CN106827993A - A kind of four culvert vertical take-off and landing hovercars - Google Patents
A kind of four culvert vertical take-off and landing hovercars Download PDFInfo
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- CN106827993A CN106827993A CN201710194022.XA CN201710194022A CN106827993A CN 106827993 A CN106827993 A CN 106827993A CN 201710194022 A CN201710194022 A CN 201710194022A CN 106827993 A CN106827993 A CN 106827993A
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- hovercar
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- 230000005611 electricity Effects 0.000 claims description 13
- 238000005096 rolling process Methods 0.000 abstract description 6
- 238000010586 diagram Methods 0.000 description 4
- 239000000295 fuel oil Substances 0.000 description 2
- 230000004888 barrier function Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000010001 crabbing Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000008450 motivation Effects 0.000 description 1
- 230000001960 triggered effect Effects 0.000 description 1
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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/56—Folding or collapsing to reduce overall dimensions of aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Transportation (AREA)
- Wind Motors (AREA)
Abstract
The invention discloses a kind of four culvert vertical take-off and landings hovercar, it is related to air-ground amphibious technical field of transportation means.Four described culvert vertical take-off and landing hovercars, it is provided with four ducted fans and two auxiliary ducted fans, can be that sufficient lifting force is provided when the hovercar takes off, hovercar is set vertically to be quickly ramped up to safe altitude, landing airdrome length and the departure time are shortened, can the significantly more efficient switching for adapting to offline mode and driving mode；By the control to the second rotating shaft, control wing is laterally-opening or longitudinal direction is packed up, and can preferably adapt to offline mode and driving mode, it is ensured that smooth flight during offline mode, it is ensured that as stock car during traveling, is not take up wide track；By the control of whole-control system, can be to the control of lifting device and auxiliary ducted fan lifting force, so that hovercar keeps state of flight or change of flight state, it is to avoid pitching rolling, the laterally phenomenon such as rolling, stall, the safe flight coefficient of hovercar is improve.
Description
Technical field
The invention belongs to air-ground amphibious technical field of transportation means, more particularly to a kind of four culvert vertical take-off and landings flight vapour
Car.
Background technology
In recent years, with the fast development of modern social economy, big-and-middle small city private car largely increases, urban transportation pressure
Power increasingly increases, and traffic congestion situation frequently occurs, and has triggered a series of energy problem, environmental problem.How effectively to solve
Modern City Traffic problem turns into a great problem, is this it is proposed that a kind of hovercar, and this hovercar can not only be
Land travels, and can also the low-latitude flying in traffic congestion.Various hovercars, mesh are developed both at home and abroad
Preceding hovercar is subject to the bad weathers such as external interference, such as air blast in hovering or flight course, it may appear that pitching is turned over
Rolling, the laterally phenomenon such as rolling, stall, have so had a strong impact on the safety of hovercar, reduce the safety coefficient of hovercar.
The content of the invention
In view of the shortcomings of the prior art, the present invention provides a kind of four culvert vertical take-off and landings hovercar.
The present invention is to solve above-mentioned technical problem by the following technical solutions：A kind of four culvert vertical take-off and landings flight
Automobile, including the car body with wheel, the car body middle part are provided with driving cabin, and power set are provided with the car body, dress is driven
Put, battery and whole-control system, the whole-control system is connected with power set, drive device, battery respectively,
The power set are connected with drive device；The front-end and back-end of the car body are respectively equipped with one group of lifting device, every group of lifting
Device includes two ducted fans, and the ducted fan is connected with the drive device；Two in every group of lifting device
Ducted fan is along car body direction of advance interval setting, and two ducted fans in every group of lifting device are horizontal by first rotating shaft
It is vertically fixed on car body to and with hovercar direction of advance, the first rotating shaft is connected with drive device, by full-vehicle control
System control drive device action, so as to control four unlatchings of ducted fan, close and turn to；Two groups of described lifting devices
It is oppositely oriented；The rear portion of the car body is provided with vertical tail.
Further, the whole-control system includes entire car controller, power plant controller, drive set controller
And power-supply management system, described entire car controller respectively with described power plant controller, drive set controller with
And power-supply management system connection, the power plant controller be connected with the power set, the drive set controller and
The drive device and power-supply management system are connected, and the power-supply management system is connected with battery, the power set.
