CN104859392B - It is a kind of using can tilting duct wheel vehicle convertible into aircraft - Google Patents
It is a kind of using can tilting duct wheel vehicle convertible into aircraft Download PDFInfo
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- CN104859392B CN104859392B CN201510258643.0A CN201510258643A CN104859392B CN 104859392 B CN104859392 B CN 104859392B CN 201510258643 A CN201510258643 A CN 201510258643A CN 104859392 B CN104859392 B CN 104859392B
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- drive link
- aircraft
- flank
- gear
- duct wheel
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Abstract
It is of the present invention it is a kind of using can tilting duct wheel vehicle convertible into aircraft, fuselage uses airflow design, short limb is fixed in fuselage both sides for the level of big edge strip blended wing-body, the tip designs of short limb system of verting, the system of verting is connected to air-ground dual-purpose duct wheel, duct wheel is set to be overturn to inboard by the system of verting, it is possible to achieve vehicle convertible into aircraft is in ground run and VTOL and flies in the air with any attitude；Fuselage both sides devise six secondary short limbs altogether, need six duct wheels altogether.The vehicle convertible into aircraft has lightweight construction, internal capacity is big, aerodynamic drag is small using the technology of fairshaped fuselage and blended wing-body；The power Differential Control of six wheels, realizes flight attitude control, and design of control law is simple, easy to operate.
Description
Technical field
The invention belongs to air-ground dual-purpose driving instrument, it is especially a kind of using can tilting duct wheel vehicle convertible into aircraft.
Background technology
Since first hovercar in 1917 comes out, people have just started to explore a large amount of of hovercar, for many years
Carry out inventor and airhogs devise the good hovercar of multiple performance.Current traffic congestion getting worse, various countries
Hovercar is competitively all being researched and developed, the research in the field is more and more important, has obtained hundreds of flight vapour in global range at present
Car patent, develops a variety of model machines that can be winged, and the model machine that small part country develops has put into small lot production.Hovercar
Development becomes trend of the times.But the world compares a few money hovercars of mainstream at present（Such as X-Hawk, Hoverbike,
Airphibian）, the power drive of its ground run and the lift system of mission phase are independent, or as lift system
It is the very big straight fixed-wing of the span, is exactly the very big autorotating rotor of size, in traveling on highway or landing, not only set influences
Normal traffic order, and wing will also be limited be subject to roadside obstructions thing.
The content of the invention
For the deficiency of above-mentioned background technology, the object of the present invention is to provide a kind of flank is smaller, dynamically stable use
Can tilting duct wheel vehicle convertible into aircraft.
The present invention uses following technical scheme to solve above-mentioned technical problem：
It is a kind of using can tilting duct wheel vehicle convertible into aircraft, including vehicle body, flank and duct wheel, the end of the flank
End connects duct wheel by system of verting, and the system of verting is connected on the end of flank by plug, and the two of system of verting
End is equipped with gear, makes system rotation of verting by gear drive, realizes that duct wheel verts.
Further, the system of verting specifically includes a hollow column three-port structure, and two of which passage substantially exists
On same straight line, another passage is vertically arranged with two passage；It is equipped with each passage of the three-port structure along affiliated
The drive link of channel direction, using the drive link in the passage of other passages as the first drive link, in another two passage
Drive link is second, third drive link；One end that three drive links are located at three-port structure intersection is equipped with gear, and respectively
Gear on drive link cooperates two-by-two；Second, third described drive link, which is located at three-port structure both ends, to be equipped with outside drive link
Gear.
Further, the three-port structure is located substantially at the both ends outer surfaces of collinear two passages and is equipped with threeway
External gear, the threeway external gear is mutually matched with gear structure makes system rotation of verting, and realizes that duct wheel verts.
Further, cavity is formed in the middle part of the flank, flank drive link is equipped with cavity；The flank drive link edge
The direction of flank is set, and drive link gear, the drive link external tooth with second, third drive link are equipped with close to one end of three-port structure
Wheel is engaged；By the rotation for being converted into the first drive link of flank drive link.
Further, the other end of first drive link is connected by bearing at the center of duct wheel, drives duct wheel
Rotate.
As a preferred embodiment, the drive link external gear, the gear on flank drive link and the tooth on the first drive link
Wheel is helical gear.
