CN107053983A - A kind of hovercar - Google Patents
A kind of hovercar Download PDFInfo
- Publication number
- CN107053983A CN107053983A CN201710330690.0A CN201710330690A CN107053983A CN 107053983 A CN107053983 A CN 107053983A CN 201710330690 A CN201710330690 A CN 201710330690A CN 107053983 A CN107053983 A CN 107053983A
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- CN
- China
- Prior art keywords
- hovercar
- external spiral
- propeller
- overarm
- duct
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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
Abstract
The invention discloses a kind of hovercar, including car body, the front and rear end of car body is respectively arranged with the first duct and the second duct being arranged symmetrically, the inner chamber of first duct is provided with the first internal propeller, the inner chamber of second duct is provided with the second internal propeller, first internal propeller is connected with the second internal propeller with setting drive mechanism in car body, it is provided with above car body in horizontally disposed overarm, vertical pivot is provided between overarm middle part and car body, rotating mechanism is connected with overarm, lockable mechanism is connected with rotating mechanism, overarm two ends are respectively arranged with the first external spiral oar and the second external spiral oar that diameter is less than width of the carbody, power drive mechanism is respectively connected with first external spiral oar and the second external spiral oar, inclining rotary mechanism is connected with power drive mechanism.The hovercar can be used in narrow road and narrow and small air environment, can strengthen stationarity during airflight again, lift the security performance of flight.
Description
Technical field
The present invention relates to technical field of vehicle, more specifically, more particularly to a kind of 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 conventional hovercar, to provide sufficiently large lift, the diameter of propeller to automobile lift-off
It is often very big, in this way, during propeller works, cross-car size is also very big, so in narrow road and narrow and small aerial
It can not be used in environment；In addition, during above-mentioned this kind of conventional hovercar flight in the air, it is easy in the impact of horizontal crosswind
Lower upset, has had a strong impact on flight safety.
The content of the invention
The technical problem to be solved in the present invention is provides a kind of hovercar, and the hovercar is by its structure design, both
It can be used in narrow road and narrow and small air environment, stationarity during airflight can be strengthened again, lift the peace of flight
Full performance.
A kind of hovercar, including car body, the front and rear end of the car body are respectively arranged with first be arranged symmetrically
The diameter of duct and the second duct, first duct and second duct is respectively less than width of the carbody and both axis are equal
Perpendicular with ground, the inner chamber of first duct is provided with the first internal propeller, and the inner chamber of second duct is provided with
Two internal propellers, first internal propeller is connected with second internal propeller with setting drive mechanism in car body, the car
It is provided with horizontally disposed overarm, is provided between the overarm middle part and the car body in vertical pivot, the overarm above body
Rotating mechanism is connected with, the rotating mechanism is used to drive the overarm to rotate in the horizontal plane using the vertical pivot as axis, institute
State and lockable mechanism is connected with rotating mechanism, the lockable mechanism is used for the positioning and locking of the overarm anglec of rotation, described
Overarm two ends are respectively arranged with the first external spiral oar and the second external spiral oar that diameter is less than width of the carbody, first external spiral
It is respectively connected with oar and the second external spiral oar on power drive mechanism, the power drive mechanism and is connected with inclining rotary mechanism,
The inclining rotary mechanism is used for the angle for adjusting the first external spiral oar and the second external spiral oar and horizontal plane.
Preferably, first internal propeller is equal to first external spiral to the distance between second internal propeller
Oar is the distance between to the second external spiral oar.
Preferably, first internal propeller, second internal propeller, the first external spiral oar, outside described second
The diameter of propeller is equal.
Preferably, first internal propeller, second internal propeller, outside the first external spiral oar and described second
The total distance regulating mechanism of independent propeller is connected on propeller.
Preferably, first duct in second duct with being provided with spoiler.
Preferably, the axis of the vertical pivot and the center of gravity of the car body are located along the same line.
Preferably, the vertical pivot is arranged on the interposition between first internal propeller and second internal propeller
Put.
Preferably, when the rotating mechanism drive it is described overarm rotation to in first internal propeller and described second
During the parallel position of propeller line, hovercar is in file and folds oar mode state.
