CN109484109A - A kind of operating system for hovercar - Google Patents
A kind of operating system for hovercar Download PDFInfo
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- CN109484109A CN109484109A CN201710818956.6A CN201710818956A CN109484109A CN 109484109 A CN109484109 A CN 109484109A CN 201710818956 A CN201710818956 A CN 201710818956A CN 109484109 A CN109484109 A CN 109484109A
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- 230000033001 locomotion Effects 0.000 claims abstract description 16
- 230000001133 acceleration Effects 0.000 claims description 2
- 230000005611 electricity Effects 0.000 claims description 2
- 230000008859 change Effects 0.000 description 6
- 238000000034 method Methods 0.000 description 6
- 230000036544 posture Effects 0.000 description 6
- 238000010586 diagram Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 230000009471 action Effects 0.000 description 3
- 230000007423 decrease Effects 0.000 description 3
- 230000007246 mechanism Effects 0.000 description 3
- 230000002238 attenuated effect Effects 0.000 description 1
- 238000010009 beating Methods 0.000 description 1
- 230000006399 behavior Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
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- 230000003247 decreasing effect Effects 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 230000010006 flight Effects 0.000 description 1
- 230000007274 generation of a signal involved in cell-cell signaling Effects 0.000 description 1
- 210000000003 hoof Anatomy 0.000 description 1
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- 239000007788 liquid Substances 0.000 description 1
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Classifications
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- 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
- B60—VEHICLES IN GENERAL
- B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
- B60K23/00—Arrangement or mounting of control devices for vehicle transmissions, or parts thereof, not otherwise provided for
- B60K23/02—Arrangement or mounting of control devices for vehicle transmissions, or parts thereof, not otherwise provided for for main transmission clutches
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60R—VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
- B60R16/00—Electric or fluid circuits specially adapted for vehicles and not otherwise provided for; Arrangement of elements of electric or fluid circuits specially adapted for vehicles and not otherwise provided for
- B60R16/02—Electric or fluid circuits specially adapted for vehicles and not otherwise provided for; Arrangement of elements of electric or fluid circuits specially adapted for vehicles and not otherwise provided for electric constitutive elements
- B60R16/023—Electric or fluid circuits specially adapted for vehicles and not otherwise provided for; Arrangement of elements of electric or fluid circuits specially adapted for vehicles and not otherwise provided for electric constitutive elements for transmission of signals between vehicle parts or subsystems
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
- B60T17/00—Component parts, details, or accessories of power brake systems not covered by groups B60T8/00, B60T13/00 or B60T15/00, or presenting other characteristic features
- B60T17/18—Safety devices; Monitoring
- B60T17/22—Devices for monitoring or checking brake systems; Signal devices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60T—VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
- B60T7/00—Brake-action initiating means
- B60T7/02—Brake-action initiating means for personal initiation
- B60T7/04—Brake-action initiating means for personal initiation foot actuated
- B60T7/06—Disposition of pedal
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C19/00—Aircraft control not otherwise provided for
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Control Devices (AREA)
Abstract
The invention discloses a kind of operating system for hovercar, which includes: the clutch pedal connecting with clutch；First angle sensor is arranged on clutch pedal, and first angle sensor is used for the operational motion according to the driver sensed, generates angle signal；The brake pedal being connect with brake apparatus；Switch sensor is arranged on brake pedal, and switch sensor is used for the operational motion according to the driver sensed, generates switching signal；Flight computer, flight computer are electrically connected with first angle sensor and switch sensor respectively, and flight computer is used for the signal sensed according to first angle sensor and/or switch sensor, adjust the flight attitude of hovercar.The present invention solves hovercar in the prior art, and, when land traveling is with airflight, bring inconvenience problem is accustomed in different manipulations.
Description
Technical field
The present invention relates to hovercar fields, it particularly relates to a kind of operating system for hovercar.
Background technique
Driver's driving is the mesh for reaching control running car by steer direction disk, clutch, brake, throttle
, and pilot driver aircraft is to achieve the purpose that control aircraft flight by manipulation control wheel, step tread plate.Since the two exists
There are biggish differences on operating habit, so that driving hovercar to driver brings huge difficulty.