As a preferred embodiment, the plug shape is consistent with flank, cavity is internally formed, the three-port structure is positioned at same
Outer surface is equipped with bearing at the both ends of two passages of one straight line, and is connected to by bearing in plug；Outside the three-port structure
Surface is additionally provided with stop ledge.
As a preferred embodiment, the flank is divided into three pairs, the both sides of vehicle body are symmetricly set on.
The present invention compared with prior art, has following technique effect using above technical scheme：
It is provided by the invention it is a kind of using can tilting duct wheel vehicle convertible into aircraft be it is a kind of both can be in the normal row in ground
Sail, park, and can be with VTOL or the sliding vehicle convertible into aircraft that runs landing and can be flown in the air with any attitude, it is used
The gear or belt of several groups of linkages make reclining device be rotated along axis, and to realize duct wheel can either vertically or horizontally turn
It is dynamic, realize bottom surface traveling and the lift-off landing of driving；
Wherein, gear structure interaction of the gear on the outside of reclining device both ends with belt or other, makes to incline
Rotary device is entirely rotated along shaft, changes the tilt angle of duct wheel；
And the drive link in the drive link and reclining device in flank mutually links, the rotation of drive link is set to be delivered to duct
On wheel, it is moved forward with rotation or provide power to lift-off, landing；The system structure of verting is simple, operation side
Just, the switching of vehicle convertible into aircraft traveling easy to implement and state of flight.
It is provided by the invention it is a kind of using can the vehicle convertible into aircraft of tilting duct wheel melted using fairshaped fuselage and wing body
The technology of conjunction, has lightweight construction, internal capacity is big, aerodynamic drag is small；The power Differential Control of six wheels, realizes flight
Gesture stability, design of control law is simple, easy to operate.
Brief description of the drawings
Fig. 1 is the general structure schematic diagram of vehicle convertible into aircraft of the present invention；
Fig. 2 is the ground run side view of the state of vehicle convertible into aircraft of the present invention；
Fig. 3 is vehicle convertible into aircraft VTOL of the present invention or sliding race landing isometric views；
Fig. 4 is vehicle convertible into aircraft VTOL of the present invention or sliding race landing side view；
Fig. 5 is vehicle convertible into aircraft airflight state isometric views of the present invention；
Fig. 6 is the front view of vehicle convertible into aircraft airflight state of the present invention；
Fig. 7 is wing and the system sectional view that verts in the present invention；
Fig. 8 is duct wheel schematic diagram in the present invention；
Fig. 9 is duct wheel schematic diagram in the present invention；
Figure 10 is three-port structure isometric views in system provided by the invention of verting；
Figure 11 is three-port structure inclining rotary mechanism and power transmission isometric views in the present invention；
In figure, 1- fuselages；2- flanks；3- duct wheels；4- drive links；5- culvert channel blades；6- duct wheel rotation axis；7- inclines
Turn system bearings；8- threeway external gears；9- stop ledges.
Embodiment
The present invention provide it is a kind of using can tilting duct wheel vehicle convertible into aircraft, to make the purpose of the present invention, technical solution
And effect is clearer, clearly, and referring to the drawings and give an actual example that the present invention is described in more detail.It should be appreciated that herein
Described specific implementation is not intended to limit the present invention only to explain the present invention.
It is provided by the invention it is a kind of using can tilting duct wheel vehicle convertible into aircraft, its overall structure diagram such as Fig. 1 institutes
Show, including vehicle body 1, flank 2 and duct wheel 3, the end of the flank 2 connects duct wheel 3 by system of verting, described to vert
System is connected to by plug on the end of flank 2, and the both ends outer surface for system of verting is equipped with gear, makes to incline by gear drive
Transfer from one department to another system rotation, realize that duct wheel verts.1 both sides of vehicle convertible into aircraft vehicle body are equipped with three pairs of flanks 2, six duct wheels 3, each wheel
The power of son is different from, and by adjusting the power of duct wheel 3, changes the transport condition of vehicle convertible into aircraft.
