A kind of electric automobile electric power system
Technical field
The invention belongs to electric automobile corollary system field, and in particular to a kind of electric automobile electric power system.
Background technology
With the popularization of electric automobile, the problem of charging electric vehicle is inconvenient is also increasingly highlighted;Electric automobile is bought at present
User be typically limited to only that city is on and off duty to be used, it is necessary to which outgoing user then still tends to use fuel oil at a distance for a long time
Car.And even city short distance is travelled, user is also required to note very much the dump energy of electric automobile, otherwise easily occurs on the way
Situation about being cast anchor without electricity.And the scheme in roadside setting charging equipment that similar two-wheeled battery truck is taken, for electric automobile
Speech is not just most suitable, and the floor space of one side electric automobile is big many with respect to the battery truck of two-wheeled, and stopping a train at a target point fills
Electricity is likely to result in traffic congestion, on the other hand, the big many of battery truck of the electric automobile power consumption also than two-wheeled, in current battery charging
In the case that technology is without significantly breaking through, the time that midway stopping for charging expends is also long.
The content of the invention
The technical problems to be solved by the invention are:In view of the deficienciess of the prior art, provide a kind of charging conveniently, and
The electric automobile electric power system of user hours underway is not delayed.
To realize the purpose of the present invention, it is achieved using following technical scheme:A kind of electric automobile electric power system, including
There are the multiple power transmission rods for being fixedly mounted on both sides of the road, the transmission guide rail between each power transmission rod rolls or slided peace
The guide rail car electrically connected on the transmission guide rail and with transmission guide rail, can be rested on electric automobile and and electric automobile
The aircraft of electrical connection, and be connected between guide rail car and aircraft electric energy is transferred into electronic vapour from transmission guide rail
Wire on car.
Preferably:Two groups are at least connected between two groups of transmission guide rails of both sides of the road to change for guide rail car
To commutation guide rail;
The transmission guide rail, commutation guide rail include two tracks be arrangeding in parallel respectively, and each track at least includes one
For guiding vertical plate portion and be integrally attached to the horizontal plate part of vertical plate portion lower end, the horizontal plate part between two tracks
It is oppositely arranged.
Preferably:The guide rail car includes sweep, and is fixedly connected on the lower sweep below sweep;
The upper sweep upper left side front and rear portions are installed with two the first motors, and the upper upper right side front and rear portions of sweep are provided with two
Individual the second motor that can be moved along guide rail car left and right directions;First motor, the second motor lower end have been respectively fixedly connected with
The driving wheel being connected is rolled with both sides transmission guide rail;
The bar shaped perforation slided for the second motor is formed on the upper sweep along upper sweep left and right directions;Pacify on the upper sweep
Equipped with to drive the second motor close to the pushing meanss of transmission guide rail;
The pushing meanss include being fixedly connected on the sliding seat of the upper both sides of perforating in bar shaped of sweep, are slidably connected at slip
In seat and horizontally disposed sliding bar, and it is set in the socket being fixedly connected on the outside of the second motor and with two sliding bar one end
Part;Compression spring is installed between the sliding bar and sliding seat;
The lower sweep both sides are connected with by axis of rotation and roll the roller that electrically connect with transmission guide rail so that the rotating shaft and
The transmission guide rail electrical connection of homonymy.
Preferably:Guide rail car bottom surface intermediary form has mounting seat, and the mounting seat bottom forms coiling
Disk mounting groove, the wire spool mounting groove intermediary form has is rotatably connected to wire spool in rotating shaft, the rotating shaft;
Axially disposed turn for having two electrodes a, two electrode a respectively with lower sweep both sides in the rotating shaft of non-conducting material
Axle is electrically connected;The wire spool intermediary form has roll;The roll intermediary form has rotating shaft interface, the wire spool
Rotated and be set on the outside of rotating shaft by rotating shaft interface;It is provided with and is slided respectively with two electrode a on the rotating shaft interface inwall
Two electrode b of dynamic electrical connection;The Wire-wound is in the wire spool, and one end of wire and two electrode b electricity
Connection;
4th motor is installed in the mounting seat;It is provided with and is connected with the output shaft of the 4th motor in the wire spool mounting groove
Drive gear;The driven internal gear with drive gear engaged transmission is formed on the wire spool;
The wire spool installs groove sidewall and forms the retractable cable mouthful passed through for wire.
