CN110450589A - A kind of flight instruments - Google Patents
A kind of flight instruments Download PDFInfo
- Publication number
- CN110450589A CN110450589A CN201910870414.2A CN201910870414A CN110450589A CN 110450589 A CN110450589 A CN 110450589A CN 201910870414 A CN201910870414 A CN 201910870414A CN 110450589 A CN110450589 A CN 110450589A
- Authority
- CN
- China
- Prior art keywords
- rotor
- car body
- cockpit
- motor
- flight
- 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
- 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
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/46—Blades
- B64C27/473—Constructional features
- B64C27/50—Blades foldable to facilitate stowage of aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Body Structure For Vehicles (AREA)
Abstract
The invention discloses a kind of flight instruments, include car body, and car body front end is provided with cockpit；Two motor connecting respectively with driving wheel are set on the vehicle frame of car body front end, the power battery and the driven wheel on body rear end vehicle frame connecting on the car body of cockpit rear end with two motor；Cockpit rear end car body is provided with rotor and folds storehouse；Rotor folds storehouse and connects flight support component by shaft respectively on the bulkhead of cockpit, and flight support component is connect by rotor motor with foldable propeller；It further include the electric-control system on the car body of driver's seat bottom, the control panel being set in cockpit being electrically connected with electric-control system；Two motor, rotor motor, control panels are connect with electric-control system and power battery.The present invention is provided with folding propeller, and the ability that automobile can be made to have flight, mobility is higher, realizes and opens or withdraw, and handover operation is simple, can be avoided the normally travel for influencing automobile after withdrawal, simple and practical.
Description
Technical field
The present invention relates to automobile technical fields, more particularly, to a kind of flight instruments.
Background technique
Considerable restraint of the use of automobile by land situation, for example, can not in the sections of road of damage, landslide, traffic congestion,
It is not available in face of marsh, river, high mountain yet.The above problem will be avoided by so that automobile is had flight function.Current automobile quantity
It is all continuing to increase every year, following trip, which is had inconvenient traffic, to be more and more obvious, and it is also not that trip can not be limited by road conditions
A kind of trend come can be with if traffic jam occurs in traveling or is in an emergency when needing quickly to leave for automobile
It is also a kind of good mode that flying method, which is quickly withdrawn, so the automobile that can fly is the good selection of future transportation tool.It is existing
Some hovercars are usually by carplane, and this hovercar is actually small-sized aircraft.Also, by carplane
There is many technical problems, such as automobile form to change for change, causes volume, weight to increase, limits the land of automobile
The flexibility and driving of ground traveling.
Summary of the invention
The object of the invention is that providing flight instruments to solve the above-mentioned problems.
The technical scheme of the present invention is realized as follows:
A kind of flight instruments, include car body, and the car body front end is provided with cockpit；
Two motor connecting respectively with driving wheel, the cockpit rear end are set on the vehicle frame of the car body front end
The power battery and the driven wheel on the body rear end vehicle frame being connect on the car body with described two motor；
Car body described in the cockpit rear end is provided with rotor and folds storehouse；
The rotor folds storehouse and connects flight support component by shaft respectively on the bulkhead of the cockpit, described
Flight support component is connect by rotor motor with foldable propeller；
It further include the electric-control system on car body described in driver's seat bottom, what is be electrically connected with the electric-control system is set to institute
State the control panel in cockpit；
Described two motor, rotor motor, control panel are connect with electric-control system and power battery.
In the above scheme, the flight support component includes two support rods；
One end of two support rods is connected to the rotor by shaft and folds storehouse close to the bulkhead of the cockpit
On, the other end stretches out the rotor and folds storehouse and be connected with fixed cross beam by shaft, and two support rods are longitudinally set to institute
It states above car body；The fixed cross beam is horizontally-parallel to be set to above the car body；
The fixed cross beam both ends are separately connected by shaft folds arm end, and the folding arm is set to the fixed cross beam
Both ends extending direction, the other end for folding arm are equipped with the rotor motor, and the output end of the rotor motor is by turning
Axis is equipped with the foldable propeller.
In the above scheme, pass through shaft connecting rod end, the pull rod other end setting in the middle part of the fixed cross beam
There is inlay card end, is detachably connected with the engaging button of car body top setting.
In the above scheme, described the present embodiment, support rod are bent rod, and bending angle is obtuse angle.
In the above scheme, parallel with the support rod when folding arm folded state.
