing 9 is respectively through back wing draw off gear 10 and the flexible connection of both sides, vehicle body 1 back upper place behind two width of cloth.
When packing up wing; Open front compartment lid 4 earlier, before horizontality left and right the outer wing of wing 6 respectively to above or below rotation, realize the wing doubling; Wing 6 is whole respectively again before left and right rotates to the top; Mode with stacked on top of one another closes in the front compartment, and front compartment lid 4 covers again, the upwards upset realization wing doubling respectively of the outer wing of the left and right back wing 9 of horizontality; Wing 9 forwards horizontally rotates around back wing draw off gear 10 integral body of wing root separately respectively behind two width of cloth then, closes at vehicle body 1 top and locking.
Referring to accompanying drawing 6, overlapping about forming after left and right preceding wing 6 folds, to receive and keep in front compartment, possibly there is the difference on the vertical dimension in the latter two in vehicle body 1 both sides therefore left and right preceding wing 6 expansion.Can wing 6 wing root S. A. 15 separately before left and right be designed to depart from the aerofoil profile string of a musical instrument; As the side on the upper side that lays respectively at the aerofoil profile string of a musical instrument is square with on the lower side; Wing 6 expansion backs are identical on vehicle body 1 both sides vertical dimension before having realized two width of cloth like this, avoided left and right sides aerodynamic characteristic asymmetric.
Embodiment three:
Referring to accompanying drawing 7; Upper surface, lower surface and the side at wing 6, back wing 9, vertical tail 18, vehicle body 1 each position all are equipped with large-area solar panel 16 before comprising; Storage battery also is installed on the car, and solar panel 16 is formed hybrid power system with storage battery.When solar panel 16 power shortages and dull thread are taken in, can switch to the storage battery power supply pattern, the perhaps battery-driven while is also utilized solar panel 16 power supplies, in the time of can prolonging voyage or the boat of hovercar greatly.
Referring to accompanying drawing 12, in when charging, preceding wing 6 can self adaptation be adjusted upper and lower dihedral degree with back wing 9, makes the sunray vertical irradiation aerofoil surface of trying one's best to improve solar energy power generating usefulness.
Other guide is with embodiment one.
Embodiment four:
Present embodiment is three hovercars of dwelling, and lives in seashore or area, rivers and lakes needs of people to satisfy.
Referring to accompanying drawing 9, hovercar car base profile is identical with the bottom of ship profile, to reduce the resistance in water; Adopt two screw propellers 5 that are installed in tailstock portion side by side as the flight propelling unit; Be installed in higher position, vehicle body 1 rear portion,, avoided the spray damage so not only apart from water surface certain altitude; And two screw propeller 5 hand of rotation are opposite, the moment of torsion of cancelling out each other.Connect as one fully between the rear wheel 3 and between vehicle body 1 bottom, constitute the manger 28 at vehicle body 1 rear portion, when avoiding in the water navigation or landing waterborne, the spray of afterbody splashes the back and damages screw propeller 5.
The rear portion is equipped with two water jet pump underwater scooters 17 side by side at the bottom of the car, be used for water sailing and advance, and spout has vector and turns to and spray function, has omitted rudder for ship, can realize various water sailing states.Vehicle body 1 inner structure is designed to a plurality of water-proff packing cabin, prevents into to sink behind the water.
Present embodiment has possessed perfect landing waterborne and water sailing, has perfectly combined the function of automobile, aircraft, three kinds of vehicle of boats and ships, under the three kinds of states in land, water and air balancing performance.
Other guide is with embodiment one.
Embodiment five:
Is that example further specifies to adopt jet engine propelling unit 27 as the hovercar of flight propelling unit.
Referring to accompanying drawing 10, present embodiment has adopted jet engine propelling unit 27 in order to satisfy customers' needs of more speed flight, and at this moment preceding wing 6, the suitably sweepback awing of back wing 9 improve airworthiness.Because the raising of speed makes the required wing load of flight increase, so the area of each wing can suitably reduce, and in the present embodiment, back wing 9 is not collapsible wing.
Other guide is with embodiment one.
More than combine the accompanying drawing specific embodiments of the invention to be described; But these explanations can not be understood that to have limited scope of the present invention; Protection scope of the present invention is limited the claims of enclosing, and any change on claim of the present invention basis is all in protection scope of the present invention.
Claims (11)
1. folded wing solar power hovercar; Comprise vehicle body, front vehicle wheel, rear wheel, driving engine, screw propeller, it is characterized in that the body forward structure both sides are turning two folding secondary preceding wings; The body tail both sides are turning two folding secondary back wings; This fourth officer wing wing root separately all passes through head and body contact, and series type aerodynamic arrangement before and after constituting along vehicle body is common as the main pneumatic bearing area that produces lift; When wing is packed up, left and right before wing close in vehicle body both sides or the stacked on top of one another income front compartment after folding through upset, left and right back wing closes at the vehicle body top or closes at the vehicle body both sides after folding through upset; The tailstock or headstock are installed at least one by engine-driven screw propeller.
