CN106427434A - Flying car - Google Patents
Flying car Download PDFInfo
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- CN106427434A CN106427434A CN201611009111.4A CN201611009111A CN106427434A CN 106427434 A CN106427434 A CN 106427434A CN 201611009111 A CN201611009111 A CN 201611009111A CN 106427434 A CN106427434 A CN 106427434A
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- wing
- vehicle body
- canard
- duct
- fan
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/003—Off the road or amphibian vehicles adaptable for air or space transport
- B60F5/006—Off the road or amphibian vehicles adaptable for air or space transport droppable
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- Aviation & Aerospace Engineering (AREA)
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Abstract
A flying car comprises a car body in the shape of a lifting body and a water-drop-shaped driving cabin positioned in the middle of the car body. A lifting fan is arranged on the front portion of the car body, an air inlet of the lifting fan is provided with shutters in vertical arrangement, an air outlet is provided with shutters in transverse arrangement, plump car lamps are arranged on two sides of the head of the car body, the rear portion of each car lamp naturally extends to be provided with a duck wing rotating shaft, a wing root of a duck wing composed of a duck wing stabilizing plane and a control plane is connected onto each duck wing rotating shaft, and a propelling pneumatic integrated system is arranged on each of two sides of the rear portion of the car body and can be folded and unfolded through a foldable wing section. Through forward-backward inclination rotating of the propelling pneumatic integrated system and combining with the lifting fan, the duck wings and the car body in the shape of the lifting body, the flying car can vertically take off and land, can fly at high speed and is wide in flying range and low in energy consumption.
Description
Technical field
The present invention relates to air-ground amphibious field of vehicles, particularly to a kind of hovercar.
Background technology
Chinese invention patent 2016101724705 discloses a kind of hovercar, and this hovercar arranges one in headstock
Individual lift fan, arranges two folding ducted fans in the tailstock, and when ducted fan folds, hovercar overall width is less, can
With in road driving, when ducted fan is opened, hovercar just becomes the aircraft of three fan layout, and three fan makes flight vapour
Car can realize VTOL, but this hovercar does not have wing, can only produce direct lift with fan and maintain flight vapour
Car flies, and speed and voyage are limited, and power consumption is also big.
Chinese invention patent 2011100865703 discloses a kind of duct aerofoil system and with duct aerofoil system
Aircraft, this duct aerofoil system can produce lift and thrust simultaneously, is high integration, propulsive gas movement and motor-driven integrative be
System, by verting of duct aerofoil system, can make to realize VTOL and height with the aircraft of this duct aerofoil system
Speed flight, but the fan of this duct aerofoil system a part in the duct wing, a part outside the duct wing, have week during work
The vibration of phase property, easily makes structural fatigue;Chinese invention patent 2014101730228 disclose a kind of duct aerofoil system and
With the aircraft of this system, above-mentioned patent is made further improve so that this duct aerofoil system and utilization
The aircraft of this system is more perfect, but this duct aerofoil system not yet applies to hovercar field.
Existing ducted fan system is also the system of propulsive gas movement and motor-driven integrative, and ducted fan system is passed through suitably to set
Put, corresponding aircraft vertical landing can be made, after tilting forward, fan can promote aircraft to advance, and duct can produce lift,
But ducted fan system not yet so applies to hovercar.
Content of the invention
It is an object of the invention to provide a kind of hovercar, this hovercar uses propulsive gas movement and motor-driven integrative system,
Lift and thrust can be produced simultaneously, so that hovercar high speed remote voyage is flown, power consumption is also few.
