CN108973561A - A kind of electronic hovercar - Google Patents
A kind of electronic hovercar Download PDFInfo
- Publication number
- CN108973561A CN108973561A CN201811054812.9A CN201811054812A CN108973561A CN 108973561 A CN108973561 A CN 108973561A CN 201811054812 A CN201811054812 A CN 201811054812A CN 108973561 A CN108973561 A CN 108973561A
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- China
- Prior art keywords
- motor
- wheel
- gear
- vehicle body
- fixedly connected
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 230000005540 biological transmission Effects 0.000 claims abstract description 29
- 230000007246 mechanism Effects 0.000 claims abstract description 10
- 238000004891 communication Methods 0.000 claims description 9
- 239000011521 glass Substances 0.000 claims description 5
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims description 3
- 229910052744 lithium Inorganic materials 0.000 claims description 3
- 238000012544 monitoring process Methods 0.000 claims description 3
- 230000005611 electricity Effects 0.000 claims 1
- 239000007787 solid Substances 0.000 claims 1
- 230000033001 locomotion Effects 0.000 description 12
- 230000000694 effects Effects 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000007667 floating Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000008450 motivation Effects 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
- 230000005570 vertical transmission 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
Abstract
The invention belongs to technical field of traffic transportation, more particularly, to a kind of electronic hovercar, including wheel and vehicle body, it is fixedly connected between the wheel and vehicle body by connection frame, first motor is separately installed on the roof of four connection frames, second motor, third motor and the 4th motor, the first motor and third motor are about vehicle body central symmetry, and second motor and the 4th motor also about vehicle body central symmetry, the first motor, second motor, third motor and the 4th motor pass through transmission mechanism respectively and connect with wheel, the transmission mechanism includes the transmission main shaft for being fixedly connected on motor output end, fixing sleeve is connected to transverse gear on the lateral wall of the transmission main shaft, longitudinal gear is engaged on the outside of the transverse gear, transmission countershaft is fixedly connected on the wheel shaft of the longitudinal direction gear.Advantage is: the present invention can reach zero emission, zero pollution, and propeller and wheel use integral structure, occupy little space.
Description
Technical field
The invention belongs to technical field of traffic transportation, more particularly, to a kind of electronic hovercar.
Background technique
Hovercar flies in the sky or travels in land, is an airplane from an on-highway motor vehicle variable body.The world is first
First-fly is realized in the U.S. at the beginning of hovercar 3 months 2009, only need to press a button and wing-folding can be reached after landing
Highway.Hovercar, with a wide range of applications and extremely strong competitiveness both at home and abroad, in addition, hovercar can be with
The case where very easily stopping into garage, meeting with traffic congestion, and can take off whenever and wherever possible, convert route.But existing flight vapour
Vehicle needs to expend a large amount of resource mostly to provide power, and the propeller of hovercar and wheel are split type structure, are accounted for
Space is larger, is unfavorable for the long-time service of hovercar.
For this purpose, it is proposed that a kind of electronic hovercar solves the above problems.
Summary of the invention
Regarding the issue above, the present invention provides a kind of no pollution and the electronic flight vapour of flight stability by force
Vehicle.
In order to achieve the above objectives, present invention employs following technical proposals: a kind of electronic hovercar, including wheel and vehicle
Body is fixedly connected between the wheel and vehicle body by connection frame, is separately installed with first on the roof of four connection frames
Motor, the second motor, third motor and the 4th motor, the first motor and third motor are about vehicle body central symmetry, and the
Two motors and the 4th motor are also about vehicle body central symmetry, the first motor, the second motor, third motor and the 4th motor point
Not Tong Guo transmission mechanism connect with wheel, the transmission mechanism includes the transmission main shaft for being fixedly connected on motor output end, described
Fixing sleeve is connected to transverse gear on the lateral wall of transmission main shaft, and longitudinal gear is engaged on the outside of the transverse gear, described vertical
Transmission countershaft is fixedly connected on the wheel shaft of gear, and the both ends of transmission countershaft are rotatablely connected with the side wall of connection frame respectively,
First gear there are two being fixedly attached on the lateral wall of the transmission countershaft, and two first gears are symmetricly set on longitudinal gear
Two sides, the upper end of the first gear is engaged with second gear, is fixedly connected with arc sprocket wheel on the outside of the wheel rim of the wheel,
The one end of the second gear far from first gear is connect with arc sprocket engagement, is also equipped on the wheel hub of four wheels
Propeller.
