CN105946484B - Hovercar - Google Patents
Hovercar Download PDFInfo
- Publication number
- CN105946484B CN105946484B CN201610433670.1A CN201610433670A CN105946484B CN 105946484 B CN105946484 B CN 105946484B CN 201610433670 A CN201610433670 A CN 201610433670A CN 105946484 B CN105946484 B CN 105946484B
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- CN
- China
- Prior art keywords
- wing
- car body
- empennage
- hovercar
- fixed frame
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/80—Technologies aiming to reduce greenhouse gasses emissions common to all road transportation technologies
- Y02T10/82—Elements for improving aerodynamics
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Soil Working Implements (AREA)
Abstract
The invention discloses a kind of hovercar, it includes car body, preceding wing mechanism, stretching, extension wing mechanism, lower empennage mechanism and upper empennage mechanism, preceding wing mechanism is arranged on below the front end of car body, stretching, extension wing mechanism is arranged on lower section in the middle part of car body, lower empennage mechanism is arranged on below the rear end of car body, and upper empennage mechanism is arranged on above body rear end.The present invention can realize ground run and airflight at the same time, and take up space during ground run sizableness with general-utility car, and travel and stop flexible, and when flight can realize the air objective of common compact aircraft.
Description
Technical field
The present invention relates to a kind of automobile, more particularly to a kind of hovercar.
Background technology
With the growth of scientific and technological development and human lives' demand rapidly, automobile has become the master of people's go off daily
The vehicles are wanted, working peak time traffic jam has become the common problem in each city.Therefore hovercar is born, can
It is as a kind of preferable vehicles, a dimension is added for the track of communications and transportation, i.e., convertible when being blocked on ground
For offline mode, the situation of traffic congestion is alleviated again while convenient go on a journey.Existing hovercar is most for folding at present
Folded wing hovercar, its wing are placed outside body both sides, thus whole hovercar physical dimension is larger and occupied space compared with
Greatly, traveling is stopped be not as flexible as general-utility car.
The content of the invention
The technical problems to be solved by the invention are to provide a kind of hovercar, it simultaneously can with general-utility car characteristic superiority
Realize air objective, physical dimension is smaller and occupied space is smaller, and traveling is stopped as general-utility car is flexible.
The present invention is to solve above-mentioned technical problem by following technical proposals：A kind of hovercar, it is characterised in that
It includes car body, preceding wing mechanism, stretching, extension wing mechanism, lower empennage mechanism and upper empennage mechanism, preceding wing mechanism and is arranged on car body
Below front end, stretching, extension wing mechanism is arranged on lower section in the middle part of car body, and lower empennage mechanism is arranged on below the rear end of car body, upper empennage machine
Structure is arranged on above body rear end；Wherein preceding wing mechanism includes front wing, the first cross link, first connecting rod, the first stopper rod, first
Cylinder barrel, the first fixed frame, the first hinged port and the first sliding groove road, the first hinged port and the first sliding groove road are all located on front wing
Surface, front wing are connected by the first cross link with the first fixed frame, and the first fixed frame is installed on car body, and the two of first connecting rod
End is connected with the first fixed frame, and one end of the first cylinder barrel is connected by the first stopper rod and the middle of first connecting rod, the first cylinder barrel
The other end is fixed with the first fixed frame；Stretching wing mechanism includes the level-one stretching, extension wing, the two level stretching, extension wing, and the level-one stretching, extension wing and two level are stretched
Spademan connects；Lower empennage mechanism is consolidated including lower empennage, the second cross link, second connecting rod, the second stopper rod, the second cylinder barrel, second
Determine frame, the second hinged port, the second sliding slot road, the second hinged port and the second sliding slot road is all located at lower empennage upper surface, lower tail
The wing is connected by the second cross link with the second fixed frame, and the second fixed frame is installed on car body, the both ends of second connecting rod and the
Two fixed frames are connected, and one end of the second cylinder barrel is connected by the second stopper rod and the middle of second connecting rod, the other end of the second cylinder barrel
Fixed with the second fixed frame；Upper empennage mechanism includes upper empennage, spoiler, stable frame, upper empennage and spoiler all with stable frame
It is connected.
Preferably, enough spaces place wing inside the vehicle bottom.
Preferably, shape is bullet type when the car body packs up wing.
