CN105946484A - Flying car - Google Patents
Flying car Download PDFInfo
- Publication number
- CN105946484A CN105946484A CN201610433670.1A CN201610433670A CN105946484A CN 105946484 A CN105946484 A CN 105946484A CN 201610433670 A CN201610433670 A CN 201610433670A CN 105946484 A CN105946484 A CN 105946484A
- Authority
- CN
- China
- Prior art keywords
- wing
- empennage
- car body
- hovercar
- fixed mount
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- 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
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D35/00—Vehicle bodies characterised by streamlining
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C37/00—Convertible aircraft
-
- 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
Abstract
The invention discloses a flying car, comprising a body, a front wing mechanism, extensible wing mechanisms, a lower tail wing mechanism and an upper tail wing mechanism; the front wing mechanism is disposed below the front end of the body, the extensible wing mechanisms are disposed below the middle of the body, the lower tail wing mechanism is disposed below the rear end of the body, and the upper tail wing mechanism is disposed above the rear end of the body. The flying car can run on a ground and fly in air, is as large as a space used by a common car when running on the ground, is flexible and easy to drive and park, and may fly as a common miniature aircraft when flying.
Description
Technical field
The present invention relates to a kind of automobile, particularly relate to a kind of hovercar.
Background technology
Along with science and technology development rapidly and the growth of human lives's demand, automobile has become as the main traffic instrument of people's go off daily, and working peak time traffic jam has become as the common problem in each city.Therefore hovercar is born, and can become a kind of preferably vehicles, and the track for transportation adds a dimension, i.e. on ground during blocking, can be exchanged into offline mode, alleviates again the situation of traffic congestion while convenient trip.Current existing hovercar majority is folding wings hovercar, and its wing is placed on body both sides, and the physical dimension of the most whole hovercar is relatively big and takes up room relatively big, travels stop all flexible not as general-utility car.
Summary of the invention
The technical problem to be solved is to provide a kind of hovercar, and it has general-utility car characteristic superiority and can realize air objective, and physical dimension is less and takes up room less, travels stop as flexible in general-utility car.
The present invention solves above-mentioned technical problem by following technical proposals: a kind of hovercar, it is characterized in that, it includes car body, front wing mechanism, stretches wing mechanism, lower empennage mechanism and upper empennage mechanism, front wing mechanism is arranged on below the front end of car body, stretch wing mechanism and be 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 most front wing mechanism includes front wing, the first cross link, first connecting rod, the first stopper rod, the first cylinder barrel, the first fixed mount, the first hinged port and the first chute road, first hinged port and the first chute road are all located at front wing upper surface, front wing is connected with the first fixed mount by the first cross link, first fixed mount is arranged on car body, the two ends of first connecting rod are connected with the first fixed mount, one end of first cylinder barrel is connected in the middle of first connecting rod by the first stopper rod, and the other end and first fixed mount of the first cylinder barrel are fixed；Stretching wing mechanism and include that one-level stretches the wing, two grades of stretching, extension wings, one-level stretches the wing and two grades of stretching, extension wings connect；Lower empennage mechanism includes lower empennage, the second cross link, second connecting rod, the second stopper rod, the second cylinder barrel, the second fixed mount, the second hinged port, the second chute road, second hinged port and the second chute road are all located at lower empennage upper surface, lower empennage is connected with the second fixed mount by the second cross link, second fixed mount is arranged on car body, the two ends of second connecting rod are connected with the second fixed mount, one end of second cylinder barrel is connected in the middle of second connecting rod by the second stopper rod, and the other end and second fixed mount of the second cylinder barrel are fixed；Upper empennage mechanism includes empennage, spoiler, stable frame, and upper empennage is all connected with stable frame with spoiler.
Preferably, enough spaces are had to place wing inside described vehicle bottom.
Preferably, described car body is shaped as bullet type when packing up wing.
Preferably, described stretching, extension wing mechanism be shaped as trapezoidal.
Preferably, described car body surface is streamlined.
Preferably, described front wing mechanism, stretching, extension wing mechanism and lower empennage mechanism are used for providing lift；Upper empennage mechanism is for controlling the attitude of hovercar.
Preferably, described front wing mechanism is contracted in vehicle body when ground run, stretches out below car body when flight.
Preferably, described stretching, extension wing mechanism two-level nested when ground run is contracted in vehicle body, stretches out from car body both sides when flight.
