CN209479339U - A kind of land, water and air three-purpose vehicle - Google Patents
A kind of land, water and air three-purpose vehicle Download PDFInfo
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- CN209479339U CN209479339U CN201920115206.7U CN201920115206U CN209479339U CN 209479339 U CN209479339 U CN 209479339U CN 201920115206 U CN201920115206 U CN 201920115206U CN 209479339 U CN209479339 U CN 209479339U
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Abstract
A kind of land, water and air three-purpose vehicle, control system including body interior, main intracorporal land and water dynamical system, connect the accumulation chamber of control system, the driving of main center and passenger compartment in main body at folding Power System of Flight Vehicle above main body.The advantages of the utility model: taking the vehicles can be achieved with the accessible traveling of sea, land and air, practical and conveniently.Use foldable inclination rotor aircraft can be with VTOL, the adjustable propeller turned to allows to high-speed flight, park or land when driving, the wing of folding undoubtedly reduces occupied area.Wind power generation can also be utilized, cruising ability is improved.
Description
Technical field
The utility model is a kind of novel vehicles, and in particular to a kind of land, water and air three-purpose vehicle.
Background technique
Information and substance are most to be in close contact with us and the thing of tight demand, and nowadays information can accomplish
Light velocity transmission, in this way, matter transportation just becomes a big factors of limitation economic development.
The high speed development in city, causes densely populated, and traffic congestion becomes normality, so the more traffic routes of three-dimensional will be at
For the developing direction of future transportation.Also the multi-functional vehicle that can be flown just is needed.
Either family goes on a tour or for searching and rescuing, is intended to a kind of vehicles that can be adapted for full landform, side
Just and it is practical.
In face of with first-class present problem, land, water and air three-purpose vehicle is undoubtedly a kind of feasible scheme.At present
There are many automobile vendors to issue the triphibian vehicle of many concepts, also some have produced entity, but fail to quantization production, throw
Enter operation.It is due to expensive, the consumer that can be undertaken is less, and course continuation mileage is short, is difficult to meet the problems such as travelling over long distances.
So realization generates electricity when walking, and stopping can also generate electricity equipped with the device using wind power generation.It improves continuous
Navigate mileage, energy conservation and environmental protection.For land and water traveling using multi-purpose blade wheel, a kind of device can satisfy two kinds of functions, reduce costs.
Utility model content
To solve the above problems, the utility model provides a kind of land, water and air three-purpose vehicle.
The technical solution of the utility model is as follows: a kind of land, water and air three-purpose vehicle, which is characterized in that including in main body
Folding Power System of Flight Vehicle above the control system in portion, main body, main intracorporal land and water dynamical system connect control in main body
The accumulation chamber of system processed, the driving of main center and passenger compartment；
The Power System of Flight Vehicle includes right-handed screw paddle two, counterpropeller two, four, aircraft power motor,
Propeller internal frame four, two groups of windmill wings outrigger, decelerating step motor four, transmission gear is multiple, diverter shell four
It is a, rotation axis four；Propeller passes through fixed device and connect with main body, and the pedestal of aircraft power motor is mounted in propeller
On frame, two propeller internal frames are installed on each group of windmill wings outrigger, diverter shell is mounted on propeller outrigger wing
On, propeller outrigger wing group is mounted on body by two rotation axis, and aircraft motor lines and steering motor pass through spiral
Control system and accumulation chamber in equipment are connected internally to by outrigger inside paddle internal frame；
The land and water dynamical system includes 4 identical combination type vane wheels, is arranged in bottom four corners, each combined type
Blade wheel includes tire, wheel hub, turbo blade group, outer universal joint, interior universal joint, outer shaft, inner shaft, power output semiaxis, small-sized
Generator, decelerating step motor, limit adjuster, transmission straight-tooth and mechanical seal group；Two sides are all provided with wheel hub, two wheels in tire
By interior axis connection between hub, turbo blade group is mounted on inside tire and outer wheel hub with rotation axis, and between each other can phase
Mutually without influencing to rotate, the outer shaft at turbo blade group center extends outwardly for outer shaft outer portion, and outer shaft outer portion passes through outer universal joint
Universal joint in connecting, outer shaft are set in inner shaft outer wall, and interior universal joint and the coincidence of the outer universal joint centre of sphere are mutually twisted, and outer shaft is in main body
Inside and outside intersection is equipped with mechanical seal, and the end of inner shaft sets gear three, and the end of outer shaft sets gear five, is also arranged on outer shaft with teeth
Wheel four, gear four are connected to the gear seven on small generator by gear six, the gear five on outer shaft and the gear in inner shaft
Three can engage with the internal gear in transmission shaft respectively, and internal gear can form engaging sleeve with gear three or gear five, and internal gear can
To be slided in transmission shaft certain position, adjusts limiter and be mounted on position limiting structure by two circular cone pressure bearings, wherein adjusting
Limiter is engaged with transmission straight-tooth, and small generator is connected with outer shaft by gear four, gear five, gear six, deceleration stepping electricity
Gear eight is installed, gear eight is engaged with transmission straight-tooth, so that control decelerating step motor can adjust adjusting limit on arbor
The position of position device and small generator；
The accumulation chamber is placed on low bottom-disc, so that center of gravity declines, improves stability, the accumulation chamber includes power electric
Pond group, energy-storage battery, fuel tank, that is to say, that the utility model can be used as the vehicles of hybrid power；
The driving and passenger compartment are located at the middle position of equipment, have larger space.