Preferably, when the rotating mechanism drive it is described overarm rotation to in first internal propeller and described second
During the perpendicular position of propeller line, hovercar interlocks four wing mode states in transverse and longitudinal.
The beneficial effects of the invention are as follows：The hovercar that the present invention is provided is by its structure design, first on car body
The first internal propeller is respectively mounted in duct and the second duct and the second internal propeller constitutes first set propeller lift unit, so
Being set afterwards on roof can set what is be made up of the first external spiral oar and the second external spiral oar with the overarm of rotational lock in overarm
Second set of propeller lift unit, that is to say, that the propeller on propeller and overarm in car body duct is respectively combined to be formed
Propeller on two sets of propeller lift units, and overarm can be rotated according to actual needs.
For existing hovercar, when the hovercar needs to travel on highway, can rotate overarm makes
Second set of propeller lift unit is placed within the scope of vehicle body, so that the body width of the hovercar will not be increased, it is convenient to be somebody's turn to do
Hovercar is travelled on narrow road；Meanwhile, hovercar can be easily in narrow and small air environment under the state
Use, above-mentioned two sets of propeller lift units can be together for the enough lift needed for hovercar provides lift-off with flight.
When the propeller in the paramount space-time of hovercar flight, overarm can be rotated to the first internal propeller and second
The perpendicular position of internal propeller line, now in car body duct along length over ends of body direction 2 propellers with overarm along car
2 propellers of body width combine to form four wing patterns, greatly improve the skyborne attitude stability of hovercar；Together
When due to being respectively connected with inclining rotary mechanism on the first external spiral oar and the second external spiral oar, by the tilt angle for adjusting inclining rotary mechanism
Degree can produce the pulling force of part horizontal direction, so as to offset or slow down 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 the main view direction schematic diagram of the hovercar disclosed in the embodiment of the present invention 1；
Fig. 3 is the overlook direction schematic diagram of the hovercar disclosed in the embodiment of the present invention 1；
Fig. 4 is the main view direction schematic diagram of the hovercar disclosed in the embodiment of the present invention 2.
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.
Embodiment 1：
Referring to Fig. 2 and Fig. 3, Fig. 2 and Fig. 3 provide a kind of the first specific embodiment of hovercar of the invention, wherein,
Fig. 2 is the main view direction schematic diagram of the hovercar disclosed in the embodiment of the present invention 1；Fig. 3 is disclosed in the embodiment of the present invention 1
The overlook direction schematic diagram of hovercar.
As shown in Figures 2 and 3, the invention provides a kind of hovercar, the hovercar can in narrow road and
Used in narrow and small air environment, stationarity during airflight can be strengthened again, lift the security performance of flight.
The hovercar include car body 1, the first duct 2, the second duct 3, the first internal propeller 4, the second internal propeller 5,
Drive mechanism 6, overarm 7, vertical pivot 8, rotating mechanism 9, lockable mechanism 10, the first external spiral oar 11, the second external spiral oar 12, power
Transmission mechanism 13 and inclining rotary mechanism 14.
In the present embodiment, car body 1 is the body supports holding mechanism of hovercar, for the carrying of occupant, is used for simultaneously
The installation of other mechanisms.Physical length, width, height and interior trim of car body 1 etc. are typically designed according to actual needs.
The front and rear end of car body 1 is respectively arranged with the first duct 2 and the second duct 3 being arranged symmetrically, the first duct 2
The width of car body 1 is respectively less than with the diameter of the second duct 3 and its axis is perpendicular with ground.That is, the first duct 2 with
The shape of second duct 3 is identical, and the line of symmetry of the first duct 2 and the second duct 3 is the transversal centerline of car body 1.
The inner chamber of first duct 2 is provided with the first internal propeller 4, and the inner chamber of the second duct 3 is provided with the second internal propeller
5.In this way, the first internal propeller 4 and the second internal propeller 5 constitute the first set propeller lift unit of the hovercar, and
The first set propeller lift unit is located inside car body 1, and diameter is less than the width of car body 1.
First internal propeller 4 is connected with the second internal propeller 5 with setting drive mechanism 6 in car body 1.Drive mechanism 6 is used for
For the first internal propeller 4 and the powered rotation of the second internal propeller 5.