As shown in Figure 10, Figure 11, the system of verting specifically includes a hollow column three-port structure, two of which passage
Substantially on same straight line, another passage is vertically arranged with two passage；It is equipped with each passage of the three-port structure
Along the drive link 4 of affiliated channel direction, lead to by the first drive link, another two of the drive link in the passage of other passages
Drive link in road is second, third drive link, and the other end of the first drive link is connected by bearing at the center of duct wheel 3,
Duct wheel 3 is driven to rotate.One end that above three drive link 4 is located at three-port structure intersection is equipped with gear, and each drive link 4
On gear cooperate two-by-two；Second, third described drive link, which is located at three-port structure both ends, is equipped with drive link external gear；Should
The both ends outer surface that three-port structure is located substantially at collinear two passages is equipped with threeway external gear, the threeway external gear
8 are mutually matched with belt or gear and make system rotation of verting, and realize that duct wheel 3 verts.As shown in fig. 7, outside above-mentioned drive link
Gear 8, the gear on flank drive link and the gear on the first drive link are helical gear.
The above-mentioned middle part of flank 2 forms cavity, and flank drive link is equipped with cavity；Direction of the flank drive link along flank
Set, be equipped with drive link gear close to one end of three-port structure, be engaged with the drive link external gear of second, third drive link；
The rotation of flank drive link is converted into the rotation of the first drive link.
Above-mentioned plug shape is consistent with flank, is internally formed cavity, and the three-port structure is located at collinear two
Outer surface is equipped with inclining rotary mechanism bearing 7 at the both ends of passage, and is connected to by bearing in plug；The three-port structure outer surface
It is additionally provided with stop ledge 9.
Referring to the drawings, vehicle convertible into aircraft of the invention includes fairshaped fuselage, the short limb and two-way of big edge strip blended wing-body
Gear drive and system of verting, and coaxial double-oar duct wheel 3.
As shown in Figure 1 and Figure 2, when vehicle convertible into aircraft is in the ground run stage, work of six duct wheels 3 with wheel of the bus
Make that mode is the same, the rotation axis of wheel is parallel to ground.
As shown in Figure 3, Figure 4, the duct wheel 3 when vehicle convertible into aircraft VTOL or sliding race landing among fuselage both sides
Turn over and turn 90 degrees to inboard, duct wheel rotation axis 6 provides pulling force vertically upward, machine perpendicular to ground, for vehicle convertible into aircraft
Four duct wheels before and after body both sides still support vehicle convertible into aircraft as the working method of wheel of the bus, until vehicle convertible into aircraft
Ground is left completely, and with reference to Fig. 5, Fig. 6, all six duct wheels 3 are overturn to inboard, all provide drawing vertically upward
Power.By controlling the power of six duct wheels 3, six duct wheels 3 are made to provide pulling force in different size, so that it may to realize straight
Driving is risen to fly with any attitude.
The vehicle convertible into aircraft for the design that the present invention designs, the exhibition of wing in itself is smaller to size, and wing is intended only as flight shape
State auxiliary provides lift, and main lift is provided by duct wheel 3, and the system of verting realizes duct wheel from ground run state
Vert to state of flight, be a kind of new duct vehicle convertible into aircraft, in following crowded urban transportation and increasingly ripe individual
In aircraft market, there is extremely wide application prospect.
It is understood that for those of ordinary skills, can be with technique according to the invention scheme and its hair
Bright design is subject to equivalent substitution or change, and all these changes or replacement should all belong to the guarantor of appended claims of the invention
Protect scope.
Claims (7)
1. it is a kind of using can tilting duct wheel vehicle convertible into aircraft, including vehicle body, flank and duct wheel, it is characterised in that：Institute
The end for stating flank connects duct wheel by system of verting, and the system of verting is connected on the end of flank by plug, inclined
The both ends for transfering from one department to another system are equipped with gear, make system rotation of verting by gear drive, realize that duct wheel verts；
The system of verting specifically includes a hollow column three-port structure, two of which passage substantially on same straight line,
Another passage is vertically arranged with two passage；The transmission along affiliated channel direction is equipped with each passage of the three-port structure
Bar, using the drive link in the passage of other passages as the first drive link, drive link in another two passage is second, the
Three drive links；One end that three drive links are located at three-port structure intersection is equipped with gear, and the gear on each drive link
Cooperate two-by-two；Second, third described drive link, which is located at three-port structure both ends, is equipped with drive link external gear.
2. it is according to claim 1 it is a kind of using can tilting duct wheel vehicle convertible into aircraft, it is characterised in that：The threeway
The both ends outer surface that structure is located substantially at collinear two passages is equipped with threeway external gear, the threeway external gear and tooth
Wheel construction, which is mutually matched, makes system rotation of verting, and realizes that duct wheel verts.