Preferably, the shape of the stretching, extension wing mechanism is trapezoidal.
Preferably, the car body surface is streamlined.
Preferably, the preceding wing mechanism, stretching, extension wing mechanism and lower empennage mechanism are used to provide lift；Upper empennage mechanism is used
In the posture of control hovercar.
Preferably, the preceding wing mechanism is contracted in vehicle body in ground run, is stretched out in flight below car body.
Preferably, stretching, extension wing mechanism two-level nested in ground run is contracted in vehicle body, in flight from car
Body both sides are stretched out.
Preferably, the lower empennage mechanism is contracted in vehicle body in ground run, is stretched in flight below car body
Go out.
Preferably, upper empennage mechanism spoiler in ground run is upturned to provide negative lift, starts flight
When spoiler rotate down to provide lift.
The positive effect of the present invention is：The present invention can travel on the ground, can also fly in the air.The present invention
Each several part wing can be hidden in completely among car body, this causes the present invention in ground run completely with general-utility car
Feature and driving mode, volume size and general-utility car take up space sizableness, and travel, stop flexible, operation
Mode is identical with general-utility car.After each several part wing full extension of the present invention is opened, the lift produced by airfoil surface can
To realize the basic function of baby plane so as to fulfill air objective.Bullet type car body design and the scalable wing due to the present invention
The combination of design so that the present invention can complete ground run and airflight task under smaller spatial volume.This hair
It is bright to alleviate serious load traffic problems, and vehicle drive is combined with flight management, by flight management become summary,
Popular, universalness.
Brief description of the drawings
Structure diagram when Fig. 1 is ground run of the present invention.
Structure diagram when Fig. 2 is airflight of the present invention.
Side view when Fig. 3 is airflight of the present invention.
Fig. 4 is front wing mechanism structure schematic diagram of the present invention.
Fig. 5 is the lower empennage mechanism structure diagram of the present invention.
Top view when Fig. 6 is airflight of the present invention.
Front view when Fig. 7 is flight in the present invention.
Embodiment
Present pre-ferred embodiments are provided below in conjunction with the accompanying drawings, with the technical solution that the present invention will be described in detail.
As shown in Figures 1 to 7, hovercar of the present invention includes car body 1, preceding wing mechanism 2, stretching, extension wing mechanism 3, lower empennage machine
Structure 4 and upper empennage mechanism 5, preceding wing mechanism 2 are arranged on below the front end of car body 1, and stretching, extension wing mechanism 3 is arranged on the middle part of car body 1
Lower section, lower empennage mechanism 4 are arranged on below the rear end of car body 1, and upper empennage mechanism 5 is arranged on above 1 rear end of car body；Wherein front wing
Mechanism 2 include front wing 21, the first cross link 22, first connecting rod 23, the first stopper rod 24, the first cylinder barrel 25, the first fixed frame 26,
First hinged port 21b and the first sliding groove road 21a, the first hinged port 21b and the first sliding groove road 21a are all located at 21 upper table of front wing
Face, front wing 21 are connected by the first cross link 22 with the first fixed frame 26, and the first fixed frame 26 is installed on car body 1, and first
The both ends of connecting rod 23 are connected with the first fixed frame 26, and one end of the first cylinder barrel 25 passes through in the first stopper rod 24 and first connecting rod 23
Between connect, the other end of the first cylinder barrel 25 is fixed with the first fixed frame 26；Stretching wing mechanism 3 includes the level-one stretching, extension wing 31, two level
The wing 32 is stretched, the level-one stretching, extension wing 31 and the two level stretching, extension wing 32 connect；Lower empennage mechanism 4 includes lower empennage 41, the second cross link
42nd, second connecting rod 43, the second stopper rod 44, the second cylinder barrel 45, the second fixed frame 46, second are hinged port 41b, the second sliding slot road
41a, the second hinged port 41b and the second sliding slot road 41a are all located at lower 41 upper surface of empennage, and lower empennage 41 intersects by second and connects
Bar 42 is connected with the second fixed frame 46, and the second fixed frame 46 is installed on car body 1, the both ends of second connecting rod 43 and the second fixed frame
46 are connected, and one end of the second cylinder barrel 45 is connected by the centre of the second stopper rod 44 and second connecting rod 43, the second cylinder barrel 45 it is another
End is fixed with the second fixed frame 46；Upper empennage mechanism 5 includes upper empennage 51, spoiler 52, stable frame 53, upper empennage 51 and flow-disturbing
Plate 52 is all connected with stable frame 53.
