CN110329499A - A kind of multifunctional intellectual aircraft - Google Patents

A kind of multifunctional intellectual aircraft Download PDF

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Publication number
CN110329499A
CN110329499A CN201910686240.4A CN201910686240A CN110329499A CN 110329499 A CN110329499 A CN 110329499A CN 201910686240 A CN201910686240 A CN 201910686240A CN 110329499 A CN110329499 A CN 110329499A
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CN
China
Prior art keywords
blade group
driving wheel
motor
linking arm
axle sleeve
Prior art date
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.)
Withdrawn
Application number
CN201910686240.4A
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Chinese (zh)
Inventor
不公告发明人
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Coix Chinensis Ice
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Coix Chinensis Ice
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Filing date
Publication date
Application filed by Coix Chinensis Ice filed Critical Coix Chinensis Ice
Priority to CN201910686240.4A priority Critical patent/CN110329499A/en
Publication of CN110329499A publication Critical patent/CN110329499A/en
Withdrawn legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60FVEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
    • B60F5/00Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
    • B60F5/02Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/08Helicopters with two or more rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • B64C27/37Rotors having articulated joints

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Transportation (AREA)
  • Toys (AREA)

Abstract

The present invention provides a kind of multifunctional intellectual aircraft, belong to aircraft field, including host, the two sides of host are each provided with a connecting shaft, and drive assembly is provided in connecting shaft, and drive assembly includes linking arm, motor and driver, the outside of motor is provided with housing, one end of linking arm connects housing, and the other end and the connecting shaft of linking arm are hinged, and pedal is connected in connecting shaft;Driver includes blade group and driving wheel, and blade group is located at the top of driving wheel, and the diameter of blade group is greater than the outer diameter of driving wheel, and blade group includes multiple blades, and blade is folding structure, and the diameter of leaf folding rear blade group is less than the outer diameter of driving wheel;Blade group is connected to the motor and blade group can mutually be separated with motor, and driving wheel is mutually separated with motor and driving wheel can be connected to the motor and connect.This Intelligent flight device flexible structure is changeable, and function is more, has more enjoyment.

