CN108859640A - Land and air double-used aircraft - Google Patents
Land and air double-used aircraft Download PDFInfo
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- CN108859640A CN108859640A CN201810990200.4A CN201810990200A CN108859640A CN 108859640 A CN108859640 A CN 108859640A CN 201810990200 A CN201810990200 A CN 201810990200A CN 108859640 A CN108859640 A CN 108859640A
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- flight
- car body
- land
- control system
- air double
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- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims abstract description 33
- 238000004804 winding Methods 0.000 claims description 17
- 239000000725 suspension Substances 0.000 claims description 16
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 9
- 238000013461 design Methods 0.000 claims description 6
- 230000007246 mechanism Effects 0.000 claims description 6
- 238000003032 molecular docking Methods 0.000 claims description 4
- 238000010586 diagram Methods 0.000 description 7
- 238000009434 installation Methods 0.000 description 7
- 230000004308 accommodation Effects 0.000 description 5
- 230000008901 benefit Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 238000007599 discharging Methods 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 238000005265 energy consumption Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000017525 heat dissipation Effects 0.000 description 2
- 230000006872 improvement Effects 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- 239000000758 substrate Substances 0.000 description 2
- 229920005372 Plexiglas® Polymers 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000037237 body shape Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 239000000295 fuel oil Substances 0.000 description 1
- 238000001727 in vivo Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 239000004926 polymethyl methacrylate Substances 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000005341 toughened glass Substances 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 230000032258 transport Effects 0.000 description 1
- 230000001755 vocal effect Effects 0.000 description 1
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)
- Motorcycle And Bicycle Frame (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of land and air double-used aircrafts, execute body including flight, can execute car body and the lifting device to draw high or put down car body relative flight execution body that body docks with flight；The flight executes the cover that car body is covered after body includes screw, docks with car body；The car body includes taking cabin, being installed on the wheel taken in cabin；Flight control system, car body operation control system and lifting device control system are provided in the seating cabin.Land and air double-used aircraft of the invention by lifting device by car body relative flight execution body draw high and butt up against flight execute body when, user by manipulate flight control system make car body combine flight execution body fly in the sky；When declining car body relative flight execution body by lifting device and be located away from flight execution body, user allows car body is independent to travel on road surface by manipulating car body operation control system.The land and air double-used aircraft can effectively alleviate the problem of traffic congestion.
Description
Technical field
The present invention relates to a kind of vehicles, more particularly to one kind can travel but also be detached from ground flying on road surface
Land and air double-used aircraft.
Background technique
As social economy continues to develop, either the traffic construction in city and rural area or mountain area or Plain are public
Road network construction, has great development to improve.More cities and towns and rural resident have purchased vapour because of improvement of living standard
Vehicle, to be convenient to go on a journey.With caused by the increase of automobile quantity congestion in road phenomenon become more and more cities be difficult to
The problem of avoidance.Even if possessing automobile, trip also may not conceptive such convenience.Traffic traffic congestion be it is some place especially
It is metropolitan traffic normality, brings inconvenience to daily life.So the problem of alleviating traffic congestion is current
One of important topic faced.
Therefore, it is necessary to provide the vehicles that one kind can on the way be travelled and be flown in the sky.
Summary of the invention
The technical problem to be solved in the present invention is to provide a kind of land and air double-used vehicles.
In order to solve the above technical problems, the present invention provides the following technical solutions：A kind of land and air double-used aircraft, including flight
It executes body, car body and the lifting dress to draw high or put down car body relative flight execution body that body docks can be executed with flight
It sets；The flight executes the cover that car body is covered after body includes screw, docks with car body；The car body includes passenger compartment
Body is installed on the wheel taken in cabin；Be provided in the seating cabin flight control system, car body operation control system and
Lifting device control system.
The present invention has the advantages that compared to the prior art：Land and air double-used aircraft of the invention passes through lifting dress
When setting and draw high car body relative flight execution body, and butting up against flight execution body, user is made by manipulating flight control system
Car body combines flight to execute body and flies in the sky；Land and air double-used aircraft is executed car body relative flight under body by lifting device
When dropping, and being located away from flight execution body, user allows car body independent on road surface by manipulating car body operation control system
Upper traveling.The land and air double-used aircraft can effectively alleviate the problem of traffic congestion.
Preferably, it further includes main part that the flight, which executes body, and several screws are distributed in the periphery of main part,
The cover is fixedly connected on main part and is located at the upside of main part.
Preferably, the screw include the cantilever for being fixedly connected on main part, the screw motor being installed on cantilever,
It is connected to the propeller of screw motor；The screw motor is controlled by flight control system.
Preferably, the edge of the main part extends the protection wing plate for constituting and surrounding several screws to the periphery, described
Protection wing plate offers several air guide channels for respectively corresponding several propellers；The propeller is inserted into air guide channel, institute
The diameter for stating air guide channel is greater than the length of propeller.
