CN110450957A - Active flight slide plate - Google Patents
Active flight slide plate Download PDFInfo
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- CN110450957A CN110450957A CN201910879454.3A CN201910879454A CN110450957A CN 110450957 A CN110450957 A CN 110450957A CN 201910879454 A CN201910879454 A CN 201910879454A CN 110450957 A CN110450957 A CN 110450957A
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- front foot
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- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 claims abstract description 42
- 238000005183 dynamical system Methods 0.000 claims abstract description 29
- 230000033001 locomotion Effects 0.000 claims abstract description 14
- 230000009471 action Effects 0.000 claims description 12
- 238000013519 translation Methods 0.000 claims description 7
- 230000008859 change Effects 0.000 claims description 6
- 230000005484 gravity Effects 0.000 claims description 4
- 230000004044 response Effects 0.000 claims description 4
- 230000000694 effects Effects 0.000 claims description 3
- 230000003028 elevating effect Effects 0.000 claims description 2
- 230000002093 peripheral effect Effects 0.000 claims description 2
- 230000007246 mechanism Effects 0.000 abstract description 3
- 230000015654 memory Effects 0.000 description 32
- 238000004891 communication Methods 0.000 description 11
- 238000010586 diagram Methods 0.000 description 6
- 238000012544 monitoring process Methods 0.000 description 5
- 238000007634 remodeling Methods 0.000 description 5
- 230000008901 benefit Effects 0.000 description 4
- 230000005055 memory storage Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000003287 optical effect Effects 0.000 description 3
- 238000012545 processing Methods 0.000 description 3
- 230000001052 transient effect Effects 0.000 description 3
- 238000012937 correction Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000007613 environmental effect Effects 0.000 description 2
- 239000004973 liquid crystal related substance Substances 0.000 description 2
- 210000001699 lower leg Anatomy 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 241001416181 Axis axis Species 0.000 description 1
- 230000006399 behavior Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000003137 locomotive effect Effects 0.000 description 1
- 238000004091 panning Methods 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 238000005303 weighing Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C19/00—Aircraft control not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Rehabilitation Tools (AREA)
Abstract
The present invention relates to a kind of active flight slide plates.The active flight slide plate includes the fuselage longitudinally extended, the dynamical system being arranged in around fuselage, flight control system, dynamical system, user's control system；Dynamical system includes preceding power plant module and rear power plant module, and in front fuselage, rear power plant module is arranged in back body for preceding power plant module setting.User's system includes user input unit and to user's display device, and user input unit includes front foot control device, rear foot control device.Flight control system is operatively associated with dynamical system and to be operable to independently control each power plant module in dynamical system include each Power Component in each power plant module of independent control.The present invention has almost liberated the both hands of people, and operation is more flexible, meets human motion mechanism, user is allowed to enjoy the experience and enjoyment of free flight in the sky.
Description
Technical field
The present invention relates to manned vehicle fields, and in particular to a kind of active flight slide plate.
Background technique
Such as with the famous plate type games of flexible operating: four skateboards, surfing, Halfpipe, vigor plate become crowd naturally
The derivative source of more personal aircrafts.
Arcaspace team, Romania in 2015 is proposed suspension of another money using 36 ducted fans as power source
Slide plate Arcaboard.The slide plate principle is substantially identical as above-mentioned Omniboard, whole in operation to come by changing operator's center of gravity
Change slide plate inclined direction, i.e. heading.Due to only operating by changing center of gravity, operator also needs whole to keep high-pressure
State, because slight mass centre changing will cause the inclination of entire fuselage, stability is low, reduces operation to keep balance
Amplitude, equally greatly limits the flying speed of slide plate, at the same the both hands to be kept into balance do not liberated completely and
Flying height is low.
Summary of the invention
The present invention is intended to provide a kind of active flight slide plate, the active flight slide plate person of can be used almost liberate operation
The both hands of person, operation is more flexible, and more flare maneuvers meet the locomotory mechanism of human body, and user is allowed to experience in the sky certainly
By the feeling flown.
Technical solution of the present invention:
A kind of active flight slide plate, including the fuselage longitudinally extended, the dynamical system being arranged in around fuselage, flight control system
System, dynamical system, user's control system；
The dynamical system includes preceding power plant module and rear power plant module, and the preceding power plant module is arranged in the front fuselage,
Power plant module is arranged in the back body after described.