Preferably:The aircraft includes main part, and the fan that the main part includes tubular is installed
Portion, is connected to the connecting tube of fan installation portion periphery and four equidistant arrangements being connected with fan installation portion, and is connected to
Each connecting tube outer end and with correspondence position connecting tube is connected goes out vane;
It is located to be connected with upper bracket, the upper bracket above connecting tube in the fan installation portion and driving wind is installed
Fan;It is located to be connected with lower carriage, the lower carriage below connecting tube in the fan installation portion and lower driving fan is installed;
It is described it is upper driving fan with it is lower driving fan steering on the contrary, and installed in the fan installation portion drive fan section it is interior
Footpath is more than in the internal diameter of driving fan section under the interior installation of fan installation portion, the fan installation portion drives fan with positioned at upper
Drive the blast superatmospheric between fan so that go out and blast is formed in vane;
It is described go out vane include the vane upper shell and vane lower house being tightly connected, the vane lower house inner circumferential upper end into
Type has interior curved wall, and the inner circumferential of the interior curved wall is connected with an air outlet guard board, air outlet guard board upper end and wind by multiple dowels
Ring upper shell inner circumferential lower end is tightly connected;Air-out gap wide at the top and narrow at the bottom, air-out are formed between the interior curved wall and air outlet guard board
The bottom width in gap is 0.8-1.5mm;The lower section that the inner circumferential of the vane lower house is located at air-out gap is wide at the top and narrow at the bottom
Training wall, the cone angle size of the taper surface is 20-30 degree;
The axial direction of the vane and the radial direction of fan installation portion are perpendicular, and go out to form 5- between the axial direction of vane and horizontal direction
20 degree of angle, and go out the rotation side of horizontal wind-force and the fan blade of upper driving fan that the wind of the air-out gap blowout of vane is produced
To opposite;
It is provided with to adjust the adjusting part that correspondence position goes out vane air-out speed, the regulation group in each described connecting tube
Part includes the 3rd motor, the coaxially connected screw rod with the 3rd motor output shaft, and the valve plate being connected with screw flight;It is described
Valve plate upper periphery, which is pressed close to, connects inside pipe wall, and valve plate lower end is located at the medium position of above-below direction in connecting tube;The connecting tube
Internal upper part forms to install the 3rd motor mounting plate of the 3rd motor, and the 3rd motor mounting plate direction goes out vane
Side be connected with the valve plate guide rod being slidably connected with the valve plate;Bottom is connected with upper end towards going out in the connecting tube
The inclined baffle plate in vane direction, forms the conducting adjustable airway of area between the baffle plate and valve plate;
The upper driving fan, lower driving fan and each the 3rd motor are electrically connected with control board respectively;
The main part is that upper shell and lower house are tightly connected composition;
The main part upper end, which is connected with the air intake cover of a semiellipse spherical shape, air intake cover, uniformly forms entering for strip
Air port.
Preferably:First electromagnet, first electromagnet are installed at the top of the air intake cover of the aircraft
Top camera is installed;
The upper camera and the first electromagnet are electrically connected with control board respectively;
The wire spool mounting groove lower end is fixedly connected with the second cover plate;Second cover plate lower end forms cross positioning mark
Note;The position of the second cover plate lower end correspondence telltale mark is connected with the permanent magnet sucked with the first electromagnet by magnetic force.
Preferably:The lower, outer perimeter of the fan installation portion is charging transmitter module installation portion, charging transmitting mould
The charging transmitter module electrically connected with control board is connected with block installation portion;
The lower carriage bottom of the aircraft is provided with lower camera, and the lower camera is electrically connected with control board;
The electromobile at top is provided with the charging receiving module electrically connected with charging transmitter module.