Preferably, it is equipped on the protection wing plate several to cooperate land and air double-used aircraft to land and can be supported in
The landing gear on ground；The landing gear includes being rotatablely connected with described in the shock-absorbing support frame for protecting wing plate, promotion to subtract
Shake the driving mechanism that the support frame relatively described protection wing plate expansion or folded；The driving mechanism is controlled by flight control system.
Preferably, one end that the shock-absorbing support frame is supported in ground is equipped with wheel.
Preferably, the lifting device include the lifting motor for being installed on the car body, be connected to motor output shaft around
Line roller, the drawstring for being wound in winding roller, the suspension hook for being bundled in drawstring；The flight executes body and is equipped with to be connected hanging for suspension hook
Ring；
Alternatively, the lifting device include be installed on it is described flight execute body lifting motor, be connected to motor output shaft around
Line roller, the drawstring for being wound in winding roller, the suspension hook for being bundled in drawstring；The car body is equipped with the hanging ring to be connected suspension hook.
Preferably, land and air double-used aircraft further includes car body is fixed on the fixation device that flight executes body.
Preferably, the fixed device include the pin shaft being installed on car body and be opened in flight execute body on accommodate pin
The flexible pin hole of axis.
Preferably, the cabin of taking includes the bearing seat to install seat, and the bearing seat is in open design, described
The pedestal portion of seat protrudes from bearing seat；When the car body butts up against flight execution body, the pedestal portion of seat is inserted into the cover
In vivo.
Detailed description of the invention
Fig. 1 is the stereoscopic schematic diagram of land and air double-used aircraft of the present invention；
Fig. 2 is the left view schematic diagram of land and air double-used aircraft in Fig. 1；
Fig. 3 is that the car body of land and air double-used aircraft of the present invention is detached in flight execution body, the opposite protection wing plate exhibition of shock-absorbing support frame
The schematic front view opened；
Fig. 4 is the elevational schematic view of land and air double-used aircraft in Fig. 1；
Fig. 5 is that the car body of land and air double-used aircraft of the present invention is detached in flight execution body, the opposite protection wing plate exhibition of shock-absorbing support frame
The stereoscopic schematic diagram opened；
Fig. 6 is the landing gear of land and air double-used aircraft of the present invention and the connection schematic diagram of protection wing plate；
Fig. 7 is the stereoscopic schematic diagram of the car body of land and air double-used aircraft of the present invention；
Fig. 8 is the cross-sectional view in Fig. 7 along line A-A；
Fig. 9 is the connection schematic diagram of the power supply of land and air double-used aircraft of the present invention；
Figure 10 is the suspension hook hanging buckle of the lifting device of land and air double-used aircraft of the present invention in the schematic diagram of hanging ring；
Figure 11 is the schematic front view of land and air double-used aircraft in another embodiment of the present invention.
Specific embodiment
A specific embodiment of the invention is described in detail with reference to the accompanying drawing, rather than to protection scope of the present invention
Limitation.The orientation or positional relationship of the instructions such as term "front", "rear", "left", "right", "upper", "lower" is based on the figure
Orientation or positional relationship is merely for convenience of description of the present invention and simplification of the description, rather than the device of indication or suggestion meaning or
Element must have a particular orientation, be constructed and operated in a specific orientation, therefore be not considered as limiting the invention.Art
Language " first ", " second " are only used for simplifying verbal description to be different from similar object, and should not be understood as between specific order
Precedence relationship.
It is involved in description of the invention and its claims that " car body 2 is located away from flight and executes body 1 and independent fortune
Row is in road surface " in " separation " refer to that car body 2 is totally independent of flight and executes body 1, there is no be connected to each other by lifting device 3
The case where.
Embodiment one
Refering to fig. 1, Fig. 2 and Fig. 3, provides a kind of land and air double-used aircraft in the present embodiment, including flight execute body 1, can group
Fill or be detached in the car body 2 and the lifting dress to draw high or put down 2 relative flight of car body execution body 1 that flight executes body 1
Set 3.Flight, which executes body 1, has screw 4, and screw 4 can be flown using air-flow in aerial.Car body 2 can be understood as
Automobile in the prior art, certain car body 2 can also be other dynamic land carrying tools of tool, such as：Electric wheelchair or
Electric bicycle etc..Land and air double-used aircraft is equipped with flight control system, car body operation control system and lifting device control
System.Land and air double-used aircraft flight is controlled by flight control system when aerial, car body 2 be located away from when flight executes body 1 by
It controls in car body operation control system.Lifting device 3 is controlled by lifting device control system, by manipulating lifting device control system
So that 2 relative flight of car body executes body 1 and draws high or put down, body 1 is executed to be convenient to the assembling of car body 2 or be detached in flight.This hair
Bright land and air double-used aircraft is drawn high 2 relative flight of car body execution body 1 by lifting device 3, and is butted up against flight and executed body 1
When, user makes car body 2 that flight execution body 1 be combined to fly in the sky by manipulating flight control system；Land and air double-used aircraft
When being declined by lifting device 3 by 2 relative flight of car body execution body 1, and being located away from flight execution body 1, user passes through manipulation vehicle
Running body control system allows car body 2 is independent to travel on road surface.The land and air double-used aircraft can effectively be alleviated
The problem of traffic congestion, additionally it is possible to be convenient to the tasks such as mountain area exploration, emergency relief.
