CN109249767A - A kind of deformation carplane - Google Patents
A kind of deformation carplane Download PDFInfo
- Publication number
- CN109249767A CN109249767A CN201811276911.1A CN201811276911A CN109249767A CN 109249767 A CN109249767 A CN 109249767A CN 201811276911 A CN201811276911 A CN 201811276911A CN 109249767 A CN109249767 A CN 109249767A
- Authority
- CN
- China
- Prior art keywords
- carplane
- lift
- engine
- undercarriage
- lift unit
- 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- Withdrawn
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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
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/52—Skis or runners
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
Abstract
A kind of deformation carplane belongs to vehicle technology field, including fuselage, pivoted arm, lift unit, power device of verting, controller, undercarriage.There are two types of operational modes, respectively Ground Vehicle mode and six rotor flying modes for carplane；When transforming to Ground Vehicle mode, undercarriage props up carplane, and pivoted arm drives lift unit in a vertical state, and undercarriage is retracted to below fuselage, four lift units provide the power of forward or backward by two power devices of verting with ground face contact and always in off-mode for carplane；When transforming to six rotor flying modes, undercarriage props up carplane, pivoted arm drives lift unit to be in horizontality, the power device that will vert also is adjusted to horizontality, four lift units and two, which are verted, power device while providing lift straight up for carplane, and carplane is flown with similar six rotorcraft flying method.The present invention is flexible；Deformation process is simple and convenient.
Description
Technical field
A kind of deformation carplane belongs to vehicle technology field more particularly to a kind of deformation carplane.
Background technique
Automobile be it is a kind of commonly using the vehicles, trip and life to people provide many convenience, existing vapour
The function of vehicle is relatively simple, and current automobile is typically only capable to travel in land, it is thus impossible to cope with complicated landform ring
Border, such as congestion in road；In view of the above problems, therefore, it is necessary to design a kind of multipurpose automobile.
Summary of the invention
In view of this, can be travelled on the ground the present invention provides a kind of deformation carplane, can also fly in the sky.
A kind of deformation carplane, including fuselage, pivoted arm, lift unit, power device of verting, controller, undercarriage.Lift
Device provides lift in the form of driven by engine propeller；There are four lift units, and corresponding pivoted arm has four, and four turn
Left and right is evenly arranged in fuselage two sides to arm two-by-two, and each lift unit is installed on a pivoted arm；Pivoted arm can be on fuselage
Lift unit, so that lift unit is in horizontality or vertical state, and can be fixed on corresponding position by rotation；It verts dynamic
Power device provides power in the form of driven by engine propeller；There are two power devices of verting, they pass through bracket pair
Claim the front-end and back-end for being arranged in fuselage；Power device of verting can run-off the straight, convert produced by lift direction；Undercarriage
Positioned at the lower section of fuselage, which is able to carry out flexible；Controller is located in fuselage, controller and lift unit and verts dynamic
The engine of power device is connected, and the work shape of the engine of lift unit and power device of verting can be controlled by controller
State also can control the tilt angle for power device of verting by controller；Controller also can control undercarriage and be extended simultaneously
Or it shrinks.There are two types of operational modes, respectively Ground Vehicle mode and six rotor flying modes for the carplane；In the carplane
When transforming to Ground Vehicle mode, carplane is propped up in undercarriage elongation, and pivoted arm drives lift unit in a vertical state, undercarriage
It is retracted to below fuselage, four lift units pass through two power devices of verting with ground face contact and always in off-mode
The power of forward or backward is provided for carplane；Control lift unit carries out deflection on pivoted arm, so that carplane is on ground
Face can be realized steering when walking；When the carplane needs to transform to six rotor flying modes, undercarriage elongation is propped up winged
Driving drives lift unit to be in horizontality, by power device of verting so that four lift units leave ground by pivoted arm
Also it is adjusted to horizontality, four lift units and two are verted at this time power device while providing straight up for carplane
Lift, lift unit and verts power device under the coordinated control of controller, and carplane is flown with similar six rotorcraft
Mode is flown.
The lift unit includes engine, propeller, wheel rim, cover tire.Engine is mounted on pivoted arm, propeller installation
On the engine, propeller tip is connected to the inner ring of wheel rim；Cover tire is placed in the outer ring of wheel rim, plays cushioning effect；It is filled in lift
The spoke for serving as wheel in use, propeller serves as wheel, cover tire and ground face contact are set, lift unit is whole in the power dress that verts
Rolling is carried out under active force caused by setting.
The power device of verting includes engine, propeller, leaning device.Leaning device is rack-mount, starts
Machine is mounted on leaning device, driven by engine propeller rotational.Leaning device can adjust engine under push-and-pull action
Tilt angle, and then change lift direction produced by engine.