Further, the top in the middle of the car body is provided with wing by the second rotating shaft, and the wing includes being symmetrical arranged
Port wing and starboard wing, second rotating shaft is connected with the drive device, and described second is controlled by drive set controller
The rotation of rotating shaft, so as to control the rotation of wing, makes wing laterally-opening or longitudinal direction is packed up, perpendicular or parallel with car body；Institute
State to be respectively symmetrically on the inside of port wing and starboard wing and be provided with auxiliary ducted fan, the auxiliary ducted fan and the drive device
Connection, to provide lift when the hovercar takes off；When hovercar is road traveling state, the second rotating shaft is controlled
Rotation port wing and starboard wing is longitudinally packed up, it is parallel with car body, it is to avoid hovercar takes wide in road traveling
Track；When hovercar is state of flight, controlling the rotation of the second rotating shaft makes port wing and starboard wing laterally-opening, with car body
Vertically, making hovercar has horizontal side stability and maneuverability, can manipulate hovercar roll, it is ensured that balance during flight.
Further, the Plane of rotation top of the auxiliary ducted fan on the wing is provided with longitudinally through in the window of wing
Mouthful, the controlling switch of control window opening and closing is provided with wing, the controlling switch is connected with the drive device；When flight vapour
When car takes off, control window is opened, and auxiliary ducted fan starts, and is the offer lift that takes off；After hovercar parallel flight, window
Mouth is closed, and auxiliary ducted fan is closed, hovercar smooth flight.
Further, the wingtip positional symmetry of the wing is provided with spoiler.
Further, the power set include turbocharged engine and electricity generation system, the turbocharged engine
It is connected with power plant controller, electricity generation system and drive device respectively, the electricity generation system is connected with power-supply management system.
Further, described drive device includes lifting device motor, auxiliary ducted fan motor, clutch
Device, the lifting device motor connects with drive set controller, ducted fan, first rotating shaft and power set respectively
Connect, the auxiliary ducted fan motor connects with drive set controller, auxiliary ducted fan, controlling switch and power set
Connect, the arrangement of clutch is connected with drive set controller, power set, wheel and the second rotating shaft.
Compared with prior art, four culvert vertical take-off and landings hovercar provided by the present invention, is provided with four ducted fans
With two auxiliary ducted fans, to provide sufficient lifting force when the hovercar takes off hovercar can be made vertically quick
Safe altitude is risen to, landing airdrome length and the departure time is shortened, cutting for offline mode and driving mode significantly more efficient can be adapted to
Change；By the control to the second rotating shaft, control wing is laterally-opening or longitudinal direction is packed up, and can preferably adapt to offline mode and traveling
Pattern, it is ensured that smooth flight during offline mode, it is ensured that as stock car during traveling, is not take up wide track；By whole
The control of vehicle control, can be to the control of lifting device and auxiliary ducted fan lifting force, so that hovercar keeps flying
Row state or change of flight state, it is to avoid pitching rolling, the laterally phenomenon such as rolling, stall, the safety that improve hovercar fly
Row coefficient.
Brief description of the drawings
In order to illustrate more clearly of technical scheme, embodiment will be described below needed for the accompanying drawing to be used
It is briefly described, it should be apparent that, drawings in the following description are only one embodiment of the present of invention, general for this area
For logical technical staff, on the premise of not paying creative work, other accompanying drawings can also be obtained according to these accompanying drawings.
Fig. 1 is the schematic diagram of four culvert vertical take-off and landings hovercar takeoff condition of the invention；
Fig. 2 is the schematic diagram of four culvert vertical take-off and landings hovercar level flight condition of the invention；
Fig. 3 is the side schematic view of four culvert vertical take-off and landings hovercar level flight condition of the invention；
Fig. 4 is the schematic diagram of four culvert vertical take-off and landings hovercar transport condition of the invention；
Fig. 5 is the schematic diagram of the upper and lower state of flight of four culvert vertical take-off and landings hovercar of the invention；
Fig. 6 is the structural representation of four culvert vertical take-off and landings hovercar whole-control system of the invention；
Wherein：1- car bodies, 2- wheels, 3- driving cabins, 4- ducted fans, 5- auxiliary ducted fans, 6- wings, 7- vertical tails,
8- spoilers.
Specific embodiment
With reference to the accompanying drawing in the embodiment of the present invention, the technical scheme in the present invention is clearly and completely described,
Obviously, described embodiment is only a part of embodiment of the invention, rather than whole embodiments.Based in the present invention
Embodiment, the every other embodiment that those of ordinary skill in the art are obtained on the premise of creative work is not made,
Belong to the scope of protection of the invention.