In above-mentioned electronic hovercar, the first motor, the second motor, third motor and the 4th motor bottom wall
On be fixedly connected to mounting base, and mounting base passes through the roof of multiple fastening bolts and connection frame and connects.
In above-mentioned electronic hovercar, rubber ring, the propeller and vehicle are fixedly connected on the outside of the wheel
Wheel is structure as a whole, and propeller is mounted on the center of wheel.
In above-mentioned electronic hovercar, X-type top-support, and X-type top are fixedly connected on the roof of the vehicle body
The front and rear sides of portion's bracket are mounted on organic glass hood.
In above-mentioned electronic hovercar, control module, communication module, video monitoring mould are also equipped in the vehicle body
Block, double Position Fixing Navigation Systems, stability contorting module and safe obstacle avoidance module.
In above-mentioned electronic hovercar, the control module includes manually controlling and automatically controlling, the communication mould
Block supports 3G/4G, Wi-Fi and Bluetooth communication, and double Position Fixing Navigation Systems include GPS and GNSS.
In above-mentioned electronic hovercar, be also equipped with power supply in the vehicle body, the power supply include motor power and
Controller power source module, power supply use solar energy and lithium battery power supply mode.
Compared with prior art, the advantages of this electronic hovercar, is:
1, using the device of this technology, zero emission, zero pollution, the reproducible electric power energy of pure green is fully achieved.
2, the design bright spot of this technology is that propeller and wheel are integrated, the rotation of wheel and the rotation of propeller, solely
Vertical operation, does not interfere with each other.And occupied space also less and when propeller is laid flat when the state that propeller is laid flat
Occupied space is little when state, can take off in any place, not need coasting distance, do not need additional aids,
And the propeller of inside is by tire protection, even if passenger safety can also be protected in the air to greatest extent by meeting, reduces accident
Odds.
3, it takes the initiative between motor and propeller operating mode, for the pulling force of propeller four corners of the world four direction
The mode for taking hydraulic stem actively to convert changes direction, hovercar of the invention by wing different from standard aircraft
What propeller was taken is active deflecting, is more advantageous to the mobility and flexibility for embodying aircraft.
Detailed description of the invention
Top view when Fig. 1 is a kind of wheel expansion of electronic hovercar provided by the invention；
Fig. 2 is a kind of wheel closed type top view of electronic hovercar provided by the invention；
Fig. 3 is a kind of transmission mechanism top view of electronic hovercar provided by the invention；
Fig. 4 is a kind of motion principle figure of electronic hovercar provided by the invention.
In figure, 1 wheel, 2 vehicle bodies, 3 connection frames, 4 first motors, 5 second motors, 6 third motors, 7 the 4th motors, 8 are passed
Motivation structure, 9 transmission main shafts, 10 transverse gears, 11 longitudinal gears, 12 transmission countershafts, 13 first gears, 14 second gears, 15 arcs
Shape sprocket wheel, 16 propellers, 17 X-type top-supports, 18 organic glass hoods.
Specific embodiment
Following embodiment only exists in illustrative purpose, limits the scope of the invention without being intended to.