Preferably, described lower empennage mechanism is contracted in vehicle body when ground run, stretches out below car body when flight.
Preferably, described upper empennage mechanism spoiler when ground run is upturned to provide negative lift, and when starting flight, spoiler rotates down to provide lift.
The most progressive effect of the present invention is: the present invention can travel on the ground, also can aloft fly.The each several part wing of the present invention can be hidden among car body completely, this makes the present invention have feature and the driving mode of general-utility car completely when ground run, volume size and general-utility car take up space sizableness, and travel, stop flexible, mode of operation is identical with general-utility car.After each several part wing full extension of the present invention is opened, the lift relying on airfoil surface to produce can realize the basic function of baby plane thus realize air objective.The combination designed with the scalable wing due to the bullet type car body design of the present invention so that the present invention can complete ground run and airflight task under less spatial volume.The present invention can alleviate serious load traffic problems, and is combined with flight management by vehicle drive, and flight management becomes summary, popular, universalness.
Accompanying drawing explanation
Fig. 1 is structural representation during ground run of the present invention.
Fig. 2 is structural representation during airflight of the present invention.
Fig. 3 is side view during airflight of the present invention.
Fig. 4 is front wing mechanism structure schematic diagram of the present invention.
Fig. 5 is empennage mechanism structural representation under the present invention.
Fig. 6 is top view during airflight of the present invention.
Fig. 7 is front view during flight in the present invention.
Detailed description of the invention
Provide present pre-ferred embodiments below in conjunction with the accompanying drawings, to describe technical scheme in detail.
As shown in Figures 1 to 7, hovercar of the present invention includes car body 1, front wing mechanism 2, stretches wing mechanism 3, lower empennage mechanism 4 and upper empennage mechanism 5, front wing mechanism 2 is arranged on below the front end of car body 1, stretch wing mechanism 3 and be arranged on lower section in the middle part of car body 1, lower empennage mechanism 4 is arranged on below the rear end of car body 1, and upper empennage mechanism 5 is arranged on above car body 1 rear end；The most front wing mechanism 2 includes front wing 21, first cross link 22, first connecting rod 23, first stopper rod 24, first cylinder barrel 25, first fixed mount 26, first hinged port 21a and the first chute road 21b, first hinged port 21a and the first chute road 21b is all located at front wing 21 upper surface, front wing 21 is connected with the first fixed mount 26 by the first cross link 22, first fixed mount 26 is arranged on car body 1, the two ends of first connecting rod 23 are connected with the first fixed mount 26, one end of first cylinder barrel 25 is connected in the middle of first connecting rod 23 by the first stopper rod 24, the other end and first fixed mount 26 of the first cylinder barrel 25 are fixed；Stretching wing mechanism 3 and include that one-level stretches 31, two grades of the wing and stretches the wing 32, one-level stretches the wing 31 and two grades of stretching, extension wings 32 connect；Lower empennage mechanism 4 includes lower empennage 41, second cross link 42, second connecting rod 43, second stopper rod 44, second cylinder barrel 45, second fixed mount 46, second hinged port 41a, second chute road 41b, second hinged port 41a and the second chute road 41b is all located at lower empennage 41 upper surface, lower empennage 41 is connected with the second fixed mount 46 by the second cross link 42, second fixed mount 46 is arranged on car body 1, the two ends of second connecting rod 43 are connected with the second fixed mount 46, one end of second cylinder barrel 45 is connected in the middle of second connecting rod 43 by the second stopper rod 44, the other end and second fixed mount 46 of the second cylinder barrel 45 are fixed；Upper empennage mechanism 5 includes empennage 51, spoiler 52, stable frame 53, and upper empennage 51 is all connected with stable frame 53 with spoiler 52.
There are enough spaces can place wing inside vehicle bottom, so save space.
It is shaped as bullet type when car body packs up wing, so saves space.
Being shaped as of stretching, extension wing mechanism is trapezoidal, and this spline structure is more stable.