Preferably:Go out position of the vane inner circumferential away from connecting tube described in each and form Holder joint of rising and falling, each
A undercarriage is respectively connected with the Holder joint of rising and falling;The undercarriage, which includes, to be fixedly connected and passes through with Holder joint of rising and falling
The connection pipe body that Holder joint of rising and falling is connected with going out inside vane, is slidably mounted on the sliding tube in connection pipe body, with connecting tube
Body rotates the support bar of connection close to Holder joint one end of rising and falling, and is connected on support bar away from Holder joint one end of rising and falling to inhale
Tight the second electromagnet in electromobile at top, and the connecting rod being connected respectively with rotation in the middle part of sliding tube middle part, support bar;
The connection pipe body forms hinged seat close to Holder joint one end side wall that rises and falls, and described support bar one end is rotated with hinged seat
Connection;The sliding tube is connected with piston close to Holder joint one end of rising and falling, and the slip pipe outer wall medium position, which is connected with, to be hinged
Head, described connecting rod one end rotates with articulated joint and is connected, and side wall of the connection pipe body away from Holder joint one end of rising and falling forms confession
The strip shape gob that articulated joint is passed through;The one end of the connection pipe body away from Holder joint of rising and falling is fixedly connected with sealing cap, sealing cap
The inner is connected with spring locating rod, the spring locating rod and is arranged with spring, and the both ends of the spring is against piston respectively
And between sealing cap is inner;The connecting rod tank that the connecting rod is accommodated in support bar collapsed state is formed on the support bar;
The support bar is in deployed condition when the spring is in extended configuration, and the upper driving fan is in running order
Afterwards, go out the driving piston of the air pressure in vane makes support bar be in collapsed state together with sliding tube movement.
Preferably:The top for being located at charging transmitter module installation portion on the fan installation portion is a circuit board
Installation cavity, the control board is arranged in circuit board installation cavity, and the circuit board installation cavity lower end is connected with an annular
The first cover plate;The upper surface of the circuit board installation cavity uniformly forms the fresh air inlet connected with fan installation portion, described
The lateral wall of circuit board installation cavity uniformly forms vent.
Compared with prior art, the beneficial effects of the invention are as follows:The present invention on transmission guide rail by travelling and keeping
With the guide rail car of electric automobile identical travel speed, the aircraft being connected with guide rail car wire is coordinated to come to be electronic in traveling
Automobile charges, and realizes electric automobile and coordinates guide rail car to realize without stopping the function that can be charged, and by aircraft
Electric energy on transmission guide rail is transferred on electric automobile, such electric automobile can be at any time in the case of fully charged or other
Depart from aircraft, limitation will not be caused to freely travelling for electric automobile.With existing in the electronic of roof setting pantograph
Bus is compared, and the present invention need to only set a charging receiving module in electromobile at top(Such as the common contact of prior art
Electrode or wireless charging receiving module that formula is electrically connected), the outward appearance of not too large influence electric automobile, and be easy to existing electricity
Electrical automobile is transformed.
Because quantity and travel direction that the electric automobile charged is needed on each section of road are random, therefore
Need to connect at least two groups commutation guide rails between two transmission guide rails of both sides of the road, in order to which guide rail car is from road side
Transmission guide rail is moved on the transmission guide rail of opposite side.
Further, due to there is corner in road in commutation guide rail and transmission guide rail junction, and transmission guide rail
Certainly exist non-directional track(Circular arc is designed as in general such as Fig. 1), therefore the second design of electrical motor of side is on guide rail car
It can be moved along guide rail car left and right directions so that when driving into the track of circular arc the driving wheel of both sides can keep guide rail car
Keep offseting with two siding tracks.
The aircraft passes through the first electromagnet in off working state(Iron core)Suck below the second cover plate forever
On magnet, when aircraft works, the first electromagnet is powered to producing makes aircraft and the second cover plate de- with the reverse magnetic field of permanent magnet
From.
When there is electric automobile to need charging, the 4th motor driving wire spool, which is rotated, releases wire, while aircraft departs from
Guide rail car is simultaneously flown on electric automobile, and aircraft sucks the gold in electromobile at top by the second electromagnet of undercarriage lower end
Belong on car shell.
The aircraft provides driving force, the part that upper driving fan is produced by the upper driving fan in fan installation portion
Air-flow blows out downwards from each air-out gap for going out vane, and combines adjusting part and adjust each to go out vane and go out wind velocity, from
And the horizontal flight or steering of aircraft are realized, due to going out vane positioned at each of aircraft periphery and only play adjustment aircraft
The effect of posture, without the fan for being provided with power, go out not being easily caused when vane and foreign object produce touching aircraft it is out of control or
Injury is produced to human or animal, security is good.The similar four-axle aircraft of aircraft outward appearance, four go out vane and only play regulation appearance
The function of state, therefore the present invention substantially should be single shaft aircraft.