Right-handed screw paddle and counterpropeller during installation, the corresponding identical propeller of diagonally opposing corner on propeller outrigger wing,
Right-handed screw paddle and counterpropeller center of rotation apart from aircraft centre distance as, it is such symmetrical to make propeller
Countertorque when rotation cancels each other out.
Diverter interior of shell is equipped with decelerating step motor, and gear one, spiral shell are equipped on decelerating step motor output shaft
The axis for revolving paddle internal frame two sides is longer, is stretched out by the circular hole of windmill wings outrigger, is equipped with bearing, bearing extension at circular hole
The axis divided is equipped with transmission gear two, and engages with the gear one on decelerating motor, and diverter shell is mounted on windmill wings
On outrigger.In this way, drop propeller internal frame can be driven to rotate in the axial direction by the rotation of decelerating motor, pass through control system
The angle of propeller Yu aircraft power motor part can be reconciled by reconciling decelerating step motor one, to meet adjustment propeller
Direction.
The folding and stretching, extension of the rotor part of aircraft fully rely on propeller power drive, this special construction of design
It can guarantee that windmill wings outrigger is rotated in folding straight down in the range of this 90 ° are unfolded horizontally outward, air-flow is to spiral shell
The active force for revolving paddle is vertical with the plane of propeller always, and outward.
Section is protrusion above middle section when the windmill wings outrigger is unfolded, and what is fallen in below is streamlined
Structure has imitated the wing of bird, according to bernoulli principle, when rapid flight, above gas flow rate it is big, below gas flow rate it is small,
Upper and lower surface forms pressure difference, and gas upwards pressure to wing generation, and upward lift is provided for aircraft.
Inner shaft connects inner shaft extension rod, and inner shaft extension rod passes through interior universal axis connection inner shaft connecting rod.Outer shaft connects outer shaft extension
Bar, outer shaft extension rod pass through outer universal axis connection outer shaft connecting rod.
The turbo blade group is that multiple groups turbine leaf fan is mounted side by side together, and turbine leaf fan outside is blade reinforcing ring,
Working efficiency can be improved, enhance power.
It uses principle: when flight, using the foldable inclination rotor aircraft of quadrotor, aircraft can be adjusted with VTOL
The direction of propeller allows to high-speed flight.Land when driving, controls the line shaft exported through differential mechanism and transmits power to
Inner shaft, inner shaft are connected by interior universal joint with tire, outer wheel hub, thus can be by power direct-drive to outer wheel hub and tire
On, control tire and outer wheel hub rotate, and equipment moves forward.In water when driving, control line shaft transmits power on outer shaft,
Outer shaft is connect by outer universal joint with turbo blade group, in this way, just transmitting power in turbo blade group, controls turbo blade
Rotation, equipment laterally travel.And when propeller blade and turbo blade group do not work, it can use wind power generation, it will be electric
It can be stored in battery pack.
The advantages of the utility model: taking the vehicles can be achieved with the accessible traveling of sea, land and air, practical and conveniently.
Use foldable inclination rotor aircraft can be with VTOL, the adjustable propeller turned to allows to high-speed flight, park or
When driving, the wing of folding undoubtedly reduces occupied area on person land.Wind power generation can also be utilized, cruising ability is improved.