In the above scheme, be respectively equipped on the vehicle frame between described two driving wheels and two driven wheels with
The ducted fan that the electric-control system and power battery connect.
In the above scheme, the air opening end of the ducted fan is covered with the wind direction pendulum connecting with the electric-control system
Page.
In the above scheme, the rotor folds storehouse open end setting protective door, the protective door and the separate driving
The rotor in cabin folds storehouse port edge and is connected by shaft, and the rotor folds and is arranged in storehouse for anti-to unlatching after vehicle
Protect the hydraulic stem of door；
The hydraulic stem is electrically connected with the electric-control system and the power battery；
In the above scheme, the protective door is provided with corresponding with the swivel mount chimeric close to the side of the cockpit
Caulking groove.
Using above-mentioned technical proposal, the invention has the benefit that folding propeller is provided in device, it can
The ability for making automobile have flight, mobility is higher, realizes and opens or withdraw, handover operation is simple, can be avoided shadow after withdrawal
The normally travel of automobile is rung, it is simple and practical.
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 without any creative labor, may be used also for those of ordinary skill in the art
To obtain other drawings based on these drawings.
Fig. 1 is structural schematic diagram in main view of the invention；
Fig. 2 is the portion A enlarged diagram in Fig. 1 of the present invention；
Fig. 3 is schematic perspective view of the invention；
Fig. 4 is top view of the invention；
Fig. 5 is foldable propeller schematic diagram of the invention；
Fig. 6 is the bottom view of ducted fan of the invention；
Fig. 7 is the left view of flight support component of the invention.
The reference numerals are as follows:
1, power battery；2, driven wheel；3, ducted fan；4, rotor folds storehouse；5, wind direction slew page；6, swivel mount；7, may be used
Fold propeller；8, rotor motor；9, pull rod；10, cockpit；11, car body；12, motor；13, driving wheel；14, fixed horizontal
Beam；15, protective door；16, arm is folded；17, front windshield；18, electric-control system；19, engaging button；71, rotor blade；72, leaf
Piece connector.
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.
As Figure 1-Figure 4, a kind of flight instruments, including car body 11,11 front end of car body are additionally provided with cockpit 10；
Two motor 12 connecting respectively with driving wheel 13,10 rear end of cockpit are set on 11 front end vehicle frame of car body
The power battery 1 and the driven wheel 2 on 11 rear end vehicle frame of car body being connect on car body 11 with two motor 12；It drives
10 front end of cabin is provided with front windshield 17；Power battery 1 is that two motor 12 provide continuous driving force, makes two motor
12 respectively drive two driving wheels 13.
10 rear end car body 11 of cockpit is provided with rotor and folds storehouse 4, and rotor folding 4 open end of storehouse is equipped with anti-by shaft
Protect door 15.
Rotor folds storehouse 4 and connects flight support component, flight support by shaft respectively on the bulkhead of cockpit 10
Component is connect by rotor motor 8 with foldable propeller 7, and foldable propeller 7 is made to be set to 11 top of car body.
In the present embodiment, further includes the electric-control system 18 on driver's seat bottom car body 11, be electrically connected with electric-control system 18
What is connect is set in cockpit 10 control panel that vehicle is controlled convenient for driver, because the present embodiment is electronic hovercar, electricity
The inner space component that control system 18 generally occupies vehicle is big, and weight is larger, driver's seat bottom is set to, compared to the centre of car body
Position not only saves out interior space and is more easier vehicle in weight distribution, convenient for keeping automobile in flight course
Balance.
The present embodiment, flight support component specifically may include two support rods 6, and one end of two support rods 6 passes through shaft
It is connected to rotor and folds storehouse 4 on the bulkhead of cockpit 10, the other end stretches out rotor and folds storehouse 4 and be connected with by shaft solid
Determine crossbeam 14, two support rods 6 are longitudinal to be set to 11 top of car body, and fixed cross beam 14 is horizontally-parallel to be set to 11 top of car body；This reality
Example is applied, support rod 6 is bent rod, and bending angle is obtuse angle, is connected to rotor folding to realize that the end of support rod 6 can rotate
On the bulkhead in folded storehouse 4, and 11 top of car body can be set to.