The leaning device includes motion bar, mounting base, push-pull rod, steering engine；The middle part of motion bar is existed by bearing removable mounting
On bracket, motor cavity is in the upper end of motion bar, and mounting base is for installing engine, the lower end of motion bar and one end of push-pull rod
It is connected, the other end of push-pull rod is connected on steering engine, and steering engine is rack-mount, and steering engine is connected with controller.Pass through control
System control steering engine drives push-pull rod movement, so that motion bar occurs to drive engine run-off the straight.
The pivoted arm is using the mechanical arm at least gathered around there are two freedom degree, and mechanical arm is connected with controller, in controller control
Under system, pivoted arm can adjust lift unit and be in horizontality or vertical state, while can also be in carplane in ground run
The deflection of lift unit is adjusted to turn to control.
Undercarriage uses Sledge type undercarriage, and undercarriage is by telescopic rod and is mounted below fuselage, by adjusting flexible
The length of bar controls the length of undercarriage.
Engine uses motor or internal combustion engine.
The propeller of lift unit at least possesses three pieces blade, and it is strong that enhancing lift unit fills structure when the wheel is in use
Degree.
A kind of deformation carplane of the invention, carplane possess two kinds of operation moulds of Ground Vehicle mode and six rotor flying modes
Formula；Lift unit can provide lift also for carplane can serve as wheel use；The carplane only needs to lead in ground running
The power device of verting for crossing itself provides the thrust moved forward or back, is driven, is reduced without using individual engine
Carplane overall weight；Since four pivoted arms have turning function, so that four lift units are filling equal energy when the wheel is in use
It is enough turned to, this makes carplane flexible when driving on the ground；Deformation process, which can be sitting in fuselage, passes through control
Device controls to realize, simple and convenient.
Detailed description of the invention
Fig. 1 is the more rotor flying mode configuration schematic top plan views of the present invention；Fig. 2 is that Ground Vehicle mode configuration of the present invention is overlooked
Schematic diagram；Fig. 3 is Ground Vehicle mode configuration schematic side view of the present invention；Fig. 4 is that the present invention is verted powerplant configuration schematic diagram；
Fig. 5 is lift unit structural schematic diagram of the present invention.
In figure, 1- fuselage, 2- pivoted arm, 3- lift unit, 31- first motor, the first propeller of 32-, 33- wheel rim, outside 34-
Tire, 4- vert power device, the second motor of 41-, the second propeller of 42-, 43- leaning device, 431- motion bar, 432- installation
Seat, 433- push-pull rod, 434- steering engine, 5- controller, 6- undercarriage, 7- bracket.
Specific embodiment
The present invention is illustrated with reference to the accompanying drawing.
A kind of deformation carplane, including fuselage 1, pivoted arm 2, lift unit 3, power device of verting 4, controller 5, undercarriage
6.Lift unit 3 provides lift in the form of motor drives propeller；There are four lift units 3, and corresponding pivoted arm 2 has four
Item, left and right is evenly arranged in 1 two sides of fuselage to four pivoted arms 2 two-by-two, and each lift unit 3 is installed on a pivoted arm 2；Pivoted arm
2 can rotate on the fuselage 1, so that lift unit 3 is in horizontality or vertical state, and can be fixed on lift unit 3
Corresponding position；Power device of verting 4 provides power in the form of motor drives propeller；There are two power devices of verting 4,
They pass through the front-end and back-end that bracket 7 is arranged symmetrically in fuselage 1；Power device of verting 4 can run-off the straight, transformation produced
The direction of raw lift；Undercarriage 6 is located at the lower section of fuselage 1, which is able to carry out flexible；
Controller 5 is located in fuselage 1, and controller 5 is connected with the motor of lift unit 3 and power device 4 of verting, and passes through control
Device 5 can control lift unit 3 and vert power device 4 motor working condition, also can control by controller 5 vert it is dynamic
The tilt angle of power device 4；Controller 5 also can control undercarriage 6 and be extended or be shunk simultaneously.
The lift unit 3 includes first motor 31, the first propeller 32, wheel rim 33, cover tire 34.First motor 31 is installed
On pivoted arm 2, the first propeller 32 is mounted in first motor 31, and the first propeller 32 possesses four blades, the tip of blade
It is connected to the inner ring of wheel rim 33；Cover tire 34 is placed in the outer ring of wheel rim 33, plays cushioning effect；Wheel is served as in lift unit 3 to use
When, the first propeller 32 serves as the spoke of wheel, and cover tire 34 and ground face contact, lift unit 3 are whole in 4 institute of power device of verting
Rolling is carried out under the active force of generation.
The power device 4 of verting includes the second motor 41, the second propeller 42, leaning device 43.Leaning device 43 is pacified
On bracket 7, the second motor 41 is mounted on leaning device 43, and the second motor 41 drives the rotation of the second propeller 42.Inclination
Mechanism 43 can adjust the tilt angle of the second motor 41 under push-and-pull action, and then change lift side produced by the second motor 41
To.