User's system, user's system include user input unit and to user's display device, user's input
Device includes front foot control device, rear foot control device.Flight control system, flight control system operatively with it is dynamic
It includes that independent control is every that Force system, which is associated and is operable to independently control each power plant module in dynamical system,
Each Power Component in a power plant module.
Active flight slide plate further includes the fixed device of front foot and the fixed device of the rear foot, and the fixed device of front foot and the rear foot fix dress
It sets and couples with the upper surface of front foot control device and rear foot control device, the fixed device of front foot and the fixed device of the rear foot can also lead to
It crosses belt, shoe cover, electromagnet and is bonded fixation with two foot bottoms of user, the fixed device of front foot in some embodiments and the rear foot
Fixed device can not use.
The method have the benefit that:
Invention introduces the conflicts that step control device stress difference limen value avoids the control of repetition footwork, almost liberate
The both hands of people, operation is more flexible, meets human motion mechanism, user is allowed to enjoy the experience and pleasure of free flight in the sky
Interest；It also introduces peripheral control unit and plays booster action, make user's flight more safety more humane.
Detailed description of the invention
In order to which the features and advantages of the present invention are more fully understood, referring now to detailed description and attached drawing of the invention,
In the accompanying drawings, corresponding appended drawing reference in different attached drawings refers to corresponding component and in the accompanying drawings:
Fig. 1 is a kind of perspective view for active flight slide plate that embodiment of the present invention provides.
Fig. 2 is the state diagram of a kind of active flight slide plate that embodiment of the present invention provides turned to the left.
Fig. 3 is the state diagram of a kind of active flight slide plate that embodiment of the present invention provides turned to the right.
Fig. 4 is a kind of state diagram of the Throttle Opening Control for active flight slide plate that embodiment of the present invention provides.
Fig. 5 is the front foot control device and rear foot control device for a kind of active flight slide plate that embodiment of the present invention provides
Structure chart.
Fig. 6 is a kind of control system block diagram of the flight slide plate for active flight slide plate that embodiment of the present invention provides.
Specific embodiment
Although realizing and using for various embodiments of the invention is described in detail below it should be appreciated that
, the present invention provides many applicable inventive concepts that can implement in each particular case.It is described herein
Specific embodiment is merely illustrative, the range being not intended to limit the present invention.It for clarity, in the present invention may be no pair
All features of actual implementation scheme are all described.Obviously it should be understood that opening in any this actual implementation mode
Many specific implementations must be all made in hair to determine, to realize the specific objective of developer, such as meet system correlation and industry
It is engaged in relevant limitation, these limitations are different with the difference of embodiment.However, it should be understood that such development
It may be complicated and time-consuming, but still can be the routine work that those benefit from those of ordinary skill in the art of the invention.
In the description, when describing the device in attached drawing, the spatial relationship and portion that are referred between all parts
The spatial orientation of the various aspects of part.However, as those skilled in the art will be recognized after the complete reading present invention, herein
Described in device, component, equipment etc. can be with any desired orientation positions.Therefore, because dress described herein
Setting can be oriented with any desired direction, thus using such as " in ... top ", " in ... lower section ", "upper", "lower", hang down
Straight term or other similar term are come the various aspects that describe the spatial relationship between all parts or describe these components
Spatial orientation should be understood as that the space for the various aspects for describing relativeness or these components between these components takes respectively
To.When component is referred to as " being fixed on " another component, it can be directly on another component or there may also be placed in the middle
Component.When a component is considered as " being set to " another component, it can be set up directly on another component or
Person may be simultaneously present component placed in the middle.As used herein, term " connection " may include by any means including
The direct or indirect connection of mobile mechanical connection and/or non-moving mechanical connection；
Unless otherwise defined, all technical and scientific terms used herein and the technology for belonging to technical field of the invention
The normally understood meaning of personnel is identical.It is specific that term as used herein in the specification of the present invention is intended merely to description
The purpose of embodiment, it is not intended that in the limitation present invention.Term as used herein "and/or" includes one or more relevant
Any and all combinations of listed item；Term " first " that the embodiment of the present invention uses, " second ", " third " and
" the 4'sth " is not have succession and importance to distinguish an element and another element；In addition, following
When being related to attached drawing, the same appended drawing reference in different attached drawings indicates the same or similar element for description.