Description

A kind of multifunctional intellectual aircraft
Technical field
The present invention relates to aircraft fields, in particular to a kind of multifunctional intellectual aircraft.
Background technique
Vehicle technology is fast-developing at present, diversified aircraft occurs.However aircraft is the most practical Function is exactly to take photo by plane, and other functions belong to entertainment more.That is aircraft function common at present is less, can not be more It is serviced for people well.
Summary of the invention
The present invention provides a kind of multifunctional intellectual aircraft, it is intended to solve the above problem in the prior art.
The present invention is implemented as follows:
A kind of multifunctional intellectual aircraft, including host, the two sides of the host are each provided with a connecting shaft, the connecting shaft On be provided with drive assembly, the drive assembly includes linking arm, motor and driver, and the outside of the motor is provided with cover One end of shell, the linking arm connects the housing, and the other end of linking arm is hinged with the connecting shaft, in the connecting shaft It is connected with pedal;
The driver includes blade group and driving wheel, and the blade group is located at the top of the driving wheel, the blade group Diameter is greater than the outer diameter of the driving wheel, and the blade group includes multiple blades, and the blade is folding structure, the blade The diameter of the blade group is less than the outer diameter of the driving wheel after folding;The blade group is connected with the motor and blade group energy Enough mutually to separate with motor, the driving wheel is mutually separated with the motor and driving wheel can be connected to the motor and connect.
Further, the blade group further includes clamping ring, and multiple blades are connected to the clamping ring;The blade Including blade root and leaf tip, the blade root is hinged with leaf tip.
Further, the motor is connected with drive shaft, and the end of the housing has hollow connecting column, the driving Axis passes through the connecting column;The driving wheel includes wheel rim, cover tire and multiple support rods, and the cover tire is connected to outside the wheel rim Side, multiple support rods are connected on the inside of the wheel rim, and one end of the support rod is fixedly connected with wheel rim, support rod it is another One end is provided with link slot, and the outside of the connecting column is circumferentially arranged multiple first connection sheets, each described support rod Link slot be connected to first connection sheet;
The drive shaft is externally connected to axle sleeve, and the axle sleeve can be rotated synchronously with drive shaft, and the end of the axle sleeve is set It is equipped with blowout patche, the blowout patche and the axle sleeve are rotatablely connected;Keyway, the outside of the axle sleeve are provided on the inside of the clamping ring It is provided with connecting key, the connecting key is inserted into the keyway, is provided with puller bolt, the end of puller bolt on the clamping ring It is abutted against with axle sleeve, unclamping the puller bolt can be such that the clamping ring mutually separates with axle sleeve, and can connect clamping ring Outside the blowout patche;The outer diameter of the axle sleeve is consistent with the outer diameter of the connecting column, and the outside of the axle sleeve is circumferentially arranged There are multiple second connection sheets;
The diameter of the blade group is less than the internal diameter of the wheel rim after the leaf folding;The link slot of the support rod can be with First connection sheet mutually separates and is connected to second connection sheet.
Further, connector sleeve is arranged in the connecting shaft, the connector sleeve and connecting shaft are rotatablely connected, the pedal It is connected to the connector sleeve, the host is internally provided with controller, gyroscope, acceleration transducer and wireless communication module, Gravity sensor and wireless communication module are provided in the pedal;The multifunctional intellectual aircraft further includes remote controler, institute It states and is also equipped with wireless communication module in remote controler.
Further, the linking arm is of a straight line type, and the end of linking arm is articulated with the end of the connecting shaft, linking arm Horizontality can be turned to by vertical state.
Further, there are two undercarriage, top and the host of the undercarriage are hinged for the bottom setting of the host, The bottom of the host is additionally provided with the holder being detachably connected with it, and the holder is located between two undercarriages.
Further, the end of the connecting shaft is provided with attachment base, and multiple connecting holes, institute are provided on the attachment base It states and is also equipped with multiple connecting holes on linking arm;Linking arm and attachment base pass through at least two when the linking arm is in a vertical state A pin shaft is connected, and the linking arm linking arm when in a horizontal state is connected with attachment base by least two pin shafts.
Further, between the blowout patche and connecting column, multiple second connection sheets are located at described the axle sleeve Between blade group and the connecting column.
Multifunctional intellectual aircraft provided by the invention, this Intelligent flight device have the function of airflight and land walking Can, user can make it have different functions according to the change that different situations make shape to Intelligent flight device when in use. This Intelligent flight device flexible structure is changeable, and function is more, has more enjoyment.
Detailed description of the invention