2. folded wing solar power hovercar according to claim 1; It is characterized in that; The wing root of wing flexibly connects through the wing frame of preceding wing-folding device and body forward structure both sides respectively before two width of cloth; The wing root of wing flexibly connects through back wing draw off gear and both sides, vehicle body back upper place respectively behind two width of cloth, and the inner wing of back wing is connected through interplane folding device with outer wing; When packing up wing; Before horizontality left and right wing earlier around the wing exhibition to axis be turned to and the basic plumbness of the earth, rotate final folding close at vehicle body both sides and locking more backward around the axis that is basically perpendicular to the earth; At this moment preceding wing exhibition is to being parallel to the vehicle body longitudinal axis, and tangential is vertical; The outer wing of the left and right back wing of horizontality respectively upwards upset realize the wing doubling, wing integral body forwards horizontally rotates around the back wing draw off gear of wing root separately respectively behind two width of cloth then, closes at vehicle body top and locking.
3. folded wing solar power hovercar according to claim 1; It is characterized in that; The wing root of wing is connected with the body forward structure both sides through preceding wing draw off gear separately before two width of cloth; The outer wing of preceding wing, back wing is connected through interplane folding device with inner wing, and the wing root of wing flexibly connects through back wing draw off gear and both sides, vehicle body back upper place respectively behind two width of cloth; When packing up wing; Open front compartment lid earlier, before horizontality left and right the outer wing of wing respectively to above or below rotation, realize the wing doubling; Wing integral body is rotated to the top respectively again before left and right; Mode with stacked on top of one another closes in the front compartment, and the front compartment lid covers again, the upwards upset realization wing doubling respectively of the outer wing of the left and right back wing of horizontality; Wing integral body forwards horizontally rotates around the back wing draw off gear of wing root separately respectively behind two width of cloth then, closes at vehicle body top and locking.
4. folded wing solar power hovercar according to claim 3; It is characterized in that; The left and right preceding wing folding and unfolding S. A. of wing root portion separately lays respectively at the square on the upper side square with on the lower side of the aerofoil profile string of a musical instrument, and the vertical dimension after wing launches fully before two width of cloth on vehicle body is identical.
5. according to each described folded wing solar power hovercar in the claim 1 to 3; It is characterized in that the battery that drives driving engine also is installed on the vehicle body, and battery can be a storage battery; Also can be fuel cell or other batteries, can also be the hybrid battery that comprises multiple battery.
6. according to each described folded wing solar power hovercar in the claim 1 to 3; It is characterized in that, comprise that upper surface, lower surface and the side at preceding wing, back wing, vertical tail, front compartment lid, each position of vehicle body all is equipped with large-area solar panel; Solar panel and battery are formed hybrid power system.
7. according to each described folded wing solar power hovercar in the claim 1 to 3; It is characterized in that; Comprise that also the body bottom profile is identical with the bottom of ship profile, body bottom is equipped with at least one underwater scooter, and interior of body is designed to a plurality of water-proff packing cabin structures.
8. according to each described folded wing solar power hovercar in the claim 1 to 3, it is characterized in that vertical tail is during more than one, an available tailplane couples together the upper end or the lower end of a plurality of vertical tails, constitutes three aerofoil layouts.
9. according to each described folded wing solar power hovercar in the claim 1 to 3, it is characterized in that, the position after preceding wing launches can the place ahead of front vehicle wheel, above or the rear.
10. according to each described folded wing solar power hovercar in the claim 1 to 3, it is characterized in that, safety air bag at the bottom of the safety air bag and car is installed on the car in the escape parachute, car.
11. according to each described folded wing solar power hovercar in the claim 1 to 3; It is characterized in that; Has a driving engine on the car at least; Driving engine can be electrical motor, also can be combustion engine, turbojet, turbofan engine, propeller turbine, and the driving engine of other types, can also be that multiple-motor is formed hybrid power.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012101217859A CN102616096A (en) | 2012-04-24 | 2012-04-24 | Solar flying automobile with folding wings |
| CN201310131317.4A CN103496305A (en) | 2012-04-24 | 2013-04-16 | Hovercar |
| PCT/CN2013/074370 WO2013159672A1 (en) | 2012-04-24 | 2013-04-18 | Flying automobile |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012101217859A CN102616096A (en) | 2012-04-24 | 2012-04-24 | Solar flying automobile with folding wings |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102616096A true CN102616096A (en) | 2012-08-01 |
Family
ID=46556439
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012101217859A Pending CN102616096A (en) | 2012-04-24 | 2012-04-24 | Solar flying automobile with folding wings |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102616096A (en) |
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| CN113427954A (en) * | 2021-08-14 | 2021-09-24 | 北京金璐东方联合物流有限公司 | Flying automobile |
| CN115091905A (en) * | 2022-07-21 | 2022-09-23 | 北京航空航天大学 | Electric flying automobile |
| CN115091905B (en) * | 2022-07-21 | 2024-05-31 | 北京航空航天大学 | Electric flying car |
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Application publication date: 20120801 |