Refering to fig. 1 and Fig. 4, in the present embodiment, it includes main part 11, the spiral shell being mounted on main part 11 that flight, which executes body 1,
Cyclone 4, the cover 12 for being fixedly connected on main part 11 and being located at 11 upside of main part.Main part 11 in a ring, is located at flight
Execute the central area of body 1.When car body 2 butts up against flight execution body 1 by lifting device 3, it is assembled in the downside of main part 11.
Car body 2 and cover 12 are located at the upper side and lower side of main part 11, and are oppositely arranged.Cover 12 is covered in the top of car body 2
To cover car body 2, so that forming enclosure space between cover 12 and car body 2.Car body 2 combines flight to execute the flight of body 1 in high-altitude
When, which can be further improved the performance that car body 2 resists atmospheric pressure.Certainly, flight executes body 1 and can not also install
Cover is realized using the closing shell of car body itself and resists atmospheric pressure；Alternatively, car body is woth no need to being arranged closing shell, i.e. vehicle
Body 2 is in open design（Sunshine automobile）, the car body 2 of the open design can use cover 12 as resistance atmospheric pressure at this time
Shell.
It is the bottom view of land and air double-used aircraft refering to Fig. 4, Fig. 4.In the present embodiment, the quantity of screw 4 is eight,
Eight screws 4 are uniformly distributed in the periphery of main part 11.The bottom face of main part 11 is equipped with installs eight spiral dresses respectively
Set 4 eight fixing seats 13.Each screw 4 includes the cantilever 41 for being fixedly connected on fixing seat 13, is installed on cantilever 41
Screw motor 42, be connected to the propeller 43 of screw motor 42.Each cantilever 41 extends to the periphery of main part 11.Eight outstanding
Arm 41 is in same plane, and the angle between two adjacent cantilevers 41 is 45 degree.Propeller 43 and screw motor 42 are spatially
It is arranged in upper and lower position, i.e. the top that is mounted on screw motor 42 of propeller 43.The beneficial effect of such setting is screw motor
42, which are powered, generates heat when rotating, propeller 43 pushes air flows down when rotating, and the air constantly flowed is conducive to spiral
The heat dissipation of motor 42.Screw motor 42 is controlled by flight control system, to push land and air double-used aircraft flight in aerial.Certainly
In other embodiments, the quantity of screw 4 can be the quantity such as two, three, four, and particular number can be according to need
It sets.Wherein, when the quantity of screw is adopted as one, which is installed on the top of main part.
Refering to fig. 1 and Fig. 4, in the present embodiment, the edge of main part 11 extends composition to the periphery and surrounds eight screws 4
Protection wing plate 14.Protection wing plate 14 is in disk form and is surrounded on the periphery of main part 11, protection wing plate 14 and main part 11 1
Body formed production.Discoidal protection wing plate 14 is conducive to flight and executes the reduction air drag of body 1, saves energy consumption, improves
Flying speed；And there is preferable rotator inertia, be conducive to turn in the sky.Eight are offered on protection wing plate 14 to respectively correspond
The air guide channel 15 of eight propellers 43.If the quantity of screw 4 is adopted as six, then protection wing plate 14 is opened accordingly
If six air guide channels.Air guide channel 15 is rounded, is convenient to make.Propeller 43 is inserted into air guide channel 15, and air guide is logical
The diameter in road 15 is greater than the length of propeller 43, and propeller 43 is located in air guide channel 15 and is rotated.At this point, spiral is electric
Machine 42 is located at the lower section of protection wing plate 14 accordingly（As shown in Figure 2）.Protection wing plate 14 equipped with multiple air guide channels 15 can be with
It prevents propeller 43 from colliding with other objects, improves the service life of screw 4, also can be avoided propeller 43 to it
His object causes to damage.
Refering to Fig. 2 to Fig. 6, in the present embodiment, protects on wing plate 14 and be equipped with eight to cooperate land and air double-used aircraft
Land and can be supported in the landing gear 5 on ground.Eight landing gears 5 are uniformly distributed on discoidal protection wing plate 14
（As shown in Figure 4）, and it is connected to the lower end surface of protection wing plate 14.Referring to Fig. 6, each landing gear 5 includes rotatably connecting
It is connected to the shock-absorbing support frame 51 of protection wing plate 14, pushes opposite driving machine protection wing plate 14 expansion or folded of shock-absorbing support frame 51
Structure 52.Shock-absorbing support frame 51 includes first body of rod 511, telescopic second body of rod 512 for being connected to first body of rod 511, connection
Adjustable spring 513 between first body of rod 511 and second body of rod 512.The lower end surface of protection wing plate 14 is welded with fixed ear base
141, the top of first body of rod 511 of shock-absorbing support frame 51 is articulated with the fixed ear base 141 by pin shaft.Second body of rod 512 is used
To be supported in ground.Second body of rod 512 is supported in the end on ground in Curved, dispersedly to face the anti-of shock-absorbing support frame 51
Active force.Preferably, one end that second body of rod 512 is supported in ground is equipped with wheel（It is not shown in the figure）, body 1 is executed in flight
Land when uneven ground, by the equalization point for rolling and finding flight and executing body 1 of taking advantage of a situation of wheel, flight can be improved and hold
Stability when row body 1 lands.