14 both ends of fixed cross beam pass through shaft and are separately connected folding 16 end of arm, fold arm 16 and are set to 14 liang of fixed cross beam
Extending direction is held, the other end for folding arm 16 is equipped with rotor motor 8, and the output end of rotor motor 8 is equipped with by shaft can
Propeller 7 is folded, is connected with 9 end of pull rod for being used to support fixed cross beam 14 in the middle part of fixed cross beam 14 by shaft, pull rod 9 is another
One end is connected to 11 top surface of car body of 6 opposite direction of swivel mount；The setting of pull rod 9 is convenient for entire flight support component is more preferable
Ground is fixed on above roof, and pull rod 9 and the rotation connection of fixed cross beam 14 are convenient for storage.
The present embodiment is preferred, the smallest in occupancy rotor folding storehouse 4 when arm 16 is in folded state for the ease of folding
Space folds parallel with swivel mount 6 when 16 folded state of arm；
As shown in figure 5, foldable propeller 7 includes two rotor blades 71 and blade connection 72, blade connection 72
It is connect by shaft with the output end of rotor motor 8；The design of this structure for the ease of rotor blade 71 to fold 16 side of arm
To folding, and folded two rotor blades 71 are arranged in parallel with folding arm 16, more preferable convenient for entire foldable propeller 7
Ground is contained in rotor and folds in storehouse 4, folds in storehouse 4 as shown in Figure 1, being accommodated in rotor after illustrating flight support member collapses
State.
The present embodiment, rotor motor 8 are brushless motor.
In the present embodiment, protective door 15 folds 4 port edge of storehouse with the rotor far from cockpit 10 and is connect by shaft；And
Rotor folds storehouse 4 and is arranged for the hydraulic stem to opening protection function door 15 after vehicle；
The present embodiment, two motor 12, hydraulic stem, rotor motor 8, control panel with electric-control system 18 and power electric
Pond 1 is electrically connected；
Protective door 15 is provided with chimeric caulking groove corresponding with swivel mount 6 close to the side of cockpit 10, for that can roll over
Coiled coil paddle 7 is fitted into swivel mount 6 when being unfolded, and setting in this way realizes that rotor folds storehouse 4 convenient for passing through rotation protective door 15
Unlatching and closure, while in automobile flight course, by swivel mount 6 in caulking groove, is prevented protective door 15 with
It collides between swivel mount 6, during realizing the expansion of foldable propeller 7, does not influence the closure behaviour of protective door 15
Make.
In the present embodiment, engaging button 19 is provided at the top of car body 11,9 movable end of pull rod is provided with inlay card end, is arranged in this way
Convenient for realizing being detachably connected for pull rod 9 and car body 11 by engaging button 19 and inlay card end after the expansion of foldable propeller 7,
Guarantee pull rod 9 to the stability of strutting system of fixed cross beam 14 simultaneously.
The present embodiment is respectively equipped with and automatically controlled system on the vehicle frame 11 between two driving wheels 13 and two driven wheels 2
The ducted fan 3 that system 18 and power battery 1 connect, as shown in fig. 6, the air opening end of ducted fan 3 is covered with and electric-control system
The wind direction slew page 5 of 18 connections, provides upward power when the setting of ducted fan 3 is in addition to automobile flight, can also be according to automatically controlled
The revolving speed of the control instruction adjustment ducted fan 3 of system 18 changes wind direction slew page 5, to realize changing for vehicle traveling direction
Become, is convenient for cooperating realization steering in automobile flight course, accelerating and brake etc. operating.The present embodiment, it is contemplated that duct wind
It is larger to fan 3 general volumes, the electric-control system 18 being set in motor room is transferred to driver's seat bottom, convenient for having by the present embodiment
Another ducted fan 3 and previous ducted fan 3 are similarly symmetrically disposed on by the one of ducted fan 3 of bigger space
Rotor folds on 4 bottom surface of storehouse or rotor folds on the vehicle frame of 4 lower end of storehouse；Realize the whole balance of car body 11；
The present embodiment, steering system, vehicle accelerator system, the brake system of steering wheel for vehicle connect with electric-control system 18
It connects, electric-control system 18 receives the action command of the steering system of analysis directions disk, vehicle accelerator system, brake system, will instruct
It is converted into the revolving speed control that control instruction realizes ducted fan 3, the swaying direction control of wind direction slew page 5, to realize steering, add
The operation such as speed and brake, the present embodiment, the steering system of the received steering wheel of electric-control system 18, vehicle accelerator system, brake
The action command of system is concretely respectively arranged on the steering system of steering wheel, vehicle accelerator system, the steering in brake system
Sensor movement relevant to pressure sensor induction identification generates instruction and sends electric-control system 18 to；Wind direction slew page 5 can be existing
Air-conditioned wind direction slew page 5 designs, and realizes wind direction adjustment.