A kind of following vehicles of individual are particularly suitable for application as, landform is ignored and goes directly to destination, and do not have flight locations
Limitation, energy conservation, environmental protection.Future may become the first-selected instrument gone on a tour.Accumulation chamber includes power battery pack, energy-storage battery,
Fuel tank, that is to say, that the utility model can be used as the vehicles of hybrid power.Driving and passenger compartment are located at the centre of equipment
Position has larger space.
Detailed description of the invention
Attached drawing is to be used to provide a further understanding of the present invention, and constitute part of specification, and following
Specific embodiment be used to explain the utility model together, but do not constitute limitations of the present invention,
In the accompanying drawings:
When Fig. 1 is the expansion of the utility model wing, i.e. the state of VTOL；
When Fig. 2 is the utility model wing-folding, i.e. the state of water, land when driving；
State when Fig. 3 is the utility model high-speed flight after propeller turning direction；
Fig. 4 is the propeller internal frame of the utility model Power System of Flight Vehicle；
Fig. 5 is the windmill wings outrigger of the utility model Power System of Flight Vehicle；
Fig. 6 is the utility model aircraft section schematic diagram；
Fig. 7 is the utility model aircraft section partial enlarged view；
Fig. 8 is the utility model diverter partial enlarged view；
Schematic diagram when Fig. 9 is the expansion of the utility model propeller；
Figure 10 is the utility model wing-folding schematic diagram；
Figure 11 is that the utility model wing-folding is partial sectional view；
Figure 12 is the utility model propeller turning direction structure chart；
Figure 13 is the utility model land and water dynamical system partial enlarged view；
Figure 14 is that the utility model land and water dynamical system locally splits structure chart；
Figure 15 is the blade-section structure chart of the utility model turbo blade group；
Figure 16 is the utility model land and water switching mechanism broken away view；
Figure 17 is that the utility model adjusts limiter；
Figure 18 is the utility model land and water dynamical system partial enlarged view；
Figure 19 is the local structural graph of the utility model land when driving；
Figure 20 is the local structural graph of the utility model in water when driving.
In figure:
Power System of Flight Vehicle 100
110 propeller 120 of aircraft power motor
130 windmill wings outrigger 140 of propeller internal frame
Diverter 150
151 decelerating step motor 1 of diverter shell
One 153 transmission gear 2 154 of gear
Body 160
Land and water dynamical system 200
Combination type vane wheel 210
211 tire 212 of outer wheel hub
Blade reinforcing ring 213
Universal joint 220
Universal joint 222 in outer universal joint 221
Inner shaft 230
231 inner shaft connecting rod 232 of inner shaft extension rod
Outer shaft 240
241 outer shaft connecting rod 242 of outer shaft extension rod
Mechanical seal 251
Turn to 252 turning-bar 1 of fixed ring
Turning-bar 2 254
Gear 260
4 261 gear 6 262 of gear
7 263 gear 5 264 of gear
3 265 gear 8 266 of gear
271 decelerating step motor 2 272 of small generator
It limits adjuster 280 and is driven straight-tooth 281
Circular cone pressure bearing 282
290 internal gear 291 of power output shaft
Control system 300
Accumulation chamber 400
Driving and passenger compartment 500
Wing rotation direction E propeller internal frame propeller rotational direction D
Gas is to propeller force direction F
Specific embodiment
Specific embodiment of the present utility model is described in detail below in conjunction with attached drawing, it should be appreciated that this place
The specific embodiment of description is only used for explanation and illustration the utility model, is not intended to limit the utility model.
In order to preferably explain, utility model full name and direction are described collectively, land, water and air three-purpose vehicle letter
Referred to as equipment；Direction of the land, water and air three-purpose vehicle in land straight-line travelling is front and back, and direction normal thereto is left and right,
It or is lateral.
The utility model is only described in detail the part of utility model innovation, the transmission device of engine and routine
Without description.
The equipment is described in detail from the operation in structure, function and driving process respectively below.
Referring to Fig. 1, the utility model is a kind of vehicles that land, water and air three are dwelt, can be on land, the water surface, low latitude
Middle traveling.The equipment includes Power System of Flight Vehicle 100, land and water dynamical system 200, control system, accumulation chamber, drives and takes
Room.