In order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, to embodiment or will show below There is attached drawing needed in technical description to be briefly described, it should be apparent that, the accompanying drawings in the following description is only this Some embodiments of invention for those of ordinary skill in the art without creative efforts, can be with It obtains other drawings based on these drawings.
Fig. 1 is the schematic top plan view of multifunctional intellectual aircraft provided in an embodiment of the present invention;
Fig. 2 is the schematic front view of multifunctional intellectual aircraft provided in an embodiment of the present invention;
Fig. 3 is the schematic top plan view of driver in multifunctional intellectual aircraft provided in an embodiment of the present invention, at this time driving wheel with Motor separation, blade group are connected to motor;
Fig. 4 is the schematic cross-sectional view of driver in multifunctional intellectual aircraft provided in an embodiment of the present invention, at this time driving wheel with Motor separation, blade group are connected to motor;
Fig. 5 is the elevational schematic view that blade group is connect with axle sleeve in multifunctional intellectual aircraft provided in an embodiment of the present invention;
Fig. 6 is the structural schematic diagram that boom end is supported in multifunctional intellectual aircraft provided in an embodiment of the present invention;
Fig. 7 is the schematic cross-sectional view of driver in multifunctional intellectual aircraft provided in an embodiment of the present invention, at this time driving wheel with Motor connection, blade group are separated with motor;
Fig. 8 is the schematic top plan view of driver in multifunctional intellectual aircraft provided in an embodiment of the present invention, at this time driving wheel with Motor connection, blade group are separated with motor;
Fig. 9 is schematic front view of the multifunctional intellectual aircraft provided in an embodiment of the present invention when using as walking device.
Appended drawing reference summarizes: host 11, connecting shaft 12, drive assembly 13, linking arm 14, motor 15, driver 16, housing 17, pedal 18, blade group 19, driving wheel 20, clamping ring 21, blade root 22, leaf tip 23, drive shaft 24, connecting column 25, wheel rim 26, cover tire 27, support rod 28, link slot 29, the first connection sheet 30, axle sleeve 31, blowout patche 32, connecting key 33, puller bolt 34, Two connection sheets 35, connector sleeve 36, undercarriage 37, attachment base 38, connecting hole 39, keyway 40.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other Embodiment shall fall within the protection scope of the present invention.
Please refer to Fig. 1-9.
A kind of multifunctional intellectual aircraft is present embodiments provided, this Intelligent flight device has airflight and land row The function of walking, user can make it have different according to the change that different situations make shape to Intelligent flight device when in use Function.This Intelligent flight device flexible structure is changeable, and function is more, has more enjoyment.
As shown in Figures 1 and 2, this multifunctional intellectual aircraft includes host 11, and the two sides of host 11 are each provided with one A connecting shaft 12, drive assembly 13 is provided in connecting shaft 12, and drive assembly 13 includes linking arm 14, motor 15 and driver 16, the outside of motor 15 is provided with housing 17, and one end of linking arm 14 connects housing 17, the other end and connecting shaft of linking arm 14 12 are hinged, and pedal 18 is connected in connecting shaft 12;
Driver 16 includes blade group 19 and driving wheel 20, and blade group 19 is located at the top of driving wheel 20, the diameter of blade group 19 Greater than the outer diameter of driving wheel 20, blade group 19 includes multiple blades, and blade is folding structure, leaf folding rear blade group 19 Diameter is less than the outer diameter of driving wheel 20;Blade group 19 is connected with motor 15 and blade group 19 can be separated with 15 phase of motor, drives Wheel 20 is separated with 15 phase of motor and driving wheel 20 can be connected with motor 15.
Host 11 is the main element of Intelligent flight device, and drive assembly 13 is driving mechanism.The interior setting battery of host 11, The devices such as controller, drive assembly 13 have the blade group 19 that Intelligent flight device can be made to fly in the sky and can make intelligence Driving wheel 20 of the aircraft in ground running.Drive assembly 13 is connect by linking arm 14 with connecting shaft 12, as aircraft Blade group 19 and driving wheel 20 are in a horizontal position in use, adjusting linking arm 14, it can after rotating blade group 19 It drives Intelligent flight device to fly in the sky, and driving wheel 20 and motor 15 is made to be in discrete state, make driving wheel in flight course 20 not can rotate, and blade group 19 is enable to obtain sufficient power.It needs using Intelligent flight device as walking device in use, rotating Linking arm 14 makes blade group 19 and driving wheel 20 be in vertical (i.e. the axis horizontal direction of driving wheel 20), makes driving wheel 20 Bottom be in lower position, and can be placed on ground, and connect driving wheel 20 with motor 15, motor 15 made to work It is able to drive the rotation of driving wheel 20, enables Intelligent flight device in ground running.Blade group 19 is interior in driving wheel 20 always Side makes blade group 19 not interfere with the work of driving wheel 20.
It is also connected with pedal 18 in the side of connecting shaft 12, pedal 18 is for people's standing.Intelligent flight device is in ground running When people can stand on pedal 18, make the Intelligent flight device can be used as walking-replacing tool use, make making for the Intelligent flight device It is more diversified with method, there is preferably entertainment.