With reference to the accompanying drawing, it elaborates to some embodiments of the present invention.In the absence of conflict, following
Feature in embodiment and embodiment can be combined with each other.
Referring to attached drawing fuselage for carrying user and installation electronic device, dynamical system 20.
As illustrated, dynamical system 20 includes the power plant module of four independent operations.Power plant module respectively be distributed in
The dynamical system 20 of fuselage left front and right front and can be referred to as before power plant module.Power plant module is respectively coupled to left back
Side and right back and power plant module after being referred to as, in other embodiments, preceding power plant module or rear power plant module are one
A power plant module, 3 power plant modules, 4 power plant modules etc., are specifically subject to actual design.
Dynamical system 20 includes that can be permanently mounted or can be attached independently to dynamical system 20 and can be driven
Multiple power plant modules that Force system 20 is dismantled.
In the present embodiment, power plant module drives propeller type to provide power, in other embodiments, power for motor
System 20 is internal combustion engine, duct, culvert type engine, jet engine or rocket type engine
In illustrated embodiment, user input unit includes front foot control device 21 and rear foot control device 22, preceding
Foot control device 21 is substantially in cylindrical body, and the lower end center of front foot control device 21 extends downwardly an axis, it will be appreciated that referred to as perpendicular
Axis, 21 upper end of front foot control device is fluted, groove be substantially in hemisphere and substantially be in semicylinder two grooves；Front foot control
Device 21 further includes the assembly for being substantially in hemisphere and two half-cylinders, and two half-cylinders setting is round in hemispheroidal upper end
On the same axis in symmetry axis two sides, two half-cylinders can be understood as horizontal axis, and assembly can be with the groove held on the cylinder
It is overlapped connection, there are many inductors, inductor to be used to capture the front foot footwork of user for setting in front foot control device
Signal and by user's front foot exert a force signal；Front foot control device 21 can be rotated by axis of horizontal axis, can also restore initially flat
Weighing apparatus state；Front foot control device 21 can also be rotated by axis of vertical pivot；Rear foot control device 22 is in substantially cylindrical body, under cylindrical body
End center extends downwardly an axis, it will be appreciated that is vertical pivot, a variety of inductors are arranged inside rear foot control device 22, make for capturing
The force signal of the action signal of user's rear foot step and user's rear foot to rear foot control device 22.
The shape that front foot control device 21 and rear foot control device 22 are arranged not necessarily substantially is in cylindrical body and is substantially in
The assembly of hemisphere and semicylinder can also be in other shapes, such as cuboid, square, ellipsoid, sphere, sphere
Combination between combination cylinder body etc., in the present embodiment, front foot control device 21 and rear foot control are that an axis and two axis revolve
Turn, in other embodiments, 22 location swap of preceding foot control device and rear foot control device, front foot control device 21 is changed to the rear foot
Control device 22, rear foot control device 22 are changed to front foot control device 21,
User's system, user's system includes user input unit, and the user input unit includes preceding foot control
Device 21 and rear foot control device 22 processed, the front foot control device 21 setting in the front fuselage portion, with the fuselage at
Predetermined angular setting, the rear foot control device 22 are arranged in the back body portion, are arranged with the fuselage at predetermined angular；
The front foot control device 21 can be tilted to the left under the foot-operated effect and/or change center of gravity of user in whole or in part
Or be tilted to the right, the rear foot control device 22 in whole or in part can be under the drive of the footwork of human body with scheduled angle
It in whole or in part can also be under the drive of the footwork of human body with scheduled angle for axis rotation or the front foot control device 21
Degree is that axis rotates；
The front foot control device 21 and the rear foot control device 22 further include motion sensor and pressure inductor, described dynamic
Make inductor and pressure inductor is arranged on the front foot control device 21 and the rear foot control device 22, the preceding foot control
The pressure that device 21 processed can capture the action signal of user's front foot and front foot applies the front foot control device 21, institute
Stating rear foot control device 22 can capture the pressure and user that user's rear foot applies the rear foot control device 22
The pressure that heel or rear foot tiptoe apply 22 left side of rear foot control device or the right afterwards；The rear foot control device 22
It in whole or in part can be under the drive of the footwork of human body using scheduled angle as axis rotation and the front foot control device 21
It can also be rotated under the drive of the footwork of human body by axis of scheduled angle in whole or in part, the rear foot control device 22