There are enough spaces to place wing inside vehicle bottom, so save space.
Shape when car body packs up wing is bullet type, so saves space.
The shape for stretching wing mechanism is trapezoidal, this spline structure is more stablized.
The operation principle of this hovercar is as follows：Car body surface is streamlined, for reducing air drag；Preceding wing mechanism,
Stretching, extension wing mechanism and lower empennage mechanism are used to provide lift；Upper empennage mechanism is used for the posture for controlling hovercar.Before wherein
Wing mechanism, stretching, extension wing mechanism, lower empennage mechanism and upper empennage mechanism are separately positioned on below the front end of car body, under car body middle part
Stabilize below side, rear end with rear end on frame.Preceding wing mechanism is contracted in vehicle body in ground run, in flight under car body
Side is stretched out.Stretching, extension wing mechanism two-level nested in ground run is contracted in vehicle body, is stretched in flight from car body both sides
Go out.The lower empennage mechanism is contracted in vehicle body in ground run, is stretched out in flight below car body.The upper empennage
Mechanism spoiler in ground run is upturned to provide negative lift, and spoiler is rotated down to provide liter when starting flight
Power.In flight, spoiler can adjust rotational angle according to demand.Level-one stretches the wing by screw drive mechanism from vehicle body
It is moved on the outside of car body, two level, which stretches the wing and driven by servo control mechanism from level-one, stretches mobile inside the wing stretch.First connecting rod,
One stopper rod and the first cylinder barrel are used to adjust the distance between front wing and the first fixed frame.Spoiler can carry out turning for certain angle
It is dynamic.Upper empennage mechanism spoiler in ground run is upturned, and to provide negative lift, spoiler turns downwards when starting flight
Dynamic, to provide lift, in flight, spoiler can adjust rotational angle according to demand.
In conclusion the present invention can realize ground run and airflight at the same time, when ground run, accounts for general-utility car
It is suitable according to space size, and travel and stop flexibly and easily.The air objective of common compact aircraft can be realized during flight.
Particular embodiments described above, technical problem, technical solution and the beneficial effect of the solution to the present invention carry out
It is further described, it should be understood that the foregoing is merely the specific embodiment of the present invention, is not limited to
The present invention, within the spirit and principles of the invention, any modification, equivalent substitution, improvement and etc. done, should be included in this
Within the protection domain of invention.
Claims (10)
- A kind of 1. hovercar, it is characterised in that it include car body, preceding wing mechanism, stretching, extension wing mechanism, lower empennage mechanism and on Empennage mechanism, preceding wing mechanism are arranged on below the front end of car body, and stretching, extension wing mechanism is arranged on lower section, lower empennage mechanism in the middle part of car body It is arranged on below the rear end of car body, upper empennage mechanism is arranged on above body rear end；Wherein preceding wing mechanism includes front wing, the first friendship Pitch connecting rod, first connecting rod, the first stopper rod, the first cylinder barrel, the first fixed frame, the first hinged port and the first sliding groove road, the first hinge Connecing port and the first sliding groove road and be all located at front wing upper surface, front wing is connected by the first cross link with the first fixed frame, and first Fixed frame is installed on car body, and the both ends of first connecting rod are connected with the first fixed frame, and one end of the first cylinder barrel passes through the first stopper rod It is connected among first connecting rod, the other end of the first cylinder barrel is fixed with the first fixed frame；Wing mechanism is stretched to stretch including level-one The wing, the two level stretching, extension wing, level-one stretch the wing and are connected with the two level stretching, extension wing；Lower empennage mechanism includes lower empennage, the second cross link, the Two connecting rods, the second stopper rod, the second cylinder barrel, the second fixed frame, the second hinged port, the second sliding slot road, the second hinged port and the Two sliding slot roads are all located at lower empennage upper surface, and lower empennage is connected by the second cross link with the second fixed frame, the second fixed frame On car body, the both ends of second connecting rod are connected with the second fixed frame, and one end of the second cylinder barrel passes through the second stopper rod and second Connection, the other end of the second cylinder barrel are fixed with the second fixed frame among connecting rod；Upper empennage mechanism include upper empennage, spoiler, Stable frame, upper empennage and spoiler are all connected with stable frame.