There are following two methods for the maneuverability pattern of current hovercar, specifically: one is pass through navigation system
The automatic driving mode of system operates hovercar, and another kind is to manipulate hovercar by rocking bar.Although the former has saved not
Few thing, but the manipulation wish of driver cannot be given full play to, while when coping with burst accident, it cannot effectively pass through people's
Wish is evaded, and the similar unmanned controller mature at present of the rocking bar maneuverability pattern of the latter manipulates habit, but cannot be had
Effect ground, if two sets of manipulations separated, not only needs additional a set of operating mechanism, makes to grasp in conjunction with ground run steerable system
Become very narrow as space, operating space range becomes larger, and is difficult to adapt in time on the operating habit of driver, empty
The level that the riding manipulation of middle flight commonly reaches technical flight person could pass through.
In addition, being equipped with corresponding sensor in the gas pedal on electronic throttle door type automobile at present, driver passes through
Lower accelerator pedal, makes the sensor generate electric signal, and electric signal is sent to automobile controller center ECU (Electronic
Control Unit, electronic control unit), ECU retransmits the connected direct current generator of instruction electron air throttle, and motor drives section
Valve rotation, throttle valve aperture changes, to complete entire manipulation process.In addition, current power steering type automobile
On steering column on be also equipped with angular transducer, but the sensor equally only sends a signal to automobile controller center ECU.This
Outside, current clutch pedal has mechanical friction type, also there is an electromagnetic type and hydraulic type, and most importantly mechanical friction type, this
Kind form does not have sensor.In addition, current brake pedal is mechanical structure, there are pneumatic type and hydraulic brake, it is hydraulic
Formula braking is that the pedal that touches on the brake under drives the push-rod piston of vacuum pump mobile, after oil liquid is moved to wheelcylinder piston, two brakings
Hoof rotates around fulcrum post, so that it is pressed on friction plate on the inner headed face of brake drum, and pneumatic type is touched on the brake under
Pedal drives brake control valve movement, changes brake chamber air pressure, and driving brake-shoe is mobile, so that friction plate be made to be pressed on system
On the inner headed face for moving drum.
For the problems in the relevant technologies, currently no effective solution has been proposed.
Summary of the invention
For the problems in the relevant technologies, the present invention proposes a kind of operating system for hovercar, and which solve existing
There is in technology hovercar when land traveling is with airflight, bring inconvenience problem is accustomed in different manipulations, leads to
It crosses under the premise of not changing the manipulation habit of automobile floor traveling, the behaviour of Lai Shixian hovercar ground run and airflight
Vertical process so that the process of pilot control hovercar become it is simple and direct, general, conveniently with can operate, meanwhile, also without
Operating mechanism need to be increased.
The technical scheme of the present invention is realized as follows:
According to an aspect of the invention, there is provided a kind of operating system for hovercar.
The operating system for being used for hovercar includes: the clutch pedal connecting with clutch；First angle sensor,
It is arranged on clutch pedal, first angle sensor is used for the operational motion according to the driver sensed, generates angle letter
Number；The brake pedal being connect with brake apparatus；Switch sensor is arranged on brake pedal, and switch sensor is used for according to sense
The operational motion of the driver measured generates switching signal；Flight computer, flight computer respectively with first angle sensor
It is electrically connected with switch sensor, flight computer is used for the letter sensed according to first angle sensor and/or switch sensor
Number, adjust the flight attitude of hovercar；Switching switch, switching switch are connect with flight computer, and switching switch is for switching
The offline mode and land mode of hovercar.
According to one embodiment of present invention, operating system further include: steering wheel, gas pedal, steering wheel and steering knot
Structure connection, the steering and gas pedal that steering wheel is used to control hovercar are connect with engine throttle, and gas pedal is used for
Control the acceleration of hovercar.
According to one embodiment of present invention, steering wheel includes: disk body and steering shaft, the opposite end of steering shaft respectively with
Steering structure is connected with disk body, and first shell and second angle sensor are arranged in steering shaft, and second angle sensor passes through
Connecting plate is connect with first shell, and first shell is connected with the car body of hovercar.
According to one embodiment of present invention, second angle sensor is electrically connected with flight computer, in offline mode
In the case of, sensing signal of the flight computer according to second angle sensor, control hovercar realization yaw maneuver.
According to one embodiment of present invention, second angle sensor includes second shell and hollow shaft, hollow shaft setting
In second shell, and hollow shaft sleeve is located at the outside of steering shaft, and first angle sensor passes through hollow shaft sensing steering
The angle of rotation.
According to one embodiment of present invention, hovercar includes third shell, is equipped with the first mounting hole in third shell,
Brake pedal includes the first pivot part, and the first pivot part is set in the first mounting hole and the inner wall of the first mounting hole is equipped with
Switch sensor.