As shown in Figs 1-4, a kind of electronic hovercar, including wheel 1 and vehicle body 2, pass through company between wheel 1 and vehicle body 2
It connects frame 3 to be fixedly connected, first motor 4, the second motor 5, third motor 6 and is separately installed on the roof of four connection frames 3
Four motors 7, specifically, first motor 4, the second motor 5, third motor 6 and the 4th motor 7 bottom wall on be fixedly connected to peace
Seat is filled, and mounting base is connect by multiple fastening bolts with the roof of connection frame 3, convenient for the installation and removal to motor, first
Motor 4 and third motor 6 are about 2 central symmetry of vehicle body, and the second motor 5 and the 4th motor 7 be also about 2 central symmetry of vehicle body,
First motor 4, the second motor 5, third motor 6 and the 4th motor 7 are connect by transmission mechanism 8 with wheel 1 respectively, transmission mechanism
8 include the transmission main shaft 9 for being fixedly connected on motor output end, and fixing sleeve is connected to transverse gear 10 on the lateral wall of transmission main shaft 9,
The outside of transverse gear 10 is engaged with longitudinal gear 11, transmission countershaft 12 is fixedly connected on the wheel shaft of longitudinal gear 11, and pass
The both ends of dynamic countershaft 12 are rotatablely connected with the side wall of connection frame 3 respectively, be fixedly attached on the lateral wall of transmission countershaft 12 there are two
First gear 13, and two first gears 13 are symmetricly set on the two sides of longitudinal gear 11, the upper end of first gear 13 is engaged with
The wheel rim outside of second gear 14, wheel 1 is fixedly connected with arc sprocket wheel 15, the one end of second gear 14 far from first gear 13
Connection is engaged with arc sprocket wheel 15, propeller 16 is also equipped on the wheel hub of four wheels 1, specifically, the outside of wheel 1 is fixed
It is connected with rubber ring, propeller 16 and wheel 1 are structure as a whole and form rotor craft, and propeller 16 is mounted on wheel 1
Center, the rotation of wheel 1 and the rotation of propeller 16, independent operating do not interfere with each other, and the state being laid flat when propeller 16
When occupied space it is also little, and occupied space is little when the state that spiral 16 is laid flat, can be in any place
It takes off, does not need coasting distance, do not need additional aids.
Wherein, X-type top-support 17 is fixedly connected on the roof of vehicle body 2, and the front and rear sides of X-type top-support 17 are equal
Organic glass hood 18 is installed, solar panel is installed on the roof of X-type top-support 17, can be built good open
Driving vision, improve safety while be also 2 solar panel of vehicle body main support structure.
Wherein, control module, communication module, video monitoring module, double Position Fixing Navigation Systems, steady is also equipped in vehicle body 2
Control module and safe obstacle avoidance module are determined, specifically, control module includes manually controlling and automatically controlling, specifically, control is former
Reason: four rotor crafts change variable rotor speed by adjusting four motor speeds, realize the variation of lift, so that control flies
The posture of row device and position, while the first motor 4 and third motor 6 of quadrotor rotate counterclockwise, the second motor 5
It is rotated clockwise with the 4th motor 7, therefore when aircraft balances flight, gyroscopic effect and air force torque effect are supported
Disappear.
According to the positional relationship in Fig. 4, four wheels of rotor craft are respectively designated as the first rotor, the second rotation
The wing, third rotor and quadrotor.
Wherein, a variety of different movements may be implemented in rotor craft:
1, it moving vertically: while increasing the output power of four motors, rotor revolving speed increases so that total pulling force increases, when
When total pulling force is enough to overcome the weight of complete machine, quadrotor just liftoff vertical ascent；Conversely, reducing four motors simultaneously
Output power, quadrotor then vertically decline, until balance landing, realizes the vertical movement along z-axis.Work as external disturbance
When amount is zero, when the lift that rotor generates is equal to the self weight of aircraft, aircraft just keeps floating state.
2, pitching movement: in (b) of Fig. 4, the revolving speed of the oneth the 4th motor 7 rises, the revolving speed decline of third motor 6
(knots modification size is answered equal), the second motor 5, the 4th motor 7 revolving speed remain unchanged.Since the lift of rotor 1 rises, rotor
The unbalanced moments of 3 drop in lift, generation rotates fuselage around y-axis, and similarly, when the revolving speed of the 4th motor 7 declines, third is electric
The revolving speed of machine 6 rises, and fuselage is just rotated around y-axis to another direction, realizes the pitching movement of aircraft.
3, rolling movement: it is identical as the principle of Fig. 4 (b), in Fig. 4 (c), change turn of the second motor 5 and the 4th motor 7
Speed keeps the revolving speed of the 4th motor 7 and third motor 6 constant, then fuselage can be made to rotate around x axis (forward and reverse), realizes and flies
The rolling movement of row device.
