CN107116981A - A kind of four wing hovercars - Google Patents
A kind of four wing hovercars Download PDFInfo
- Publication number
- CN107116981A CN107116981A CN201710330249.2A CN201710330249A CN107116981A CN 107116981 A CN107116981 A CN 107116981A CN 201710330249 A CN201710330249 A CN 201710330249A CN 107116981 A CN107116981 A CN 107116981A
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- Prior art keywords
- car body
- duct
- hovercar
- wings
- hand
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Classifications
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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
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Transportation (AREA)
- Transition And Organic Metals Composition Catalysts For Addition Polymerization (AREA)
Abstract
The invention discloses a kind of four wings hovercar, including car body, the front and rear end of car body is respectively arranged with the preceding duct and rear duct being arranged symmetrically, the axis of preceding duct and rear duct is perpendicular with ground, the inner chamber of preceding duct is provided with front propeller, the inner chamber of duct is provided with rear screw shaft afterwards, front propeller is connected with rear screw shaft with setting drive mechanism in car body, car body upper horizontal is provided with overarm, overarm and the length direction of car body are perpendicular, overarm left end is provided with Left Drive mechanism, left-hand airscrew is connected with Left Drive mechanism, overarm right-hand member is provided with right transmission mechanism, right-hand screw oar is connected with right transmission mechanism, left-leaning rotation mechanism is provided with Left Drive mechanism, Right deviation rotation mechanism is provided with right transmission mechanism.Four wings hovercar can either provide larger lift to hovercar, can strengthen balance during hovercar flight in the air again, lift security performance.
Description
Technical field
The present invention relates to technical field of vehicle, more specifically, more particularly to a kind of four wings hovercar.
Background technology
Hovercar refers to can both travel on land, the automobile that can be flown in the air again.In the 1940s, working as vapour
Car, aeronautical technology have after sizable development, and Ford Motor Company founder enjoys Li Fute and just audaciously sends " flight
Automobile occurs sooner or later " science prophesy.To the fifties, people have just started the practical action of the modern hovercar of research.
In the journey for climbing modern hovercar technology, the person of standing in the breach carried forward the cause of the older generation and break new ground is the U.S. for being named as Taylor More
People, he passed through unremitting effort, in 1986, and Hyundai Motor and aeronautical technology perfect pair are gone out into one kind finally can be on the ground
Run, the hovercar that can fly in the air again, and obtain the traffic pass that relevant government department signs and issues.
The patent of Application No. 201110047409.5 provides a kind of existing hovercar, as shown in figure 1, this flies
Row automobile on car body by that can be hidden in the front wing 01 of interior of body, flying wing 02, jet engine 03 and can roll over
The rudder 04 risen is constituted.When hovercar flight in the air, thrust that hovercar is produced in jet engine 03 and
Under the lift that flying wing 02 is produced, can fly in the air, front wing 01 and rudder 04 can adjust hovercar balance and
Heading；When hovercar is exercised on ground, front wing 01, flying wing 02 and jet engine 03, which can shrink, to be hidden in
The inside of automobile, rudder 04 is inwardly folded on the tail body for being placed on automobile, so, and the external form of hovercar is just and common
Automobile is the same, can exercise on the ground.
For above-mentioned this kind of hovercar, because automobile is frequently necessary to the row in narrow road and narrow and small air environment
Sail, therefore the width of flying wing 02 is often smaller, in this way, the lift that can be improved to hovercar is also smaller, strongly limit
The flight altitude and airspeed of hovercar；In addition, during above-mentioned this automobile flight in the air, two are relied solely on close to horizontal
Flying wing 02 maintains the balance of vehicle body, is so easy to overturn in the case where beam wind is acted on, has had a strong impact on driving safety.
The content of the invention
The technical problem to be solved in the present invention is provides a kind of four wings hovercar, and four wings hovercar passes through its structure
Design, larger lift can either be provided to hovercar, can strengthen balance during hovercar flight in the air again, is lifted
Security performance.