As shown in figure 1, four culvert vertical take-off and landings hovercar provided by the present invention, including the car body 1 with wheel 2,
The middle part of the car body 1 is provided with driving cabin 3, the car body 1 and is provided with power set, drive device, battery and full-vehicle control
System, the whole-control system is connected with power set, drive device, battery respectively, and the power set are filled with driving
Put connection；The front-end and back-end of the car body 1 are respectively equipped with one group of lifting device, and every group of lifting device includes two ducted fans
4, the ducted fan 4 is connected with the drive device；Before two ducted fans 4 in every group of lifting device are along car body 1
Enter direction interval setting, two ducted fans 4 in every group of lifting device are by first rotating shaft transverse direction and and hovercar
Direction of advance is vertically fixed on car body 1, and the first rotating shaft is connected with drive device, and dress is driven by whole-control system control
Action is put, so as to control four unlatchings of ducted fan 4, close and turn to；Two groups of described lifting devices it is oppositely oriented；Institute
The rear portion for stating car body is provided with vertical tail 7.
As shown in fig. 6, the whole-control system includes entire car controller, power plant controller, drive device control
Device and power-supply management system, described entire car controller respectively with described power plant controller, drive set controller
And power-supply management system is connected, the power plant controller is connected with the power set, the drive set controller
It is connected with the drive device and power-supply management system, the power-supply management system is connected with battery, the power set.
Top in the middle of the car body 1 is provided with wing 6 by the second rotating shaft, and the wing 6 includes symmetrically arranged left machine
The wing and starboard wing, second rotating shaft are connected with the drive device, and second rotating shaft is controlled by drive set controller
Rotate, so as to control the rotation of wing, make wing laterally-opening or longitudinal direction is packed up, it is perpendicular or parallel with car body；In the left machine
It is respectively symmetrically on the inside of the wing and starboard wing and is provided with auxiliary ducted fan 5, the auxiliary ducted fan 5 connects with the drive device
Connect.
The Plane of rotation top of the auxiliary ducted fan 5 on the wing 6 is provided with longitudinally through in the window of wing, in machine
The controlling switch of control window opening and closing is provided with the wing 6, the controlling switch is connected with the drive device.
The wingtip positional symmetry of the wing 6 is provided with spoiler 8.
The power set include turbocharged engine and electricity generation system, the turbocharged engine respectively with power
Setup Controller, electricity generation system and drive device connection, the electricity generation system are connected with power-supply management system.
Described drive device includes lifting device motor, auxiliary ducted fan motor, arrangement of clutch, described
Lifting device motor is connected with drive set controller, ducted fan 4, first rotating shaft and power set respectively, described auxiliary
Ducted fan motor is helped to be connected with drive set controller, auxiliary ducted fan 5, controlling switch and power set, it is described
Arrangement of clutch is connected with drive set controller, power set, the rotating shaft of wheel 2 and second.
Using the hovercar in the present embodiment, when whole-control system is in offline mode, as shown in figure 1, vertical
When taking off, drive set controller controls two groups of lifting devices to be in horizontality and open by controlling lifting device motor
Open；It is connected with the second rotating shaft by controlling arrangement of clutch, control wing 6 is laterally-opening, is that wing 6 provides transmission power；Pass through
Control auxiliary ducted fan motor control auxiliary ducted fan 5 is opened, window is opened, four ducted fans 4 and two it is auxiliary
Ducted fan 5 is helped to provide enough lift for hovercar takes off, it is ensured that hovercar is vertically quickly ramped up to safe altitude；As schemed
Shown in 2 and 3, when hovercar rises to safe altitude and horizontal flight, drive set controller is by controlling auxiliary duct wind
Fan motor control auxiliary ducted fan 5 is closed, close, and entire car controller switches to fixed wing control model, with
Control the control mode control hovercar flight of fixed wing aircraft；Drive set controller is driven by controlling lifting device
Motor control first rotating shaft rotate, respectively control 1 outermost two ducted fan 4 of car body rotate, and with the perpendicular shape of car body 1
State is that hovercar is forward provides power, it is to avoid hovercar stall in flight course, it is ensured that hovercar steadily flies safely
OK.
As shown in figure 4, when the whole-control system of the hovercar in the present embodiment is in driving mode, drive device control
Device processed controls two groups of lifting devices to be closed by controlling lifting device motor；By controlling auxiliary ducted fan
Motor control auxiliary ducted fan 5 is closed, close；The second rotating shaft is controlled by controlling arrangement of clutch, wing 6 is controlled
Longitudinal direction is packed up, parallel with car body 1, and hereafter, control arrangement of clutch is disconnected with the second rotating shaft, and the rotary shaft with wheel 2 is connected,
Power is provided for wheel 2 is rotated；Entire car controller switches to the control model of general-utility car traveling, to control the control of general-utility car
Mode processed controls hovercar in road traveling.