Further, it is described go out vane air-out gap spray air-flow can be along training wall stream according to Coanda principle
It is dynamic, the wind film of a taper is formed, and the wind film of taper can drive out the air of vane inner circumferential to flow downward in the lump, so fly
When the part in air-out gap is stopped in row device flight course, the overall airflow influence that air-out gap is formed is small, is conducive to flying
The stabilization of row device flight attitude.
Further, the axial direction of the vane and the radial direction of fan installation portion are perpendicular, and go out axial direction and the level of vane
The angle of 5-20 degree is formed between direction, and goes out horizontal wind-force and upper driving fan that the wind of the air-out gap blowout of vane is produced
Fan blade rotation direction it is opposite.Pass through such design so that the wind energy for going out the air-out gap blowout of vane enough offsets drive
Dynamic fan, or the reaction force produced when upper driving fan and the rotation of lower driving fan;Also, adjusted by adjusting each simultaneously
Component change vane go out wind velocity, the overall forward or reverse of aircraft can be achieved.Adjusted by adjusting one or two
Section component makes what one or two went out vane to go out wind velocity, and aircraft can be achieved generally in heeling condition, can so drive
Aircraft flies in the horizontal direction.
The undercarriage is packed up or deployed as the rising of aircraft, drop are corresponding, when aircraft is in state of flight, is gone out
Blast in vane makes piston be moved together with sliding tube to sealing cap one end, so that sliding tube drivening rod one end is to sealing cap
Direction is moved, so that support bar lower end is also rotated to sealing cap one end, so that undercarriage is in collapsed state.Work as aircraft
During landing, the blast gone out in vane reduces, and Spring driving sliding tube is moved together with piston toward hinged seat direction, so that sliding tube
Drivening rod one end is moved to hinged seat direction, so that support bar lower end turns to extreme position to hinged seat one end, so that
Undercarriage is set to be in deployed condition.
The strip shape gob plays a part of articulated joint on limit slippage pipe, and the position of strip shape gob end just causes spring to stretch
After length, support bar turn to it is vertical with horizontal direction after be rotated further 3-10 degree so that aircraft landing after, each support bar is equal
In stable state.
Brief description of the drawings
Fig. 1 is the structural representation of the present invention.
Fig. 2, Fig. 3 are the structural representations of aircraft and guide rail car.
Fig. 4, Fig. 5 are the structural representations of guide rail car.
Fig. 6 is the explosive view of guide rail car.
Fig. 7 is the structural representation of lower sweep and each part on lower sweep.
Fig. 8 is the structural representation of wire spool.
Fig. 9 is the structural representation of aircraft stopped status.
Figure 10 is the structural representation of aircraft flight state.
Figure 11 is the cross section structure diagram of aircraft.
Figure 12 is Figure 11 A portions schematic enlarged-scale view.
Figure 13 is Figure 11 B portions schematic enlarged-scale view.
The structural representation of each part that Figure 14 is upper shell and is connected with upper shell.
Figure 15 is the structural representation of lower housing section.
Figure 16 is the cross section structure diagram of lower housing section.
Figure 17 is the structural representation of air intake cover.
Figure 18 is the decomposition texture schematic diagram of undercarriage part.
Figure 19 is the cross section structure diagram of undercarriage part.
1st, power transmission rod;2nd, transmission guide rail;3rd, commutate guide rail;4th, guide rail car;5th, wire;9th, aircraft;41st, upper sweep;
411st, bar shaped is perforated;412nd, driving wheel;414th, the first motor;415th, the second motor;416th, Coupling;417th, sliding seat;418、
Sliding bar;42nd, lower sweep;422nd, roller;423rd, mounting seat;4231st, retractable cable mouthful;424th, the 4th motor;425th, wire spool is pacified
Tankage;426th, rotating shaft;427th, drive gear;43rd, wire spool;433rd, roll;435th, driven internal gear;437th, rotating shaft grafting
Mouthful;44th, the second cover plate;441st, telltale mark;91st, main part;91a, upper shell;91b, lower house;910th, fan installation portion;
9101st, upper bracket;9102nd, lower carriage;9103rd, charge transmitter module installation portion;9104th, circuit board installation cavity;9105th, air intake
Hole;9106th, vent;9107th, lower camera;911st, vane is gone out;9110th, rise and fall Holder joint;9111st, vane upper shell;9112、
Vane lower house;91121st, interior curved wall;91122nd, dowel;91123rd, air outlet guard board;91124th, training wall;912nd, connecting tube;
9121st, the 3rd motor mounting plate;9122nd, valve plate guide rod;9123rd, baffle plate;913rd, the first cover plate;92nd, charge transmitter module;93、
Undercarriage;931st, connection pipe body;9311st, hinged seat;9312nd, strip shape gob;932nd, sliding tube;9321st, piston;9322nd, articulated joint;
933rd, sealing cap;9331st, spring locating rod;934th, connecting rod;935th, support bar;9351st, connecting rod tank;936th, the second electromagnet;
937th, spring;94th, air intake cover;941st, the first electromagnet;942nd, upper camera;951st, upper driving fan;952nd, lower driving fan;
96th, adjusting part;961st, the 3rd motor;962nd, screw rod;963rd, valve plate;97th, control board.