The driving mechanism 52 of landing gear 5 include motor 521, be connected to motor output shaft gear 522, engaged transmission in
The rack gear 523 of gear 522, the sliding groove 524 for installing rack gear 523 and the catch bar 525 for being rotatablely connected with rack gear 523.
Motor 521 and sliding groove 524 are fixedly connected in the lower end surface of protection wing plate 14.Flight control system drives 521 turns of the motor
When dynamic, rack gear 523 is slided with respect to sliding groove 524.One end of catch bar 525 is articulated with rack gear 523, and the other end is articulated with the first bar
The middle part of body 511.Forward direction by motor 521 with rotate backward, shock-absorbing support frame 51 can opposite protection wing plate 14 be unfolded or
It folds.Shock-absorbing support frame 51 and rack gear 523 are spatially arranged in a staggered manner, i.e. shock-absorbing support frame 51 and rack gear 523 is located at and pushes away
The two sides of lever 525 can avoid rack gear 523 and motor 521 when so that the opposite protection wing plate 14 of shock-absorbing support frame 51 folding.
In other embodiments, the quantity of landing gear 5 can be the quantity such as three, four, five, and particular number can be according to need
It sets；The driving mechanism 52 can also be cylinder or electric pushrod.
The driving mechanism 52 of landing gear 5 is controlled by flight control system.When land and air double-used aircraft flight when aerial,
The opposite protection wing plate 14 of the shock-absorbing support frame 51 of landing gear 5 is in folded state（As shown in Figure 2）, to reduce windage；When car body 2
Need to be located away from flight execute body 1, it is independent on road surface when driving, flight execute body 1 start to land, 51 phase of shock-absorbing support frame
It is in unfolded state to protection wing plate 14（As shown in figs. 3 and 5）.Flight executes body 1 and is supported in ground, car body by landing gear 5
2 by lifting device 3 with respect to ground transfer and be located away from flight execute body 1, car body 2 be detached in flight execution body 1 after, pass through
Car body operation control system can drive car body 2 to be displaced into ground.
Refering to Fig. 7, in the present embodiment, car body 2 is in open design.Car body 2 includes the passenger compartment taken and driven for user
Body 21 is installed on the wheel 22 taken in cabin 21.The rounded bowl body shape of cabin 21 is taken, the diameter of end face is greater than thereon
The diameter of lower end surface.Circular seating cabin 21 is conducive to car body 2 and reduces air drag, saves energy consumption.Certainly, passenger compartment
Body 21 can also be square or spherical shape.Take the seat 23 being equipped in cabin 21 for users to use.Car body operation control system,
Flight control system and lifting device control system, which are all set in, to be taken in cabin 21.Car body operation control system is applied to land
Driving mode, flight-control system is in flight management mode.Car body operation control system and flight control system are existing
Have in technology and drives operating system.User can be according to required driving mode in car body operation control system and flight control system
It is switched between system.
Refering to Fig. 8, taking cabin 21 includes installing the firm banking 212 of wheel 22, being fixedly connected on firm banking 212
Bearing seat 211 to install seat 23 and provide the power supply 213 of operating power to land and air double-used aircraft.It is installed on solid
The quantity for determining the wheel 22 on pedestal 212 is three, three wheels 22 bottom triangular in shape for being installed on firm banking 212（Such as
Shown in Fig. 4）.One of wheel 22 is installed on the front of car body 2, other two wheel 22 is installed on the rear portion of car body 2.Rear portion
Two wheels 22 driving motor is installed, driving motor is connected to power supply 213 and is controlled by car body operation control system, front
Wheel 22 be driven in the wheel 22 at rear portion.Alternatively, a wheel 22 of front is equipped with driving motor, two wheels at rear portion
22 are driven in a wheel 22 of front；Again alternatively, three wheels 22 of front and rear are mounted on driving motor.This implementation
In example, the wheel 22 for being equipped with driving motor is adopted as hub motor wheel, can reduce installation volume.
