CN108557065A - A kind of flight for unmanned plane and road row switching device - Google Patents
A kind of flight for unmanned plane and road row switching device Download PDFInfo
- Publication number
- CN108557065A CN108557065A CN201711424341.1A CN201711424341A CN108557065A CN 108557065 A CN108557065 A CN 108557065A CN 201711424341 A CN201711424341 A CN 201711424341A CN 108557065 A CN108557065 A CN 108557065A
- Authority
- CN
- China
- Prior art keywords
- support shaft
- flight
- runner
- unmanned plane
- wheel
- 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.)
- Pending
Links
Classifications
-
- 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
- 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
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Transportation (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
The invention belongs to flight instruments technical fields, and in particular to a kind of flight for unmanned plane and road row switching device, including connection arm mechanism that propeller is connect with propeller；The wheel connected by central rotating shaft, connection arm mechanism include the first linking arm, shaft, the second linking arm；It is provided with motor on second linking arm, which connect with propeller；Wheel includes runner, support shaft, secondary support shaft and directive wheel；It is provided with U-shaped guide groove on the left of runner, the left end of support shaft is provided with the connector of center pivot, and the right end of support shaft is connected with secondary support shaft, and axis connection directive wheel is supported by pair；The right side of runner is provided with multiple latches；This is used for the flight of unmanned plane and road row switching device, and unmanned plane can be provided to the motor of the power of propeller flight, and the wheel for being converted to road traveling provides power so that unmanned function has the multifunctional usage of road surface carrier for a long time in ground run.
Description
Technical field
The invention belongs to flight instruments technical fields, and in particular to a kind of flight with for unmanned plane is filled with road row switching
It sets.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and is provided for oneself
The not manned aircraft that presetting apparatus manipulates.Without cockpit on machine, but automatic pilot, presetting apparatus, letter are installed
Cease the equipment such as harvester.On ground, naval vessels or machine tool remote control station personnel are by equipment such as radars, to its into line trace, positioning,
Remote control, telemetering and Digital Transmission.Can it is wireless electric-controlled it is lower take off as conventional airplane or launched with booster rocket, also may be used
Aerial launch is taken to by machine tool to fly.
Unmanned plane includes at least fuselage, engine, mast and paddle clamp pin axis.Wherein, mast and paddle clamp pin axis
It is end to be arranged in unmanned aerial vehicle body, and engine is arranged in the inside of unmanned aerial vehicle body, with for the rotor wing rotation without other
Power is provided.
The motor of existing unmanned plane only provides the power of propeller flight, for support fuselage before take-off or after landing
The sliding wheel run does not provide power, and therefore, unmanned plane cannot be for a long time in ground run, this causes existing unmanned plane can only be
Airflight does not have the multifunctional usage of road surface carrier.
Invention content
The purpose of the present invention is overcome the problems, such as that existing unmanned plane does not have long-time road traveling.
For this purpose, the present invention provides a kind of flight for unmanned plane and road row switching device, including propeller and spiral
The connection arm mechanism of paddle connection；The wheel connected by central rotating shaft, is used to support fuselage, and the connection arm mechanism includes first
Linking arm, shaft, the second linking arm, left and right is flexible in the horizontal direction across wheel for the right end of first linking arm, and passes through
Shaft is connect with the second linking arm；
It is provided with motor on second linking arm, which connect with propeller；
The wheel includes runner, support shaft, secondary support shaft and directive wheel；
It is provided with U-shaped guide groove on the left of the runner, the notch of the guide groove is towards the axle center of runner；
The left end of the support shaft is provided with the connector of center pivot, and the right end of support shaft is connected with secondary support shaft, leads to
Secondary support axis connection directive wheel is crossed, which is arranged in the top surface guide groove of runner；
The right side of runner is provided with multiple latches, and the latch is using the bottom center of runner as axle center, in center radiation row
Row.
Second linking arm rotates to be vertical state using shaft as fulcrum by horizontality.
The lower end of the support shaft is additionally provided with damper, the lower end of the damper and secondary support axis connection.
Beneficial effects of the present invention：This flight for unmanned plane provided by the invention and road row switching device, can
The motor that unmanned plane is provided to the power of propeller flight, the wheel for being converted to road traveling provide power so that unmanned plane
Can have the multifunctional usage of road surface carrier for a long time in ground run.
The present invention is described in further details below with reference to attached drawing.
Description of the drawings
Fig. 1 is the flight and road row switching device state of flight figure for unmanned plane.