Before the footwork signal or the front foot control device 21 that user's rear foot can also be captured can also capture user
The action signal of foot；
As described in this article, each power plant module is individually controllable, so that certain power plant module is in distributed propulsion system
Interior operation change, which can be realized, controls the forward-reverse of aircraft, steering and translation during VTOL operation.For example, passing through
The thrust for changing preceding power plant module relative to rear power plant module exports, and realizes forward-reverse control.As another example, pass through
Change thrust output of the power plant module of left front, left back relative to right front, right back power plant module, realizes translation control
System.The thrust for changing specified power system 20 exports to realize course changing control.Dynamical system 20 can be optionally standardization and
Interchangeable unit, unit can optionally be easily fitted to active flight slide plate and remove from active flight slide plate
Route replaceable units.In addition, the use of route replaceable units is in the faulty situation of one of discovery propulsion assembly
It is beneficial in terms of repair.In such a case, it is possible to pass through shirtsleeve operation --- for example, unloading structural elements
Bolt disconnects communication line and other suitable operations --- and the power plant module of failure and active flight slide plate are disconnected and joined
It connects.Then can by connection communication line, structural elements is linked together with bolt and operation that other are suitable will
Another propulsion assembly is attached to active flight slide plate.
Active flight slide plate has electric energy, which is depicted as being accommodated in fuselage, and the electric energy is via in fuselage
Communication line be supplied to each propulsion assembly to be directly provided with power to electric motor.
Alternative or additionally, body can accommodate one or more electricity for the electric energy that can be used as dynamical system 20
Pond.Battery can be electrically charged at earth station.Battery can also be removed and is mounted to enable in a manner of interchangeable
Effective battery again, this may be particularly advantageous in the embodiment that only electric energy of active flight slide plate is battery
's.In the embodiment with both battery and electric energy generating system, battery can provide non-firm power source so that power
Flight slide plate being capable of the safe landing in the case where electric energy generating system breaks down.
Referring additionally to Fig. 6 in attached drawing, block diagram, which depicts, to be operable to make together with active flight slide plate of the invention
Power skateboard control system 100.In illustrated embodiment, system 100 includes three sons based on master computer
System；That is, autonomous system 102, pilot's system 104 and remote system 106.As described in this article, power of the invention
Flight slide plate can automatically be operated, flight control system 108 in response to the order that is generated by flight control system 108
Non-transient computer readable storage medium is preferably included, non-transient computer readable storage medium includes that can be held by processor
One group of capable computer instruction.Flight control system 108 can be in one or more general purpose computers, special purpose computer
Or the triplex level redundancy system realized on the other machines with memory and processing capacity.For example, flight control system 108 can
To include one or more memory memory modules, including but not limited to: storage inside memory such as random access memory
Device, nonvolatile memory such as read-only memory, removable memory such as magnetic storage memory, are consolidated optical storage memory
State stores memory or other suitable memory storage entities.Flight control system 108 can be is based on microprocessor
System, the system are operable to execute the program code in machine-executable instruction form.In addition, 108 energy of flight control system
Enough via proprietary encryption network, public encryption network, internet or other conjunctions that may include both wired connection and wireless connection
Suitable communication network and be selectively connected to other computer systems.
In illustrated embodiment, flight control system 108 includes command module 110 and monitoring module 112.Ability
Field technique personnel should be understood that can be in a variety of manners by these and other modules that flight control system 108 executes ---
Including hardware, software, firmware, application specific processor and their combination --- Lai Shixian.The reception of flight control system 108 comes from
The input of each provenance, each provenance include: inside sources, for example, for sensor 114, controller 116, power plant module 118,120,
122,124 and pilot's system 104；And external source, such as remote system 106, GPS satellite or other positioning
System etc..For example, it includes task that flight control system 108 can be received from pilot's system 104 and/or remote system 106
The flight plan of starting position and end position.Hereafter, flight control system 108 is operable to automatically control of the invention
All aspects of the flight of active flight slide plate.