According to one embodiment of present invention, the both ends of the first pivot part each extend over out one first flat part and one first
Press section, brake pedal further include the first spring, and the both ends of the first spring are connected to the first flat part and the first mounting hole respectively
Inner wall, the first spring make the first flat part set back after being used to make to trample the first press section.
According to one embodiment of present invention, switch sensor is electrically connected with flight computer, is pressed and is braked in driver
When pedal, the first flat part is abutted with switch sensor upwards, and switch sensor senses switching signal, and flight computer will be opened
OFF signal and other sensing signals combine, and control hovercar realizes different flight attitudes.
According to one embodiment of present invention, hovercar includes the 4th shell, is equipped with the second mounting hole in the 4th shell,
Clutch pedal includes the second pivot part, and the second pivot part is set in the second mounting hole, and second pivoting portion fills at center of rotation
Equipped with first angle sensor, when driver presses clutch pedal, first angle sensor senses angle signal, flight
Computer combines switching signal and angle signal, and control hovercar realizes pitching motion
According to one embodiment of present invention, the both ends of the second pivot part each extend over out one second flat part and one second
Press section, clutch pedal further include second spring, and the both ends of second spring are connected to the second flat part and the second installation respectively
Hole inner wall, second spring after driver tramples the second press section for making the second flat part set back.
The beneficial technical effect of the present invention lies in:
Switch sensor is also arranged by the way that angular transducer is arranged on clutch pedal in the present invention on brake pedal,
And the signal sensed by flight computer according to above-mentioned angular transducer and/or switch sensor, adjust hovercar
Flight attitude, thus do not change driver driving manipulation habit on the basis of, by be arranged on manipulation device
The sensing signal that sensor generates, to adjust the flight attitude of hovercar, and then can rapidly learn and grasp hovercar
Aerial mode when control action, to solve in the prior art, hovercar is when land traveling is with airflight, no
Bring inconvenience problem is accustomed in same manipulation.
Detailed description of the invention
It in order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, below will be to institute in embodiment
Attached drawing to be used is needed to be briefly described, it should be apparent that, the accompanying drawings in the following description is only some implementations of the invention
Example, for those of ordinary skill in the art, without creative efforts, can also obtain according to these attached drawings
Obtain other attached drawings.
Fig. 1 is the schematic diagram of the operating system according to an embodiment of the present invention for hovercar；
Fig. 2 is the schematic diagram of steering wheel according to an embodiment of the present invention and second angle sensor；
Fig. 3 is the schematic diagram of brake and switch sensor according to an embodiment of the present invention；
Fig. 4 is clutch according to an embodiment of the present invention and first angle sensor or throttle and third angle sensor
Schematic diagram；
Fig. 5 is the schematic diagram of the lift unit of hovercar according to an embodiment of the present invention.
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, those of ordinary skill in the art's every other embodiment obtained belong to what the present invention protected
Range.
According to an embodiment of the invention, providing a kind of operating system for hovercar.
As shown in Figure 1, the operating system according to an embodiment of the present invention for hovercar includes: to connect with clutch
Clutch pedal；First angle sensor 3 is arranged on clutch pedal, and first angle sensor 3 is used for what basis sensed
The operational motion of driver generates angle signal；The brake pedal being connect with brake apparatus；Switch sensor 5, setting are being braked
On pedal, switch sensor 5 is used for the operational motion according to the driver sensed, generates switching signal；Flight computer 1,
Flight computer 1 is electrically connected with first angle sensor 3 and switch sensor 5 respectively, and flight computer 1 is used for according to first jiao
The signal that degree sensor 3 and/or switch sensor 5 sense, adjusts the flight attitude of hovercar；Switch switch 2, switching is opened
It closes 2 to connect with flight computer 1, switching switch 2 is used to switch the offline mode and land mode of hovercar.
By means of above-mentioned technical proposal of the invention, by the way that angular transducer is arranged on clutch pedal, also braking
Switch sensor is set on pedal, and sensed by flight computer according to angular transducer and/or switch sensor
Signal adjusts the flight attitude of hovercar, to pass through on the basis of not changing the manipulation habit of driver's driving
The sensing signal that sensor generates on manipulation device is set, to adjust the flight attitude of hovercar, and then can rapidly be learned
Control action when practising and grasping the aerial mode of hovercar travels to solve hovercar in the prior art on land
When with airflight, bring inconvenience problem is accustomed in different manipulations.
In order to preferably describe technical solution of the present invention, below by specific embodiment to technical solution of the present invention
It is described in detail.