Fig. 2 is the flight and road row switching device switching intermediate state figure for unmanned plane.
Fig. 3 is the flight and road row switching device ground run state diagram figure for unmanned plane.
Fig. 4 is wheel mechanism schematic diagram.
In figure：1, runner；2, support shaft；3, damper；4, latch；5, secondary support shaft；6, directive wheel；7, center pivot；
8, U-shaped guide groove；9, blade；10, motor；11, the first linking arm；12, shaft；13, the second linking arm；14, wheel.
Specific implementation mode
Reach the technological means and effect that predetermined purpose is taken for the present invention is further explained, below in conjunction with attached drawing and reality
Example is applied to specific implementation mode, structure feature and its effect of the present invention, detailed description are as follows.
Embodiment 1：
In order to solve the problems, such as that existing unmanned plane does not have long-time road traveling, the present invention provides one kind such as Fig. 1 institutes
The flight for unmanned plane shown and road row switching device, including connection arm mechanism that propeller 9 is connect with propeller 9；Pass through
The wheel 14 that central rotating shaft 7 connects, is used to support fuselage, and the connection arm mechanism includes the first linking arm 11, shaft 12, and second
Linking arm 13, the right end of first linking arm 11 passes through wheel 14, and left and right is flexible in the horizontal direction, and passes through shaft 12 and the
Two linking arms 13 connect；
It is provided with motor 10 on second linking arm 13, which connect with propeller 9；
The wheel 14 includes runner 1, support shaft 2, secondary support shaft 5 and directive wheel 6；
The left side of the runner 1 is provided with U-shaped guide groove 8, and the notch of the guide groove 8 is towards the axle center of runner 1；
The left end of the support shaft 2 is provided with the connector of center pivot 7, and the right end of support shaft 2 is connected with secondary support shaft
5, directive wheel 6 is connected by secondary support shaft 5, which is arranged in the top surface guide groove 8 of runner 1；
The right side of runner 1 is provided with multiple latches 4, which, using the bottom center of runner 1 as axle center, is in center spoke
Penetrate arrangement.
As shown in Fig. 2, above-mentioned second linking arm 13 is fulcrum with shaft 12, vertical state is rotated to be by horizontality；So
The first linking arm 11 is shunk to the left afterwards, and propeller 9 is driven to be moved to the left, and motor 10 is inserted into the hollow position of wheel 14, final spiral shell
The blade for revolving paddle 9 and the latch of wheel right side coincide, as shown in figure 3, thus providing state by flying power is switched to road
Face driving dynamics provide state.
Unmanned plane can be provided the electronic of the power of propeller flight by the flight for unmanned plane and road row switching device
Machine, the wheel for being converted to road traveling provide power so that unmanned function has the more of road surface carrier for a long time in ground run
Function and usage.
Embodiment 2：
The right end of the support shaft 2 is additionally provided with damper 3, and the right end of the damper 3 is connect with secondary support shaft 5, is had
Good cushioning effect so that unmanned plane is advanced more steady；And damper 3 installation using be clamped by the way of, dismantling side
Just, for safeguarding that wheel is also very easy to.
As shown in figure 4, the support shaft 2 is provided with 3, corresponding directive wheel 6 is provided with 3, and with the top of runner 1
The axle center in face is that the angle that vertex is distributed each two support shaft 2 in uniform angle is 120 °, takes full advantage of triangle stabilization in this way
Specific, the support column fuselage that unmanned plane traveling during can stablize highly stable for the support of runner 1 of property.
The above content is a further detailed description of the present invention in conjunction with specific preferred embodiments, and it cannot be said that
The specific implementation of the present invention is confined to these explanations.For those of ordinary skill in the art to which the present invention belongs, exist
Under the premise of not departing from present inventive concept, a number of simple deductions or replacements can also be made, all shall be regarded as belonging to the present invention's
Protection domain.