For example, command module 110 provides order to controller 116 in the various operation modes of active flight slide plate.These
Order make it possible to each power plant module 118,120,122,124 of independent operation, including for example control rotor rotation speed,
Adjust thrust powers etc..Flight control system 108 receives the feedback from controller 116 and each power plant module.The feedback is
It is handled by monitoring module 112, monitoring module 112 can provide correction number to command module 110 and/or controller 116
According to and other information.Sensor 114 such as alignment sensor, attitude transducer, velocity sensor, environmental sensor, fuel pass
Sensor, temperature sensor, position sensor etc. also provide information to flight control system 108 to further enhance autonomous control energy
Power.
Some autonomous control abilities of flight control system 108 or whole autonomous control abilities can be controlled by distance flight
The enhancing of system 106 replaces.Remote system 106 may include can general purpose computer, special purpose computer or have memory and
One or more computing systems realized on the other machines of processing capacity.For example, computing system may include one or more
Multiple memory memory modules, including but not limited to: storage inside memory such as random access memory, non-volatile memories
Device such as read-only memory, removable memory such as magnetic storage memory, optical storage memory, solid-state storage memory or its
His suitable memory storage entity.Computing system can be microprocessor-based system, which is operable to execute
In the program code of machine-executable instruction form.In addition, computing system can be via may include wired connection and wireless connection
Proprietary encryption network, public encryption network, internet or other suitable communication networks of the two and be connected to other computers
System.Communication network can be the network of local area network, wide area network, internet or any other type, these network connections are multiple
Computer is by using the communication technology appropriate --- such as transmission control protocol/internet protocol, File Transfer Protocol, super literary
This transport protocol, Internet Protocol Security Protocol, Point to Point Tunnel Protocol, secure socket layer protocol or other suitable agreements ---
And various communication patterns are realized via internet message.Remote system 106 is via including wired connection and both wireless connections
Communication link 130 is communicated with flight control system 108.
Remote system 106, which preferably includes, is configured to display information related with one or more aircraft of the invention
One or more flying quality display devices 126.Display device 126 can be configured to any suitable form, including example
As liquid crystal display, light emitting diode indicator, cathode-ray tube display, VR equipment or any suitable type display.
Remote system 106 can also include audio output and input unit, such as microphone, loudspeaker and/or audio port, to permit
Perhaps operator communicates with the user on such as active flight slide plate.If using touch-screen display embodiment,
Display device 126 is also used as remote entry unit 128, but can also alternatively use other remote entry units,
Such as keyboard or control stick, to allow operator response to provide control command to the aircraft just operated in long-range control.
For example, in the various operation modes of active flight slide plate --- bind foot walk control model one, step control model two and
Conversion between them --- period, command module 110 provide order to controller 116.These orders make it possible to independent behaviour
Make each power plant module 118,120,122,124, including rotation speed, the adjusting thrust powers etc. for for example controlling rotor.In addition,
These orders enable aircraft 10 to be turned between vertical lift orientation, backward thrust orientation and forward thrust orientation
It changes.In the embodiment for the pitch that can change blade, these orders make it possible to each power plant module of independent operation, including example
It such as controls the rotation speed of rotor, adjust thrust powers.Flight control system 108 receives from controller 116 and each dynamic
The feedback of power module.The feedback is handled by monitoring module 112, monitoring module 112 can to command module 110 and/
Or controller 116 provides correction data and other information.Sensor 114 such as alignment sensor, attitude transducer, velocity pick-up
Device, environmental sensor, battery sensor, temperature sensor, position sensor etc. also to flight control system 108 provide information with
Further enhance autonomous control ability.
Some autonomous flight controls of aircraft of the invention and/or distance flight control or whole autonomous flight controls
And/or distance flight control can fly control from the airborne user of user's system 104 with origin to enhance or replace.It uses
Person's system 104 can be with the integrated either autonomous system of autonomous system 102, the autonomous system preferably include it is non-transient
Computer readable storage medium, non-transient computer readable storage medium include can by processor execute and can be by general
Computer, special purpose computer or the one group of computer instruction realized with memory and the other machines of processing capacity.Power flies
Row sledge system 104 may include one or more memory memory modules, and memory memory module includes but is not limited to: interior
Portion stores memory such as random access memory, nonvolatile memory such as read-only memory, removable memory such as
Magnetic storage memory, optical storage memory, solid-state storage memory or other suitable memory storage entities.User's system
104 can be microprocessor-based system, which is operable to execute the program generation in machine-executable instruction form
Code.In addition, pilot's system 104 can be via may include wired connection and the proprietary encryption network, public both being wirelessly connected
Refined net, internet or other suitable communication networks and be connected to other computer systems.User's system 104 can be with
It is communicated via the communication channel 136 for preferably including wired connection with flight control system 108.