Technical solution of the present invention is to hovercar in land driving mode when driving and driver in the prior art
The driving habit of driving is consistent, and the present invention is configured by the drive manner of the offline mode to hovercar, passes through
The sensing signal that sensor generates on manipulation device is set, to adjust the flight attitude of hovercar, so that driver is flying
Hovercar is driven under row mode to be not necessarily to change the manipulation habit of driver, meanwhile, which also makes pilot control
The process of hovercar become it is simple and direct, general, conveniently with can operate, meanwhile, without increase operating mechanism.
As shown in Figure 1, the operating system for hovercar in the present invention includes: 3, second jiaos of first angle sensor
Spend sensor 4, switch sensor 5, third angle sensor 6, wherein first angle sensor 3 is arranged on clutch pedal,
The clutch pedal is connected with the clutch of hovercar, and second angle sensor 4 is arranged in the steering shaft of steering wheel, the party
It is connected to disk with the steering structure of hovercar, switch sensor 5 is arranged on brake pedal, the brake pedal and hovercar
Brake apparatus connection, third angle sensor 6 be arranged in gas pedal, the engine oil of the gas pedal and hovercar
Door connection, above-mentioned multiple sensors, to the operational motion of its corresponding operating device, generate sensing signal according to driver, and will
Sensing signal is sent to flight computer 1, the flight computer 1 respectively with first angle sensor 3, second angle sensor 4,
Switch sensor 5 and third angle sensor 6 connect, and the flight computer 1 is by receiving sensing signal, and according to receiving
Sensing signal determines the operational order of the corresponding hovercar of the sensing signal, for example, according to one embodiment of present invention,
The second angle sensor 4 senses a driver left side and beats steering wheel, so that the angular transducer 4 being somebody's turn to do generates angle signal, and will
The angle signal is sent on flight computer 1, which determines brake according to the angle signal received
Whether pedal is trampled, and in the case where the pedal of the brake is not trampled, which determines the first angle signal
The flight attitude of corresponding hovercar is to turn left, and then generation one, which instructs, controls corresponding servo motor, so that this flies
Row automobile can be realized left-hand rotation movement under offline mode.In addition, Fig. 1 also shows servo motor 7, servo motor 8, servo electricity
Machine 9, servo motor 10 are connect with flight computer 1, meanwhile, above-mentioned multiple servo motors are by the control of the flight computer 1
System.Meanwhile operating system further include: switching switch 2, the switching switch 2 are connect with flight computer 1,2 energy of switching switch
Enough switch the land mode and aerial mode of hovercar, meanwhile, above-mentioned multiple sensors and flight computer 1 are in flight vapour
It works when the aerial mode of vehicle, and when hovercar is in land mode, above-mentioned multiple sensors and flight computer 1 are equal
Driver be will not influence to the normal driving of hovercar.
Although in addition, of course it is to be understood that show four sensors and four servo motors in Fig. 1, this field
Personnel it is understood that those skilled in the art can according to actual needs be configured sensor and servo motor, for example,
According to one embodiment of present invention, as shown in figure 3, the third shell being oppositely arranged there are two the brake pedal tools of hovercar
18, it is equipped with switch sensor 5 on two third shells 18, which is not limited by the present invention.
In addition, the disk body 11, which is fixed at, to be turned figure it is seen that direction disk includes disk body 11 and steering shaft 12
To on axis 12, and the steering system of the other end of the steering shaft 12 and hovercar connects, so that driver can pass through rotation
Disk body 11 transmits torque to steering shaft 12, meanwhile, first shell 13 and second angle sensor are arranged in the steering shaft 12
4, which is positioned close to the side of disk body 11, which is the shell of steering shaft 12, which can
It is rotated in first shell 13, connects disk body 11 in 13 one end of first shell, the is additionally provided on the other end of first shell 13
Two angular transducers 4, the second angle sensor 4 are integrated with hollow shaft 14 and second shell 15, wherein hollow shaft 14 is hollow
Column structure, and hollow shaft 14 is rotated around second shell 15, and which is set in steering shaft 12, passes through this knot
Structure enables to second angle sensor 4 that can rotate together with steering shaft 12, and then is able to detect the rotational angle of steering wheel
With the information such as rotation direction.In addition, second shell 15 is equipped with interface 17, which can feel second angle sensor 4
The angle signal of survey is sent to flight computer 1, i.e., the interface 17 is for the logical of second angle sensor 4 and flight computer 1
Letter.In addition, the first shell 13 is connected with the car body of hovercar, second shell 15 is connected to first shell by fixed plate 16
On 13, so as to accurately sense the rotation information of steering wheel.