The top of car body 1 is provided with horizontally disposed overarm 7, is provided with vertical pivot 8 between the middle part of overarm 7 and car body 1, is hung oneself from a beam
Rotating mechanism 9 is connected with 7, rotating mechanism 9 is used to drive overarm 7 to be that axis rotates in the horizontal plane with vertical pivot 8, rotating mechanism
Lockable mechanism 10 is connected with 9, lockable mechanism 10 is used for the positioning and locking of 7 anglecs of rotation of overarm, and 7 two ends of overarm are set respectively
There is diameter to be less than the first external spiral oar 11 and the second external spiral oar 12 of width of the carbody.
In this way, the first external spiral oar 11 and the second external spiral oar 12 constitute second set of propeller lift of the hovercar
Device, and second set of propeller lift unit can rotate centered on vertical pivot 8, when rotating mechanism 9 drives the rotation of overarm 7 to the
When one internal propeller 4 and the parallel position of the oar line of the second inside spin 5, hovercar is in file and folds oar mode state.Now,
The flight locomotive is in small width, the situation of lift.
When rotating mechanism 9 drive overarm 7 rotation to the first internal propeller 4 and the perpendicular position of the line of the second internal propeller 5
When putting, hovercar interlocks four wing mode states in transverse and longitudinal.Now, the flight locomotive is in big width, lift, Gao Ping
The situation of stability.
It is two conventional patterns of hovercar of the present invention that file, which folds oar mode state and transverse and longitudinal four wing mode states that interlock,
State.Fig. 2 and Fig. 3 that the present embodiment is provided both were in transverse and longitudinal for hovercar and interlocked the structural representations of four wing mode states.
Power drive mechanism 13, power drive mechanism 13 are respectively connected with first external spiral oar 11 and the second external spiral oar 12
For providing power to the first external spiral oar 11 and the second external spiral oar 12., can be by power transmission machine for this programme
Structure 13 is directly connected in the drive mechanism 6 set in car body 1 by gearbox etc., is provided power by vehicle-mounted drive mechanism 6, is entered
And drive the first external spiral oar 11 and the second external spiral oar 12 to rotate.Just may be used in this way, relying solely on the drive mechanism 6 that car body carries
It is very convenient to realize traveling of the automobile on road and aerial flight.
Further, it is also possible to connect independent drive mechanism respectively on power drive mechanism 13, such as motor, in implementation
It is extra in overarm 7 that motor is installed, then power drive mechanism 13 is connected on above-mentioned motor, passes through peripheral hardware motor
Respectively the first external spiral oar 11 and the second external spiral oar 12 provide rotary power.
It is connected with inclining rotary mechanism 14 on power drive mechanism 13, inclining rotary mechanism 14 is used to adjusting the first external spiral oar 11 and the
The angle of two external spiral oars 12 and horizontal plane.In this way, can be controlled by adjusting inclining rotary mechanism 14 first external spiral oar 11 and
The tilt angle of second external spiral oar 12, offsets parts transversely crosswind, it is ensured that the stationarity that the hovercar flies in the air.
In addition, by the regulation of inclining rotary mechanism 14, the first external spiral oar 11 and the second external spiral oar 12 can produce part
The pulling force of horizontal direction, more convenient realize flies before the hovercar, flown afterwards or horizontal winged function, allows the hovercar quick
Flight and stabilized flight.
Generally speaking, the hovercar that provides of the present invention on car body 1 first duct 2 with pacifying respectively in the second duct 3
Fill the first internal propeller 4 and the second internal propeller 5 constitutes first set propeller lift unit, then being set on roof to revolve
Second set of propeller liter being made up of the first external spiral oar 11 and the second external spiral oar 12 is set in the overarm 7 of twist lock tightly, overarm 7
Power apparatus, that is to say, that the propeller on propeller and overarm in car body duct is respectively combined to form two sets of propeller lift
Propeller on device, and overarm can be rotated according to actual needs.