Embodiment
Embodiment 1
According to Fig. 1 to Figure 17, the present embodiment is a kind of electric automobile electric power system, includes and is fixedly mounted on both sides of the road
Multiple power transmission rods 1, the transmission guide rail 2 between each power transmission rod rolled or is slidably mounted on the transmission guide rail
And the guide rail car 4 electrically connected with transmission guide rail, the aircraft 9 that can be rested on electric automobile and be electrically connected with electric automobile,
And be connected between guide rail car and aircraft to the wire 5 that is transferred to electric energy from transmission guide rail on electric automobile.
Two groups are at least connected between two groups of transmission guide rails of both sides of the road is used for the commutation guide rail that guide rail car commutates
3;The transmission guide rail, commutation guide rail include two tracks be arrangeding in parallel respectively, and each track at least includes a use
In guiding vertical plate portion and be integrally attached to the horizontal plate part of vertical plate portion lower end, the horizontal plate part phase between two tracks
To setting.
The guide rail car includes sweep 41, and is fixedly connected on the lower sweep 42 below sweep;It is described to get on the bus
Plate upper left side front and rear portions are installed with two the first motors 414, and the upper upper right side front and rear portions of sweep are provided with two energy
Enough the second motors 415 moved along guide rail car left and right directions;First motor, the second motor lower end be respectively fixedly connected with
Both sides transmission guide rail rolls the driving wheel 412 of connection.
The bar shaped perforation 411 slided for the second motor 415 is formed on the upper sweep along upper sweep left and right directions;It is described
The pushing meanss for driving the second motor close to transmission guide rail are installed on upper sweep.
The pushing meanss include being fixedly connected on the sliding seat 417 of the upper both sides of perforating in bar shaped of sweep, the company of slip
It is connected in sliding seat and horizontally disposed sliding bar 418, and is set on the outside of the second motor and solid with two sliding bar one end
Surely the Coupling 416 connected;Compression spring is installed between the sliding bar and sliding seat.
The lower sweep both sides are connected with by axis of rotation and roll the roller 422 electrically connected with transmission guide rail so that institute
Rotating shaft is stated to electrically connect with the transmission guide rail of homonymy.The lower sweep is being at least non-conductive material with the link position of rotating shaft
Material.
The driving wheel coordinates to roll with the vertical plate portion of the track to be connected, the horizontal plate part of the roller then with track
Rolling is electrically connected, and the roller is metal wheel, and each side of lower sweep sets 2-3 roller, is so on the one hand beneficial to guide rail car
Steady traveling on transmission guide rail, on the other hand ensure that good between roller and transmission guide rail electrically connect.Further
Say, can be connected between roller and rotating shaft by bearing, then also form Electricity Federation between metal material inner ring, outer ring and the ball of bearing
Connect, and there is lubricant medium between ball and inner ring, outer ring and be likely to result in larger resistance, therefore guide rail car passes through 2-3 per side
Roller is rolled with transmission guide rail and is connected, and ensure that the continuity transmitted electricity between guide rail car and transmission guide rail, it is ensured that stable electricity
Pressure, electric current.
Because quantity and travel direction that the electric automobile charged is needed on each section of road are random, therefore
Need to connect at least two groups commutation guide rails between two transmission guide rails of both sides of the road, in order to which guide rail car is from road side
Transmission guide rail is moved on the transmission guide rail of opposite side.