Firm banking 212 is in concave shaped and the first accommodation groove for constituting installation power supply 213.Bearing seat 211 is covered in fixation
212 top of pedestal.Bearing seat 211 is recessed to 212 direction of firm banking relative to the wall body of firm banking 212, and constitutes installation
Second accommodation groove of seat 23.The bottom of second accommodation groove is inserted into the first accommodation groove of firm banking 212, the second accommodation groove
Bottom wall and firm banking 212 be encircled into installation power supply 213 closing accommodating space.It is set on firm banking 212 and bearing seat 211
There is heat release hole, in order to the heat dissipation of power supply 213.It is provided with charging interface on firm banking 212, which is connected by power supply line
It is connected to power supply 213.
Refering to Fig. 2 and Fig. 8, bearing seat 211 is in open design, and the pedestal portion 231 of seat 23 protrudes from bearing seat 211.Vehicle
When body 2 butts up against the main part 11 of flight execution body 1, the pedestal portion 231 of seat 23 is inserted into cover 12.The pedestal of seat 23
Portion 231 runs through the main part 11 of annular and extends to inside cover 12, opposite can reduce car body 2 and butt up against flight execution body 1
When overall volume, reduce air drag.Cover 12 is in hemispheroidal shape.Hemispheric cover 12 is meeting air conducting
On the basis of can further increase accommodating space, can make car body 2 further be inserted into flight execute body 1 cover 12 in
Portion.Main part 11 is equipped with the fixation bracket 13 of fixed enclosure 12, to improve the installation fastness of cover 12.Cover 12 is adopted as
Bright substrate, such as：Tempered glass or plexiglas.Be conducive to user and observe external situation through cover 12.It needs to illustrate
It is：When user observes external circumstances, which can not also use transparent substrate, it is only necessary to execute the periphery of body 1 in flight
Multiple cameras are installed, camera is connected to the image display system for being mounted on and taking in cabin 21, and image display system is equipped with
Display screen.
Refering to Fig. 9, in the present embodiment, the power supply 213 being mounted on 2 firm banking 212 of car body is electrically connected in above-mentioned
Each control system, the driving motor being mounted on wheel 22, lifting device 3 31, eight screws 4 of lifting motor and
Eight landing gears 5.Each control system refers to flight control system, car body operation control system and lifting device control system.
Wherein, each control system, the driving motor being mounted on wheel 22, lifting device 3 lifting motor 31 be installed in car body 2
On；Eight screws 4 and eight landing gears 5 are installed in flight and execute on body 1.For the electricity that will be mounted on car body 2
Source 213 is easily electrically connected to eight screws 4 and eight landing gears 5 being mounted on flight execution body 1, car body 2
Bearing seat 211 is equipped with the pin end of connection power supply line, and the main part 11 that flight executes body 1 is equipped with the mother cooperated with pin end
Connector.Pin end is connected to power supply 213 by power supply line, and female connector is electrically connected to eight screws 4 by power supply line respectively
With eight landing gears 5.When the bearing seat 211 of car body 2 butts up against the main part 11 of flight execution body 1, pin end is inserted accordingly
Enter in female connector, the power supply 213 in realization between lower body is connected to.Certainly in other embodiments, which can also
Flight is mounted on to execute on body 1（That is, not installing power supply on car body, such situation is suitable for car body woth no need to isolated operation in road
The case where face）, the power electric connection on flight execution body 1 is mounted in eight screws and eight landing gears, also can
The liter of installation wheel drive motors on the car body, each control system and lifting device 3 is electrically connected to by pin and box sub
Motor 31 drops；Alternatively, executing separately installed another power supply on body 1 in flight（That is, car body 2 and flight execute the respectively installation one of body 1
Power supply 213）, filled at this point, being installed on another power electric connection that flight executes on body 1 in eight screws 4 and eight landings
Set 5；The power supply 213 being installed on car body 2 is electrically connected to lifting motor 31, each control system and the wheel of lifting device 3
Driving motor；It is convenient to the wiring of power supply 213.It should be noted that：The present invention is supplied to the power of land and air double-used aircraft operation
Source is not restricted to power supply 213, can also be the energy using fuel oil by engine conversion generation, alternatively, oil electricity mixing turns
The energy changed.
It is additionally provided with the pin and box sub of communications signals line on bearing seat 211 and main part 11, is conducive to land and air double-used aircraft
In flight management mode, user has eight screws 4 of line traffic control and eight landing gears 5 by flight control system.When
Right flight control system can also control eight screws 4 and eight landing gears 5 by wireless control mode.
Refering to Fig. 5 and Figure 10, in the present embodiment, the quantity of lifting device 3 is four, and four lifting devices 3 are installed respectively
In the front and rear of car body 2, front and rear respectively there are two lifting device 3 and is oppositely arranged.Each lifting device 3 includes peace
Lifting motor 31 on the bearing seat 211 of car body 2, is wound in winding roller at the winding roller 33 for being connected to motor output shaft 32
33 drawstring 34, the suspension hook 35 for being bundled in drawstring 34.The main part 11 that flight executes body 1 is equipped with to be connected hanging for suspension hook 35
Ring 16.The lifting motor 31 being mounted on car body 2 is electrically connected to the power supply 213 being mounted on car body 2 and is controlled by lifting device
Control system.Make car body 2 that can draw high or put down with relative flight execution body 1 by manipulating lifting device control system, with reality
Existing 2 relative flight of car body executes the docking of body 1 and separates.Lifting device 3 is equipped with the locking member of limiting motor output shaft rotation, should
Locking member can prevent motor output shaft unintentional rotation, execute body 1 when car body 2 butts up against flight and fly when aerial, can be with
It avoids car body 2 from being detached in flight and executes body 1, ensure that the safety of flight.