A kind of four wing hovercars, including car body, the front and rear end of the car body is respectively arranged with what is be arranged symmetrically
Preceding duct and rear duct, the axis of the preceding duct and the rear duct are perpendicular with ground, the inner chamber of the preceding duct
Be provided with front propeller, the inner chamber of the rear duct is provided with rear screw shaft, the front propeller and the rear screw shaft with
Drive mechanism connection is set in car body, the car body upper horizontal is provided with overarm, the overarm and the length direction of the car body
Perpendicular, the overarm left end, which is provided with Left Drive mechanism, the Left Drive mechanism, is connected with left-hand airscrew, and the overarm is right
End, which is provided with right transmission mechanism, the right transmission mechanism, is connected with right-hand screw oar, and "Left"-deviationist is provided with the Left Drive mechanism
Rotation mechanism, the left-leaning rotation mechanism is used to adjust the angle between the axis of the left-hand airscrew and horizontal plane, the right biography
Be provided with Right deviation rotation mechanism on motivation structure, the Right deviation rotation mechanism be used to adjusting the right-hand screw oar axis and horizontal plane it
Between angle.
Preferably, the diameter of the preceding duct and the rear duct is respectively less than width of the carbody.
Preferably, the front propeller is equal to the left-hand airscrew to the right spiral shell to the distance between the rear screw shaft
Revolve the distance between oar.
Preferably, the diameter of the front propeller, the rear screw shaft, the left-hand airscrew and the right-hand screw oar is homogeneous
Deng.
Preferably, connected respectively on the front propeller, the rear screw shaft, the left-hand airscrew and the right-hand screw oar
There is the total distance regulating mechanism of independent propeller.
Preferably, the preceding duct in the rear duct with being provided with spoiler.
Preferably, the car body top is provided with vertical pivot, and the vertical pivot lower end is fixed on the car body, on the vertical pivot
End is connected with the overarm.
Preferably, the axis of the vertical pivot and the center of gravity of the car body are located along the same line.
The beneficial effects of the invention are as follows：Four wings hovercar that the present invention is provided is by its structure design, on car body
Preceding duct and rear duct are directly set, and preceding duct is with being respectively mounted front propeller and rear screw shaft composition first set spiral shell in rear duct
Oar lift unit is revolved, then sets left-hand airscrew to constitute second set of propeller liter with right-hand screw oar in the horizontal overarm on roof
Power apparatus, that is to say, that along width of the carbody direction on 2 propellers arranged in car body duct along length over ends of body direction and overarm
2 propellers of arrangement combine to form four wing patterns, for existing hovercar, and the four of two sets of propeller combination compositions
Wing pattern has obviously increased considerably lift, makes four wings hovercar possess the lift of abundance to realize landing of easily taking off
And rapid flight.
In addition, along width of the carbody direction cloth in 2 propellers arranged in car body duct along length over ends of body direction and overarm
2 propellers put combine to form four wing patterns, greatly improve the skyborne attitude stability of hovercar.Simultaneously because
Left-hand airscrew on right-hand screw oar with being separately installed with left-leaning rotation mechanism and Right deviation rotation mechanism, by adjusting left-leaning rotation mechanism and Right deviation
The tilt angle of rotation mechanism can produce the pulling force of part horizontal direction, preferably offset the impact of horizontal crosswind, it is ensured that flight
Safety.
Brief description of the drawings
In order to illustrate more clearly about the embodiment of the present invention or technical scheme of the prior art, below will be to embodiment or existing
There is the accompanying drawing used required in technology description to be briefly described, it should be apparent that, drawings in the following description are only this
The embodiment of invention, for those of ordinary skill in the art, on the premise of not paying creative work, can also basis
The accompanying drawing of offer obtains other accompanying drawings.