In order to meet flight function: referring to Fig. 6, aircraft includes: aircraft power motor 110, propeller 120, spiral
Paddle internal frame 130, windmill wings outrigger 140, diverter 150, body 160, if wherein in diverter comprising decelerating step motor,
Dry transmission gear, shell；
Referring to Fig. 7, propeller 120 passes through fixed device and is connected with aircraft power motor 110, motor base installation
On propeller internal frame 130, propeller internal frame 130 is mounted on windmill wings outrigger 140, on windmill wings outrigger 140
Diverter 150 is installed, diverter 150 connects propeller internal frame 130.Right-handed screw and counterpropeller need symmetrically during installation, and four
It is identical, and each propeller rotational centre distance aircraft center that the corresponding propeller of rotor craft diagonally opposing corner is positive and negative
Distance is the same.It is such symmetrical countertorque when propeller rotational to be made to cancel each other out.
Referring to Fig. 8, decelerating step motor 1 is installed inside diverter shell 151, decelerating step motor 1
Gear 1 is installed, referring to fig. 4, the axis of 130 two sides of propeller internal frame is longer, passes through windmill wings outrigger on output shaft
140 circular hole stretches out, and is equipped with bearing at circular hole, and the axis of extension is equipped with transmission gear 2 154, and on decelerating motor
Gear 1 engage.Diverter shell 151 is mounted on windmill wings outrigger.In this way, the rotation by decelerating motor can
To drive drop propeller internal frame 130 to rotate in the axial direction.Reconciling decelerating step motor 1 by control system can adjust
The angle of uncoiling paddle and power motor part, to meet the direction of adjustment propeller, referring to Figure 12.When rising and falling, propeller is
Aircraft provides power vertically upward, and in high-speed flight, propeller power direction is consistent with direction of advance, and air-flow is to machine
The lifting vehicle of the wing keeps height.
In order to meet wing-folding function: referring to Figure 10, windmill wings outrigger 140 and body 160 by axis due to being connected
It connects, windmill wings outrigger 140 can be around axis along lateral rotation, when turning to straight down, propeller outrigger inside and body
160 contacts, prevent it from continuing to rotate.When being rotated upwardly into level, contacted on the outside of wing rotation axis with 160 upper side of body,
Prevention continues up rotation.Figure 11 is rotation axis partial section view when wing folds completely, when wing turns to horizontality
When, wing support shown in figure side is contacted with 160 side of main body, is hindered and is continued to rotate, to be maintained at horizontal
State.
In order to meet folder function: the folding and stretching, extension of the rotor part of aircraft fully rely on propeller power drive,
This special construction of design can guarantee that windmill wings outrigger 140 is folding straight down and this 90 ° are unfolded horizontally outward
In the range of rotate, air-flow is vertical with the plane of propeller always to the active force of propeller, and outward, referring to Fig. 9.This
Sample, in lift, gravity, under the action of rack holding power, with the increase of speed, propeller folded portion pivoting, spiral
140 Automatic-expanding of paddle wing outrigger, is blocked when being deployed into level by the structure of upper rack, wing stretching process terminates, and spiral shell
When revolving paddle lower than this speed, windmill wings outrigger 140 rotates gradually downward, is kept off when turning to straight down by body 160
Firmly, wing-folding process terminates.The stretching, extension and folding of wing rely on certain revolving speed of propeller, and this revolving speed is far below flight
When speed normal flight will not be had an impact so wing is constantly in unfolded state when normal flight.Thus simplify
Whole structure, reduces weight, energy saving, practical.
The section of windmill wings outrigger 140 is as shown in figure 12, and protrusion above middle section falls in below, and is
Fairshaped structure has imitated the wing of bird, according to bernoulli principle, when rapid flight, above gas flow rate it is big, below gas
Flow velocity is small, and upper and lower surface forms pressure difference, and gas upwards pressure to wing generation, and upward lift is provided for aircraft.