In the present embodiment, land and air double-used aircraft includes car body 2 is fixed on the fixation device that flight executes body 1.
Fixed device includes the pin hole of pin shaft and cooperation pin shaft limit.Pin shaft is mounted on the bearing seat 211 of car body 2, and pin hole opens up
In on the main part 11 that flight executes body 1, which can accommodate pin shaft stretching, extension and shrink.The bearing seat 211 of car body 2 butts up against
When flight executes the main part 11 of body 1, pin shaft is positioned at pin hole manually by user, so that car body 2 firmly butts up against flight and holds
Row body 1.The fixation device can be kept away in the case where unintentional rotation occurs for motor output shaft and unexpected loosen occurs for locking member
Exempt from car body 2 and be detached in flight execution body 1, further ensures the safety of flight.In addition, car body 2, which is detached in flight, executes body 1
When, need user that pin shaft is located away from pin hole.
Certainly in other embodiments, which can also be a snap close piece.Snap close piece includes being installed on main body
The locking bar in portion 11, the fixed part for being installed on bearing seat 211, the lock ring for being rotatably connected at fixed part, the handle for being connected to lock ring
Handle.When the bearing seat 211 of car body 2 butts up against the main part 11 of flight execution body 1, user pulls handle and lock ring is made to be buckled in lock
Bar, so that car body 2 firmly butts up against flight and executes body 1.In addition, needing user anti-when car body 2 is detached in flight execution body 1
To handle is pulled lock ring is detached from locking bar.
State of the land and air double-used aircraft by 2 independent operating of car body in road surface, which is converted to car body 2, combines flight execution body 1 to fly
Row needs to draw high and butt up against flight 2 relative flight of car body execution body 1 executing body 1, wherein power supply when aerial state
Line pin and box sub and signal wire pin and box sub can also dock accordingly.Specific docking operation includes the following steps：It flies at this time
It executes body 1 and ground is supported in by landing gear 5, the screw 4 that flight executes body 1 is in halted state.Car body 2 passes through vehicle
The manipulation of running body control system is moved to the lower section that flight executes the main part 11 of body 1, and user closes car body operation control system
System is so that car body 2 stops movement；User manipulates lifting device control system and opens lifting motor 31, and lifting motor 31 rotates forward
And release is wound on the drawstring 34 of winding roller 33；When 34 length of drawstring to be released enables suspension hook 35 to touch hanging ring 16,
Stop lifting motor 31 to rotate forward；The manual hanging buckle of the suspension hook of four lifting devices 3 35 is executed body 1 in flight respectively by user
On four hanging rings 16, after hanging buckle, user manipulates lifting device control system and lifting motor 31 is rotated backward, and will
The drawstring 34 of release is wound on winding roller 33；Band 2 relative flight of motor vehicles bodies while winding drawstring 34 of lifting device 3 executes
Body 1 is mobile, and car body 2 butts up against flight accordingly and executes body 1, and power supply line pin and box sub and signal wire pin and box sub also can be corresponding
Docking；User opens flight control system, and the propeller 43 for controlling eight screws 4 is rotated and flown in aerial；To
After land and air double-used aircraft leaves ground, user controls eight landing gears 5 by flight control system, by shock-absorbing support frame 51
Opposite protection wing plate 14 is folded.So far it completes land and air double-used aircraft and is converted by 2 independent operating of car body in the state on road surface
Flight is combined to execute the flight of body 1 in aerial state to car body 2.
Land and air double-used aircraft combines flight execution body 1 flight to convert in aerial state to car body 2 is independent and transports by car body 2
Row needs to execute 2 relative flight of car body body 1 and declines and be located away from flight execution body 1, wherein power supply when the state on road surface
Line pin and box sub and signal wire pin and box sub can also separate accordingly.Specific separation process includes the following steps：User passes through
Flight control system reduces flying speed, and flies to the top in target level point；User passes through flight control system control eight
The opposite protection wing plate 14 of shock-absorbing support frame 51 is unfolded a landing gear 5；The flight for reducing land and air double-used aircraft is high
Degree, when shock-absorbing support frame 51 can be contacted with ground and can be stable when being supported in ground（Car body 2 butts up against flight and holds at this time
Row body 1 is simultaneously outstanding as aerial）, user's closing flight control system；User manipulates lifting device control system and opens lifting motor
31, lifting motor 31 rotates forward and discharges the drawstring 34 wound on winding roller 33；Lifting device 3 is while discharging drawstring 34
Band 2 relative flight of motor vehicles bodies executes body 1 and separates and level off to ground, and car body 2 is detached in flight accordingly and executes body 1, power supply line
Pin and box sub and signal wire pin and box sub can also separate accordingly；34 length of drawstring to be released makes the wheel 22 of car body 2
After being supported in ground, stops lifting motor 31 and rotate forward；The suspension hook 35 of four lifting devices 3 is detached in by user manually respectively
Flight executes four hanging rings 16 of body 1, and after separating, user manipulates lifting device control system and makes lifting motor 31 anti-
It is wound on winding roller 33 to rotation, and by the drawstring of release 34；User opens car body operation control system and makes car body 2 mobile
And independent run on road surface.So far it completes land and air double-used aircraft and combines flight to execute the flight of body 1 in aerial shape by car body 2
State is converted to 2 independent operating of car body in the state on road surface.