Hovercar of the present invention, including the vehicle body of lifting body profile, the driving cabin of the water-drop-shaped in the middle part of vehicle body, vehicle body
Front portion is provided with lift fan, and lift fan air inlet is provided with vertically disposed shutter, and exhaust outlet is provided with transversely arranged
Shutter, vehicle body head both sides are provided with the car light heaved, and car light rear portion is extended naturally has canard rotating shaft to be pacified by canard
The wing root determining the canard of face and canard rudder face composition is connected in canard rotating shaft, and the canard span approximates the half of body width,
Canard can be outwardly opened by the rotation of the canard rotating shaft of wing root or fold inward upwards upwards, the canard two wing tip phase after folding
Connect, and be placed horizontally above headstock, the sharp vehicle body trailing edge of vehicle body is connected with vehicle body by hinge, and vehicle body trailing edge can pass through
Hinge is folded up, body bottom both sides, from headstock to front-wheel before, be provided with lower end prelaminar part, from after front-wheel to trailing wheel
Above, it is provided with the middle part of bottom plate, to tail of the body, being provided with lower end postlaminar part after trailing wheel, body tail both sides are symmetrical
Be each provided with a propulsive gas movement and motor-driven integrative system, at the edge of body tail top both sides, with propulsive gas movement and motor-driven integrative system
The corresponding position of system, is provided with rotating shaft, and propulsive gas movement and motor-driven integrative system is connected with rotating shaft with folding wing panel by wing panel of verting,
The wing root folding wing panel is connected with rotating shaft, and the wingtip of wing panel of verting is connected with propulsive gas movement and motor-driven integrative system, the wing of wing panel of verting
Root by one open up to rotating shaft with fold wing panel wingtip be connected.
In the present invention, it has been respectively adopted a propulsive gas movement and motor-driven integrative system in body tail both sides, pneumatic due to advancing
Integral system is passed through folding wing panel and is connected with the rotating shaft of body tail with wing panel of verting, and so passes through the inside rotation of rotating shaft,
Fold the fold inward of wing panel, the corresponding fold inward of propulsive gas movement and motor-driven integrative system of vehicle body both sides gets up, and so that hovercar is existed
Vehicle condition width is less, can travel on road;Being turned out by rotating shaft, folds outwardly opening of wing panel, vehicle body
The propulsive gas movement and motor-driven integrative system of both sides accordingly outwardly opens, then coordinates the lift fan of vehicle body head, so that hovercar is being flown
Row device state can VTOL, then verting by wing panel of verting, propulsive gas movement and motor-driven integrative system accordingly tilts forward, and makes to push away
Air inlet movement and motor-driven integrative system can produce lift and thrust simultaneously, cooperation vehicle body head both sides are opened simultaneously canard and lifting body
The vehicle body of profile, enables hovercar high speed remote voyage to fly, less energy intensive simultaneously.
Beneficial effects of the present invention:It is gas-operated integrated that hovercar of the present invention is respectively provided with a propulsion in body tail both sides
Change system, verts by before and after propulsive gas movement and motor-driven integrative system, then coordinates lift fan and canard and lifting body vehicle body, make
Hovercar can VTOL, high-speed flight, and voyage is remote, power consumption is few.
Brief description
Fig. 1 is the front perspective view in vehicle condition for the first hovercar of the present invention;
Fig. 2 is the front perspective view in helicopter state for the first hovercar of the present invention;
Fig. 3 is the front perspective view in fixed wing aircraft state for the first hovercar of the present invention;
Fig. 4 is the backsight parallax stereogram in fixed wing aircraft state for the first hovercar of the present invention;
Fig. 5 is the front perspective view in vehicle condition for the second hovercar of the present invention;
Fig. 6 is the front perspective view in helicopter state for the second hovercar of the present invention;
Fig. 7 is the front perspective view in fixed wing aircraft state for the second hovercar of the present invention;
Fig. 8 is the rear perspective view in fixed wing aircraft state for the second hovercar of the present invention.
In figure:1. vehicle body;2. driving cabin;3. shutter;4. car light;5. canard rotating shaft;6. canard stabilization;7. canard rudder
Face;8. upper head plate;9. duct;10. fan;11. folding wing panels;12. vert wing panel;13. horizontal support stabilizations;14. flap pairs
The wing;15. vertical support stabilizations;16. rudders;17. vehicle body trailing edges;18. rotating shafts;19. air intake ducts;20. lower end prelaminar parts;
In the middle part of 21. bottom plates;22. lower end postlaminar parts;The 23. duct wings;24. flaperons;Rudder on 25.;26. times rudders;Under 27.
Wing flap;Wing flap in 28.
Specific embodiment
The present invention is described in further detail with reference to the accompanying drawings and examples.