In order to meet the function of land and water traveling: referring to Figure 13, Figure 16, turbo blade group is mounted on tire 212 with rotation axis
It can mutually be rotated without influence inside outer wheel hub 211, and between each other.Turbo blade group and outer shaft 230 pass through outer universal joint
221 connections, tire 212, outer wheel hub 211 are connect with inner shaft 230 by interior universal joint 222, and interior universal joint 222 is mounted in outer ten thousand
To the inside of section 221, the centre of sphere of two universal joints 220 is overlapped.Outer shaft 230 is equipped with mechanical seal 251 in the inside and outside intersection of equipment, interior
Part of the axis 230 in equipment is equipped with gear 3 265, and outer shaft 230 is respectively tooth there are two gear in the installation of equipment inner part
4 261, gear 5 264 is taken turns, gear 4 261 is connected to the gear seven on small generator 271, outer shaft 230 by gear 6 262
On gear 5 264 can be engaged respectively with the internal gear 291 in transmission shaft with the gear 3 265 in inner shaft 230.Internal gear
291 can slide in the certain position of transmission shaft, such as Figure 16.Limit adjuster 280 and small generator 271, transmission straight-tooth 281
Installation is fixed, and internal gear 291 is blocked among limiter, control internal gear 291 is mobile, and it is defeated with power to limit adjuster 280
There is gap among shaft 290, be not directly contacted with, so that the rotation of power output shaft does not influence to limit adjuster 280.Limit is adjusted
Device 280 is mounted on position limiting structure by two circular cone pressure bearings 282, wherein limit adjuster 280 is stung with transmission straight-tooth 281
It closes, small generator 271 is connected with outer shaft by gear four, gear five, gear six, is installed on 2 272 axis of decelerating step motor
There is gear eight, gear eight is engaged with transmission straight-tooth, so that control decelerating step motor 2 272 can adjust limit adjuster
280 with the position of small generator.
Figure 14 is please referred to, inner shaft connects inner shaft extension rod, and inner shaft extension rod passes through interior universal axis connection inner shaft connecting rod.Outer shaft
Outer shaft extension rod is connect, outer shaft extension rod passes through outer universal axis connection outer shaft connecting rod.
Land when driving, decelerating step motor 2 272 rotates, and control limit adjuster 280 is mobile, so that power output
Internal gear 291 in axis 290 is moved along axis, is disengaged from the gear 5 264 on outer shaft 230, internal gear 291 moves to always
It is engaged with the gear 3 265 in inner shaft 230, at this point, 265 on small generator 271 are engaged with gear 6 262.Power at this time
Output shaft 290 rotates torque transmission to outer wheel hub 211 and tire 212, outer wheel hub 211 and tire 212, and equipment moves forward,
In this way, the steering of control power output shaft 290 can control equipment and travel forward or backward.
On land when driving or when equipment is parked, referring to Figure 19, at this time since small generator 271 and outer shaft 230 are logical
Gear is crossed to be connected, when there is lateral wind to flow through wheel, turbo blade group just be can rotate, it just will drive the rotation of small generator 271,
Then electric energy is stored in battery.Since the force direction of turbo blade and air-flow is laterally, before and after equipment when driving not
It is impacted.
Land travel turn when, by the control of steering wheel so that turning-bar 1 shown in Figure 18 to the left or to
It moves right, is connect with the steering fixed ring 252 of outer 221 outside of universal joint by turning-bar 2 254, so that turning-bar indirectly controls
Outer universal joint 221 rotates, to control wheel steering.
In water when driving, decelerating step motor 2 272 controls to adjust limiter movement, so that in power output shaft 290
Internal gear 291 be disengaged from the gear 3 265 in inner shaft 230, be moved to and engaged with the gear 5 264 on outer shaft 230, this
When small generator 271 be disengaged from gear 5 264.In this way, power output shaft 290 is by torque transmission to turbo blade group,
The rotation of power output shaft 290 drives the rotation of turbo blade group, and equipment laterally travels.
When turning in water, the revolving speed for directly controlling two sides turbo blade group can be turned to.
It can float and stablize in water to meet equipment, mechanism heavier in equipment accumulation chamber is placed on bottom
Disk improves stability so that center of gravity declines.Equipment lower part is using integrated structure, so that waterproof performance enhances.
It will be described below from specific driving process.
Equipment is parked on land, and such as Figure 19, decelerating step motor 2 272 controls internal gear 291 by limit adjuster 280
It is engaged with inner shaft 230, small generator 271 is connect by gear with outer shaft 230 with outer shaft 230 at this time, and power output shaft drives
Outer wheel hub 211 and tyre rotation, equipment move forward, will as long as flowing through wheel with lateral wind when driving process or stopping
The rotation power generation of small generator 271 is driven, is stored in battery.