The leaning device 43 includes motion bar 431, mounting base 432, push-pull rod 433, steering engine 434；
Through bearing removable mounting on bracket 7, the second 41, motor is located at the upper end of motion bar 431 at the middle part of motion bar 431, installation
For installing the second motor 41, the lower end of motion bar 431 is connected seat 432 with one end of push-pull rod 433, push-pull rod 433 it is another
One end is connected on steering engine 434, and steering engine 434 is mounted on bracket 7, and steering engine 434 is connected with controller 5.It is controlled by control
Steering engine 434 drives push-pull rod 433 to move, so that motion bar 431 occurs to drive 41 run-off the straight of the second motor.
The pivoted arm 2 is using the mechanical arm at least gathered around there are two freedom degree, and mechanical arm is connected with controller 5, in controller 5
Under control, pivoted arm 2 can adjust lift unit 3 and be in horizontality or vertical state, while can also be in carplane in ground row
The deflection of lift unit 3 is adjusted when sailing to turn to control.
Undercarriage 6 uses Sledge type undercarriage 6, and undercarriage 6 is by telescopic rod and is mounted on 1 lower section of fuselage, by adjusting
The length of telescopic rod controls the length of undercarriage 6.
There are two types of operational modes, respectively Ground Vehicle mode and six rotor flying modes for the carplane；In the flight
When vehicle transforms to Ground Vehicle mode, telescopic rod elongation drives undercarriage 6 to prop up carplane, and pivoted arm 2 drives lift unit 3 to be in perpendicular
Straight state, undercarriage 6 are retracted to 1 lower section of fuselage, the cover tire 34 and ground face contact and four first motors 31 of four lift units 3
Always it is in off-mode；Change the tilt angle of the second motor 41 by the movement of control steering engine 434；In two the second motors
41 when turning forward, and two the second motors 41 can provide the thrust of advance for carplane；Two the second motors 41 to
When rear-inclined, two the second motors 41 can provide the thrust of retrogressing for carplane；Lift unit 3 is controlled by pivoted arm 2 to carry out
Deflection enables carplane to change driving direction in ground running；Need to transform to six rotors in the carplane
When offline mode, telescopic rod elongation drives undercarriage 6 to prop up carplane, so that the cover tire 34 of four lift units 3 leaves ground,
Lift unit 3 is driven to be in horizontality by pivoted arm 2, the power device that will vert 4 is also adjusted to horizontality, and four the at this time
One motor 31 and two the second motors 41 provide lift straight up simultaneously for carplane, and four first motors 31 and two the
Two motors 41 under the coordinated control of controller 5, flown with similar six rotorcraft flying method by carplane.
Claims (9)
1. a kind of deformation carplane, it is characterised in that: including fuselage (1), pivoted arm (2), lift unit (3), power device of verting
(4), controller (5), undercarriage (6)；Lift unit (3) provides lift in the form of driven by engine propeller；Lift dress
It sets there are four (3), left and right is arranged in fuselage (1) two sides to four pivoted arms (2) two-by-two, and each lift unit (3) is installed in one
On pivoted arm (2)；Power device of verting (4) provides power in the form of driven by engine propeller；Power device of verting (4) has
Two, they pass through the front-end and back-end that bracket (7) is arranged symmetrically in fuselage (1)；Undercarriage (6) is located under fuselage (1)
Side；Controller (5) is located in fuselage (1), the engine progress of controller (5) and lift unit (3) and power device of verting (4)
Electric signal connection.
2. a kind of deformation carplane according to claim 1, it is characterised in that: lift unit (3) includes engine, spiral
Paddle, wheel rim (33), cover tire (34)；Engine is mounted on pivoted arm (2), and propeller is installed on the engine, and propeller tip connects
It is connected to the inner ring of wheel rim (33)；Cover tire (34) is placed in the outer ring of wheel rim (33).
3. a kind of deformation carplane according to claim 1, it is characterised in that: the power device of verting (4) includes hair
Motivation, propeller, leaning device (43)；Leaning device (43) is mounted on bracket (7), and engine is mounted on leaning device (43)
On, driven by engine propeller rotational.
4. a kind of deformation carplane according to claim 3, it is characterised in that: the leaning device (43) includes motion bar
(431), mounting base (432), push-pull rod (433), steering engine (434)；The middle part of motion bar (431) is by bearing removable mounting in bracket
(7) on, motor cavity is connected in the upper end of motion bar (431), the lower end of motion bar (431) with one end of push-pull rod (433),
The other end of push-pull rod (433) is connected on steering engine (434), and steering engine (434) is mounted on bracket (7), steering engine (434) and control
The connection of device (5) electric signal.