As shown in Fig. 1,2,3,4,5,6,7,8, the present invention includes the vehicle body 1 of lifting body profile, the water in the middle part of vehicle body
Drip the driving cabin 2 of shape, vehicle body 1 front portion is provided with lift fan, and lift fan air inlet is provided with vertically disposed shutter 3,
Exhaust outlet is provided with transversely arranged shutter, and vehicle body 1 head both sides are provided with the car light 4 heaved, and car light 4 rear portion extends naturally
It is provided with canard rotating shaft 5, the wing root of the canard being made up of canard stabilization 6 and canard rudder face 7 is connected in canard rotating shaft 5, duck
Cautiously exhibition approximates the half of body width, and canard can be outwardly opened by the rotation of the canard rotating shaft 5 of wing root or upwards upwards
Fold inward, canard two wing tip after folding is connected, and is placed horizontally above headstock, and the sharp vehicle body trailing edge 17 of vehicle body 1 leads to
Cross hinge to be connected with vehicle body 1, vehicle body trailing edge 17 can be folded up by hinge, vehicle body 1 two bottom sides, from headstock to front-wheel before
Face, is provided with lower end prelaminar part 20, to trailing wheel, being provided with after front-wheel 21 in the middle part of bottom plate, from after trailing wheel to car
Body afterbody, is provided with lower end postlaminar part 22, and vehicle body 1 rear portion both sides are symmetrically each provided with a propulsive gas movement and motor-driven integrative system,
At the edge of vehicle body 1 rear portion top both sides, the position corresponding with propulsive gas movement and motor-driven integrative system, it is provided with rotating shaft 18, propulsion
Gas-operated integratedization system is connected with rotating shaft 18 with folding wing panel 11 by wing panel 12 of verting, and folds wing root and the rotating shaft 18 of wing panel 11
Be connected, the wingtip of wing panel of verting 12 is connected with propulsive gas movement and motor-driven integrative system, the wing root of wing panel of verting 12 by one open up to
Rotating shaft is connected with the wingtip folding wing panel 11.
In the present invention, it has been respectively adopted a propulsive gas movement and motor-driven integrative system in vehicle body 1 rear portion both sides, pneumatic due to advancing
Integral system is passed through folding wing panel 11 and is connected with the rotating shaft 18 at vehicle body 1 rear portion with wing panel 12 of verting, and so passes through rotating shaft 18
Inwardly rotate, fold the fold inward of wing panel 11, the corresponding fold inward of propulsive gas movement and motor-driven integrative system of vehicle body 1 both sides gets up,
Make hovercar less in vehicle condition width, can travel on road;By being turned out of rotating shaft 18, fold wing panel 11
Outwardly open, the propulsive gas movement and motor-driven integrative system of vehicle body 1 both sides accordingly outwardly opens, then coordinates the lift wind of vehicle body 1 head
Fan, enables hovercar in flight state VTOL, then verting by wing panel 12 of verting, propulsive gas movement and motor-driven integrative system
Accordingly tilt forward, enable propulsive gas movement and motor-driven integrative system to produce lift and thrust simultaneously, coordinate vehicle body 1 head both sides simultaneously
The canard opened and the vehicle body 1 of lifting body profile, enable hovercar high speed remote voyage to fly, less energy intensive simultaneously.
Two kind propulsive gas movement and motor-driven integrative systems are set forth below be illustrated:
Embodiment one:As shown in Figure 1,2,3, 4, propulsive gas movement and motor-driven integrative system is ducted fan system, ducted fan system bag
Include duct 9, fan 10, horizontal support stabilization 13, the flaperon 14 of horizontal support stabilization 13 trailing edge, vertical support stabilization
15, the rudder 16 of vertical support stabilization 15 trailing edge.
This embodiment is conventional ducted fan system, and duct 9 section is symmetrical airfoil, and fan 10 is coaxial fan, level
Support stabilization 13 and vertical support stabilization 15 right-angled intersection, to support the motor driving fan 10, at ducted fan
In horizontal attitude, direct lift can be produced, so that hovercar is taken off vertically, when ducted fan system is in hanging down of low incidence
Straight attitude, the aerofoil of horizontal support stabilization 13 and flaperon 14 composition and duct 9 can produce lift, fan 10 energy simultaneously
Enough produce thrust, flown before hovercar with promoting.