When needing flight, aircraft as shown in Figure 2 folds completely in ground parked state wing, standby for takeoff.Four fly
Row device power motor 110 starts, and revolving speed is gradually increased, and when reaching certain revolving speed, wing starts gradually to open up with the increase of revolving speed
It opens.When wing turns to horizontality, wing stretching, extension terminates, as shown in Figure 1.Revolving speed continues growing, and increases to certain speed
When, aircraft initially moves off ground, by the conciliation of control system, steadily takes off, when rising to certain height, and steering system
It starts to work, control propeller gradually rotates level, and the revolving speed of propeller gradually increases at this time, to provide necessary liter
Power, aircraft front flight upwards at this time, when propeller rotational is to horizontality, lift is mentioned by active force of the gas to wing
For the power direction of propeller is consistent with direction of advance, rapid flight, such as Fig. 3.It is first when close to destination or when needing to land
It first needing to slow down, aircraft motor gradually slows down, and steering system control propeller axis is rotated to vertical direction at this time, when
When turning to vertical direction, the speed reduction of aircraft horizontal direction can be made by adjusting the velocity of rotation of four propellers
To zero.As Fig. 1 when taking off.Next the revolving speed for being gradually reduced propeller makes stable landing, and speed drops to certain turn
Wing starts gradually to fold when fast, and when dropping to the more slow-speed of revolution, folding process terminates.Revolving speed is slowly reduced to zero, and landing terminates.
Turbo blade group is that multiple groups turbine leaf fan is mounted side by side together, and turbine leaf fan outside is blade reinforcing ring 213.
When in water, decelerating step motor 2 272 controls the tooth on control internal gear 291 and inner shaft 230 by limiter
Wheel three disconnects engagement, engages with outer shaft 230, and small generator 271 is engaged with the disconnection of gear 6 262 at this time.Power output shaft 290
The rotation of turbo blade group is driven, control equipment laterally travels.
Claims (6)
1. a kind of land, water and air three-purpose vehicle, which is characterized in that foldable above control system, main body including body interior
Power System of Flight Vehicle, main intracorporal land and water dynamical system, accumulation chamber that control system is connected in main body, main center drive
It sails and passenger compartment；
The Power System of Flight Vehicle includes right-handed screw paddle two, counterpropeller two, four, aircraft power motor, spiral
Paddle internal frame four, two groups of windmill wings outrigger, decelerating step motor four, transmission gear is multiple, diverter shell four, turn
Moving axis four；Propeller passes through fixed device and connect with main body, and the pedestal of aircraft power motor is mounted on propeller internal frame,
Two propeller internal frames are installed, diverter shell is mounted on propeller outrigger wing, spiral shell on each group of windmill wings outrigger
Rotation paddle outrigger wing group is mounted on body by two rotation axis, and aircraft motor lines and steering motor pass through propeller internal frame
Inside is connected internally to control system and accumulation chamber in equipment by outrigger；
The land and water dynamical system includes 4 identical combination type vane wheels, is arranged in bottom four corners, each combination type vane
Wheel includes tire, wheel hub, turbo blade group, outer universal joint, interior universal joint, outer shaft, inner shaft, power output semiaxis, small power generation
Machine, decelerating step motor, limit adjuster, transmission straight-tooth and mechanical seal group；Two sides are all provided with wheel hub in tire, two wheel hubs it
Between by interior axis connection, turbo blade group is mounted on inside tire and outer wheel hub with rotation axis, and between each other can mutual nothing
Rotation is influenced, the outer shaft at turbo blade group center extends outwardly for outer shaft outer portion, and outer shaft outer portion is connected by outer universal joint
Interior universal joint, outer shaft are set in inner shaft outer wall, and interior universal joint and the coincidence of the outer universal joint centre of sphere are mutually twisted, and outer shaft is in inside and outside of the main body
Intersection is equipped with mechanical seal, and the end of inner shaft sets gear three, and the end of outer shaft sets gear five, is also arranged with gear on outer shaft
Four, gear four is connected to the gear seven on small generator by gear six, the gear five on outer shaft and the gear three in inner shaft
It can be engaged respectively with the internal gear in transmission shaft, internal gear can form engaging sleeve with gear three or gear five, and internal gear can be with
It is slided in transmission shaft certain position, adjusts limiter and be mounted on position limiting structure by two circular cone thrust bearings, wherein adjusting limit
Position device is engaged with transmission straight-tooth, and small generator is connected with outer shaft by gear four, gear five, gear six, decelerating step motor
Gear eight is installed, gear eight is engaged with transmission straight-tooth, so that control decelerating step motor can adjust adjusting limit on axis
The position of device and small generator；
Accumulation chamber is placed on low bottom-disc, and the accumulation chamber includes power battery pack, energy-storage battery, fuel tank；
The driving and passenger compartment is located at the middle position of equipment, the control of set direction disk, turning-bar in driving and passenger compartment
One to the left or moves right, and is connect with the steering fixed ring outside outer universal joint by turning-bar two.