For existing hovercar, when the hovercar needs to travel on highway, can rotate overarm 7 makes
Second set of propeller lift unit is placed within the scope of vehicle body, so that the body width of the hovercar will not be increased, it is convenient to be somebody's turn to do
Hovercar is travelled on narrow road；Meanwhile, hovercar can be easily in narrow and small air environment under the state
Use, above-mentioned two sets of propeller lift units can be together for the enough lift needed for hovercar provides lift-off with flight.
When the hovercar flies paramount space-time, the propeller in overarm 7 can be rotated to the first internal propeller 4 and the
The perpendicular position of the line of two internal propeller 5, now in car body duct along along 2 propellers and overarm 7 in length over ends of body direction
Combine to form four wing patterns along 2 propellers in width of the carbody direction, greatly improve the skyborne attitude stabilization of hovercar
Property；Simultaneously because being respectively connected with inclining rotary mechanism 14 on the first external spiral oar 11 and the second external spiral oar 12, verted by regulation
The tilt angle of mechanism 14 can produce the pulling force of part horizontal direction, so as to offset or slow down the impact of horizontal crosswind, it is ensured that
Flight safety.
It is stationarity when further lifting the hovercar flight, it is preferable that the first internal propeller 4 in the present embodiment
It is equal to the distance between first the 11 to the second external spiral of external spiral oar oar 12 to the distance between the second internal propeller 5.In first
Propeller 4, the second internal propeller 5, the first external spiral oar 11, the second external spiral oar 12 diameter it is equal.
In the present embodiment, for convenience of each propeller always away from regulation, so that the lift size required for adjusting hovercar,
It is connected on first internal propeller 4, the second internal propeller 5, the first external spiral oar 11 and the second external spiral oar 12 independent
The total distance regulating mechanism of propeller.
In this way, controlling hovercar tilt angle and propeller total distance regulating mechanism control propeller total in inclining rotary mechanism 14
Away from synergic adjustment under, can easily realize hovercar driftage steering, spin, the control of the function such as horizontal flight.
For this programme, the first internal propeller 4, the second internal propeller 5, the first external spiral oar 11, second are designed with altogether
12 4 propellers of external spiral oar, wherein, the total distance regulating mechanism of propeller is to each propeller always away from regulation according to flight vapour
The requirement of car flight attitude and be mutually matched regulation.In addition, being typically provided with being connected with the total distance regulating mechanism of propeller on car body 1
The electric-control system connect, thus by electric-control system to each propeller always away from carry out more precisely, easily coordinate match control.
In the present embodiment, to further facilitate the regulation of hovercar flight attitude.Preferably, the first duct 2 and second
Spoiler 15 is provided with duct 3.
Specifically, the anglec of rotation by adjusting spoiler 15, can adjust air-flow and pass through the first duct 2 and the second duct
3 uninterrupted and direction, so that, it is more convenient the regulation of the hovercar flight attitude.In practical operation, spoiler 15 is general
Coordinate to realize the control to hovercar flight attitude together with the total distance regulating mechanism of above-mentioned propeller, inclining rotary mechanism 14.
In the present embodiment, to further facilitate the balance control of hovercar, it is preferable that the axis of vertical pivot 8 and car body 1
Center of gravity be located along the same line.Vertical pivot 1 is arranged on the centre position between the first internal propeller 4 and the second internal propeller 5.
Embodiment 2：
Another specific embodiment of hovercar of the present invention is provided referring to Fig. 4, Fig. 4, wherein, Fig. 4 is real for the present invention
Apply the main view direction schematic diagram of the hovercar disclosed in example 2.
In the present embodiment, it can see that the top of car body 1 is provided with horizontally disposed overarm 7, the middle part of overarm 7 with clearer
It is provided with vertical pivot 8 between car body 1, rotating mechanism 9 is connected with overarm 7, and (rotating mechanism 9 is arranged on vertical pivot 8 in the present embodiment
On, 7 it is indirectly connected with overarm), lockable mechanism 10 is connected with rotating mechanism 9, and 7 two ends of overarm are respectively arranged with the first external spiral
The external spiral oar 12 of oar 11 and second.Power drive mechanism 13 is respectively connected with first external spiral oar 11 and the second external spiral oar 12,
Inclining rotary mechanism 14 is connected with power drive mechanism 13.