It is such work:When the hovercar with ducted fan system is in vehicle condition, due to rotating shaft 18 to
Interior rotation, fold wing panel 11 fold inward, ducted fan system also get up by respective folded, wing panel of verting 12 with folding wing panel 11 phase
Vertically, the top making duct 9 air inlet of two ducted fan systems contacts, and makes two ducted fan systems form triangle knot
Structure, makes hovercar less wide in vehicle condition simultaneously, can be easily in road driving;When with ducted fan system
When hovercar will take off vertically, by being turned out of rotating shaft 18, fold wing panel 11 and outwardly open, make ducted fan system
Accordingly outwardly open, keep vert wing panel 12 and the Relative vertical attitude folding wing panel 11, make ducted fan system be in horizontal appearance
State, is turned out canard rotating shaft 5 simultaneously, opens the canard of vehicle body 1 head, the canard rudder face 7 of lower inclined canard stabilization 6 trailing edge,
Open the shutter 3 of vehicle body 1 head lift fan air inlet and the shutter of exhaust outlet, put down the vehicle body trailing edge of tail of the body
17, rotate the motor driving lift fan, so that lift fan is started working, rotate the motor driving fan 10, make fan
10 start working, and lift fan and ducted fan system will produce direct lift, and direct lift exceedes the weight suffered by hovercar
Power, and keep vertical and horizontal to balance, so that hovercar is taken off vertically, exceed certain altitude when hovercar takes off vertically
Afterwards, suitably reduce lift fan and fan 10 rotating speed and reduce lift with suitable, hovercar enters floating state;Work as hovercar
Gradually to tilt forward ducted fan system when floating state switchs to level cruise state of flight, simultaneously gradually to post deflection
The transversely arranged shutter of lift fan exhaust outlet, makes hovercar flight forward, meanwhile, canard stabilization 6 and canard rudder face 7
The aerofoil that the canard of composition, duct 9, horizontal support stabilization 13 and flaperon 14 are formed, and the vehicle body 1 of lifting body profile will
Produce lift, continue to strengthen this trend, ducted fan system is by the angle of attack angle leaning forward little, canard stabilization 6 and canard
The aerofoil that the canard of rudder face 7 composition, duct 9, horizontal support stabilization 13 and flaperon 14 are formed, and the car of lifting body profile
Body 1 will produce the lift maintaining hovercar horizontal flight enough, and fan 10 promotion hovercar is up to the standard cruising speed, this
When, stop lift fan work, close lift fan air inlet shutter 3 and exhaust outlet shutter, after packing up canard stabilization 6
The canard rudder face 7 of edge, hovercar enters level cruise state of flight, after hovercar enters level cruise state, uses canard
Rudder face 7 carries out fore-and-aft control, carries out lateral control, integrated use canard rudder face 7, flaperon 14 and rudder 16 with flaperon 14
Carry out directional control;When hovercar will switch to floating state from level cruise state of flight, suitably reduce fan 10 rotating speed
To reduce thrust, put down canard rudder face 7 and flaperon 14, hovercar is gradually reduced forward flight speed, when before hovercar simultaneously
Rapidly degree is reduced to and is unable to maintenance level flight, opens lift fan air inlet shutter 3 and exhaust outlet shutter, makes lift wind
Fan is started working and is produced direct lift, ducted fan system of simultaneously gradually verting backward, makes fan 10 produce direct lift, when winged
Row automobile continues to slow down, and ducted fan system is gradually verted for horizontal attitude, and hovercar loses forward flight speed, lift fan and
Fan 10 produces direct lift makes hovercar enter floating state;When hovercar will be fitted in floating state vertical landing
When reducing lift fan and fan 10 rotating speed, the direct lift that hovercar produces is made to be slightly less than suffered gravity, hovercar
Slowly decline, when front wheels and rear wheels contact ground, hovercar vertical landing process terminates;When hovercar needs from helicopter
When state switchs to vehicle condition, rotating shaft 18 inwardly rotates, and folds wing panel 11 fold inward, makes duct by wing panel 12 of verting simultaneously
Fan system fold inward, closes the shutter 3 of lift fan air inlet and the shutter of exhaust outlet, packs up canard rudder face 7, duck
Wing rotating shaft 5 inwardly rotates, and makes canard fold inward upwards, and is placed horizontally at vehicle body 1 head upper surface, packs up vehicle body 1 afterbody
Vehicle body 1 trailing edge 17, make vehicle body 1 reduce length, and increase vehicle body 1 afterbody intensity, hovercar is changed into vehicle condition.