In the Intelligent flight device, blade group 19 has larger-size blade, smaller, the leaf of the size design of driving wheel 20 There is the size greater than 20 outer diameter of driving wheel after piece expansion, keep aircraft more stable in flight.Blade is foldable Structure can be folded up when not in use, when being used as walking device by leaf folding, make the diameter of blade group 19 compared with It is small, it can be placed at driving wheel 20 on ground, in ground running, blade will not touch ground, enable driving wheel 20 just Often operation.
As shown in Figures 3 and 4, blade group 19 further includes clamping ring 21, and multiple blades are connected to clamping ring 21;Blade includes Blade root 22 and leaf tip 23, blade root 22 are hinged with leaf tip 23.Multiple blades, which are connected on clamping ring 21, makes blade Group 19 facilitates adjusting.
As shown in Figures 4 and 5, motor 15 is connected with drive shaft 24, and the end of housing 17 has hollow connecting column 25, drives Moving axis 24 passes through connecting column 25;Driving wheel 20 includes wheel rim 26, cover tire 27 and multiple support rods 28, and cover tire 27 is connected to wheel rim 26 Outside, multiple support rods 28 are connected to the inside of wheel rim 26, and one end of support rod 28 is fixedly connected with wheel rim 26, support rod 28 it is another One end is provided with link slot 29, and the outside of connecting column 25 is circumferentially arranged multiple first connection sheets 30, each support rod 28 Link slot 29 be connected to first connection sheet 30;
Drive shaft 24 is externally connected to axle sleeve 31, and axle sleeve 31 can be rotated synchronously with drive shaft 24, the end setting of axle sleeve 31 There is blowout patche 32, blowout patche 32 and axle sleeve 31 are rotatablely connected;The inside of clamping ring 21 is provided with keyway 40, and the outside of axle sleeve 31 is provided with Connecting key 33, connecting key 33 are inserted into keyway 40, are provided with puller bolt 34, the end of puller bolt 34 and axle sleeve on clamping ring 21 31 abut against, and unclamping puller bolt 34 can be such that clamping ring 21 separates with 31 phase of axle sleeve, and clamping ring 21 can be connected to axis Outside circle 32;The outer diameter of axle sleeve 31 is consistent with the outer diameter of connecting column 25, and the outside of axle sleeve 31 is circumferentially arranged to have multiple second to connect Contact pin 35;
The diameter of leaf folding rear blade group 19 is less than the internal diameter of wheel rim 26;The link slot 29 of support rod 28 can be connect with first 30 phase of piece separates and is connected to the second connection sheet 35.
By above-mentioned setting, enable driving wheel 20 fast implement with the connection of motor 15 with separate, and can be realized The stabilization of driving wheel 20.Blade group 19 and motor 15 can be disconnected again when driving wheel 20 works, enable driving wheel 20 It is enough efficiently to work, more pure experience is brought to user.
Motor 15 connects drive shaft 24 by shaft coupling, axle sleeve 31 is arranged in drive shaft 24, drive shaft 24 is able to drive axis 31 rotation of set, and blowout patche 32 is arranged in the end of axle sleeve 31, blowout patche 32 and axle sleeve 31 are rotatablely connected, make blowout patche 32 and axle sleeve 31 it Between will not rotate synchronously, axle sleeve 31 rotation when blowout patche 32 may slightly be rotated because of inertial force, make blowout patche 32 The energy of motor 15 will not be consumed.
Blade group 19 has clamping ring 21 and multiple blades, and blade has 6 in figure, and multiple blades can make Intelligent flight device More stable flight.When Intelligent flight device as aircraft in use, blade group 19 is connect by clamping ring 21 with axle sleeve 31, Under the restriction effect of connecting key 33 and keyway 40, axle sleeve 31 is made to be able to drive the synchronous rotation of blade group 19.And by holding out against spiral shell Bolt 34 holds out against effect, and blade group 19 in flight course is enable to be stably connected with the holding of axle sleeve 31.
In use, screw puller bolt 34, separate connecting key 33 with keyway 40 as walking device, and by clamping ring 21 It is moved at blowout patche 32, is detached from clamping ring 21 and axle sleeve 31, and pre-tightened clamping ring 21 in blowout patche 32 by puller bolt 34 On, so that blade group 19 will not consume the energy of motor 15 when motor 15 works.
Driving wheel 20 has wheel rim 26, and wheel rim 26 is rigid element, external setting cover tire 27 flexible, inside wheel rim 26 Support rod 28 is set, is connected to driving wheel 20 in drive assembly 13 by the supporting role of support rod 28.Support rod 28 and wheel Circle 26 makes that shaking or displacement will not be generated between support rod 28 and wheel rim 26, support rod 28 is connected to be fixedly connected with relationship It can guarantee the stabilization of driving wheel 20 after in the first connection sheet 30 or in the second connection sheet 35.
When Intelligent flight device as aircraft in use, the end of support rod 28 is connected to first outside connecting column 25 In connection sheet 30, makes motor 15 not and will drive the more bulky rotation of driving wheel 20, so that motor 15 is able to drive blade group 19 fast Speed rotation, it is ensured that Intelligent flight device being capable of stabilized flight.When Intelligent flight device as walking device in use, making 28 end of support rod It is connected in the second connection sheet 35 outside axle sleeve 31, so that motor 15 is able to drive driving wheel 20 and slowly run.First connection sheet 30 is consistent with the structure of the second connection sheet 35, and number is also consistent, and the first connection sheet 30 and the second connection sheet 35 are along drive shaft 24 Direction interval setting.After support rod 28 and the first connection sheet 30 are disconnected, push and drive along the direction of drive shaft 24 Driving wheel 20 makes the end of support rod 28 close to the second connection sheet 35, and support rod 28 can be connected with the second connection sheet 35.