User's system 104 preferably includes the cockpit display device 132 for being configured to that information is shown to airborne user.
Cockpit display device 132 can be configured to any suitable form, including such as such as liquid crystal display, light emitting diode are shown
Show one or more display screens of device or the like or including such as display panel, instrument panel display VR equipment, AR equipment, increasing
The suitable display of any other type of strong reality displays etc..Pilot's system 104 can also include audio output with
Input unit, such as microphone, loudspeaker and/or audio port, so that airborne user be allowed to manage with such as air traffic
Or the operator of remote system communicates.If using AR equipment embodiment, cockpit display device 132 can also be used
Make user input unit 134, however, it is also possible to alternatively using other users interface equipment to allow airborne user to ring
Should in external control equipment for example including but be not limited to control panel, machine control unit, hand controller, voice controller,
The airborne user of E.E.G controller or other control systems controls to the active flight slide plate just operated and provides control command
It at least can control the elevating movement of active flight slide plate.As for those of ordinary skills it is evident that passing through
Using system 100, power aerial vehicle of the invention can be in response to including autonomous flight control, distance flight control or airborne making
The fly flight control protocol of control and their combination of user operates.
As indicated with 1, in this configuration, it is contemplated that the posture of active flight slide plate, each rotor have general horizontal
Orientation.Flight control system independently controls each power plant module and control thrust powers to generate lift and provide pitching control
System, course changing control and translation control.
Next the control mode of description active flight skateboarding mode of the present invention is as follows:
When the front foot tiptoe or heel of user is to the right force of the front foot control device 21 or the front foot step of user
Movement makes the front foot control device 21 with the axial right rotation of horizontal axis, and the front foot control device 21 captures user's front foot
The action signal that turns to the right and it is transmitted to the flight control system, further controls the output of the dynamical system 20, make
The tilting rotor flight slide plate turns to the right, when the front foot tiptoe or heel of user is to the left side of the front foot control device 21
The front foot footwork of side force or user make the front foot control device 21 with the axial anticlockwise of horizontal axis, the preceding foot control
Device 21 processed captures the action signal that user's front foot turns to the left and is transmitted to the flight control system, further controls
The output of the dynamical system 20 turns to the tilting rotor flight slide plate to the left, and the front foot control device 21 is with horizontal axis
Axis left rotation and right rotation is provided with adjustable threshold, understandable to be, the front foot control device 21 is rotated left and right by axis of horizontal axis,
It is better to rotate the more big then turning efficiency of angle；When the rear foot tiptoe or heel of user is to the right of the front foot control device 21
Force, the rear foot control device 22 capture user's rear foot to right translation action signal and be transmitted to the flight and control
System processed further controls the output of the dynamical system 20, makes the tilting rotor flight slide plate to right translation, works as user
Front foot tiptoe or heel exert a force to the left side of the front foot control device 21, the rear foot control device 22 captures user
The translation of moving to the left of the rear foot makees signal and is transmitted to the flight control system, further controls the defeated of the dynamical system 20
Out, make the tilting rotor flight slide plate to left, heel or tiptoe are right to the rear foot control device 22 after user
Side or the right exert a force, and more big then panning effect is faster, and described 22 the right of rear foot control device and the left side are respectively provided with strong adjustable threshold
Value, it is contemplated that the power of user's rear foot tiptoe or heel is greater than the adjustable threshold on both sides, and it is then adjustable threshold that power, which is greater than adjustable threshold,
Maximum value in being worth；Reach when the movement of user's front foot drives the front foot control device 21 to rotate clockwise using vertical pivot as axis
The big purpose of throttle is controlled, or when the movement drive front foot control device 21 of user's front foot is reached using vertical pivot as axis rotation