Hovercar in the present embodiment, drive set controller is by controlling lifting device to the lifting force of car body 1
The torque on vertical plane produced to car body 1, the torque can offset hovercar and be produced by the influence of external environment
Torque on vertical plane, it is to avoid pitching rollover phenomenon；By controlling the auxiliary ducted fan 5 on wing 6 to the liter of car body 1
Power and to car body 1 produce vertical plane on torque, the torque can offset hovercar by external environment influence and produce
The raw torque on vertical plane, it is to avoid horizontal rollover phenomenon.
Under offline mode, hovercar or so flight is controlled by vertical tail 7；Car is controlled by controlling first rotating shaft
The steering of the ducted fan 4 of the rearmost end of body 1, so as to adjust the angle between the ducted fan 4 of rearmost end and car body 1, controls car
Body 1 ducted fan 4 foremost is vertical with car body to control hovercar to fly up and down, as shown in Figure 5；By controlling to be lifted
Device reaches the advance or retrogressing of hovercar to the lifting force of car body 1, and drive set controller is by controlling the front end of car body 1
Lifting device to the lifting force of car body 1 more than the lifting device positioned at the rear end of car body 1 to the lifting force of car body 1, make car body 1
Front end is raised, direction backward side skew of two groups of lifting devices to the lifting force of car body 1 so that hovercar is moved rearwards by；It is logical
The lifting device for crossing control car body 1 rear end is more than the lifting device positioned at the front end of car body 1 to car body 1 to the lifting force of car body 1
Lifting force, raises the rear end of car body 1, direction forward side skew of two groups of lifting devices to the lifting force of car body 1 so that flight
Automobile is moved forward.
The crabbing of hovercar is reached by controlling to aid in ducted fan 5 on wing 6 to the lifting force of car body 1,
Drive set controller aids in ducted fan 5 by controlling on wing 6 so that left side aids in lifting of the ducted fan 5 to car body 1
Power is more than lifting force of the right side auxiliary ducted fan 5 to car body 1 so that the left side of car body 1 is raised, two auxiliary ducted fans 5
Direction to the lifting force of car body 1 offsets to the right so that hovercar offsets to the right；Drive set controller passes through control machine
Ducted fan 5 is aided on the wing 6 so that right side aids in ducted fan 5 to aid in ducted fan 5 more than left side to the lifting force of car body 1
To the lifting force of car body 1 so that the right side of car body 1 is raised, two auxiliary ducted fans 5 to the direction of the lifting force of car body 1 to
Left avertence move so that hovercar offsets to the left, it is this control flight mode can avoid front or behind barrier and to
It is preceding or be moved rearwards by.
Hovercar in the present embodiment has three kinds of modes of offer power, first way：Fuel oil is sent out for turbocharging
Motivation provides power, so as to drive electricity generation system to be generated electricity, the electric energy of electricity generation system is assigned to driving by power-supply management system
Setup Controller and charged to battery, so as to control each drive device to drive corresponding portion by drive set controller
Part carries out corresponding control operation；The second way：Fuel oil provides power for turbogenerator, and the power is directly over ratcheting opening
Pass is transferred to each drive device, controls each drive device to drive corresponding component to be acted accordingly；The third mode：Power supply pipe
The electric energy that reason system will have been laid in the battery of sufficient electrical energy distributes to drive set controller, by drive set controller
Controlling each drive device drive corresponding component carries out corresponding control operation；The mode for providing power is entered by entire car controller
Row control.
Above disclosed is only specific embodiment of the invention, but protection scope of the present invention is not limited thereto,
Any one skilled in the art the invention discloses technical scope in, can readily occur in change or modification, all
Should be included within the scope of the present invention.
Claims (8)
1. a kind of four culvert vertical take-off and landings hovercar, it is characterised in that：Including the car body with wheel, the car body middle part sets
There is driving cabin, power set, drive device, battery and whole-control system, the full-vehicle control are provided with the car body
System is connected with power set, drive device, battery respectively, and the power set are connected with drive device；The car body
Front-end and back-end are respectively equipped with one group of lifting device, and every group of lifting device includes two ducted fans, the ducted fan and institute
State drive device connection；Two ducted fans in every group of lifting device are described every along car body direction of advance interval setting
Two ducted fans in group lifting device laterally and with hovercar direction of advance are vertically fixed on car body by first rotating shaft
On, the first rotating shaft is connected with drive device, is acted by whole-control system control drive device, controls four ducted fans
Unlatching, close and turn to；Two groups of described lifting devices it is oppositely oriented；The rear portion of the car body is provided with vertical tail.