Fig. 1 is a kind of structural representation of hovercar of prior art；
Fig. 2 is a kind of overlook direction schematic diagram of four wings hovercar disclosed in the embodiment of the present invention；
Fig. 3 is a kind of overlook direction schematic diagram of four wings hovercar disclosed in the embodiment of the present invention.
Embodiment
In order that those skilled in the art more fully understand the technical scheme in the application, it is real below in conjunction with the application
The accompanying drawing in example is applied, the technical scheme in the embodiment of the present application is clearly and completely described, it is clear that described implementation
Example only some embodiments of the present application, rather than whole embodiments.
Based on the embodiment in the application, those of ordinary skill in the art are obtained under the premise of creative work is not made
The every other embodiment obtained, should all belong to the scope of the application protection.
Referring to Fig. 2 and Fig. 3, Fig. 2 and Fig. 3 provide a kind of the first specific embodiment of four wings hovercar of the present invention,
Wherein, Fig. 2 is a kind of overlook direction schematic diagram of four wings hovercar disclosed in the embodiment of the present invention；Fig. 3 is real for the present invention
Apply a kind of overlook direction schematic diagram of four wings hovercar disclosed in example.
As shown in Figures 2 and 3, the invention provides a kind of four wings hovercar, can with it is highly stable, quickly in the air
Flight.
Four wings hovercar includes car body 1, preceding duct 2, rear duct 3, front propeller 4, rear screw shaft 5, drive mechanism
6, overarm 7, Left Drive mechanism 8, left-hand airscrew 9, right transmission mechanism 10, right-hand screw oar 11, left-leaning rotation mechanism 12 is made a connection with Right deviation
Structure 13.Wherein, four wings include front propeller 4, rear screw shaft 5, left-hand airscrew 9 and right-hand screw oar 11.
In this programme, the car body 1 of four wings hovercar is body supports holding mechanism, for the carrying of occupant, simultaneously
Installation for other mechanisms.Physical length, width, height and interior trim of car body 1 etc. are typically designed according to actual needs.
The front end of car body 1 is provided with preceding duct 2, and the rear end of car body 1 is provided with rear duct 3, the axis of preceding duct 2 and rear duct 3
Line is perpendicular with ground.Preceding duct 2 is arranged symmetrically with rear duct 3, that is to say, that preceding duct 2 and the rear shape of duct 3 are complete
Identical, the line of symmetry of preceding duct 2 and rear duct 3 is the transversal centerline of car body 1.
Specifically, preceding duct 2 is generally the cylinder for the up/down perforation being set directly on car body 1, preceding duct with rear duct 3
2 carry out matched design with the general airscrew diameter according to needed for the weight of car body 1 of the internal diameter size of rear duct 3.
The inner chamber of preceding duct 2 is provided with front propeller 4, and the inner chamber of rear duct 3 is provided with rear screw shaft 5, front propeller 4 with
Rear screw shaft 5 is connected with setting drive mechanism 6 in car body 1.Drive mechanism 6 is used for the rotation with rear screw shaft 5 for front propeller 4
Power is provided.
The upper horizontal of car body 1 is provided with overarm 7, and overarm 7 and the length direction of car body 1 are perpendicular, and 7 left ends of overarm are provided with
Left-hand airscrew 9 is connected with Left Drive mechanism 8, Left Drive mechanism 8, Left Drive mechanism 8 is used to provide for the rotation of left-hand airscrew 9
Power is inputted.7 right-hand members of hanging oneself from a beam are provided with right transmission mechanism 10, right transmission mechanism 10 and are connected with right-hand screw oar 11, right driver
Structure 10 is used to input for the powered rotation of right-hand screw oar 11.
In the present embodiment, Left Drive mechanism 8 can be directly connected to right transmission mechanism 10 by equipment such as gearboxes
In the drive mechanism 6 set in car body 1, power is provided by vehicle-mounted drive mechanism 6, and then drive left-hand airscrew 9 and right-hand screw oar
11 rotations.In this way, relying solely on the drive mechanism 6 that car body carries just can realize traveling of the automobile on road and aerial fly
OK, it is very convenient.