Embodiment two:As shown in Fig. 5,6,7,8, propulsive gas movement and motor-driven integrative system is duct aerofoil system, duct wing system
System includes the duct wing 23, fan 10, the flaperon 24 of duct wing upper back edge, braced wing, the middle wing flap 28 of braced wing trailing edge, contains
The lower wing flap 27 of road underwing trailing edge, the upper rudder 25 of the duct wing 23 facade trailing edge upper portion, the duct wing 23 facade trailing edge bottom
Lower rudder 26, on fan 10 rear, the duct wing 23 top, have one to run through duct Yi23Feng road.
The duct wing 23 top of this embodiment, bottom, and braced wing are all asymmetric aerofoil profile, and fan 10 is coaxial wind
Fan, the slip-stream of generation does not have race rotation, can be good to braced wing, and the duct wing 23 upper and lower is entered action edge and increased
Rise, and fan 10 slip-stream can also pass through the seam road on the duct wing 23 top, carry out power-boosting to the duct wing 23 top, work as duct
When aerofoil system is in big angle of attack attitude, put down flaperon 24, middle wing flap 28 and lower wing flap 27, fan slip can be to duct
The wing 23 and braced wing carry out power-boosting, and the lift producing upwards is made a concerted effort, when duct aerofoil system is in little angle of attack angle,
Pack up flaperon 24, middle wing flap 28 and lower wing flap 27, fan 10 slip-stream also can carry out power-boosting to the duct wing 23 and braced wing,
And fan 10 slip-stream moreover it is possible to produce thrust forward, flies before promoting hovercar after flowing through duct aerofoil system.
It is such work:When the hovercar with duct aerofoil system is in vehicle condition, due to rotating shaft 18 to
Interior rotation, folds wing panel 11 fold inward, and wing panel of verting 12 is opened up to aliging with folding wing panel 11, and duct aerofoil system is also accordingly rolled over
Gather into folds, so that two duct aerofoil system is contacted and form three-legged structure, this makes hovercar less wide in vehicle condition,
Can be easily in road driving;When the hovercar with duct aerofoil system needs to be changed into helicopter shape from vehicle condition
During state, by being turned out of rotating shaft 18, fold wing panel 11 and outwardly open, so that duct aerofoil system is also accordingly outwardly opened, so
Vert backward by wide-angle for hypsokinesis rotor section 12, makes duct aerofoil system be in big angle of attack angle, after putting down duct aerofoil system
The flaperon 24 of edge, middle wing flap 28, lower wing flap 27, it is turned out canard rotating shaft 5 simultaneously, open the canard of vehicle body head, lower inclined
The canard rudder face 7 of canard stabilization 6 trailing edge, opens the shutter 3 of vehicle body 1 head lift fan air inlet and the blinds of exhaust outlet
Window, puts down the vehicle body trailing edge 17 of vehicle body 1 afterbody, and the hovercar with duct aerofoil system is changed into helicopter from vehicle condition
State;When the hovercar with duct aerofoil system needs to take off vertically in helicopter state, rotate and drive lift fan
Motor, so that lift fan is started working, rotate drive fan motor, so that fan 10 is started working, lift fan will
Produce direct lift, duct aerofoil system will produce lift and make a concerted effort, direct lift makes a concerted effort to be added to exceed hovercar with lift
Suffered gravity, and keep vertical and horizontal to balance, so that hovercar is taken off vertically, when hovercar takes off vertically more than one
After determining highly, suitably reduce lift fan and fan 10 rotating speed to reduce lift, hovercar enters floating state;When flight vapour
Car needs, when floating state switchs to level cruise state of flight, gradually to tilt forward duct aerofoil system, gradually pack up flap pair
The wing 24, middle wing flap 28, lower wing flap 27, simultaneously gradually to the shutter that post deflection lift fan exhaust outlet is transversely arranged, make flight
Automobile flight forward, meanwhile, the canard of canard stabilization 6 and canard rudder face 7 composition, and the vehicle body 1 of lifting body profile will produce