The operation principle of this hovercar is as follows: car body surface is streamlined, is used for reducing air drag；Front wing mechanism, stretching, extension wing mechanism and lower empennage mechanism are used for providing lift；Upper empennage mechanism is for controlling the attitude of hovercar.The most front wing mechanism, stretching, extension wing mechanism, lower empennage mechanism and upper empennage mechanism are separately positioned on below the front end of car body, in the middle part of car body to be stabilized on frame with rear end below lower section, rear end.Front wing mechanism is contracted in vehicle body when ground run, stretches out below car body when flight.Described stretching, extension wing mechanism two-level nested when ground run is contracted in vehicle body, stretches out from car body both sides when flight.Described lower empennage mechanism is contracted in vehicle body when ground run, stretches out below car body when flight.Described upper empennage mechanism spoiler when ground run is upturned to provide negative lift, and when starting flight, spoiler rotates down to provide lift.When flight, spoiler can adjust rotational angle according to demand.The one-level stretching, extension wing is driven by screw mechanism and moves to car body from vehicle body, and two grades are stretched the wings and pass through servo control mechanism driving from the internal mobile stretching, extension of the one-level stretching, extension wing.First connecting rod, the first stopper rod and the first cylinder barrel are for regulating the distance between front wing and the first fixed mount.Spoiler can carry out the rotation of certain angle.Upper empennage mechanism spoiler when ground run is upturned, and to provide negative lift, when starting flight, spoiler rotates down, and to provide lift, when flight, spoiler can adjust rotational angle according to demand.
In sum, the present invention can realize ground run and airflight simultaneously, and take up space during ground run sizableness with general-utility car, and it is flexible to travel stop.The air objective of common compact aircraft can be realized during flight.
Particular embodiments described above; solve the technical problem that the present invention, technical scheme and beneficial effect are further described; it is it should be understood that; the foregoing is only the specific embodiment of the present invention; it is not limited to the present invention; all within the spirit and principles in the present invention, any modification, equivalent substitution and improvement etc. done, should be included within the scope of the present invention.
Claims (10)
1. a hovercar, it is characterized in that, it includes car body, front wing mechanism, stretches wing mechanism, lower empennage mechanism and upper empennage mechanism, front wing mechanism is arranged on below the front end of car body, stretch wing mechanism and be 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 most front wing mechanism includes front wing, the first cross link, first connecting rod, the first stopper rod, the first cylinder barrel, the first fixed mount, the first hinged port and the first chute road, first hinged port and the first chute road are all located at front wing upper surface, front wing is connected with the first fixed mount by the first cross link, first fixed mount is arranged on car body, the two ends of first connecting rod are connected with the first fixed mount, one end of first cylinder barrel is connected in the middle of first connecting rod by the first stopper rod, and the other end and first fixed mount of the first cylinder barrel are fixed；Stretching wing mechanism and include that one-level stretches the wing, two grades of stretching, extension wings, one-level stretches the wing and two grades of stretching, extension wings connect；Lower empennage mechanism includes lower empennage, the second cross link, second connecting rod, the second stopper rod, the second cylinder barrel, the second fixed mount, the second hinged port, the second chute road, second hinged port and the second chute road are all located at lower empennage upper surface, lower empennage is connected with the second fixed mount by the second cross link, second fixed mount is arranged on car body, the two ends of second connecting rod are connected with the second fixed mount, one end of second cylinder barrel is connected in the middle of second connecting rod by the second stopper rod, and the other end and second fixed mount of the second cylinder barrel are fixed；Upper empennage mechanism includes empennage, spoiler, stable frame, and upper empennage is all connected with stable frame with spoiler.
2. hovercar as claimed in claim 1, it is characterised in that have enough spaces to place wing inside described vehicle bottom.
3. hovercar as claimed in claim 1, it is characterised in that described car body is shaped as bullet type when packing up wing.
4. hovercar as claimed in claim 1, it is characterised in that being shaped as of described stretching, extension wing mechanism is trapezoidal.
5. hovercar as claimed in claim 1, it is characterised in that described car body surface is streamlined.
6. hovercar as claimed in claim 1, it is characterised in that described front wing mechanism, stretching, extension wing mechanism and lower empennage mechanism are used for providing lift；Upper empennage mechanism is for controlling the attitude of hovercar.
7. hovercar as claimed in claim 1, it is characterised in that described front wing mechanism is contracted in vehicle body when ground run, stretches out below car body when flight.
8. hovercar as claimed in claim 1, it is characterised in that described stretching, extension wing mechanism two-level nested when ground run is contracted in vehicle body, stretches out from car body both sides when flight.
9. hovercar as claimed in claim 1, it is characterised in that described lower empennage mechanism is contracted in vehicle body when ground run, stretches out below car body when flight.