Further, it is also possible to be connected independent drive mechanism respectively with right transmission mechanism 10 in Left Drive mechanism 8, such as it is electric
Motivation, additionally installs motor in 7 left and right ends of hanging oneself from a beam in implementation, then distinguishes Left Drive mechanism 8 with right transmission mechanism 10
It is connected on above-mentioned motor, is respectively that left-hand airscrew 9 and right-hand screw oar 11 provide rotary power by peripheral hardware motor.
Left-leaning rotation mechanism 12 is provided with Left Drive mechanism 8, left-leaning rotation mechanism 12 is used for the axis for adjusting left-hand airscrew 9
Right deviation rotation mechanism 13 is provided with angle between horizontal plane, right transmission mechanism 10, Right deviation rotation mechanism 13 is used to adjust right spiral shell
Revolve the angle between the axis of oar 11 and horizontal plane.
The accompanying drawing that Fig. 3 is provided is that left-leaning rotation mechanism 12 drives left-hand airscrew 9 to turn forward the situation of certain angle, when
So "Left"-deviationist rotation mechanism 12 can also drive left-hand airscrew 9 backward, to the left, be tilted to the right, specifically determined by being actually needed.Certainly,
Right deviation rotation mechanism 13 can also drive right-hand screw oar 11 to do similar tilting action.
In this way, when four wings hovercar meets horizontal crosswind in the air, just can be by adjusting left-leaning rotation mechanism 12
The tilt angle of left-hand airscrew 9 and right-hand screw oar 11 is controlled with Right deviation rotation mechanism 13, parts transversely crosswind is offset, it is ensured that this four
The stationarity that wing hovercar flies in the air.
In addition, by the regulation of left-leaning rotation mechanism 12 and Right deviation rotation mechanism 13, left-hand airscrew 9 and right-hand screw oar 11 can be produced
The pulling force of first portion horizontal direction, more convenient realize flies before four wings hovercar, flown afterwards or horizontal winged function, flies four wing
Row automobile can be with rapid flight and economic flight.
Generally speaking, four wings hovercar that the present invention is provided directly sets preceding duct 2 and rear duct 3 on car body 1,
Preceding duct 2 is with being respectively mounted front propeller 4 and the composition first set propeller lift unit of rear screw shaft 5, Ran Hou in rear duct 3
Left-hand airscrew 9 is set to constitute second set of propeller lift unit with right-hand screw oar 11 in horizontal overarm 7 on the roof of car body 1,
That is, along the width of car body 1 arrangement on 2 propellers arranged in car body duct along the length direction of car body 1 and overarm 7
2 propellers combine four wing patterns that to be formed, namely four wing hovercars of the invention.
Four wing hovercars of the present invention are compared for existing hovercar, four wing moulds that two sets of propeller combinations are constituted
Formula has obviously increased considerably lift, four wings hovercar is possessed the lift of abundance and lands and fast to conveniently realize to take off
Speed flight.
In addition, along width of the carbody direction in 2 propellers arranged in car body duct along the length direction of car body 1 and overarm 7
2 propellers of arrangement combine to form four wing patterns, greatly improve the skyborne attitude stability of hovercar.Simultaneously because
Left-leaning rotation mechanism 12 and Right deviation rotation mechanism 13 are separately installed with left-hand airscrew 9 and right-hand screw oar 11, by adjusting left-leaning turn
The tilt angle of mechanism 12 and Right deviation rotation mechanism 13 can produce the pulling force of part horizontal direction, preferably offset horizontal crosswind
Impact, it is ensured that flight safety.