Raw lift, the lift of duct aerofoil system makes a concerted effort to be increasingly turned to front, continues to strengthen this trend, duct aerofoil system will lean forward
To little angle of attack angle, flaperon 24, middle wing flap 28, lower wing flap 27 is packed up completely, canard stabilization 6 and 7 groups of canard rudder face
The canard becoming, the duct wing 23, the aerofoil of braced wing and middle wing flap 28 formation, and the vehicle body 1 of lifting body profile will produce enough
Maintain the lift of hovercar horizontal flight, fan 10 promotes hovercar to be up to the standard cruising speed, now, stop lift wind
Fan work, closes lift fan air inlet shutter 3 and exhaust outlet shutter, packs up the canard rudder face of canard stabilization 6 trailing edge
7, hovercar enters level cruise state of flight, after hovercar enters level cruise state, carries out longitudinal direction with canard rudder face 7
Manipulate, carry out lateral control, integrated use canard rudder face 7, flaperon 24, and upper rudder 25 and lower direction with flaperon 24
Rudder 26 carries out directional control;When hovercar will switch to floating state from level cruise state of flight, suitably reduce fan 10
Rotating speed, to reduce thrust, puts down canard rudder face 7 and flaperon 24, middle wing flap 28, lower wing flap 27, hovercar is gradually reduced simultaneously
Forward flight speed, is unable to maintenance level flight when hovercar forward flight speed is reduced to, opens lift fan air inlet shutter 3 He
Exhaust outlet shutter, makes lift fan start working the direct lift of generation, simultaneously gradually tilting duct aerofoil system backward, makes culvert
The lift that road aerofoil system produces makes a concerted effort to be increasingly turned to rear, reduces propulsion forward, when hovercar continues to slow down, duct
Aerofoil system gradually verts for big angle of attack attitude, and hovercar loses forward flight speed, and lift fan produces direct lift, duct
Aerofoil system produces lift and makes a concerted effort, and direct lift and lift make a concerted effort to make hovercar enter floating state;When hovercar will be
During floating state vertical landing, suitably reduce lift fan and fan 10 rotating speed, direct lift and lift that hovercar produces
Make a concerted effort to be slightly less than suffered gravity, so that hovercar is slowly declined, when front wheels and rear wheels contact ground, hovercar vertical landing
Process terminates;When hovercar needs to switch to vehicle condition from helicopter state, wing panel of verting 12 tilts forward, and makes duct machine
Wing system is in little angle of attack angle, and rotating shaft 18 inwardly rotates, and folds wing panel 11 fold inward, is made by wing panel 12 of verting simultaneously
Duct aerofoil system fold inward, closes the shutter 3 of lift fan air inlet and the shutter of exhaust outlet, packs up canard rudder face
7, canard rotating shaft 5 inwardly rotates, and makes canard fold inward, and is placed horizontally at vehicle body 1 head upper surface, packs up vehicle body 1 afterbody
Vehicle body trailing edge 17, make vehicle body 1 reduce length, and increase vehicle body 1 afterbody intensity, hovercar is changed into vehicle condition.
As Fig. 1,2,3,4,5,6,7, shown in 8, passenger cabin 2 width is less than vehicle body 1 width, in vehicle body 1 top both sides of the edge, duck
Between wing rotating shaft 5 and rotating shaft 18, it is provided with upper head plate 8.
Because the vehicle body aspect ratio of lifting body profile is too little, there is strong wing tip vortex, upper head plate can reduce wing-tip vortex
Stream, increases the lift coefficient of vehicle body 1 lifting body.
As Fig. 1,2,3, shown in 4, wing panel of verting 12 leading edge is without departing from duct 9 air inlet, trailing edge and elevator 14 trailing edge pair
Together.
Wing panel of verting 12 leading edge, without departing from duct 9 air inlet, makes duct air inlet smooth;Trailing edge and elevator 14 trailing edge pair
Together, make that corresponding resistance is less, profile is succinct.
As Fig. 5,6,7, shown in 8, wing panel of verting 12 leading edge is without departing from the duct wing 23 air inlet, trailing edge and middle wing flap 28 trailing edge
Alignment.