In the present embodiment, rotating mechanism 9 has driven the rotation of overarm 7 to connect to the first internal propeller 4 and the oar of the second inside spin 5
During the parallel position of line, now, hovercar is in file and folds oar mode state.Now, the flight locomotive is in small width,
The situation of lift.
A kind of hovercar provided by the present invention is described in detail above.Specific case pair used herein
The principle and embodiment of the present invention is set forth, and the explanation of above example is only intended to the method for helping to understand the present invention
And its core concept.It should be pointed out that for those skilled in the art, before the principle of the invention is not departed from
Put, some improvement and modification can also be carried out to the present invention, these are improved and modification also falls into the guarantor of the claims in the present invention
In the range of shield.
Claims (9)
1. a kind of hovercar, it is characterised in that including car body, the front and rear end of the car body is respectively arranged with symmetrical cloth
The first duct and the second duct put, the diameter of first duct and second duct are respectively less than width of the carbody and both
Axis is perpendicular with ground, and the inner chamber of first duct is provided with the first internal propeller, the inner chamber of second duct
The second internal propeller is provided with, first internal propeller connects with second internal propeller with setting drive mechanism in car body
Connect, be provided with above the car body in horizontally disposed overarm, be provided with vertical pivot between the overarm middle part and the car body, institute
State and be connected with rotating mechanism in overarm, the rotating mechanism be used to driving the overarm using the vertical pivot as axis in the horizontal plane
Lockable mechanism is connected with rotation, the rotating mechanism, the lockable mechanism is used for positioning and the lock of the overarm anglec of rotation
Tightly, the overarm two ends are respectively arranged with the first external spiral oar and the second external spiral oar that diameter is less than width of the carbody, described the
It is respectively connected with to be connected with power drive mechanism, the power drive mechanism on one external spiral oar and the second external spiral oar and inclines
Rotation mechanism, the inclining rotary mechanism is used for the angle for adjusting the first external spiral oar and the second external spiral oar and horizontal plane.
2. hovercar according to claim 1, it is characterised in that first internal propeller to second inside spin
The distance between oar is equal to the distance between described first external spiral oar to the second external spiral oar.
3. hovercar according to claim 1, it is characterised in that first internal propeller, second inside spin
Oar, the first external spiral oar, the second external spiral oar diameter it is equal.
4. hovercar according to claim 1, it is characterised in that first internal propeller, second inside spin
The total distance regulating mechanism of independent propeller is connected on oar, the first external spiral oar and the second external spiral oar.
5. hovercar according to claim 1, it is characterised in that first duct in second duct with being all provided with
It is equipped with spoiler.
6. hovercar according to claim 1, it is characterised in that the axis of the vertical pivot and the center of gravity of the car body
It is located along the same line.
7. hovercar according to claim 1, it is characterised in that the vertical pivot be arranged on first internal propeller with
Centre position between second internal propeller.
8. hovercar according to claim 7, it is characterised in that when the rotating mechanism drives the overarm rotation extremely
During position parallel with first internal propeller and the second internal propeller line, hovercar is in file and folds oar pattern
State.
9. hovercar according to claim 7, it is characterised in that when the rotating mechanism drives the overarm rotation extremely
During with first internal propeller and the perpendicular position of the second internal propeller line, hovercar interlocks four wings in transverse and longitudinal
Mode state.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710330690.0A CN107053983A (en) | 2017-05-11 | 2017-05-11 | A kind of hovercar |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710330690.0A CN107053983A (en) | 2017-05-11 | 2017-05-11 | A kind of hovercar |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107053983A true CN107053983A (en) | 2017-08-18 |
Family
ID=59597778
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710330690.0A Pending CN107053983A (en) | 2017-05-11 | 2017-05-11 | A kind of hovercar |
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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 |
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| 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 |
| CN106827993A (en) * | 2017-03-28 | 2017-06-13 | 刘宾 | A kind of four culvert vertical take-off and landing hovercars |
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2017
- 2017-05-11 CN CN201710330690.0A patent/CN107053983A/en active Pending
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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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| CN106827993A (en) * | 2017-03-28 | 2017-06-13 | 刘宾 | A kind of four culvert vertical take-off and landing hovercars |
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Application publication date: 20170818 |
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