It is the flexibility of four wing hovercars of further lifting in the present embodiment, it is to avoid propeller is too wide and four wings are flown
Row automobile produces interference in the traveling of limited road and narrow and small air environment, it is preferable that the diameter of preceding duct 2 and rear duct 3 is equal
Less than the width of car body 1.In this way, the propeller in preceding duct 2 and rear duct 3 is not extended to outside the width of car body 1,
Avoid vehicle body overall too wide and take action limited.
It is four wing hovercar traveling comforts of further lifting, it is preferable that after front propeller 4 is arrived in the present embodiment
The distance between propeller 5 is equal to left-hand airscrew 9 and arrives the distance between right-hand screw oar 11.Front propeller 4, rear screw shaft 5, left spiral shell
The diameter for revolving oar 9 and right-hand screw oar 11 is equal.
In the present embodiment, for convenience of each propeller always away from regulation, so as to adjust the lift required for four wing hovercars
Independent propeller is connected to always away from tune on size, front propeller 4, rear screw shaft 5, left-hand airscrew 9 and right-hand screw oar 11
Save mechanism.In this way, left-leaning rotation mechanism 12 and Right deviation rotation mechanism 13 control four wing hovercar tilt angles and propeller always away from
Governor motion control propeller always away from synergic adjustment under, can easily realize the driftage of four wing hovercars turn to, it is spin, horizontal
The control of the functions such as flight.
For this programme, front propeller 4, rear screw shaft 5,11 4 spiral shells of left-hand airscrew 9 and right-hand screw oar are designed with altogether
Oar is revolved, wherein, the total distance regulating mechanism of propeller is to each propeller always away from regulation according to four wing hovercar flight attitudes
It is required that and being mutually matched regulation.
In addition, the electric-control system being connected with the total distance regulating mechanism of propeller is typically provided with car body 1, so as to pass through electricity
Control system to each propeller always away from carry out more precisely, easily coordinate match control.
In the present embodiment, for convenience of the regulation of four wing hovercar flight attitudes.Preferably, in preceding duct 2 and rear duct 3
It is provided with spoiler 14.Specifically, the anglec of rotation by adjusting spoiler 14, can adjust air-flow by preceding duct 2 with
The uninterrupted of duct 3 and direction afterwards, so that, it is more convenient the regulation of four wings hovercar flight attitude.
In practical operation, spoiler 14 is typically made a connection with the total distance regulating mechanism of above-mentioned propeller, left-leaning rotation mechanism 12, Right deviation
Structure 13 coordinates to realize the control to four wing hovercar flight attitudes together.
In the present embodiment, for convenience of the installation of overarm 7, the top of car body 1 is provided with vertical pivot 15, and the lower end of vertical pivot 15 is fixed on car
On body 1, the upper end of vertical pivot 15 is connected with overarm 7.
In the present embodiment, to further facilitate the balance control of four wing hovercars, axis and the car body 1 of vertical pivot 15
Center of gravity is located along the same line.
A kind of four wings hovercar provided by the present invention is described in detail above.It is used herein specifically individual
Example is set forth to the principle and embodiment of the present invention, and the explanation of above example is only intended to help to understand the present invention's
Method and its core concept.It should be pointed out that for those skilled in the art, not departing from the principle of the invention
On the premise of, some improvement and modification can also be carried out to the present invention, these are improved and modification also falls into the claims in the present invention
Protection domain in.
Claims (8)
1. a kind of four wings hovercar, it is characterised in that including car body, the front and rear end of the car body be respectively arranged with pair
Claim the preceding duct and rear duct of arrangement, the axis of the preceding duct and the rear duct is perpendicular with ground, the preceding culvert
The inner chamber in road is provided with front propeller, and the inner chamber of the rear duct is provided with rear screw shaft, the front propeller and the rear spiral shell
Rotation oar is connected with setting drive mechanism in car body, and the car body upper horizontal is provided with overarm, the overarm and the car body
Length direction is perpendicular, and the overarm left end, which is provided with Left Drive mechanism, the Left Drive mechanism, is connected with left-hand airscrew, institute
State overarm right-hand member to be provided with right transmission mechanism, the right transmission mechanism and be connected with right-hand screw oar, set in the Left Drive mechanism
Left-leaning rotation mechanism is equipped with, the left-leaning rotation mechanism is used to adjust the angle between the axis of the left-hand airscrew and horizontal plane,
Be provided with Right deviation rotation mechanism on the right transmission mechanism, the Right deviation rotation mechanism be used to adjusting the axis of the right-hand screw oar with
Angle between horizontal plane.