2. four culvert vertical take-off and landings hovercar as claimed in claim 1, it is characterised in that：The whole-control system includes
Entire car controller, power plant controller, drive set controller and power-supply management system, described entire car controller difference
It is connected with described power plant controller, drive set controller and power-supply management system, the power plant controller
It is connected with the power set, the drive set controller is connected with the drive device and power-supply management system, the electricity
Management system is connected with battery, the power set.
3. four culvert vertical take-off and landings hovercar as claimed in claim 2, it is characterised in that：Top in the middle of the car body leads to
Cross the second rotating shaft and be provided with wing, the wing includes symmetrically arranged port wing and starboard wing, second rotating shaft and the drive
Dynamic device connection, the rotation of second rotating shaft is controlled by drive set controller, controls the rotation of wing, wing is laterally beaten
Open or longitudinal direction is packed up, it is perpendicular or parallel with car body.
4. four culvert vertical take-off and landings hovercar as claimed in claim 3, it is characterised in that：In the port wing and starboard wing
Inner side be respectively symmetrically and be provided with auxiliary ducted fan, the auxiliary ducted fan is connected with the drive device, so as to described
Lift is provided when hovercar takes off.
5. four culvert vertical take-off and landings hovercar as claimed in claim 4, it is characterised in that：Auxiliary duct on the wing
The Plane of rotation top of fan is provided with longitudinally through in the window of wing, and the control that control window opening and closing is provided with wing is opened
Close, the controlling switch is connected with the drive device.
6. four culvert vertical take-off and landing hovercars as described in claim 3 or 4, it is characterised in that：The wingtip position of the wing
Put and be arranged with spoiler.
7. four culvert vertical take-off and landings hovercar as claimed in claim 2, it is characterised in that：The power set include turbine
Engine with supercharger and electricity generation system, the turbocharged engine are filled with power plant controller, electricity generation system and driving respectively
Connection is put, the electricity generation system is connected with power-supply management system.
8. four culvert vertical take-off and landings hovercar as claimed in claim 5, it is characterised in that：Described drive device includes carrying
Device motor, auxiliary ducted fan motor, arrangement of clutch are risen, the lifting device motor is filled with driving respectively
Put the connection of controller, ducted fan, first rotating shaft and power set, the auxiliary ducted fan motor and drive device control
Device processed, auxiliary ducted fan, controlling switch and power set connection, the arrangement of clutch are filled with drive set controller, power
Put, wheel and the second rotating shaft are connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710194022.XA CN106827993A (en) | 2017-03-28 | 2017-03-28 | A kind of four culvert vertical take-off and landing hovercars |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710194022.XA CN106827993A (en) | 2017-03-28 | 2017-03-28 | A kind of four culvert vertical take-off and landing hovercars |
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| Publication Number | Publication Date |
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| CN106827993A true CN106827993A (en) | 2017-06-13 |
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ID=59142565
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710194022.XA Pending CN106827993A (en) | 2017-03-28 | 2017-03-28 | A kind of four culvert vertical take-off and landing hovercars |
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Cited By (11)
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| CN107053983A (en) * | 2017-05-11 | 2017-08-18 | 湖南顶立科技有限公司 | A kind of hovercar |
| CN107175999A (en) * | 2017-06-21 | 2017-09-19 | 江阴市翔诺电子科技有限公司 | Hovercar |
| CN107471936A (en) * | 2017-09-21 | 2017-12-15 | 张龙 | Hovercar |
| CN107985580A (en) * | 2017-12-14 | 2018-05-04 | 西南交通大学 | A kind of multi-modal deformable rotor robot |
| CN108944306A (en) * | 2018-07-04 | 2018-12-07 | 天津超算科技有限公司 | Automobile aerocraft |
| CN108944307A (en) * | 2018-07-04 | 2018-12-07 | 天津超算科技有限公司 | Automobile aerocraft |
| CN109878282A (en) * | 2019-04-04 | 2019-06-14 | 江苏航空职业技术学院 | A kind of four ducts control VTOL variant hovercar |
| WO2019148464A1 (en) * | 2018-02-02 | 2019-08-08 | 浙江吉利控股集团有限公司 | Flying car wing, carrier module structure, power system, flying car, and control method for flying car wing |
| CN111098649A (en) * | 2018-10-25 | 2020-05-05 | 长城汽车股份有限公司 | Aerocar control system and method and aerocar |
| TWI738299B (en) * | 2020-04-17 | 2021-09-01 | 財團法人工業技術研究院 | Flight equipment |
| CN113665803A (en) * | 2021-09-02 | 2021-11-19 | 涵涡智航科技(玉溪)有限公司 | Aircraft |
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Application publication date: 20170613 |