CN106143031A - Driving - Google Patents
Driving Download PDFInfo
- Publication number
- CN106143031A CN106143031A CN201610446960.XA CN201610446960A CN106143031A CN 106143031 A CN106143031 A CN 106143031A CN 201610446960 A CN201610446960 A CN 201610446960A CN 106143031 A CN106143031 A CN 106143031A
- Authority
- CN
- China
- Prior art keywords
- driving
- lift fan
- fan
- lift
- ground
- 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.)
- Pending
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
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
A kind of driving is that dynamic or motorized motions the lift fan of the built-in oil of distributing installation multiple stage produces normal thrust and aloft can fly with VTOL or at the two-purpose traffic tool of ground run below the chassis seat of surface car.
Description
Technical field
Ben Fatong relates to the vehicles.
Background technology
Modern vehicle is intended for ground and uses.
Summary of the invention
The driving of the present invention be a kind of can be at ground run and the two-purpose traffic tool aloft flown.
The method of the present invention be above vehicle chassis, below seat or cargo hold distributing installation multiple stage can independent operating
The normal thrust that lift fan produces required for enough loading realizes VTOL and airflight.Driving does not has wing and tradition
Aircraft is completely different.
Driving lift fan power can be electronic or fuel system.
The present invention uses the multi-cylinder high-power hub shape that the special bright technology of published CN2012102909930 Chinese invention manufactures
Aviation piston type engine drives lift fan work.
The power-actuated electromotor of the lift fan of the present invention and Multi-stage rotary impeller are all arranged on columnar duct
Inside, does not has ex-ternal transmission system, takes up room little, and duct barrel shrond is in parallel on carriage chassis to be installed in order, similar honeybee
Socket structure.The intensity increased in rain can make the driving of the present invention bear ground and dual section of aerial lotus.
The operation principle of the impeller that the multiple stage lift fan of these distributions rotates naked paddle outer with multiaxis rotor is identical.
The multi-rotor aerocraft of the present invention be cylindrical shape duct built-in multi-disc multi-stage impeller rotate produce thrust efficiency apparently higher than
Common rotor, the most built-in many rotors are arranged on interior and have the neat and artistic feature easy to install and use of profile.
The high pressure draught exit of lift fan is installed two dimension and is aligned the aerodynamic rudder of four direction all around.Levelling
Rudder face inclination angle can balance fitful wind suffered by driving and the interference of uncertain external force in good time, keeps stability and the free flight of driving
OK.It is aided with the timely adjustment flight speed of every lift fan engine output, directivity and safe take-off landing
Artificial and the electronic intelligence actuation means obtained on driving realizes.The lift fan that can freely dally can carry when driving declines
For slow effect.Can avoid falling and automatically join.Equipped with unilateral bearing on every electromotor or electric machine main shaft, parking aft-fan
Impeller can freely revolve
Accompanying drawing explanation
Accompanying drawing 1 driving side schematic view
The sectional view of accompanying drawing 2 driving
Detailed description of the invention
The present invention is further illustrated below in conjunction with the accompanying drawings.
Accompanying drawing 1 is the side schematic view of driving of the present invention, in FIG it is clear that body shell 6 seat 7 times
Side's floor 8 vertical four lift fans 1 installed below, the upper impeller 2 of lift fan, hub shape piston engine 3, under
Impeller 4 and the aerodynamic rudder 5. that can vert install four lift fans 1 too at the another side of vehicle body, and they have eight
Platform.Every lift fan is all identical with lift fan in Fig. 11, and the lift fan of every electromotor 3 driving can send 350
Horsepower, the lift-off power of driving adds up to 2800 horsepowers, can be realized by liftoff this fully loaded driving of 22 seven tons completely
Aloft fly.
In Fig. 1,9 is position of driver, and the dynamical system of position, foreground 10 original mini-bus automobile, the present invention does not has silk to this
Milli changes.Still can as usual travel with ground with front-wheel drive, not set wing simultaneously, profile is only led at lift fan air intlet 11
Normal venetian blind type is slightly different, the genuine feature of the driving that be the present invention similar to the mini-bus of automobile.This is one
There is the air-ground dual-purpose driving of two set dynamical systems.The impeller that lift is rotated by lift fan completely provides.