2. four wings hovercar according to claim 1, it is characterised in that the diameter of the preceding duct and the rear duct
Respectively less than width of the carbody.
3. four wings hovercar according to claim 2, it is characterised in that the front propeller to the rear screw shaft it
Between distance be equal to described left-hand airscrew the distance between to the right-hand screw oar.
4. four wings hovercar according to claim 2, it is characterised in that the front propeller, the rear screw shaft, institute
The diameter for stating left-hand airscrew and the right-hand screw oar is equal.
5. four wings hovercar according to claim 1, it is characterised in that the front propeller, the rear screw shaft, institute
State and be connected to the total distance regulating mechanism of independent propeller on left-hand airscrew and the right-hand screw oar.
6. four wings hovercar according to claim 1, it is characterised in that the preceding duct in the rear duct with being all provided with
It is equipped with spoiler.
7. four wings hovercar according to claim 1, it is characterised in that the car body top is provided with vertical pivot, described
Vertical pivot lower end is fixed on the car body, and the vertical pivot upper end is connected with the overarm.
8. four wings hovercar according to claim 7, it is characterised in that the axis of the vertical pivot and the car body
Center of gravity is located along the same line.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710330249.2A CN107116981A (en) | 2017-05-11 | 2017-05-11 | A kind of four wing hovercars |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710330249.2A CN107116981A (en) | 2017-05-11 | 2017-05-11 | A kind of four wing hovercars |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107116981A true CN107116981A (en) | 2017-09-01 |
Family
ID=59728083
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710330249.2A Pending CN107116981A (en) | 2017-05-11 | 2017-05-11 | A kind of four wing hovercars |
Country Status (1)
| Country | Link |
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| CN (1) | CN107116981A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109878283A (en) * | 2019-04-10 | 2019-06-14 | 江苏航空职业技术学院 | A kind of hovercar oil electric mixed dynamic system |
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| WO2016066848A1 (en) * | 2014-10-31 | 2016-05-06 | Schwöller Johann | Driving module for a motor vehicle, and motor vehicle comprising a driving module of said type |
| CN105752320A (en) * | 2016-04-01 | 2016-07-13 | 陈方平 | Duct type unmanned aerial vehicle and control method thereof |
| CN205930082U (en) * | 2016-08-18 | 2017-02-08 | 湖南星思科技有限公司 | Electronic hovercar of coaxial anti - oar double -duct formula |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201419624Y (en) * | 2009-03-27 | 2010-03-10 | 谢雁洲 | Double-bypass propeller aerocar capable of vertical taking off and landing |
| CN104176235A (en) * | 2013-05-23 | 2014-12-03 | 中国直升机设计研究所 | Rotatable wing of rotor craft |
| CN103395491A (en) * | 2013-08-07 | 2013-11-20 | 龙川 | Slotting duct propeller systems and hovercar applying same |
| WO2016066848A1 (en) * | 2014-10-31 | 2016-05-06 | Schwöller Johann | Driving module for a motor vehicle, and motor vehicle comprising a driving module of said type |
| CN105752320A (en) * | 2016-04-01 | 2016-07-13 | 陈方平 | Duct type unmanned aerial vehicle and control method thereof |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN109878283A (en) * | 2019-04-10 | 2019-06-14 | 江苏航空职业技术学院 | A kind of hovercar oil electric mixed dynamic system |
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Application publication date: 20170901 |
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