To the purpose of control throttle, the front foot control device 21 is rotated by axis of vertical pivot, and rotation angle is also equipped with adjustable threshold, is surpassed
Threshold value is crossed not rotate then, it is contemplated that the left foot of user in the preceding situation of preceding or right crus of diaphragm, the front foot control device 21 with
Vertical pivot is axis rotation, and specific direction of rotation is to increase Throttle Opening Control counterclockwise or clockwise, and direction of rotation is adjustable；Work as use
The movement of person's rear foot drives the rear foot control device 22 to finely tune using vertical pivot as axis rotation to achieve the purpose that control throttle, described
Rear foot control device 22 is rotated by axis of vertical pivot, and rotation angle is also equipped with adjustable threshold, is not rotating then more than threshold value, is considered
To user left foot in the posterior situation of rear or right crus of diaphragm, the rear foot control device 22 is rotated by axis of vertical pivot, specific to rotate
Direction is to increase Throttle Opening Control counterclockwise or clockwise, and direction of rotation is adjustable；When the front foot control device 21 is made
The power of user's front foot relative to the rear foot control device 22 by user's rear foot power difference in the positive threshold value of adjustable height, institute
It states front foot control device 21 and rear foot control device 22 captures the signal of user to travel forward and is transmitted to the flight
Control system further controls the output of the dynamical system 20, so that the tilting rotor flight slide plate is travelled forward, when described
Front foot control device 21 is poor by the power of user's rear foot relative to the rear foot control device 22 by the power of user's front foot
Value in adjustable Low threshold, believe by the movement for the hovering that the front foot control device 21 and rear foot control device 22 capture user
Number and be transmitted to the flight control system, further control the output of the dynamical system 20, the tilting rotor flight is slided
Plate hovering movement, when the front foot control device 21 by user's front foot power relative to the rear foot control device 22 by
For the power difference of user's rear foot in adjustable height negative threshold value, the front foot control device 21 and rear foot control capture user's
Motor message and it is transmitted to the flight control system backward, further controls the output of the dynamical system 20, makes described to incline
Switch rotor flight slide plate is moved or is braked backward, the front foot control device 21 by user's front foot power relative to after described
Foot control device 22 by user's rear foot power difference the more big then described dynamical system 20 of the positive threshold value of adjustable height and fuselage to
Top rake is more obvious, the front foot control device 21 by user's front foot power relative to the rear foot control device 22 by
The power difference of user's rear foot is smaller in adjustable height negative threshold value, and the dynamical system 20 and fuselage are tilted backwards and be more obvious；It examines
Consider the front foot control device 21 by user's front foot power relative to the rear foot control device 22 by user after
The case where power difference of foot is greater than the positive threshold value of adjustable height or is less than adjustable height negative threshold value, the front foot control device 21 is used
The power of person's front foot is greater than the positive threshold value of adjustable height by the power difference of user's rear foot relative to the rear foot control device 22
Maximum value in the positive threshold value of adjustable height.
For the purpose of diagram and description, the foregoing description of the embodiments of the present invention is had been presented for.This not anticipates
It is being exhaustion or is limiting the invention to invented precise forms, and in view of teachings above, remodeling and modification is possible
Or it according to the present invention can practice to know.Each embodiment is chosen and described to illustrate the principle of the present invention and its practice
Using, and then enable those skilled in the art in various embodiments using the present invention and by being suitable for contemplated spy
The various remodeling for determining purposes come using the present invention.Each embodiment can be set without departing substantially from the scope of the present invention
Other alternatives, remodeling, modification and omission are made in meter, operating condition and setting.To those skilled in the art, work as reference
When specification, these remodeling of illustrated embodiment and combination and other embodiments be will be apparent.Therefore, appended power
Benefit requires to be intended to these any remodeling or embodiment.