Further, due to there is corner in road in commutation guide rail and transmission guide rail junction, and transmission guide rail
Certainly exist non-directional track(Circular arc is designed as in general such as Fig. 1), therefore the second design of electrical motor of side is on guide rail car
It can be moved along guide rail car left and right directions so that when driving into the track of circular arc the driving wheel of both sides can keep guide rail car
Keep offseting with two siding tracks.
Guide rail car bottom surface intermediary form has mounting seat 423, and the mounting seat bottom forms wire spool mounting groove
425, the wire spool mounting groove intermediary form has is rotatably connected to wire spool 43 in rotating shaft 426, the rotating shaft;Non-conducting material
The rotating shaft on axially disposed there are two rotating shafts of electrode a, two electrode a respectively with lower sweep both sides to electrically connect;It is described
Wire spool intermediary form has roll 433;The roll intermediary form has rotating shaft interface 437, and the wire spool is by turning
Axle interface, which is rotated, to be set on the outside of rotating shaft;It is provided with to slide with two electrode a respectively on the rotating shaft interface inwall and is electrically connected
The two electrode b connect;The Wire-wound is in the wire spool, and one end of wire is electrically connected with two electrode b;Institute
State and the 4th motor 424 is installed in mounting seat;It is provided with what is be connected with the output shaft of the 4th motor in the wire spool mounting groove
Drive gear 427;The driven internal gear 435 with drive gear engaged transmission is formed on the wire spool;The wire spool peace
Dress groove sidewall forms the retractable cable mouthful 4231 passed through for wire.
The controller electrically connected with the first motor, the second motor, the 4th motor is installed, controller leads on the guide rail car
Wireless network and server are crossed, and the control system of electric automobile is communicated, and charging is needed when server receives electric automobile
Request when, the controller of the guide rail car of server controls nearby communicates with the electric automobile of request charging;Then guide rail car control
Aircraft processed is flown on electric automobile to charge to electric automobile.
In the guide rail car working condition, wire spool releases wire under the driving of the 4th motor, enables aircraft
Fly on electric automobile to be charged;Wire spool is rolled wire by the driving of the 4th motor in guide rail car off working state, is kept away
Exempt from that vehicular traffic is caused to hinder.
The aircraft includes main part 91, and the main part includes the fan installation portion 910 of tubular, is connected to
Fan installation portion periphery and the connecting tube 912 for four equidistant arrangements being connected with fan installation portion, and it is connected to each company
That takes over outer end and be connected with correspondence position connecting tube goes out vane 911.
It is located to be connected with upper bracket 9101, the upper bracket above connecting tube in the fan installation portion and is provided with
Drive fan 951;It is located to be connected with lower carriage 9102, the lower carriage below connecting tube in the fan installation portion and installs
There is lower driving fan 952;The upper driving fan is with the lower steering for driving fan on the contrary, and being installed in the fan installation portion
The internal diameter of fan section is driven to be more than position in the internal diameter for installing lower driving fan section in fan installation portion, the fan installation portion
Blast superatmospheric between upper driving fan and lower driving fan so that go out and blast is formed in vane.
It is described go out vane include the vane upper shell 9111 and vane lower house 9112 being tightly connected, the vane lower casing
Internal Zhou Shangduan forms interior curved wall, and the inner circumferential of the interior curved wall is connected with an air outlet guard board by multiple dowels 91122,
Air outlet guard board upper end is tightly connected with vane upper shell inner circumferential lower end;Shape between the interior curved wall 91121 and air outlet guard board 91123
Into air-out gap wide at the top and narrow at the bottom, the bottom width in air-out gap is 0.8-1.5mm;The inner circumferential of the vane lower house is located at
The lower section in air-out gap is training wall 91124 wide at the top and narrow at the bottom, and the cone angle size of the taper surface is 20-30 degree.
The axial direction of the vane and the radial direction of fan installation portion are perpendicular, and go out shape between the axial direction of vane and horizontal direction
Into the angle of 5-20 degree, and go out turn of horizontal wind-force and the fan blade of upper driving fan that the wind of the air-out gap blowout of vane is produced
It is dynamic in opposite direction.