4, yawing rotation: during rotor rotational due to air drag effect will form it is opposite with rotation direction anti-twisted
Square can make two in four rotors to rotate forward to overcome reaction torque to influence, two reversions, and each rotor on diagonal line
Rotation direction is identical.The size of reaction torque is related with rotor revolving speed, and when four motor speeds are identical, four rotors generate anti-
Torque mutually balances, and quadrotor does not rotate；When four motor speeds are not exactly the same, unbalanced reaction torque
Quadrotor can be caused to rotate.In Fig. 4 (d), when the revolving speed of the oneth the 4th motor 7 and third motor 6 rises, second is electric
When the revolving speed of machine 5 and the 4th motor 7 declines, the first rotor and third rotor are greater than the second rotor and the 4th to the reaction torque of fuselage
Rotor just rotates the reaction torque of fuselage, fuselage under the action of reaction torque more than needed around z-axis, realizes the yawing rotation of aircraft,
It turns to opposite with the 4th motor 7, the steering of third motor 6.
5, move forward and backward: to realize aircraft in the horizontal plane front and rear, left and right movement, it is necessary in the horizontal plane to fly
Row device applies certain power.In Fig. 4 (e), increases by 6 revolving speed of third motor, increase pulling force, it is corresponding to reduce 7 turns of the 4th motor
Speed reduces pulling force, keeps simultaneously, and reaction torque still will keep balancing.By Fig. 4 (b), aircraft occurs a degree of first
So that rotor thrust be made to generate horizontal component, therefore the preceding winged movement of aircraft may be implemented in inclination.It flies and flies forward backward
Row is exactly the opposite.(in Fig. 4 (b) Fig. 4 (c), aircraft can also be generated while generating pitching, tumbling motion along x, y-axis
Horizontal movement.)
6, tendency movement: in Fig. 4 (f), due to symmetrical configuration, so being inclined to the working principle flown and having moved forward and backward
It is complete the same.
Wherein, one: 2 vehicle frame of vehicle body is all made of independent McPherson suspension system, does not interfere with each other, simultaneously because wheel 1 half
Diameter is big, improves the passability in complex road surface.
Two: 2 lower part of vehicle body is totally-enclosed, in addition the buoyancy of four tires, and floating is also able to achieve after paddling.
Three: single propeller is equipped with four active hydraulic lifting arms, improves the handling of propeller.
More specifically, communication module supports 3G/4G, Wi-Fi and Bluetooth communication, double Position Fixing Navigation Systems include GPS and
GNSS, wherein stability contorting module includes gyroscope, accelerometer, the sensors such as barometer, and can obtain aspect
Then the relevant informations such as position stablize aircraft by controlling the revolving speed of four paddles, adjust posture, in addition, safe obstacle avoidance module
Infrared sensor including multiple installations comprehensive on machine can be used to realize Real Time Obstacle Avoiding, and pass through and obtain in real time
Battery capacity is accomplished to give warning in advance and automatically control landing etc., strengthens safety.
Wherein, power supply is also equipped in vehicle body 2, power supply includes motor power and controller power source, this power supply system passes through
Solar energy and lithium battery power supply mode improve cruising ability.
Although wheel 1, vehicle body 2, connection frame 3, first motor 4, the second motor 5, third motor is used more herein
6, the 4th motor 7, transmission mechanism 8, transmission main shaft 9, transverse gear 10, longitudinal gear 11, transmission countershaft 12, first gear 13,
The terms such as second gear 14, arc sprocket wheel 15, propeller 16, X-type top-support 17, organic glass hood 18, but be not precluded
A possibility that using other terms.The use of these items is only for be more convenient to describe and explain essence of the invention；?
They, which are construed to any additional limitation, is disagreed with spirit of that invention.
Claims (7)
1. a kind of electronic hovercar, including wheel (1) and vehicle body (2), which is characterized in that the wheel (1) and vehicle body (2) it
Between be fixedly connected by connection frame (3), first motor (4), the second electricity are separately installed on the roof of four connection frames (3)
Machine (5), third motor (6) and the 4th motor (7), the first motor (4) and third motor (6) are about vehicle body (2) center pair
Claim, and the second motor (5) and the 4th motor (7) are also about vehicle body (2) central symmetry, the first motor (4), the second motor
(5), third motor (6) and the 4th motor (7) are connect by transmission mechanism (8) with wheel (1) respectively, the transmission mechanism (8)
Transmission main shaft (9) including being fixedly connected on motor output end, fixing sleeve is connected to transverse direction on the lateral wall of the transmission main shaft (9)
Gear (10) is engaged with longitudinal gear (11) on the outside of the transverse gear (10), solid on the wheel shaft of the longitudinal direction gear (11)
Surely it is connected with transmission countershaft (12), and the both ends of transmission countershaft (12) are rotatablely connected with the side wall of connection frame (3) respectively, the biography
Be fixedly attached on the lateral wall of dynamic countershaft (12) there are two first gear (13), and two first gears (13) be symmetricly set on it is vertical
To the two sides of gear (11), the upper end of the first gear (13) is engaged with second gear (14), outside the wheel rim of the wheel (1)
Side is fixedly connected with arc sprocket wheel (15), the second gear (14) one end and arc sprocket wheel (15) far from first gear (13)
Engagement connects, and is also equipped with propeller (16) on the wheel hub of four wheels (1).