The car body 2 of land and air double-used aircraft combine flight execute body 1 fly in the sky passenger above and below needs when, specifically include
Following steps：Driver reduces flying speed by flight control system, and flies to target passenger position or target level point
Top；Driver controls eight landing gears 5 by flight control system, by the opposite protection wing plate 14 of shock-absorbing support frame 51 into
Row expansion；The flying height for reducing land and air double-used aircraft, can be contacted with ground to shock-absorbing support frame 51 and can be stable
When being supported in ground（Car body 2 butts up against flight and executes body 1 and hang as aerial at this time）, driver's closing flight control system；
Driver manipulates lifting device control system and opens lifting motor 31, and lifting motor 31 is rotated forward and discharged wound on winding roller
33 drawstring 34；Band 2 relative flight of motor vehicles bodies while discharging drawstring 34 of lifting device 3 executes body 1 and separates and level off to ground
Face, car body 2 are detached in flight accordingly and execute body 1, and power supply line pin and box sub and signal wire pin and box sub can also be torn open accordingly
From；After 34 length of drawstring to be released makes the wheel 22 of car body 2 be supported in ground, stops lifting motor 31 and rotate forward；Mesh
Scalar multiplication visitor enters in car body 2, alternatively, the passenger in car body 2 leaves car body 2, the program of upper and lower passenger can be completed；Driver behaviour
Control lifting device control system rotates backward lifting motor 31, and the drawstring of release 34 is wound on winding roller 33；It rises
Band 2 relative flight of motor vehicles bodies while winding drawstring 34 of falling unit 3 executes the movement of body 1, and car body 2 butts up against flight accordingly and holds
Row body 1, power supply line pin and box sub and signal wire pin and box sub can also dock accordingly；Driver opens flight control system,
And the propeller 43 for controlling eight screws 4 is rotated and is flown in aerial；After land and air double-used aircraft leaves ground, drive
Person controls eight landing gears 5 by flight control system, and the opposite protection wing plate 14 of shock-absorbing support frame 51 is folded.
It should be noted that：The implementation steps of above-mentioned three kinds of forms are mounted on car body 2 with power supply 213 and lifting device 3
The technical solution that upper and each control system is controlled by way of having line traffic control is to illustrate basis.In other embodiment party
In formula, which can also be mounted on flight and execute on body 1, and flies to execute and be equipped with another power supply on body 1, separately
One power supply is electrically connected in lifting device 3, screw 4 and landing gear 5.The each control system being mounted on car body 2
System is incorporated into car body 2 and controls lifting device 3, screw 4 and landing when flight executes body 1 by way of having line traffic control
Device 5；The each control system being mounted on car body 2 is detached in when flight executes body 1 by way of wireless control in car body 2
Control lifting device 3, screw 4 and landing gear 5.Concrete operation step can refer to aforesaid operations step.
When lifting device 3 is mounted on flight execution body 1, lifting device 3 includes the lifting motor for being installed on flight and executing body 1
31, it is connected to the winding roller 33 of motor output shaft 32, the drawstring 34 of winding roller 33 is wound in, is bundled in the suspension hook 35 of drawstring 34.
The bearing seat 211 of car body 2 is equipped with the hanging ring 16 to be connected suspension hook 35.
Another power supply be mounted on flight execute body 1 when, another power electric connection in lifting device 3, screw 4 and
Land device 5.When land and air double-used aircraft needs passenger up and down, driver can not close flight control system, and pass through nothing
The mode of line traffic control controls flight and executes body 1.The flight, which executes body 1, can not be unfolded shock-absorbing support frame 51, be controlled by flight
Flight is executed the hovering of body 1 in the air by system, and car body 2 is transferred by lifting device 3 with respect to ground, is supported in car body 2
When ground, passenger can leave car body 2, and car body 2, which is risen with respect to ground by lifting device 3 again and butts up against flight, executes body 1,
Flight executes body 1 and is flown again in aerial at this time.