Claims (3)
1. a kind of flight for unmanned plane and road row switching device, including linking arm that propeller (9) is connect with propeller (9)
Mechanism；The wheel (14) connected by central rotating shaft (7), is used to support fuselage, it is characterised in that：The connection arm mechanism includes
The right end of first linking arm (11), shaft (12), the second linking arm (13), first linking arm (11) passes through wheel (14) edge
Horizontal direction or so is flexible, and is connect with the second linking arm (13) by shaft (12)；
It is provided with motor (10) on second linking arm (13), which connect with propeller (9)；The wheel
(14) include runner (1), support shaft (2), secondary support shaft (5) and directive wheel (6)；
It is provided with U-shaped guide groove (8) on the left of the runner (1), the axle center of the notch of the guide groove (8) towards runner (1)；
The left end of the support shaft (2) is provided with the connector of center pivot (7), and the right end of support shaft (2) is connected with secondary support
Axis (5) connects directive wheel (6) by secondary support shaft (5), which is arranged in the top surface guide groove (8) of runner (1)；
The right side of runner (1) is provided with multiple latches (4), which, using the bottom center of runner (1) as axle center, is in center spoke
Penetrate arrangement.
2. as described in claim 1 for the flight of unmanned plane and road row switching device, it is characterised in that：The support shaft
(2) right end is additionally provided with damper (3), and the right end of the damper (3) is connect with secondary support shaft (5).
3. as described in claim 1 for the flight of unmanned plane and road row switching device, it is characterised in that：Second connection
For fulcrum, vertical state is rotated to be by horizontality with shaft (12) for arm (13).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711424341.1A CN108557065A (en) | 2017-12-25 | 2017-12-25 | A kind of flight for unmanned plane and road row switching device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711424341.1A CN108557065A (en) | 2017-12-25 | 2017-12-25 | A kind of flight for unmanned plane and road row switching device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108557065A true CN108557065A (en) | 2018-09-21 |
Family
ID=63530570
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711424341.1A Pending CN108557065A (en) | 2017-12-25 | 2017-12-25 | A kind of flight for unmanned plane and road row switching device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108557065A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109455051A (en) * | 2018-10-30 | 2019-03-12 | 佛山市神风航空科技有限公司 | A kind of 4 wheel driven hovercar |
| CN110194264A (en) * | 2019-05-13 | 2019-09-03 | 艾欣创科技(北京)有限公司 | A kind of unmanned plane |
-
2017
- 2017-12-25 CN CN201711424341.1A patent/CN108557065A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109455051A (en) * | 2018-10-30 | 2019-03-12 | 佛山市神风航空科技有限公司 | A kind of 4 wheel driven hovercar |
| CN110194264A (en) * | 2019-05-13 | 2019-09-03 | 艾欣创科技(北京)有限公司 | A kind of unmanned plane |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP3466812B1 (en) | Tiltrotor aircraft having a downwardly tiltable aft rotor | |
| CN109305357B (en) | Double-tilting-wing aircraft with quadrilateral link mechanism | |
| CN109018320B (en) | X-shaped tilt wing aircraft | |
| US9475575B2 (en) | Convertible compounded rotorcraft | |
| US20170183088A1 (en) | Multi-Rotor Passenger-Carrying Aircraft | |
| RU2724006C1 (en) | Aircraft | |
| US4662588A (en) | Airplane configured with a moveable disk structure | |
| CN102627146A (en) | Tilt rotor aircraft with fixed engine arrangement | |
| CN103895860A (en) | Novel coaxial double-rotary double-degree-of-freedom eight-rotor-wing amphibious aircraft | |
| CN105151296A (en) | Multi-axis manned aircraft | |
| CN105730676A (en) | Aircraft | |
| CN111196346A (en) | Distributed electric propulsion tilt rotor unmanned aerial vehicle | |
| CN102673780A (en) | Double-configuration aircraft | |
| CN108557065A (en) | A kind of flight for unmanned plane and road row switching device | |
| CN104843183A (en) | Tail rotor pitch structure of unmanned helicopter | |
| CN105059525A (en) | Aerodynamic layout of small-sized vertical takeoff and landing aircraft | |
| CN206954510U (en) | It is a kind of can VTOL fixed-wing unmanned plane | |
| CN107150806A (en) | It is a kind of can VTOL fixed-wing unmanned plane | |
| CN107757914A (en) | Double dynamical VTOL fixed-wing unmanned plane | |
| CN206437196U (en) | A kind of vee tail unmanned plane of the foldable rotor arm of band | |
| CN105000177A (en) | Multi-axis unmanned aerial vehicle | |
| CN103818551B (en) | Vertical takeoff and landing rotary wind type unmanned vehicle | |
| CN203698662U (en) | Vertical take-off and landing rotary wing type unmanned aerial vehicle | |
| CN204507267U (en) | A kind of tail-rotor distance changing mechanism of depopulated helicopter | |
| CN103803081B (en) | Vertical takeoff and landing rotary wind type unmanned vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180921 |