In addition, being equipped with the from figure 3, it can be seen that the brake pedal includes third shell 18, while in the third shell 18
One mounting hole 24, the brake pedal further include the first pivot part 23, and the first pivot part 23 is set in the first mounting hole 24, Yi Ji
The inner wall of one mounting hole 24 is equipped with switch sensor 5, in addition, to each extend over out one first flat at the both ends of first pivot part 23
Plate portion 22 and one first press section 19, brake pedal further include the first spring 21, and the both ends of the first spring 21 are connected to respectively
The inner wall of one flat part 22 and the first mounting hole 24, first spring 21 can make to trample make after the first press section 19 it is first flat
Plate portion sets back, in addition, the switch sensor 5 is for sensing whether the first pivot part 23 turns to having for switch sensor 5
In the sensing range of effect, specifically: when brake pedal is not trampled, it is effective that the first pivot part 23 is not at switch sensor 5
Sensing range, export as "Off" signal；When brake pedal is trampled, 23 access switch sensor 5 of the first pivot part has
In the sensing range of effect, exporting as "ON" signal, it is also likely to be high level that certain "on" and "off" signal, which may be low level, this
Circuit can be connected according to sensor to set, the switching signal of sensing belt is sent to flight and calculated by the subsequent switch sensor 5
Machine 1.
In addition, the 4th shell 25 is interior equipped with the second peace from fig. 4, it can be seen that the clutch pedal includes the 4th shell 25
Hole 29 is filled, clutch pedal includes the second pivot part 27, and the second pivot part 27 is set in the second mounting hole 29, second pivoting portion 27
First angle sensor 3 is installed at center of rotation, meanwhile, the both ends of the second pivot part 27 each extend over out one second plate
Portion 30 and one second press section 26, clutch pedal further include second spring 28, and the both ends of second spring 28 are connected to respectively
The inner wall of two flat parts 30 and the second mounting hole 30, second spring 28 make second after making driver trample the second press section 26
Flat part 30 sets back.In addition, the first angle sensor 3 and above-mentioned second pivot part 27 are arranged concentrically and relatively rotate,
Wherein, which is Hall-type angular transducer, i.e., by by first angle sensor 3 and the second pivot part
27 are arranged concentrically, and in the case where relative rotation power variation in magnetic field occurs for the two, to realize the strong and weak variation of signal, separately
Outside, first angle sensor 3 includes the shell and axis body of sensor, can be relatively rotated between shell and axis body, shell and work
Moved end is pivotally connected, and axis body is connect with the second pivot part 27, since angular transducer itself has relative rotation just can be angled
Signal generates, so its shell and axis body must be a fixation, another relative rotation in sensing.In addition, this field
Technical staff can also according to actual needs be configured first angle sensor 3, for example, an implementation according to the present invention
Example, which is potentiometric transducer, while the first angle sensor 3 may be provided at the second mounting hole
On 29 inner wall, to change resistance sizes in circuit by the rotation of the second pivot part 27, the strong and weak of Lai Shixian signal becomes
Change, which can also be regarded to the slide rheostat of arc as, which is not limited by the present invention.
In addition, the hovercar includes the 5th shell of course it is to be understood that since clutch is similar with the structure of throttle,
Third mounting hole is equipped in 5th shell, gas pedal includes third pivot part, and third pivot part is set in third mounting hole, the
Three articulated sections are installed with third angle sensor 6 at center of rotation, in addition, the both ends of third pivot part each extend over out one
Three flat parts and a third press section, gas pedal further include third spring, and it is flat that the both ends of third spring are connected to third respectively
Plate portion and third inner wall of the hole installing, third spring make third flat part restore former after making driver trample third press section
Position, similar structure can refer to Fig. 4.
In addition, Serve Motor Control corresponds to engine air throttle opening size, it is solid that driven by engine is mounted on hovercar
The lift unit operating set is positioned, the posture of hovercar changes with the variation of each lift unit operating revolving speed.
In addition, from fig. 5, it can be seen that the quantity for the multiple lift units being arranged on the vehicle body of hovercar be four,
Aforementioned four lift unit specifically includes lift unit n1, lift unit n2, lift unit n3, lift unit n4.Although in addition,
Fig. 5 shows four lift units, but those skilled in the art is with according to actual needs to the quantity of lift unit and setting
Position is configured, for example, according to one embodiment of present invention, be arranged eight on the vehicle body of hovercar and rise unit, and
And the position of four be arranged in Fig. 5 the lift unit of above-mentioned eight lift units two-by-two, this is not limited by the present invention.