In the present embodiment, charge port is provided on the outside of power battery 1.
The present embodiment, it should be noted that flight support component and foldable propeller 7 enter offline mode in automobile
It needs manually to fold flight support component and foldable propeller 7 in storehouse 4 from rotor before and carries out expansion fixation after pull-out,
Evade existing intelligent design and be in order to reduce realize automatic stretching, extension or fold needed for device weight, including it is electronic
Mechanical, electrical motivation connector etc., so that the weight of entire hovercar be made to reach most light, compared to full automatic hovercar,
This hovercar flight time for simplifying structure is longer.
The present embodiment is preferred, as shown in fig. 7, in order to keep hovercar more intelligent, fixed cross beam 14 and pull rod 9 and folding
Rotating electric machine 20 is respectively set in the junction of folded arm 16, and rotating electric machine 20 is electrically connected with power battery 1 and electric-control system 18, is convenient for
Electric car realizes the expansion and folding of flight support component automatically.
The operation principle of the present invention is that: driver is located inside cockpit 10, and controls automobile, when automobile is normal
When driving, the electric energy when offer of power battery 1 automobilism, two work of motor 12 drive driving wheels 13 to be rotated, match
The trackability for closing driven wheel 2 realizes the movement of car body 11, and foldable propeller 7 is located at rotor and folds inside storehouse 4 at this time, works as automobile
Encounter blocking or other can not continue traveling the case where when, driver can control automobile starting offline mode, in the work of hydraulic stem
Under, protective door 15 rotates backward opening, opens rotor and folds storehouse 4, at this time by flight support component and foldable propeller 7 from
Rotor folds and carries out expansion fixation in storehouse 4 after pull-out, and engaging is fixed with button 19 is engaged in 9 inlay card end of pull rod, realizes to fixation
The support of crossbeam 14 operates, and 7 two rotor blades 71 of foldable propeller are unfolded, and carries out flight preparation work, rotor motor
8 work drive foldable propeller 7 to rotate, and realize the takeoff operational of automobile, at the same time, ducted fan 3 inhales outside air
Enter and sprayed after being spun up by inner turbine, realization is taken off acceleration, steering system of the driver by steer direction disk, vehicle
Throttle system, brake system realize the operation such as steering, acceleration and brake of hovercar, fly over congested link or other can not
Behind the section of normal pass, protective door 15 is opened, flight support component and foldable propeller 7 are folded and withdraw rotor folding storehouse
In 4, and closes protective door 15 and can carry out mobility operation again.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all in essence of the invention
Within mind and principle, any modification, equivalent replacement, improvement and so on be should all be included in the protection scope of the present invention.
Claims (9)
1. a kind of flight instruments, it is characterised in that: include car body (11), car body (11) front end is provided with cockpit (10)；
Two motor (12) connecting respectively with driving wheel (13) are set on the vehicle frame of the car body (11) front end, it is described to drive
It sails the power battery (1) connecting on car body (11) described in cabin (10) rear end with described two motor (12) and is set to the vehicle
Driven wheel (2) on the vehicle frame of body (11) rear end；
Car body (11) described in cockpit (10) rear end is provided with rotor and folds storehouse (4)；
The rotor folds storehouse (4) and connects flight support component by shaft respectively on the bulkhead of the cockpit (10),
The flight support component is connect by rotor motor (8) with foldable propeller (7)；
Further include the electric-control system (18) on car body (11) described in driver's seat bottom, is electrically connected with the electric-control system (18)
Be set to the cockpit (10) in control panel；
Described two motor (12), rotor motor (8), control panel connect with power battery (1) with electric-control system (18)
It connects.
2. flight instruments according to claim 1, it is characterised in that: the flight support component includes two support rods (6)；
One end of two support rods (6) is connected to the rotor by shaft and folds storehouse (4) close to the cockpit (10)
Bulkhead on, the other end, which stretches out the rotor and folds storehouse (4), to be simultaneously connected with fixed cross beam (14) by shaft, and described two support
Bar (6) is longitudinally set to above the car body (11)；The fixed cross beam (14) is horizontally-parallel to be set to above the car body (11)；
Fixed cross beam (14) both ends are separately connected by shaft folds arm (16) end, and the folding arm (16) is set to described
Fixed cross beam (14) both ends extending direction, the other end for folding arm (16) are equipped with the rotor motor (8), the rotor
The output end of motor (8) is equipped with the foldable propeller (7) by shaft.