Claims (7)
1. a kind of active flight slide plate, it is characterised in that: the active flight slide plate includes the fuselage longitudinally extended, is arranged in machine
Dynamical system, flight control system, user's system around body；
The dynamical system includes preceding power plant module and rear power plant module, and the preceding power plant module is arranged in the front fuselage,
Power plant module is arranged in the back body after described；
User's system, user's system includes user input unit, and the user input unit includes preceding foot control
Device and the rear foot control device processed, the front foot control device are arranged in the front fuselage portion, with the fuselage at predetermined angle
Degree setting, the rear foot control device are arranged in the back body portion, are arranged with the fuselage at predetermined angular；The front foot
Control device can be tilted to the left under center of gravity or in the foot-operated effect and/or change of user to Right deviation in whole or in part
Tiltedly, the rear foot control device in whole or in part can the footwork of human body drive under using scheduled angle be axis rotation or
The front foot control device can also rotate under the drive of the footwork of human body by axis of scheduled angle in whole or in part；
The front foot control device and the rear foot control device further include motion sensor and pressure inductor, the sense of movement
Device and pressure inductor is answered to be arranged on the front foot control device and the rear foot control device, the front foot control device can
To capture the action signal and the pressure that applies to the front foot control device of front foot of user's front foot, the rear foot control dress
Set heel or rear foot foot after can capture the pressure and user that user's rear foot applies the rear foot control device
The pressure that point applies the rear foot control device left side or the right；The rear foot control device in whole or in part can be in human body
Footwork drive under using scheduled angle be axis rotation or the front foot control device in whole or in part can also be in human body
Footwork drive under using scheduled angle be axis rotation, the rear foot control device can also capture user's rear foot
Footwork signal or the front foot control device can also capture the action signal of user's front foot；
Flight control system, the flight control system is operatively associated with the dynamical system and can grasp
It includes each in the independent each power plant module of control for being made each power plant module independently controlled in the dynamical system
A Power Component；
The flight control system can also be associated with the user input unit, and user's front foot and/or the rear foot are to institute
It states front foot control device and/or rear foot control device carries out different operation to control the advance, retrogressing, brake of the power aerial vehicle
Vehicle, advance, steering, translation, hovering movement.
2. active flight slide plate as described in claim 1, it is characterised in that: the front foot control device can also be with before described
The upward vertical line in foot control device upper surface center is axis rotation, and the upward vertical line in front foot control device upper surface center is
Axis rotary setting has threshold rotating value, and the front foot control device can also capture the action signal of user's front foot and front foot is applied
Under power is big.
3. active flight slide plate as described in claim 1, it is characterised in that: the rear foot control device can also be with after described
The upward vertical line in foot control device upper surface center is axis rotation, and the upward vertical line in rear foot control device upper surface center is
Axis rotary setting has threshold rotating value, and the rear foot control device can also capture the action signal of user's rear foot.
4. active flight slide plate as claimed in claim 3, it is characterised in that: the front foot control device can also be with before described
The upward vertical line in foot control device upper surface center is axis rotation, and the upward vertical line in front foot control device upper surface center is
Axis rotary setting has threshold rotating value, and the front foot control device can also capture the action signal of user's front foot and front foot is applied
Under power is big.
5. such as the described in any item active flight slide plates of claims 1 to 4, it is characterised in that: the user input unit is also
Including external control devices, the external control devices include but is not limited to hand controller, voice controller, E.E.G control
Device, the peripheral control unit at least can control the elevating movement of the active flight slide plate, the flight control system response
Control, distance flight control, autonomous flight control and combinations thereof are flown in airborne user to grasp
Control the operation of the rotor.
6. active flight slide plate as claimed in claim 5, it is characterised in that: user further includes showing to believe to airborne user
The display device of breath, it is described to user's display device include but is not limited to AR equipment, display.
7. such as the described in any item active flight slide plates of claims 1 to 6, it is characterised in that: the active flight slide plate also wraps
The fixed device of front foot and the fixed device of the rear foot are included, the fixed device of the front foot and the rear foot fix device and the front foot control device
Couple with the upper surface of rear foot control device, the fixed device of the front foot and the fixed device of the rear foot can also by belt, shoe cover,
Electromagnet is bonded fixation with two foot bottoms of user.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910879454.3A CN110450957A (en) | 2019-09-18 | 2019-09-18 | Active flight slide plate |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910879454.3A CN110450957A (en) | 2019-09-18 | 2019-09-18 | Active flight slide plate |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110450957A true CN110450957A (en) | 2019-11-15 |
Family
ID=68492256
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910879454.3A Pending CN110450957A (en) | 2019-09-18 | 2019-09-18 | Active flight slide plate |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110450957A (en) |
-
2019
- 2019-09-18 CN CN201910879454.3A patent/CN110450957A/en active Pending
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Application publication date: 20191115 |