2. a kind of land, water and air three-purpose vehicle according to claim 1, which is characterized in that right-handed screw paddle and counterpropeller
During installation, the corresponding identical propeller of diagonally opposing corner, right-handed screw paddle and counterpropeller center of rotation on propeller outrigger wing
It is the same apart from aircraft centre distance.
3. a kind of land, water and air three-purpose vehicle according to claim 1, which is characterized in that the installation of diverter interior of shell
There is decelerating step motor one, gear one is installed on one output shaft of decelerating step motor, the axis of propeller internal frame two sides is longer, leads to
The circular hole for crossing windmill wings outrigger stretches out, and is equipped with bearing at circular hole, and the axis of bearing extension is equipped with transmission gear two,
And engaged with the gear one on decelerating motor, diverter shell is mounted on windmill wings outrigger.
4. a kind of land, water and air three-purpose vehicle according to claim 1, which is characterized in that inner shaft connects inner shaft extension rod,
For inner shaft extension rod by interior universal axis connection inner shaft connecting rod, outer shaft connects outer shaft extension rod, and outer shaft extension rod passes through outer universal shaft
Connect outer shaft connecting rod.
5. a kind of land, water and air three-purpose vehicle according to claim 1, which is characterized in that the expansion of windmill wings outrigger
When section be middle section above protrusion, the streamlined structure fallen in below.
6. a kind of land, water and air three-purpose vehicle according to claim 1, which is characterized in that turbo blade group is multiple groups whirlpool
Wheel blade fan is mounted side by side together, and turbine leaf fan outside is blade reinforcing ring.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920115206.7U CN209479339U (en) | 2019-01-23 | 2019-01-23 | A kind of land, water and air three-purpose vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920115206.7U CN209479339U (en) | 2019-01-23 | 2019-01-23 | A kind of land, water and air three-purpose vehicle |
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| CN209479339U true CN209479339U (en) | 2019-10-11 |
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| CN201920115206.7U Expired - Fee Related CN209479339U (en) | 2019-01-23 | 2019-01-23 | A kind of land, water and air three-purpose vehicle |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109606042A (en) * | 2019-01-23 | 2019-04-12 | 南昌航空大学 | A kind of land, water and air three-purpose vehicle |
| CN110861454A (en) * | 2019-11-29 | 2020-03-06 | 吉林大学 | Reconfigurable air-submersible amphibious robot |
| CN111703575A (en) * | 2020-06-29 | 2020-09-25 | 金卫明 | Multifunctional unmanned aerial vehicle |
| WO2022011802A1 (en) * | 2020-07-13 | 2022-01-20 | 陈晨 | Flying car |
| WO2023070913A1 (en) * | 2021-10-25 | 2023-05-04 | 浙江大学台州研究院 | Sea-water-air three-purpose safe intelligent robot |
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2019
- 2019-01-23 CN CN201920115206.7U patent/CN209479339U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109606042A (en) * | 2019-01-23 | 2019-04-12 | 南昌航空大学 | A kind of land, water and air three-purpose vehicle |
| CN110861454A (en) * | 2019-11-29 | 2020-03-06 | 吉林大学 | Reconfigurable air-submersible amphibious robot |
| CN110861454B (en) * | 2019-11-29 | 2020-12-25 | 吉林大学 | Reconfigurable air-submersible amphibious robot |
| CN111703575A (en) * | 2020-06-29 | 2020-09-25 | 金卫明 | Multifunctional unmanned aerial vehicle |
| CN111703575B (en) * | 2020-06-29 | 2021-09-14 | 南京拓恒无人系统研究院有限公司 | Multifunctional unmanned aerial vehicle |
| WO2022011802A1 (en) * | 2020-07-13 | 2022-01-20 | 陈晨 | Flying car |
| WO2023070913A1 (en) * | 2021-10-25 | 2023-05-04 | 浙江大学台州研究院 | Sea-water-air three-purpose safe intelligent robot |
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