2. electronic hovercar according to claim 1, which is characterized in that the first motor (4), the second motor (5),
Be fixedly connected to mounting base on the bottom wall of third motor (6) and the 4th motor (7), and mounting base by multiple fastening bolts with
The roof of connection frame (3) connects.
3. electronic hovercar according to claim 1, which is characterized in that be fixedly connected on the outside of the wheel (1)
Rubber ring, the propeller (16) and wheel (1) are structure as a whole, and propeller (16) is mounted on the center of wheel (1).
4. electronic hovercar according to claim 1, which is characterized in that be fixedly connected on the roof of the vehicle body (2)
Have X-type top-support (17), and the front and rear sides of X-type top-support (17) are mounted on organic glass hood (18).
5. electronic hovercar according to claim 1, which is characterized in that be also equipped with control mould in the vehicle body (2)
Block, communication module, video monitoring module, double Position Fixing Navigation Systems, stability contorting module and safe obstacle avoidance module.
6. electronic hovercar according to claim 5, which is characterized in that the control module is including manually controlling and certainly
Dynamic control, the communication module support 3G/4G, Wi-Fi and Bluetooth communication, and double Position Fixing Navigation Systems include GPS and GNSS.
7. electronic hovercar according to claim 1, which is characterized in that be also equipped with power supply in the vehicle body (2), institute
Stating power supply includes motor power and controller power source module, and powers and use solar energy and lithium battery power supply mode.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811054812.9A CN108973561A (en) | 2018-09-11 | 2018-09-11 | A kind of electronic hovercar |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811054812.9A CN108973561A (en) | 2018-09-11 | 2018-09-11 | A kind of electronic hovercar |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108973561A true CN108973561A (en) | 2018-12-11 |
Family
ID=64545423
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811054812.9A Pending CN108973561A (en) | 2018-09-11 | 2018-09-11 | A kind of electronic hovercar |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108973561A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110103652A (en) * | 2019-05-14 | 2019-08-09 | 安徽信息工程学院 | Car body with offline mode |
| CN112339515A (en) * | 2020-11-09 | 2021-02-09 | 北京理工大学 | Split type automobile and passenger cabin, aircraft unit and chassis part thereof |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104369635A (en) * | 2014-10-31 | 2015-02-25 | 蔡闯 | Air-ground amphibious vehicle |
| CN205707323U (en) * | 2016-04-15 | 2016-11-23 | 山东工商学院 | A kind of quadrotor |
| CN107093344A (en) * | 2016-09-19 | 2017-08-25 | 滨州学院 | A kind of four rotor wing unmanned aerial vehicle demonstrators |
-
2018
- 2018-09-11 CN CN201811054812.9A patent/CN108973561A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104369635A (en) * | 2014-10-31 | 2015-02-25 | 蔡闯 | Air-ground amphibious vehicle |
| CN205707323U (en) * | 2016-04-15 | 2016-11-23 | 山东工商学院 | A kind of quadrotor |
| CN107093344A (en) * | 2016-09-19 | 2017-08-25 | 滨州学院 | A kind of four rotor wing unmanned aerial vehicle demonstrators |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110103652A (en) * | 2019-05-14 | 2019-08-09 | 安徽信息工程学院 | Car body with offline mode |
| CN112339515A (en) * | 2020-11-09 | 2021-02-09 | 北京理工大学 | Split type automobile and passenger cabin, aircraft unit and chassis part thereof |
| CN112339515B (en) * | 2020-11-09 | 2022-04-08 | 北京理工大学 | Split type automobile and passenger cabin, aircraft unit and chassis part thereof |
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Application publication date: 20181211 |