No matter support rod 28 is connected in the first connection sheet 30 or is connected in the second connection sheet 35, by multiple support rods 28 mutual restriction effect, driving wheel 20 can keep stable, and driving wheel 20 can be in radial directions and on axis direction It keeps stablizing, makes one sufficiently stable after standing on pedal 18.
Intelligent flight device with above structure, as aircraft in use, be connected to clamping ring 21 on axle sleeve 31, It is connected to the end of support rod 28 in first connection sheet 30, so that motor 15 is able to drive 19 high-speed rotation of blade group, and make Driving wheel 20 and motor 15 are in discrete state;Blade group 19 is located at the outside of wheel rim 26 at this time, and blade is in the shape of expansion State.
Intelligent flight device in use, be connected to clamping ring 21 on blowout patche 32, makes the end of support rod 28 as walking device Portion is connected in the second connection sheet 35, so that motor 15 is able to drive driving wheel 20 and is slowly run, and makes blade group 19 and motor 15 are in discrete state;Blade group 19 is located at the inside of wheel rim 26 at this time, and blade is in folded state.Inside wheel rim 26 Blade group 19 can be driven wheel 20 protection, make Intelligent flight device blade group 19 in ground running be not readily susceptible to damage Wound.
As shown in Fig. 2, being arranged with connector sleeve 36 in connecting shaft 12, connector sleeve 36 and connecting shaft 12 are rotatablely connected, pedal 18 It is connected to connector sleeve 36, host 11 is internally provided with controller, gyroscope, acceleration transducer and wireless communication module, pedal Gravity sensor and wireless communication module are provided in 18;Multifunctional intellectual aircraft further includes remote controler, is also set in remote controler It is equipped with wireless communication module.
Using connector sleeve 36, make to make pedal 18 when in use for the relationship being flexibly connected between pedal 18 and connecting shaft 12 It can sway forwards and backwards.The inclination angle that pedal 18 can be calculated using gravity sensor and acceleration transducer, when pedal 18 tilts When can generate analog signal, controller is transferred to by wireless transport module, generates control signal, make motor 15 accelerate or Slow down, and then controls the traveling of Intelligent flight device.Gyroscope is arranged in host 11 can measure the inclined angle speed of host 11 Degree can make the turning walking of Intelligent flight device, and can complete creeping motion.
In order to enable the Intelligent flight device to take into account quick airflight and stablize the function of ground run, each component can be with What is made is more frivolous, so that the Intelligent flight device is served only for the lesser child's traveling of carrying weight, it is larger to be not used to carrying weight Adult.
The end of support rod 28 forms two parallel lugs, and link slot 29 is located between two lugs, opens on lug Equipped with fixation hole, fixation hole is also offered in the first connection sheet 30 and the second connection sheet 35.It is all provided in support rod 28 and connection sheet Fixation hole is set, support rod 28 is enable to connect with connection sheet by pin shaft, makes more stable at tie point, gap is smaller, driving Wheel 20 can be more stable.
As shown in Fig. 1 and Fig. 9, linking arm 14 is of a straight line type, and the end of linking arm 14 is articulated with the end of connecting shaft 12, even Horizontality can be turned to by vertical state by connecing arm 14.
As shown in Fig. 2, the bottom setting of host 11, there are two undercarriage 37, top and 11 phase of host of undercarriage 37 are cut with scissors It connects, can be accepted undercarriage 37 when being used as walking device, making undercarriage 37 not influences the walking of Intelligent flight device.It is main The holder being detachably connected with it can be set in the bottom of machine 11, and holder is set between two undercarriages 37.It can on holder To connect video camera, the Intelligent flight device is enable to complete the task of taking photo by plane.Holder can be removed when walking.
As shown in Fig. 2, the end of connecting shaft 12 is provided with attachment base 38, multiple connecting holes 39 are provided on attachment base 38, Multiple connecting holes 39 are also equipped on linking arm 14;Linking arm 14 and attachment base 38 are by extremely when linking arm 14 is in a vertical state Few two pin shafts are connected, and the linking arm 14 when in a horizontal state of linking arm 14 is connected with attachment base 38 by least two pin shafts.
The end of linking arm 14 is connected to attachment base 38.Multiple connecting holes 39 can be set in the end of linking arm 14, even Also multiple connecting holes 39 can be set on joint chair 38 so that no matter linking arm 14 is under which state, linking arm 14 with connect Can have at least two tie points between seat 38, drive assembly 13 is made to be able to maintain stabilization.
As shown in figure 4, axle sleeve 31, between blowout patche 32 and connecting column 25, multiple second connection sheets 35 are located at blade group 19 And between connecting column 25.This positional relationship makes blade group 19 and driving wheel 20 can be suitable along the axis direction of drive shaft 24 It adjusts sharply.
The foregoing description of the disclosed embodiments enables those skilled in the art to implement or use the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, as defined herein General Principle can be realized in other embodiments without departing from the spirit or scope of the present invention.Therefore, of the invention It is not intended to be limited to the embodiments shown herein, and is to fit to and the principles and novel features disclosed herein phase one The widest scope of cause.