Technical solution of the present invention is described in detail below by table 1.
Table 1
In above-mentioned table 1 as can be seen that the rotation speed change of four lift units can be realized the different flights of hovercar
Posture, specifically:
Driver can be realized the flight attitude of the lifting of hovercar to the operation of the pedal of throttle, for example, driving
For member in the case where trampling the pedal of throttle downwards, third angle sensor 6 generates angle signal 1, and flight computer 1, which receives, to be produced
Raw above-mentioned angle signal 1, and according to the angle signal 1 determines the flight attitude of hovercar to rise, and by aforementioned four liter
The revolving speed control of power unit is identical, and in driver in the case where the pedal of lift throttle upwards, third angle sensor 6 produces
A raw angle signal 2, flight computer 1 receive the angle signal 2 generated, and according to the angle signal 2, determine hovercar
Flight attitude be decline, and it is identical that the revolving speed of aforementioned four lift unit, which is controlled,；
Driver can be realized the flight attitude of the pitching of hovercar to the operation of the pedal and brake pedal of clutch,
For example, driver the pedal not touched on the brake and meanwhile downwards trample the pedal of clutch in the case where, first angle sensor
3 generate an angle signal 3, and flight computer 1 receives the angle signal 3 generated, and according to the angle signal 3, determines flight
The flight attitude of automobile is bowed before being, and sets n1=n2 < n3=n4, while lift list for the revolving speed of aforementioned four lift unit
First n3, lift unit n4 are greater than lift unit n1, the amplitude of lift unit n2 is determined by angular dimension, situation class below
Seemingly, later in driver in the case where being lifted away from the pedal of clutch upwards, which generates an angle signal
4, flight computer 1 receives the angle signal 4 generated, and according to the angle signal 4, after determining that the flight attitude of hovercar is
It faces upward, and sets n1=n2 > n3=n4 for the revolving speed of aforementioned four lift unit.In addition, another situation is: driver thinks elder generation
Realize backward wing, then must be realized in conjunction with the pedal of brake, for example, driver trample downwards brake pedal,
In the case where the pedal for trampling clutch still further below, which generates an angle signal 3, and brake pedal produces
A raw switching signal, flight computer 1 receive the angle signal 3 generated and switching signal 1, and according to the angle signal 3 with
Switching signal 1 determines that the flight attitude of hovercar is layback, and sets n1=n2 for the revolving speed of aforementioned four lift unit
> n3=n4, in the case where trampling the pedal of brake under in driver later, be lifted away from the pedal of clutch upwards again, this first jiao
It spends sensor 3 and generates an angle signal 4 and switching signal 2, flight computer 1 receives the angle signal 4 generated and switch is believed
Numbers 2, and according to the angle signal 4 and switching signal 2, determine that the flight attitude of hovercar is bowed before being, and by aforementioned four liter
The revolving speed of power unit is set as n1=n2 < n3=n4；
Driver can be realized the roll posture of hovercar to the operation of the pedal and steering wheel of brake, for example, driving
In the case that the person of sailing tramples downwards the pedal of brake and steering wheel is beaten to the left, which generates a switching signal
1, second angle sensor 4 generates an angle signal 5, and flight computer 1 receives the switching signal 1 generated and angle signal 5,
A combination signal is generated, and according to the combination signal, determines that the flight attitude of hovercar turns over for a left side, and by aforementioned four liter
The revolving speed of power unit is set as n1=n3 < n2=n4, and tramples the pedal of brake downwards in driver and steering wheel is beaten to the right
In the case where, which generates a switching signal 2, and second angle sensor 4 generates an angle signal 6, flight
Computer 1 receives the switching signal 2 generated and angle signal 6, and according to the switching signal 2 and angle signal 6, generates a group
Signal is closed, to determine that the flight attitude of hovercar turns over for the right side according to the combination signal, and by aforementioned four lift unit
Revolving speed is set as n1=n3 > n2=n4, in addition, in the case where hovercar is in offline mode, and in steering wheel, clutch
In the state that device, throttle are in initially, driver's foot touches on the brake to control hovercar realization hovering movement, and outstanding
When stopping signal generation, if other signals change, attitude signal responsively changes；
Driver can be realized the yaw-position of hovercar to the operation of steering wheel, for example, in driver to not stepping on
In the case that the pedal and steering wheel for stepping on brake are beaten to the left, which generates an angle signal 5, flight
Computer 1 receives the angle signal 5 generated, and according to the angle signal 5, determines that the flight attitude of hovercar is left-hand rotation, and
N1=n4 < n2=n3 is set by the revolving speed of aforementioned four lift unit, and does not tread on pedal and the side of brake in driver
In the case where beating to the right to disk, which generates an angle signal 6, and flight computer 1 receives the angle generated
Signal 6 is spent, and according to the angle signal 6, determines the flight attitude of hovercar to turn right, and by aforementioned four lift unit
Revolving speed is set as n1=n4 > n2=n3.