It is provided with to adjust the adjusting part 96 that correspondence position goes out vane air-out speed in each described connecting tube, it is described
Adjusting part includes the 3rd motor 961, the coaxially connected screw rod 962 with the 3rd motor output shaft, and connects with screw flight
The valve plate 963 connect;The valve plate upper periphery, which is pressed close to, connects inside pipe wall, and valve plate lower end is located at the middle part of above-below direction in connecting tube
Position;The connecting tube internal upper part forms to install the 3rd motor mounting plate of the 3rd motor, the 3rd motor
Installing plate 9121 is connected with the valve plate guide rod 9122 being slidably connected with the valve plate towards the side for going out vane;In the connecting tube
Bottom is connected with a upper end towards the inclined baffle plate 9123 in vane direction is gone out, and conducting area is formed between the baffle plate and valve plate
Adjustable airway.
The upper driving fan, lower driving fan and each the 3rd motor are electrically connected with control board 97 respectively.
The main part is that upper shell 91a and lower house 91b is tightly connected composition.
The main part upper end is connected with the air intake cover 94 of a semiellipse spherical shape, air intake cover and uniformly forms bar
The air inlet of shape.
Aircraft provides driving force, upper driving fan production by the upper driving fan in fan installation portion, lower driving fan
Raw fraction is blown out downwards from each air-out gap for going out vane, and combines the air-out that adjusting part adjustment each goes out vane
Speed, so as to realize the horizontal flight or steering of aircraft, due to going out vane positioned at each of aircraft periphery and only play tune
The effect of whole attitude of flight vehicle, without the fan for being provided with power, goes out when vane produces touching with foreign object and is not easily caused aircraft
Out of control or produce injury to human or animal, security is good.The similar four-axle aircraft of aircraft outward appearance, therefore with four-axle aircraft
It is named, four go out the function that vane i.e. so-called " four axles " only plays regulation posture, therefore this aircraft substantially should be single shaft
Aircraft.
Further, it is described go out vane air-out gap spray air-flow can be along training wall stream according to Coanda principle
It is dynamic, the wind film of a taper is formed, and the wind film of taper can drive out the air of vane inner circumferential to flow downward in the lump, so fly
When the part in air-out gap is stopped in row device flight course, the overall airflow influence that air-out gap is formed is small, is conducive to flying
The stabilization of row device flight attitude.
Further, the axial direction of the vane and the radial direction of fan installation portion are perpendicular, and go out axial direction and the level of vane
The angle of 5-20 degree is formed between direction, and goes out horizontal wind-force and upper driving fan that the wind of the air-out gap blowout of vane is produced
Fan blade rotation direction it is opposite.Pass through such design so that the wind energy for going out the air-out gap blowout of vane enough offsets drive
The reaction force produced when dynamic fan and the rotation of lower driving fan;Also, change air-out by adjusting each adjusting part simultaneously
Ring goes out wind velocity, and the overall forward or reverse of aircraft can be achieved.Make one by adjusting one or two adjusting part
Or two go out vane go out wind velocity, aircraft can be achieved generally in heeling condition, aircraft can be so driven in level
Fly in direction.
First electromagnet 941 is installed, the top of first electromagnet is installed at the top of the air intake cover of the aircraft
There is upper camera 942;The upper camera and the first electromagnet are electrically connected with control board respectively;The wire spool is installed
Groove lower end is fixedly connected with the second cover plate 44;Second cover plate lower end forms cross telltale mark 441;Second cover plate
The position of lower end correspondence telltale mark is connected with the permanent magnet sucked with the first electromagnet by magnetic force.
The aircraft passes through the first electromagnet in off working state(Iron core)Suck below the second cover plate forever
On magnet, when aircraft works, the first electromagnet is powered to producing makes aircraft and the second cover plate de- with the reverse magnetic field of permanent magnet
From.The upper camera is used for the position for judging aircraft opposite rail car, in order to which aircraft can be by accurately resting in
On guide rail car.The upper camera shoots the position for obtaining aircraft opposite rail car, can be by manually operating remote control to fly
Device is accommodated on corresponding guide rail car by the first electromagnet, can also be automatically accommodated to by aircraft by machine vision technique
On corresponding guide rail car.
The lower, outer perimeter of the fan installation portion is on charging transmitter module installation portion 9103, charging transmitter module installation portion
It is connected with the charging transmitter module 92 electrically connected with control board;The lower carriage bottom of the aircraft is provided with lower camera
9107, the lower camera is electrically connected with control board;The electromobile at top is provided with to be electrically connected with charging transmitter module
The charging receiving module connect.