Wing panel of verting 12 leading edge, without departing from the duct wing 23 air inlet, makes duct wing air inlet smooth;After trailing edge and middle wing flap 28
Edge aligns, and makes that corresponding resistance is less, and profile is succinct.
The lower end prelaminar part 20 of vehicle body 1 two bottom sides, 21 and lower end postlaminar part 22 in the middle part of bottom plate, can reduce further
The wing tip vortex of vehicle body lifting body, reduces the aerodynamic drag of front wheels and rear wheels, strengthens fountain effect during hovercar VTOL
Should;Driving cabin 2 is in water-drop-shaped, to reduce aerodynamic drag, and makes outward appearance more beautiful, can take 2 people in driving cabin 2;Dynamical system
Air intake duct 19 be arranged on driving cabin 2 top, disturbing of may being subject to can be reduced, dynamical system can be pure power driven system,
Suitable dynamical system is oil electric mixed dynamic system at this stage;Nature Link between car light 4 and canard rotating shaft 5, to reduce resistance
Power;The lift fan of embodiment one is identical with the diameter of the fan 10 of ducted fan system, the lift fan of embodiment two and culvert
The diameter of the fan 10 of road aerofoil system is identical, so can reduce cost, and succinctly attractive in appearance;Except two kinds of above-mentioned propulsions
Gas-operated integratedization system, hovercar also can also can reach corresponding function using other propulsive gas movement and motor-driven integrative systems.
Finally illustrate, above example only in order to technical scheme to be described and unrestricted, although with reference to relatively
Good embodiment has been described in detail to invention, it will be understood by those within the art that, can be to the technology of the present invention
Scheme is modified or equivalent, the objective without deviating from technical solution of the present invention and scope, and it all should be covered at this
In the middle of bright right.
Claims (6)
1. a kind of hovercar, including the vehicle body of lifting body profile(1), the driving cabin of the water-drop-shaped in the middle part of vehicle body(2), car
Body(1)Front portion is provided with lift fan, and lift fan air inlet is provided with vertically disposed shutter(3), exhaust outlet is provided with
Transversely arranged shutter, vehicle body(1)Head both sides are provided with the car light heaved(4), car light(4)Rear portion is extended naturally to be had
Canard rotating shaft(5), by canard stabilization(6)With canard rudder face(7)The wing root of the canard of composition is connected to canard rotating shaft(5)On,
The canard span approximates the half of body width, and canard can pass through the canard rotating shaft of wing root(5)Rotation outwardly open upwards or
Fold inward upwards, canard two wing tip after folding is connected, and is placed horizontally above headstock, vehicle body(1)The sharp car of afterbody
Edge after one's death(17)By hinge and vehicle body(1)It is connected, vehicle body trailing edge(17)Can be folded up by hinge, vehicle body(1)Bottom
Both sides, from headstock to front-wheel before, be provided with lower end prelaminar part(20), it is provided with bottom plate from after front-wheel to trailing wheel
Middle part(21), from after trailing wheel to vehicle body(1)Afterbody, is provided with lower end postlaminar part(22)It is characterised in that:Vehicle body(1)Rear portion
Both sides are symmetrically each provided with a propulsive gas movement and motor-driven integrative system, in vehicle body(1)The edge of rear portion top both sides, with propulsive gas
The corresponding position of movement and motor-driven integrative system, is provided with rotating shaft(18), propulsive gas movement and motor-driven integrative system is by wing panel of verting(12)With
Fold wing panel(11)With rotating shaft(18)It is connected, fold wing panel(11)Wing root and rotating shaft(18)It is connected, wing panel of verting(12)The wing
The tip is connected with propulsive gas movement and motor-driven integrative system, wing panel of verting(12)Wing root by one open up to rotating shaft with fold wing panel(11)
Wingtip be connected.
2. hovercar according to claim 1 is it is characterised in that described propulsive gas movement and motor-driven integrative system is ducted fan
System, ducted fan system includes duct(9), fan(10), horizontal support stabilization(13), horizontal support stabilization(13)Afterwards
The flaperon of edge(14), vertical support stabilization(15), vertical support stabilization(15)The rudder of trailing edge(16).