3. it is according to claim 1 it is a kind of using can tilting duct wheel vehicle convertible into aircraft, it is characterised in that：The flank
Middle part forms cavity, and flank drive link is equipped with cavity；The flank drive link is set along the direction of flank, close to three-port structure
One end be equipped with drive link gear, be engaged with the drive link external gear of second, third drive link；By the rotation of flank drive link
It is converted into the rotation of the first drive link.
4. it is according to claim 1 it is a kind of using can tilting duct wheel vehicle convertible into aircraft, it is characterised in that：Described first
The other end of drive link is connected by bearing at the center of duct wheel, drives duct wheel to rotate.
5. it is according to claim 3 using can tilting duct wheel vehicle convertible into aircraft, it is characterised in that：Outside the drive link
Gear, the gear on flank drive link and the gear on the first drive link are helical gear.
6. it is according to any one of claims 1 to 4, using can tilting duct wheel vehicle convertible into aircraft, it is characterised in that：
The plug shape is consistent with flank, is internally formed cavity, and the three-port structure is located at the two of collinear two passages
Outer surface is equipped with bearing at end, and is connected to by bearing in plug；The three-port structure outer surface is additionally provided with stop ledge.
7. it is according to claim 6 it is a kind of using can tilting duct wheel vehicle convertible into aircraft, it is characterised in that：The flank
It is divided into three pairs, is symmetricly set on the both sides of vehicle body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510258643.0A CN104859392B (en) | 2015-05-20 | 2015-05-20 | It is a kind of using can tilting duct wheel vehicle convertible into aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510258643.0A CN104859392B (en) | 2015-05-20 | 2015-05-20 | It is a kind of using can tilting duct wheel vehicle convertible into aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104859392A CN104859392A (en) | 2015-08-26 |
| CN104859392B true CN104859392B (en) | 2018-04-17 |
Family
ID=53905747
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510258643.0A Expired - Fee Related CN104859392B (en) | 2015-05-20 | 2015-05-20 | It is a kind of using can tilting duct wheel vehicle convertible into aircraft |
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| CN (1) | CN104859392B (en) |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105196815A (en) * | 2015-10-27 | 2015-12-30 | 陈晓春 | Synchronous turnover mechanism applied to aerocar |
| CN105329056A (en) * | 2015-11-24 | 2016-02-17 | 宁波市镇海怡福莱文化创意有限公司 | Wheel type rotor wing vehicle |
| CN106143031A (en) * | 2016-06-21 | 2016-11-23 | 王启振 | Driving |
| CN106347049B (en) * | 2016-12-01 | 2018-09-11 | 吉林大学 | A kind of electric vehicle wheel position conversion device and land and air double-used electric vehicle |
| CN110891859B (en) * | 2017-07-27 | 2023-03-10 | 株式会社辰巳菱机 | Suspension type mobile device |
| CN109249768A (en) * | 2018-10-30 | 2019-01-22 | 佛山市神风航空科技有限公司 | A kind of car of new model |
| CN109353176B (en) * | 2018-11-30 | 2023-10-27 | 南京航空航天大学 | Tricycle is experienced in flight |
| DE102019001130B3 (en) * | 2019-02-13 | 2020-02-13 | Friedrich Grimm | Wheel propellers and vehicles with wheel propellers |
| CN113512981A (en) * | 2021-07-09 | 2021-10-19 | 河北卓尔正科技开发有限公司 | Novel high-intelligence fog gun machine based on big data intelligent control |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102004063205B3 (en) * | 2004-12-23 | 2006-05-04 | Julian Kuntz | Aircraft for transporting persons, has rotors/propellers with sheathings, which enable independent drive movement of aircraft on land according to function of wheel rims based on direct power transmission from aircraft to land |
| CN103213466B (en) * | 2013-04-08 | 2015-12-02 | 龙川 | The carplane of carplane wheel system and utilization carplane wheel system |
| CN104085530B (en) * | 2014-06-10 | 2016-07-13 | 南京航空航天大学 | The coaxial multi-rotor aerocraft of duct |
| CN204774450U (en) * | 2015-05-20 | 2015-11-18 | 南京航空航天大学 | Can vert driving of lifting vertically of duct wheel of use |
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2015
- 2015-05-20 CN CN201510258643.0A patent/CN104859392B/en not_active Expired - Fee Related
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| CN104859392A (en) | 2015-08-26 |
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