Described charging transmitter module, charging receiving module can be the electrodes of contact or by wireless charging
Power technology carries out the coil of power transmission.
The top for being located at charging transmitter module installation portion on the fan installation portion is a circuit board installation cavity 9104, institute
Control board is stated in circuit board installation cavity, the circuit board installation cavity lower end is connected with a first annular cover plate
913;The upper surface of the circuit board installation cavity uniformly forms the fresh air inlet 9105 connected with fan installation portion, the circuit
The lateral wall of plate installation cavity uniformly forms vent 9106.
A small amount of air-flow of the fan installation portion enters from fresh air inlet and from vent discharge, plays scattered to control board
Heat effect.
Go out position of the vane inner circumferential away from connecting tube described in each and form Holder joint 9110 of rising and falling, each described undercarriage
A undercarriage 93 is respectively connected with joint;The undercarriage is provided with to suck the second electromagnet in electromobile at top
936。
When there is electric automobile to need charging, the 4th motor driving wire spool, which is rotated, releases wire, while aircraft departs from
Guide rail car is simultaneously flown on electric automobile, and aircraft sucks the gold in electromobile at top by the second electromagnet of undercarriage lower end
Belong on car shell.
Embodiment 2
With reference to Figure 18 to Figure 19, the present embodiment also makes following improvement on the basis of embodiment 1:Go out vane inner circumferential described in each
Holder joint 9110 of rising and falling is formed away from the position of connecting tube, a undercarriage is respectively connected with Holder joint of rising and falling described in each
93;The undercarriage includes the company for being fixedly connected and being connected by Holder joint of rising and falling with going out inside vane with Holder joint of rising and falling
Adapter body 931, is slidably mounted on the sliding tube 932 in connection pipe body, and company is rotated close to Holder joint one end of rising and falling with connection pipe body
The support bar 935 connect, is connected on support bar away from Holder joint one end of rising and falling to suck the second of electromobile at top
Electromagnet 936, and the connecting rod 934 being connected respectively with rotation in the middle part of sliding tube middle part, support bar.
The connection pipe body forms hinged seat 9311, described support bar one end and hinge close to Holder joint one end side wall that rises and falls
Joint chair rotates connection;The sliding tube is connected with position in the middle part of piston 9321, the slip pipe outer wall close to Holder joint one end of rising and falling
Put and be connected with articulated joint 9322, described connecting rod one end rotates with articulated joint and is connected, the connection pipe body is away from Holder joint one of rising and falling
The side wall at end forms the strip shape gob 9312 passed through for articulated joint;The one end of the body of connecting tube 912 away from Holder joint of rising and falling is consolidated
Surely sealing cap 933 is connected with, the inner of sealing cap, which is connected with spring locating rod 9331, the spring locating rod, to be arranged with
Spring 937, the both ends of the spring is against between piston and sealing cap the inner respectively;Form and received in support bar on the support bar
The connecting rod tank 9351 of the connecting rod is accommodated during the state of rising.
The support bar is in deployed condition when the spring is in extended configuration, and the upper driving fan is in work shape
After state, go out the driving piston of the air pressure in vane makes support bar be in collapsed state together with sliding tube movement.
The undercarriage is packed up or deployed as the rising of aircraft, drop are corresponding, when aircraft is in state of flight, is gone out
Blast in vane makes piston be moved together with sliding tube to sealing cap one end, so that sliding tube drivening rod one end is to sealing cap
Direction is moved, so that support bar lower end is also rotated to sealing cap one end, so that undercarriage is in collapsed state.Work as aircraft
During landing, the blast gone out in vane reduces, and Spring driving sliding tube is moved together with piston toward hinged seat direction, so that sliding tube
Drivening rod one end is moved to hinged seat direction, so that support bar lower end turns to extreme position to hinged seat one end, so that
Undercarriage is set to be in deployed condition.
The strip shape gob plays a part of articulated joint on limit slippage pipe, and the position of strip shape gob end just causes spring to stretch
After length, support bar turn to it is vertical with horizontal direction after be rotated further 3-10 degree so that aircraft landing after, each support bar is equal
In stable state.