Claims (8)

1. a kind of multifunctional intellectual aircraft, which is characterized in that including host, the two sides of the host are each provided with a connection Axis, is provided with drive assembly in the connecting shaft, and the drive assembly includes linking arm, motor and driver, the motor Outside is provided with housing, and one end of the linking arm connects the housing, and the other end of linking arm is hinged with the connecting shaft, Pedal is connected in the connecting shaft;
The driver includes blade group and driving wheel, and the blade group is located at the top of the driving wheel, the blade group Diameter is greater than the outer diameter of the driving wheel, and the blade group includes multiple blades, and the blade is folding structure, the blade The diameter of the blade group is less than the outer diameter of the driving wheel after folding;The blade group is connected with the motor and blade group energy Enough mutually to separate with motor, the driving wheel is mutually separated with the motor and driving wheel can be connected to the motor and connect.
2. multifunctional intellectual aircraft according to claim 1, which is characterized in that the blade group further includes clamping ring, Multiple blades are connected to the clamping ring;The blade includes blade root and leaf tip, the blade root and leaf tip phase Hingedly.
3. multifunctional intellectual aircraft according to claim 2, which is characterized in that the motor is connected with drive shaft, institute The end for stating housing has hollow connecting column, and the drive shaft passes through the connecting column;The driving wheel includes wheel rim, cover tire And multiple support rods, the cover tire are connected on the outside of the wheel rim, multiple support rods are connected on the inside of the wheel rim, described One end of support rod is fixedly connected with wheel rim, and the other end of support rod is provided with link slot, and the outside of the connecting column is circumferentially Multiple first connection sheets are provided with, the link slot of each support rod is connected to first connection sheet;
The drive shaft is externally connected to axle sleeve, and the axle sleeve can be rotated synchronously with drive shaft, and the end of the axle sleeve is set It is equipped with blowout patche, the blowout patche and the axle sleeve are rotatablely connected;Keyway, the outside of the axle sleeve are provided on the inside of the clamping ring It is provided with connecting key, the connecting key is inserted into the keyway, is provided with puller bolt, the end of puller bolt on the clamping ring It is abutted against with axle sleeve, unclamping the puller bolt can be such that the clamping ring mutually separates with axle sleeve, and can connect clamping ring Outside the blowout patche;The outer diameter of the axle sleeve is consistent with the outer diameter of the connecting column, and the outside of the axle sleeve is circumferentially arranged There are multiple second connection sheets;
The diameter of the blade group is less than the internal diameter of the wheel rim after the leaf folding;The link slot of the support rod can be with First connection sheet mutually separates and is connected to second connection sheet.
4. multifunctional intellectual aircraft according to claim 3, which is characterized in that be arranged with connection in the connecting shaft Set, the connector sleeve and connecting shaft are rotatablely connected, and the pedal is connected to the connector sleeve, and the host is internally provided with control Device, gyroscope, acceleration transducer and wireless communication module are provided with gravity sensor and wireless telecommunications mould in the pedal Block;The multifunctional intellectual aircraft further includes remote controler, is also equipped with wireless communication module in the remote controler.
5. multifunctional intellectual aircraft according to claim 3, which is characterized in that the linking arm is of a straight line type, connection The end of arm is articulated with the end of the connecting shaft, and linking arm can turn to horizontality by vertical state.
6. multifunctional intellectual aircraft according to claim 5, which is characterized in that there are two the bottom settings of the host Undercarriage, top and the host of the undercarriage are hinged, and the bottom of the host is additionally provided with the cloud being detachably connected with it Platform, the holder are located between two undercarriages.
7. multifunctional intellectual aircraft according to claim 5, which is characterized in that the end of the connecting shaft is provided with company Joint chair is provided with multiple connecting holes on the attachment base, multiple connecting holes is also equipped on the linking arm;At the linking arm Linking arm is connected with attachment base by least two pin shafts when vertical state, the linking arm linking arm when in a horizontal state It is connected with attachment base by least two pin shafts.
8. multifunctional intellectual aircraft according to claim 3, which is characterized in that the axle sleeve is located at the blowout patche and company It connects between column, multiple second connection sheets are between the blade group and the connecting column.
CN201910686240.4A 2019-07-29 2019-07-29 A kind of multifunctional intellectual aircraft Withdrawn CN110329499A (en)