5. a kind of deformation carplane according to claim 1, it is characterised in that: the pivoted arm (2), which uses, at least possesses two
The mechanical arm of a freedom degree.
6. a kind of deformation carplane according to claim 1, it is characterised in that: undercarriage (6) uses Sledge type undercarriage
(6), undercarriage (6) is mounted below fuselage (1) by telescopic rod.
7. a kind of deformation carplane according to claim 1, it is characterised in that: engine uses motor or internal combustion engine.
8. a kind of deformation carplane according to claim 1, it is characterised in that: the propeller of lift unit (3) is at least gathered around
There is three pieces blade.
9. any a kind of deformation carplane according to claim 1 ~ 8, it is characterised in that: there are two types of fortune for the carplane
Row mode, respectively Ground Vehicle mode and six rotor flying modes；When the carplane transforms to Ground Vehicle mode, undercarriage
(6) it extends, props up carplane, pivoted arm (2) drives lift unit (3) in a vertical state, and undercarriage (6) is retracted to fuselage (1)
Lower section, four lift units (3) are winged by two power devices of verting (4) with ground face contact and always in off-mode
Driving provides the power moved forward or back；Control lift unit (3) carries out deflection on pivoted arm (2), so that carplane exists
It can be realized steering when ground running；When the carplane needs to transform to six rotor flying modes, undercarriage (6) elongation,
Carplane is propped up, so that four lift units (3) leave ground, drives lift unit (3) to be in horizontal by pivoted arm (2)
State, the power device that will vert (4) are also adjusted to horizontality, at this time four lift units (3) and two power devices of verting (4)
Lift straight up, lift unit (3) and power device of verting (4) are provided in the coordination of controller (5) simultaneously for carplane
Under control, carplane is flown with similar six rotorcraft flying method.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811276911.1A CN109249767A (en) | 2018-10-30 | 2018-10-30 | A kind of deformation carplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811276911.1A CN109249767A (en) | 2018-10-30 | 2018-10-30 | A kind of deformation carplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109249767A true CN109249767A (en) | 2019-01-22 |
Family
ID=65043102
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811276911.1A Withdrawn CN109249767A (en) | 2018-10-30 | 2018-10-30 | A kind of deformation carplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109249767A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110371284A (en) * | 2019-07-15 | 2019-10-25 | 谌薏冰 | A kind of deformable four-axle aircraft |
| WO2021078205A1 (en) * | 2019-10-22 | 2021-04-29 | 深圳市道通智能航空技术有限公司 | Land-air dual-use unmanned aerial vehicle |
| JP6952380B1 (en) * | 2020-08-11 | 2021-10-20 | 株式会社エアロネクスト | Mobile |
| CN113635721A (en) * | 2021-08-19 | 2021-11-12 | 西安戴森电子技术有限公司 | Air-land amphibious biped wheel multi-mode walking flying bionic robot |
| CN115520376A (en) * | 2022-09-27 | 2022-12-27 | 哈尔滨工业大学 | Air-ground dual-purpose mobile operation platform based on vector rotor wing and pose control system and method thereof |
| CN116834487A (en) * | 2021-01-30 | 2023-10-03 | 武汉发明家创新科技有限公司 | Vertical take-off and landing suspension movable wing tilting flying electric automobile, take-off and landing method and lifting steering method |
-
2018
- 2018-10-30 CN CN201811276911.1A patent/CN109249767A/en not_active Withdrawn
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110371284A (en) * | 2019-07-15 | 2019-10-25 | 谌薏冰 | A kind of deformable four-axle aircraft |
| WO2021078205A1 (en) * | 2019-10-22 | 2021-04-29 | 深圳市道通智能航空技术有限公司 | Land-air dual-use unmanned aerial vehicle |
| JP6952380B1 (en) * | 2020-08-11 | 2021-10-20 | 株式会社エアロネクスト | Mobile |
| CN116834487A (en) * | 2021-01-30 | 2023-10-03 | 武汉发明家创新科技有限公司 | Vertical take-off and landing suspension movable wing tilting flying electric automobile, take-off and landing method and lifting steering method |
| CN113635721A (en) * | 2021-08-19 | 2021-11-12 | 西安戴森电子技术有限公司 | Air-land amphibious biped wheel multi-mode walking flying bionic robot |
| CN115520376A (en) * | 2022-09-27 | 2022-12-27 | 哈尔滨工业大学 | Air-ground dual-purpose mobile operation platform based on vector rotor wing and pose control system and method thereof |
| CN115520376B (en) * | 2022-09-27 | 2023-08-25 | 哈尔滨工业大学 | Space-ground-based dual-purpose mobile operation platform and pose control system and control method thereof |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
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| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20190122 |
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| WW01 | Invention patent application withdrawn after publication |