It in addition, above-mentioned flight attitude can be mutually indepedent, while can also be the combination of two or more sets movements, for example, in foot
While stepping on clutch, steering wheel rotation, while open out, the then movement generated are roll, pitching and go up and down moving after combining
Make.
In addition, technical solution of the present invention is described in detail again by table 2 below.
Table 2
One-to-one relationship of the above-mentioned table 2 between sensor signal and attitudes vibration is not involved in wherein " --- " represents
Combined signal, "+" represent enhancing signal, and "-" represents attenuated signal, and " 00 " represents initial position signal, and " 1 " represents and opens letter
Number, " 0 " represents OFF signal.
In addition, from Table 2, it can be seen that in addition to hovering, other postures can generate combinative movement between each other.(note:
Hovering is a kind of special state in a kind of lifting posture, it occupies highly importantly in the safety Design of aircraft
Position, as long as can rise it is liftoff, then it can hover in the sky in specific gasoline throttle angle, that is to say, that floating state
The speed of lower controlled lift unit be it is certain, if driver wants to obtain hovering posture in a certain height, drive
The person of sailing obtains be added to throttle to a certain degree first, then reduces throttle, then maintain the gasoline throttle angle, then hovering shape will be obtained
State；On the other hand, there are the lift unit speed that when ON signal of switch sensor 5, the original state of throttle is controlled for setting
It is the speed under floating state, then, by braking to a switching signal, while upper lift throttle is until being returned to initial shape
State is exactly the signal that hovers after the two signals combination at this time, as shown in table 2.It can be seen that two kinds of floating states can mutually be cut
It changes, such as: when not having strap brake, control throttle may be implemented to hover, but the floating state is not very stable.In this case, under
It touches on the brake, while being gradually reduced throttle until being totally released, switch to floating state again at this time, and the floating state is stablized, because
It is indeclinable in certain angular range for the "ON" or "Off" signal of switch sensing.In this case, releasing of brake flies
Row automobile is begun to decline, therefore driver should be gradually increased throttle, and hovercar decrease speed reduces at this time, when being decreased to 0
When, and it is converted into floating state.)
In conclusion by means of above-mentioned technical proposal of the invention, by the way that angular transducer is arranged on clutch pedal,
Switch sensor is also set on brake pedal, and is passed by flight computer according to above-mentioned angular transducer and/or switch
The signal that sensor senses adjusts the flight attitude of hovercar, thus in the manipulation habit for not changing driver's driving
On the basis of, by the way that the sensing signal that sensor generates on manipulation device is arranged in, to adjust the flight attitude of hovercar, into
And control action when can rapidly learn and grasp the aerial mode of hovercar, to solve flight vapour in the prior art
For vehicle when land traveling is with airflight, bring inconvenience problem is accustomed in different manipulations.
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 (10)
1. a kind of operating system for hovercar characterized by comprising
The clutch pedal being connect with clutch；
First angle sensor is arranged on the clutch pedal, and the first angle sensor is used for what basis sensed
The operational motion of driver generates angle signal；
The brake pedal being connect with brake apparatus；
Switch sensor is arranged on the brake pedal, and the switch sensor is used for the behaviour according to the driver sensed
It acts, generates switching signal；
Flight computer, the flight computer are electrically connected with the first angle sensor and the switch sensor respectively,
The flight computer is used for the signal sensed according to the first angle sensor and/or the switch sensor, adjustment
The flight attitude of the hovercar；
Switching switch, the switching switch are connect with the flight computer, and the switching switch is for switching the flight vapour
The offline mode and land mode of vehicle.
2. operating system according to claim 1, which is characterized in that the operating system further include: steering wheel, throttle are stepped on
Plate, the steering wheel are connected with steering structure, the steering wheel be used for control the hovercar steering and the throttle
Pedal is connect with engine throttle, and the gas pedal is used to control the acceleration of the hovercar.
3. operating system according to claim 2, which is characterized in that the steering wheel includes: disk body and steering shaft, described
The opposite end of steering shaft is connect with the steering structure and the disk body respectively, be arranged in the steering shaft first shell and
Second angle sensor, the second angle sensor are connect by connecting plate with the first shell, the first shell with
The car body of the hovercar connects.