10. hovercar as claimed in claim 1, it is characterised in that described upper empennage mechanism spoiler when ground run is upturned to provide negative lift, and when starting flight, spoiler rotates down to provide lift.
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 true CN105946484A (en) | 2016-09-21 |
| CN105946484B 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) |
Cited By (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 |
| 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 |
| CN112839829A (en) * | 2018-08-14 | 2021-05-25 | 埃弗隆股份有限公司 | Private autonomous aircraft |
| CN114347737A (en) * | 2021-12-29 | 2022-04-15 | 北京国家新能源汽车技术创新中心有限公司 | Deformable low-resistance hovercar body structure and automobile |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4203286A1 (en) * | 1992-02-03 | 1993-08-05 | Hektor Steinhilber | Car capable of road travel and aerial flight - uses Frisbee-type skimmer disc to control vehicle during forward level flight. |
| DE19639823A1 (en) * | 1996-09-27 | 1998-04-02 | Reza Nazer | Flying vehicle, e.g. helicopter |
| US20030094536A1 (en) * | 2001-10-25 | 2003-05-22 | Labiche Mitchell G. | Flyable automobile |
| US6786450B1 (en) * | 2001-03-09 | 2004-09-07 | Harry Einstein | Rapidly-convertible roadable aircraft |
| 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 |
| 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 |
| CN203469460U (en) * | 2011-12-16 | 2014-03-12 | 美泰有限公司 | Reconfigurable toy vehicle |
-
2016
- 2016-06-18 CN CN201610433670.1A patent/CN105946484B/en not_active Expired - Fee Related
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4203286A1 (en) * | 1992-02-03 | 1993-08-05 | Hektor Steinhilber | Car capable of road travel and aerial flight - uses Frisbee-type skimmer disc to control vehicle during forward level flight. |
| 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 |
| CN203469460U (en) * | 2011-12-16 | 2014-03-12 | 美泰有限公司 | Reconfigurable 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 |
Cited By (6)
| 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 |
| CN112839829A (en) * | 2018-08-14 | 2021-05-25 | 埃弗隆股份有限公司 | Private autonomous aircraft |
| 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 |
| CN114347737A (en) * | 2021-12-29 | 2022-04-15 | 北京国家新能源汽车技术创新中心有限公司 | Deformable low-resistance hovercar body structure and automobile |
| 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 |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105946484B (en) | 2018-05-01 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105946484A (en) | Flying car | |
| CN102530238B (en) | Unmanned aerial vehicle with variable sweepbacks and spans of wings | |
| CN102229357B (en) | Empennage with installing angle and adjustable horizontal tail | |
| CN206031778U (en) | Wing can twist reverse and can realize miniature flapping wing aircraft of many flight motions | |
| CN106143903B (en) | A kind of wing can reverse and can realize the micro flapping wing air vehicle of more sporting flyings | |
| CN205381319U (en) | Tail wing structure that automatically controlled formula of FSE equation motorcycle race is adjustable | |
| CN205768418U (en) | Modified model distributed electric ducted fan wing flap high-lift system and hovercar thereof | |
| CN205801516U (en) | A kind of fixed-wing unmanned plane of VTOL | |
| CN105235889B (en) | Self-adaptive rhombic wing layout of air vehicles | |
| CN209617451U (en) | A kind of aircraft | |
| CN109484634A (en) | A kind of culvert type aircraft | |
| CN209366454U (en) | A kind of culvert type aircraft | |
| CN108437722A (en) | A kind of vertical take-off and landing flying car | |
| CN106427437B (en) | A kind of hovercar | |
| CN111923672B (en) | Flying automobile | |
| CN108437714A (en) | A kind of hovercar | |
| CN204688240U (en) | A kind of automobile spoiler draw off gear of fluid control | |
| CN101941365B (en) | Personal triphibious transport tool | |
| CN201989946U (en) | Small-size double-wheel foldable wing airplane | |
| CN107487440A (en) | A kind of deformable flexible oil storage wing of scounting aeroplane | |
| CN2467345Y (en) | Flying vehicle | |
| CN107651165A (en) | A kind of adjustable wing of the thickness of scounting aeroplane | |
| CN213007448U (en) | Aerocar capable of adjusting ground grabbing force and lifting force | |
| CN213007446U (en) | Hovercar who contains formula of accomodating flight driving system | |
| CN107161322A (en) | One kind becomes sweepback STOL Fixed Wing AirVehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| 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 |