Embodiment two
Refering to fig. 11, it is on car body 20 wheel not to be installed in place of the difference of the present embodiment two and embodiment one.At this point, the car body
20 can be understood as a driving cabin.The car body 20 without want isolated operation in road surface.
Finally it should be noted that：Above embodiments are only to illustrate the present invention and not limit technology described in the invention
Scheme；Therefore, although this specification is referring to the above embodiments, the present invention has been described in detail, this field
It is to be appreciated by one skilled in the art that still can modify to the present invention or equivalent replacement；And all do not depart from the present invention
Spirit and scope technical solution and its improvement, should all cover within the scope of the claims of the present invention.
Claims (10)
1. a kind of land and air double-used aircraft, it is characterised in that：Execute body including flight, the car body that dock of body can be executed with flight and
To the lifting device that car body relative flight execution body is drawn high or put down；It includes screw and vehicle that the flight, which executes body,
The cover of car body is covered after body docking；The car body includes taking cabin, being installed on the wheel taken in cabin；The passenger compartment
Flight control system, car body operation control system and lifting device control system are provided on body.
2. land and air double-used aircraft according to claim 1, it is characterised in that：It further includes main body that the flight, which executes body,
Portion, several screws are distributed in the periphery of main part, and the cover is fixedly connected on main part and is located at main part
Upside.
3. land and air double-used aircraft according to claim 2, it is characterised in that：The screw includes being fixedly connected on
The cantilever of main part, the screw motor being installed on cantilever, the propeller for being connected to screw motor；The screw motor is controlled by
Flight control system.
4. land and air double-used aircraft according to claim 3, it is characterised in that：The edge of the main part extends to the periphery
The protection wing plate for surrounding several screws is constituted, the protection wing plate offers several air guides for respectively corresponding several propellers
Channel；The propeller is inserted into air guide channel, and the diameter of the air guide channel is greater than the length of propeller.
5. land and air double-used aircraft according to claim 4, it is characterised in that：Several use are installed on the protection wing plate
To cooperate land and air double-used aircraft to land and the landing gear on ground can be supported in；The landing gear includes rotatably connecting
The driving machine for being connected to the shock-absorbing support frame of protection wing plate, pushing the relatively described protection wing plate expansion of the shock-absorbing support frame or folding
Structure；The driving mechanism is controlled by flight control system.
6. land and air double-used aircraft according to claim 5, it is characterised in that：The shock-absorbing support frame is supported in ground
One end is equipped with wheel.
7. land and air double-used aircraft as claimed in any of claims 1 to 6, it is characterised in that：The lifting device
Including being installed on the lifting motor of the car body, the winding roller for being connected to motor output shaft, the drawstring for being wound in winding roller, binding
In the suspension hook of drawstring；The flight executes body equipped with the hanging ring to be connected suspension hook；
Alternatively, the lifting device include be installed on it is described flight execute body lifting motor, be connected to motor output shaft around
Line roller, the drawstring for being wound in winding roller, the suspension hook for being bundled in drawstring；The car body is equipped with the hanging ring to be connected suspension hook.
8. land and air double-used aircraft according to claim 7, it is characterised in that：Land and air double-used aircraft further includes to incite somebody to action
Car body is fixed on the fixation device that flight executes body.
9. land and air double-used aircraft according to claim 8, it is characterised in that：The fixed device includes being installed on car body
On pin shaft and be opened in flight and execute and accommodate the flexible pin hole of pin shaft on body.
10. land and air double-used aircraft according to claim 7, it is characterised in that：The seating cabin includes to install
The bearing seat of seat, the bearing seat are in open design, and the pedestal portion of the seat protrudes from bearing seat；The car body butts up against
When flight executes body, the pedestal portion of seat is inserted into the cover.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810990200.4A CN108859640B (en) | 2018-08-28 | 2018-08-28 | Air-ground dual-purpose aircraft |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810990200.4A CN108859640B (en) | 2018-08-28 | 2018-08-28 | Air-ground dual-purpose aircraft |
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| CN108859640B CN108859640B (en) | 2024-02-27 |
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| CN201810990200.4A Active CN108859640B (en) | 2018-08-28 | 2018-08-28 | Air-ground dual-purpose aircraft |
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| CN110303843A (en) * | 2019-06-28 | 2019-10-08 | 长城汽车股份有限公司 | Operation method and device for flight vehicle |
| CN110303839A (en) * | 2019-06-28 | 2019-10-08 | 长城汽车股份有限公司 | Operation method and device for flight vehicle |
| CN110303842A (en) * | 2019-06-28 | 2019-10-08 | 长城汽车股份有限公司 | Operation method and device for flight vehicle |
| CN110303841A (en) * | 2019-06-28 | 2019-10-08 | 长城汽车股份有限公司 | Operation method and device for flight vehicle |
| CN110303838A (en) * | 2019-06-28 | 2019-10-08 | 长城汽车股份有限公司 | Operation method and device for flight vehicle |
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|---|---|
| CN108859640B (en) | 2024-02-27 |
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