4. operating system according to claim 3, which is characterized in that the second angle sensor and the flight calculate
Mechatronics, in the case where the offline mode, the flight computer is believed according to the sensing of the second angle sensor
Number, it controls the hovercar and realizes yaw maneuver.
5. operating system according to claim 3, which is characterized in that the second angle sensor include second shell and
Hollow shaft, the hollow shaft is arranged in the second shell, and the hollow shaft sleeve is located at the outside of the steering shaft, institute
State the angle that first angle sensor senses the steering axes by the hollow shaft.
6. operating system according to claim 1, which is characterized in that the hovercar includes third shell, and described
The first mounting hole is equipped in three shells, the brake pedal includes the first pivot part, and first pivot part is set to described first
In mounting hole and the inner wall of first mounting hole is equipped with the switch sensor.
7. operating system according to claim 6, which is characterized in that the both ends of first pivot part each extend over out one
First flat part and one first press section, the brake pedal further include the first spring, and the both ends of first spring are supported respectively
It is connected to the first flat part and the first inner wall of the hole installing, first spring is for making to make first after trampling first press section
Flat part sets back.
8. operating system according to claim 6, which is characterized in that the switch sensor and flight computer electricity
Connection, when the driver presses the brake pedal, first flat part is abutted with the switch sensor upwards, institute
It states switch sensor and senses the switching signal, the flight computer is by the switching signal and other sensing signal groups
It closes, controls the hovercar and realize different flight attitudes.
9. operating system according to claim 1, which is characterized in that the hovercar includes the 4th shell, and described the
It is equipped with the second mounting hole in four shells, the clutch pedal includes the second pivot part, and second pivot part is set to described the
In two mounting holes, the second pivoting portion is installed with the first angle sensor at center of rotation, presses in the driver
When pressing the clutch pedal, the first angle sensor senses the angle signal, and the flight computer will be described
Switching signal and angle signal combination, control the hovercar and realize pitching motion.
10. operating system according to claim 9, which is characterized in that the both ends of second pivot part each extend over out
One second flat part and one second press section, the clutch pedal further include second spring, the both ends point of the second spring
Be not connected to the second flat part and the second inner wall of the hole installing, the second spring be used for the driver trample described second by
The second flat part is set to set back after splenium.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710818956.6A CN109484109A (en) | 2017-09-12 | 2017-09-12 | A kind of operating system for hovercar |
| PCT/CN2018/079750 WO2019052141A1 (en) | 2017-09-12 | 2018-03-21 | Operating system for flying car |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710818956.6A CN109484109A (en) | 2017-09-12 | 2017-09-12 | A kind of operating system for hovercar |
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| Publication Number | Publication Date |
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| CN109484109A true CN109484109A (en) | 2019-03-19 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710818956.6A Pending CN109484109A (en) | 2017-09-12 | 2017-09-12 | A kind of operating system for hovercar |
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| CN (1) | CN109484109A (en) |
| WO (1) | WO2019052141A1 (en) |
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| CN110027373A (en) * | 2019-05-14 | 2019-07-19 | 北京理工大学 | A kind of hovercar safety assisting system based on pulse high explosive powder attitude regulation |
| WO2021213480A1 (en) * | 2020-04-22 | 2021-10-28 | Ningbo Geely Automobile Research & Development Co., Ltd. | Pedal system for road and flight operational use vehicle |
| CN113879053A (en) * | 2021-11-17 | 2022-01-04 | 广东汇天航空航天科技有限公司 | Multifunctional aircraft control method and system and multifunctional aircraft |
| CN113879054A (en) * | 2021-11-17 | 2022-01-04 | 广东汇天航空航天科技有限公司 | Flying automobile control processing method, control processing system and flying automobile |
| CN113879055A (en) * | 2021-11-17 | 2022-01-04 | 广东汇天航空航天科技有限公司 | Multifunctional aircraft and operation method and system thereof |
| CN113895190A (en) * | 2021-11-17 | 2022-01-07 | 广东汇天航空航天科技有限公司 | Control system of flying automobile and flying automobile |
| CN114393964A (en) * | 2022-01-25 | 2022-04-26 | 广东汇天航空航天科技有限公司 | Flying automobile control method and system and flying automobile |
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| CN113895190A (en) * | 2021-11-17 | 2022-01-07 | 广东汇天航空航天科技有限公司 | Control system of flying automobile and flying automobile |
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