3. hovercar according to claim 1 is it is characterised in that described propulsive gas movement and motor-driven integrative system is duct wing
System, duct aerofoil system includes the duct wing(23), fan(10), flaperon(24), braced wing, the middle wing flap of braced wing trailing edge
(28), lower wing flap(27), the duct wing(23)The upper rudder of facade trailing edge upper portion(25), the duct wing(23)Facade trailing edge bottom
Lower rudder(26), in fan(10)Rear, the duct wing(23)Top, has one to run through the duct wing(23)Seam road.
4. the hovercar according to claim 2 and 3 is it is characterised in that passenger cabin(2)Width is less than vehicle body(1)Width,
Vehicle body(1)Top both sides of the edge, canard rotating shaft(5)And rotating shaft(18)Between, it is provided with upper head plate(8).
5. hovercar according to claim 2 is it is characterised in that wing panel of verting(12)Leading edge is without departing from duct(9)Enter
Gas port, trailing edge and flaperon(14)Trailing edge aligns.
6. hovercar according to claim 3 is it is characterised in that wing panel of verting(12)Leading edge is without departing from the duct wing(23)
Air inlet, trailing edge and middle wing flap(28)Trailing edge aligns.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201611009111.4A CN106427434A (en) | 2016-11-16 | 2016-11-16 | Flying car |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201611009111.4A CN106427434A (en) | 2016-11-16 | 2016-11-16 | Flying car |
Publications (1)
Publication Number | Publication Date |
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CN106427434A true CN106427434A (en) | 2017-02-22 |
Family
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Cited By (8)
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CN107139665A (en) * | 2017-05-11 | 2017-09-08 | 湖南顶立科技有限公司 | A kind of folded paddle hovercar |
CN109501539A (en) * | 2017-09-15 | 2019-03-22 | 冯军 | One kind downsizes aircraft |
CN109649512A (en) * | 2018-12-13 | 2019-04-19 | 华南理工大学 | Vehicle-mounted active air power device and its application method |
CN110065352A (en) * | 2019-05-24 | 2019-07-30 | 上海应用技术大学 | A kind of hovercar of tilting duct formula structure |
CN110282117A (en) * | 2019-07-10 | 2019-09-27 | 黄山鲸鲨飞行器科技有限公司 | A kind of city VTOL aircraft having wing-folding storage function |
CN111469618A (en) * | 2020-04-27 | 2020-07-31 | 上海应用技术大学 | Air-ground dual-purpose aerocar and using method thereof |
CN112622548A (en) * | 2020-12-30 | 2021-04-09 | 朱上翔 | Flying automobile |
CN116834487A (en) * | 2021-01-30 | 2023-10-03 | 武汉发明家创新科技有限公司 | Vertical take-off and landing suspension movable wing tilting flying electric automobile, take-off and landing method and lifting steering method |
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2016
- 2016-11-16 CN CN201611009111.4A patent/CN106427434A/en active Pending
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107139665A (en) * | 2017-05-11 | 2017-09-08 | 湖南顶立科技有限公司 | A kind of folded paddle hovercar |
CN109501539A (en) * | 2017-09-15 | 2019-03-22 | 冯军 | One kind downsizes aircraft |
CN109649512A (en) * | 2018-12-13 | 2019-04-19 | 华南理工大学 | Vehicle-mounted active air power device and its application method |
CN110065352A (en) * | 2019-05-24 | 2019-07-30 | 上海应用技术大学 | A kind of hovercar of tilting duct formula structure |
CN110282117A (en) * | 2019-07-10 | 2019-09-27 | 黄山鲸鲨飞行器科技有限公司 | A kind of city VTOL aircraft having wing-folding storage function |
CN111469618A (en) * | 2020-04-27 | 2020-07-31 | 上海应用技术大学 | Air-ground dual-purpose aerocar and using method thereof |
CN112622548A (en) * | 2020-12-30 | 2021-04-09 | 朱上翔 | Flying automobile |
CN116834487A (en) * | 2021-01-30 | 2023-10-03 | 武汉发明家创新科技有限公司 | Vertical take-off and landing suspension movable wing tilting flying electric automobile, take-off and landing method and lifting steering method |
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