Accompanying drawing 2 is the sectional view of driving of the present invention.It is more clearly seen installation site and the air inlet of lift fan 1 in fig. 2
The left pore of venetian blind type 4 and right air inlet 3, equally left and right two row below body shell 6 seat 7 underlying floor 5 are the most right
Claim the lift fan 1 and 2 installed often to arrange 4 totals of installation successively and have eight same lift fans 1 and 2, under fan
Side's high pressure draught nozzle is provided with the aerodynamic rudder 8,9,10 and 11 keeping horizontal side stability, and every all has left-right and front-back power
Rudder.Whole eight lift fans are that symmetrical barycenter is installed.Levelling balances the effect elevator than fixed-wing of stability, direction
Rudder and aileron facilitate, reliability is high.
Claims (9)
1. some lift fans generation normal thrusts are installed for special below the chassis seat at surface car or cargo hold
That levies can be with VTOL flight with at the two-purpose traffic tool of ground run.
The lift fan of the distributed installation of driving the most according to claim 1 has independent power device.Can operate with unit
The lift fan of multi-stage impeller that drives of electronic or fuel power.
The outlet of the air intlet of the lift fan of driving the most according to claim 1 and ejection air-flow is along about vehicle body
Both sides dispose the most in order, are provided with shutter or valve.
The profile of driving the most according to claim 1 does not set wing, and whole normal thrusts are peaceful flies component from vehicle
The multiple stage lift fan put.
5. the pitching of driving is the multiple stage lift fan nozzle by relative driving barycenter symmetrical placement with horizontal side stability
Aerodynamic rudder and the difference driving fan to rotate output are implemented the most artificial or electronics auto-control.
6. the power demand that departs of driving can be any by the mode of the number of units and tandem drive power that increase lift fan
Strengthen.
7. the lift fan of driving be provided with can when landing the slow one-way clutch rotating freely blast fan.
8. land and the aerial dynamical system of driving is respectively provided with.Can aloft select respectively on ground.
9. driving exactly like surface car, useful at ground run be the principal character of the present invention in narrow regions landing
One of.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610446960.XA CN106143031A (en) | 2016-06-21 | 2016-06-21 | Driving |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610446960.XA CN106143031A (en) | 2016-06-21 | 2016-06-21 | Driving |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106143031A true CN106143031A (en) | 2016-11-23 |
Family
ID=57353473
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610446960.XA Pending CN106143031A (en) | 2016-06-21 | 2016-06-21 | Driving |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106143031A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20090116573A (en) * | 2008-05-06 | 2009-11-11 | 김순곤 | Vertical takeoff and landing flying vehicle |
| MX2011004239A (en) * | 2008-10-20 | 2011-09-28 | Soo-Cheol Jung | Aircraft system that enables ground traveling. |
| CN103303083A (en) * | 2012-11-30 | 2013-09-18 | 中国南方航空工业(集团)有限公司 | Navigation system for vehicle, vehicle provided with same and aerocar |
| CN104859392A (en) * | 2015-05-20 | 2015-08-26 | 南京航空航天大学 | Vertical lifting aerodyne employing tiltable ducted wheels |
| CN105644283A (en) * | 2016-03-24 | 2016-06-08 | 航沃科技（上海）有限公司 | Vertical take-off and landing hovercar |
-
2016
- 2016-06-21 CN CN201610446960.XA patent/CN106143031A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20090116573A (en) * | 2008-05-06 | 2009-11-11 | 김순곤 | Vertical takeoff and landing flying vehicle |
| MX2011004239A (en) * | 2008-10-20 | 2011-09-28 | Soo-Cheol Jung | Aircraft system that enables ground traveling. |
| CN103303083A (en) * | 2012-11-30 | 2013-09-18 | 中国南方航空工业(集团)有限公司 | Navigation system for vehicle, vehicle provided with same and aerocar |
| CN104859392A (en) * | 2015-05-20 | 2015-08-26 | 南京航空航天大学 | Vertical lifting aerodyne employing tiltable ducted wheels |
| CN105644283A (en) * | 2016-03-24 | 2016-06-08 | 航沃科技（上海）有限公司 | Vertical take-off and landing hovercar |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20161123 |