- 2. hovercar as claimed in claim 1, it is characterised in that there are enough spaces to place machine inside the vehicle bottom The wing.
- 3. hovercar as claimed in claim 1, it is characterised in that shape is bullet type when the car body packs up wing.
- 4. hovercar as claimed in claim 1, it is characterised in that the shape of the stretching, extension wing mechanism is trapezoidal.
- 5. hovercar as claimed in claim 1, it is characterised in that the car body surface is streamlined.
- 6. hovercar as claimed in claim 1, it is characterised in that the preceding wing mechanism, stretching, extension wing mechanism and lower empennage Mechanism is used to provide lift；Upper empennage mechanism is used for the posture for controlling hovercar.
- 7. hovercar as claimed in claim 1, it is characterised in that the preceding wing mechanism is contracted in car body in ground run Inside, stretches out in flight below car body.
- 8. hovercar as claimed in claim 1, it is characterised in that stretching, extension wing mechanism two-level nested in ground run Vehicle body is contracted in, is stretched out in flight from car body both sides.
- 9. hovercar as claimed in claim 1, it is characterised in that the lower empennage mechanism is contracted in car in ground run Internal portion, stretches out in flight below car body.
- 10. hovercar as claimed in claim 1, it is characterised in that upper empennage mechanism spoiler in ground run It is upturned to provide negative lift, spoiler is rotated down to provide lift when starting flight.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610433670.1A CN105946484B (en) | 2016-06-18 | 2016-06-18 | Hovercar |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610433670.1A CN105946484B (en) | 2016-06-18 | 2016-06-18 | Hovercar |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105946484A CN105946484A (en) | 2016-09-21 |
| CN105946484B true CN105946484B (en) | 2018-05-01 |
Family
ID=56905867
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610433670.1A Expired - Fee Related CN105946484B (en) | 2016-06-18 | 2016-06-18 | Hovercar |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105946484B (en) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107599767A (en) * | 2017-11-06 | 2018-01-19 | 吉林工程技术师范学院 | Hovercar with folding wing |
| CN108177699A (en) * | 2018-01-26 | 2018-06-19 | 新日(无锡)发展有限公司 | A kind of electric vehicle detects trigger-type spademan ventilation safety protective device |
| EP3837124A4 (en) * | 2018-08-14 | 2022-08-24 | Everon Corporation | Personal auto-craft |
| CN110774848A (en) * | 2019-11-05 | 2020-02-11 | 北京信息科技大学 | Four-duct air-ground dual-purpose vehicle with telescopic wings |
| CN114347737B (en) * | 2021-12-29 | 2024-03-12 | 北京国家新能源汽车技术创新中心有限公司 | Deformable low-resistance flying car body structure and car |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4203286C2 (en) * | 1992-02-03 | 1993-10-21 | Hektor Steinhilber | Flight car |
| DE19639823A1 (en) * | 1996-09-27 | 1998-04-02 | Reza Nazer | Flying vehicle, e.g. helicopter |
| US6786450B1 (en) * | 2001-03-09 | 2004-09-07 | Harry Einstein | Rapidly-convertible roadable aircraft |
| US20030094536A1 (en) * | 2001-10-25 | 2003-05-22 | Labiche Mitchell G. | Flyable automobile |
| US20080018133A1 (en) * | 2006-07-24 | 2008-01-24 | Keng Lien Industrial Co., Ltd. | Spoiler accessory for a car |
| CN102133847A (en) * | 2011-02-28 | 2011-07-27 | 孙洪胜 | Automobile capable of flying |
| US9962618B2 (en) * | 2011-12-16 | 2018-05-08 | Mattel, Inc. | Toy vehicle |
| WO2014007883A1 (en) * | 2012-04-09 | 2014-01-09 | Smith Frick A | Aircraft with freewheeling engine |
| CN103522858A (en) * | 2013-10-16 | 2014-01-22 | 北京航空航天大学 | Flying passenger car |
-
2016
- 2016-06-18 CN CN201610433670.1A patent/CN105946484B/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| CN105946484A (en) | 2016-09-21 |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
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| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180501 Termination date: 20210618 |