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Application Number Priority Date Filing Date Title
CN201910686240.4A CN110329499A (en) 2019-07-29 2019-07-29 A kind of multifunctional intellectual aircraft

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CN201910686240.4A CN110329499A (en) 2019-07-29 2019-07-29 A kind of multifunctional intellectual aircraft

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Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080048065A1 (en) * 2004-12-23 2008-02-28 Julian Kuntz Flying Device With Improved Movement on The Ground
CN101559702A (en) * 2009-03-27 2009-10-21 谢雁洲 Longitudinal-line-type dual-culvert vertical-lifting air-ground vehicle
CN105882959A (en) * 2015-02-13 2016-08-24 空中客车防卫和太空有限责任公司 Aircraft capable of vertical takeoff
CN207141389U (en) * 2017-08-15 2018-03-27 深圳市道通智能航空技术有限公司 Fold propeller, Power Component and unmanned vehicle
CN207225642U (en) * 2017-09-01 2018-04-13 高吉忠 More rotor balance aircraft and flight equipment
WO2018216825A1 (en) * 2017-05-22 2018-11-29 주식회사 케이엠씨로보틱스 Hybrid unmanned aerial vehicle capable of driving and flying

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080048065A1 (en) * 2004-12-23 2008-02-28 Julian Kuntz Flying Device With Improved Movement on The Ground
CN101559702A (en) * 2009-03-27 2009-10-21 谢雁洲 Longitudinal-line-type dual-culvert vertical-lifting air-ground vehicle
CN105882959A (en) * 2015-02-13 2016-08-24 空中客车防卫和太空有限责任公司 Aircraft capable of vertical takeoff
WO2018216825A1 (en) * 2017-05-22 2018-11-29 주식회사 케이엠씨로보틱스 Hybrid unmanned aerial vehicle capable of driving and flying
CN207141389U (en) * 2017-08-15 2018-03-27 深圳市道通智能航空技术有限公司 Fold propeller, Power Component and unmanned vehicle
CN207225642U (en) * 2017-09-01 2018-04-13 高吉忠 More rotor balance aircraft and flight equipment

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Application publication date: 20191015