3. flight instruments according to claim 2, it is characterised in that: connected and drawn by shaft in the middle part of the fixed cross beam (14)
Bar (9) end, pull rod (9) other end are provided with inlay card end, can with the engaging button (19) being arranged at the top of the car body (11)
Dismantling connection.
4. flight instruments according to claim 2, it is characterised in that: described the present embodiment, support rod (6) they are bent rod,
Bending angle is obtuse angle.
5. flight instruments according to claim 2, it is characterised in that: when folding arm (16) folded state with the support
Bar (6) is parallel.
6. flight instruments according to claim 1, it is characterised in that: be located at described two driving wheels (13) and two driven wheels
(2) ducted fan connecting with the electric-control system (18) and power battery (1) is respectively equipped on the vehicle frame (11) between
(3)。
7. flight instruments according to claim 6, it is characterised in that: the air opening end of the ducted fan (3) be covered with
The wind direction slew page (5) being connect with the electric-control system (18).
8. flight instruments according to claim 1, it is characterised in that: the rotor folds storehouse (4) open end and protective door is arranged
(15), the protective door (15) and the rotor far from the cockpit (10) fold storehouse (4) port edge and are connected by shaft
It connects, and the rotor folds in storehouse (4) setting for the hydraulic stem for opening the protective door (15) after vehicle；
The hydraulic stem is electrically connected with the electric-control system (18) and the power battery (1)；
9. flight instruments according to claim 1, it is characterised in that: the protective door (15) is close to the cockpit (10)
Side is provided with chimeric caulking groove corresponding with the swivel mount (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910870414.2A CN110450589A (en) | 2019-09-16 | 2019-09-16 | A kind of flight instruments |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910870414.2A CN110450589A (en) | 2019-09-16 | 2019-09-16 | A kind of flight instruments |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110450589A true CN110450589A (en) | 2019-11-15 |
Family
ID=68492028
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910870414.2A Pending CN110450589A (en) | 2019-09-16 | 2019-09-16 | A kind of flight instruments |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110450589A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112249322A (en) * | 2020-10-19 | 2021-01-22 | 东风汽车集团有限公司 | Portable rotor type single aircraft for vehicle and vehicle |
-
2019
- 2019-09-16 CN CN201910870414.2A patent/CN110450589A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112249322A (en) * | 2020-10-19 | 2021-01-22 | 东风汽车集团有限公司 | Portable rotor type single aircraft for vehicle and vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US20180065737A1 (en) | Personal aircraft | |
| TWI538852B (en) | Personal aircraft | |
| CN108146169B (en) | Wing rear-folding type air-ground dual-purpose carrier | |
| EP2928772B1 (en) | Vertical takeoff and landing aircraft | |
| US7874512B2 (en) | System and method for a flyable and roadable vehicle | |
| KR100537173B1 (en) | Micro Aerial Vehlcle | |
| CN112896501A (en) | Aircraft suitable for vertical take-off and horizontal flight | |
| CN111098649B (en) | Aerocar control system and method and aerocar | |
| CN109532361A (en) | Manned air-ground amphibious aircraft and its group control system | |
| CN110450589A (en) | A kind of flight instruments | |
| CN108437712A (en) | A kind of folding wings hovercar of VTOL | |
| CN108437711A (en) | A kind of more paddle hovercars | |
| JP2013244898A (en) | Automobile | |
| CN105922830B (en) | Flight electric car | |
| CN211592135U (en) | Flying automobile | |
| AU2014202607B2 (en) | Personal aircraft | |
| CN111846191A (en) | Combined power airship | |
| DE102021133301B3 (en) | VTOL aircraft with battery electric propulsion and internal combustion engine | |
| CN110562438B (en) | Multi-rotor aircraft and control method thereof | |
| CN107745804A (en) | Aircraft and cruising level flight method | |
| CN108394241B (en) | One kind going straight up to fixed-wing gliding multi-mode driving | |
| CN117508567A (en) | Novel duct (hub) driving aircraft | |
| AU2011282250B2 (en) | Personal aircraft | |
| JPH04257799A (en) | Helicopter | |
| NZ621370B2 (en) | Personal aircraft |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination |