CN109018381A - Jet-propelled Electric aircraft - Google Patents
Jet-propelled Electric aircraft Download PDFInfo
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- CN109018381A CN109018381A CN201811035797.3A CN201811035797A CN109018381A CN 109018381 A CN109018381 A CN 109018381A CN 201811035797 A CN201811035797 A CN 201811035797A CN 109018381 A CN109018381 A CN 109018381A
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/16—Aircraft characterised by the type or position of power plants of jet type
- B64D27/20—Aircraft characterised by the type or position of power plants of jet type within, or attached to, fuselages
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of jet-propelled Electric aircrafts, belong to technical field of aerospace, it include: wind-tunnel 02, machine leaf 09, go up and down leaf 016, landing gear 015 is constituted: being characterized in: using wind-tunnel as propeller power, automatic vacuum jet high-speed motor 08 is equipped in wind-tunnel, as long as medium reaches the boiling point of setting in vacuum, heat can be transmitted moment and radiating airflow is sprayed outward with supersonic velocity, in conjunction with the dual acceleration of the first wind wheel and the second wind wheel, aircraft is further pushed to accelerate to advance, the information that unmanned middle computer 05 is transmitted according to wireless camera and radar antenna, the angular dimension of the mobile butterfly valve door 011 of rapid process instruction stepper motor 012, it is precisely controlled left and right spray air flow, cooperation lifting 016 safe flight of leaf；It makes a silk purse out of a sow's ear, it solves and is restricted for a long time by temperature rise heat, motor cannot replace difficulty of the internal combustion engine as jet high-speed propeller, have the characteristics that energy conservation and environmental protection, zero-emission, noise is low, structure is simple, high-efficient, be the original breakthrough of modern Electric aircraft system.
Description
Technical field
The present invention relates to technical field of aerospace, a kind of jet-propelled Electric aircraft is special using wind-tunnel propeller as power
Be not related to one kind in wind-tunnel motor can automatic vacuum operating, convert vacuum jet power for internal damaging heat,
The jet-propelled Electric aircraft of the automatic superposing control of power.
Background technique
In the prior art, electric airplane is using electric power propulsion system instead of combustion engine powered, to obtain many excellent
Point and distinguishing character, most prominent advantage are energy conservation and environmental protections, and close to zero-emission, noise and level of vibration are very low, and structure is simple, at
This is low；But there are two the technical issues of aspect to limit the development of Electric aircraft；It the first, is battery problems, in aircraft
On, each gram weight can mean that the increase of cost, and for the angle of energy density, fuel oil is 60 times of lithium battery, therefore
Drive manned aircraft cost high with lithium battery, currently, having had the electric airplane to fly up into the sky, mainly with electronic light-duty fixation
Based on winged petiole aircraft or electric helicopter, bearing capacity is limited；The second, crucially problem in terms of main motor, due to coil
The heat that resistance and pot-motor generate can not discharge in time, limit the raising of motor power (output) and weight ratio, because
This up to the present, electric airplane can only also calculate the product of a conceptual phase.
Summary of the invention
Object of the present invention is to overcome drawbacks described above, realized using a kind of technical solution of jet-propelled Electric aircraft.
A kind of jet-propelled Electric aircraft, comprising: wind-tunnel 02 and shell 022, fitting machine leaf 09, liter in wind-tunnel shell two sides
Drop leaf 016, landing gear 015 and remote controler 001 are constituted: being characterized in: jet propeller power is used as using wind-tunnel 02, in wind-tunnel
Equipped with automatic vacuum jet high-speed motor 08, as long as medium reaches the boiling point of setting in vacuum, moment heat can be transmitted
Amount sprays radiating airflow with supersonic velocity outward, in conjunction with the dual acceleration of the first wind wheel and the second wind wheel, further pushes flight
Device accelerates to advance, the information that unmanned middle computer 05 is transmitted according to wireless camera and radar antenna, rapid process instruction step
Into the angular dimension of the mobile butterfly valve door 011 of motor 012, it is precisely controlled left and right spray air flow, cooperation lifting 016 safe flight of leaf；
It makes a silk purse out of a sow's ear, solves and restricted for a long time by temperature rise heat, motor cannot replace internal combustion engine to promote as jet high-speed
Device flies the difficulty in upper blue sky, has the characteristics that energy conservation and environmental protection, zero-emission, noise is low, structure is simple, high-efficient, is modern electronic
The original breakthrough of propulsion system can install side by side several wind-tunnel, jet direction is consistent, both increases as long as power supply is abundant enough
Conduct is spare again for strong power, makes flying speed faster, safer.
A kind of jet-propelled Electric aircraft, the motor 08 are jet-propelled internal rotor high-speed motor, comprising: two
Turntable 2 or X superimposed type turntable 201 are fixed on the convex shelves backer two sides of main shaft 01, turntable 2 with flat key and follower bolt 23 respectively
Or 3. permanent magnet 10 of magnetic guiding loop, fan blade 12 or reinforcing rib 9 are each provided in X superimposed type turntable 201；01 both ends of main shaft lead to respectively
It crosses bearing 7 and connects first end cover 1 and second end cover 101, the outer nose circle of two end caps is a with stator 6 or S each by bolt, 11
Superimposed type stator 601 is tightly connected, and gap 12, sensor 21, the terminal block in terminal box are equipped between stator and plane of rotor disc
It is drawn with after seal stator by conducting wire 19；The difference is that: stator 6 or S superimposed type stator 601, by circuitron
Winding 5 is made in plate, under high vacuum ultra low temperature state, with non-magnetic metal packing sealed package, with powder metallurgic method, vacuum
High temperature compacting is sintered, and winding 5 is made to keep high vacuum state and ultralow temperature and high temperature traces of memory forever in stator,
Magnet ring 22 and permanent magnet 10 cooperation being arranged in ultrathin stator generate the floating effect of magnetic, and control gap 12 arrives minimum, makes electricity
Engine efficiency is up to 95% or more, carries out jet heat dissipation in conjunction with motor automatic vacuum-pumping apparatus, automatic vacuum-pumping apparatus includes: dynamic
Seal member and several uniaxial pressure intake valves 04 being located in first end cover 1 and several being located in second end cover 101
One-way exhaust valve 014 and the fan blade 18 being located on turntable are constituted；Motor rotate when fan blade promote internal heat and air-flow from
One-way exhaust valve is discharged rapidly, since the vacuum degree that uniaxial pressure intake valve will arrive setting can just be opened, so causing vacuum negative
Operating status is pressed, as long as medium has reached the boiling point of setting in vacuum, moment can absorb a large amount of heat, with the speed of ultrasonic sound
Heat is transmitted to distal end, so that the heat eliminating medium recycled in gap 12 is undergone phase transition generation " superconduction " phenomenon, transient absorption first big
The heat of amount is radiated with ultrasonic speed from one-way exhaust valve discharge jet, meanwhile, uniaxial pressure intake valve and one-way exhaust valve
Between generate interaction, frequency realizes resonance close to synchronous, and since jet heat dissipation flow velocity is fast, inner wall generates refrigeration effect, containment
The temperature of stator winding 5 and permanent magnet 10 rises, and band plays with winding superconduction or Asia superconductivity effects in high-intensity magnetic field and vacuum,
The load-bearing capacity of motor is greatly improved, makes the volume and weight of motor and traditional silicon steel sheet motor of Same Efficieney
It compares, 10 times of volume-diminished, the conventional motors of power ratio Same Efficieney increase 10 times, convert damaging heat inside motor to
Jet power especially adapts to use in aircraft, wherein X or S is natural number.
Barrel shape is made by Ti-Al alloy material in the shell 022, up and down each one circle boss slot of rolling, for circle bracket
06 uses with circle 010 fixed motor 08 of bracket, 02 front end of shell setting shield, hull outside left and right settings machine leaf 09, or
Person can be with the machine leaf 09 of automatic open-close by the control of computer 05, and setting photovoltaic cell supplements power supply, shell to battery 07 on machine leaf
Interior reserved air duct 020.
The motor main shaft 01 is made of austenite heavy wall stainless steel tube or round steel, the convex shelves conduct being arranged in main shaft
The backer between two turntables is fixed, convex shelves thickness is chosen and is assured that permanent magnet 10 and stator plane between two turntables
Between there are the size in gap 12, the distance in gap 12 be depending on motor power (output) size, can be 0.02~4.5mm's
Selection in range, main shaft are equipped with the sealing shelves of installation dynamic sealing component, and the external diameter surface roughness requirements for sealing shelves are≤
0.004mm, the diameter of axle straightness and circularity for sealing shelves require≤0.002 へ 0.004mm, are adapted in -50 DEG C~300 DEG C temperature
Automatic compensation gap in range is spent, constitutes good dynamic sealing with the cooperation of dynamic sealing component；The setting of 01 top of main shaft is greater than
The cone of major axis diameter is convenient for keeping concentricity in high speed rotation.
The dynamic sealing component is inner oil seal lid 15, and outer oil seal lid 17 sets ripple compensation set in outer oil seal lid lid, mechanical
The sealing shelves of requirement on machining accuracy and main shaft 1 are mating.
Winding 5 is made by double-sided printed-circuit board, according to the plane of a permanent magnet 10 in rotor in the motor stator
Several coils all stayed on the outside of copper foil windings end to end are made in long-pending and shape, the quantity of permanent magnet 10 in number of coils and rotor
It is identical to form a circle, it is connected in series between each coil and coil, then with spraying nanometer coatings under high vacuum state
Bonding is shaped into a phase monolithic winding, then by tri- groups of monolithic windings of a, b, c by 120 ° of phase shift angle stacking positioning, dry by vacuum
Dry processing sprays high-temperature resistant nano insulating coating under high vacuum low-temperature condition, and three-phase windings 5 are made in unified sizing bonding, or
Six phase windings 5 are made by 60 ° of phase shift angle stacking positioning, bonding in six groups of monolithic windings of person, and magnetic floating ring 22 is arranged in winding periphery.
First wind wheel 03 and the second turbine 013 are turbine fan or centrifugal vortex wind wheel, by no magnetic metal material system
At in the hope of big wind-force, high revolving speed, low voice.
The third bracket 21, upper end are cross triangular steel stainless steel frame, activity lifting butterfly valve door on the seat of center
011, lower end be set threaded round steel polished rod, for stepper motor 012 pass through be sleeved on the seat of center, stepper motor both ends with
Butterfly valve door is flexible coupling, the method that operation stepper motor is moved forward or rearward, and pushes butterfly valve door or so angular dimension to reach control
Spray air flow and left and right directions processed.
2 semicircle tab (s) are made by aluminum alloy materials in the butterfly valve door 011, are movably arranged on third pedestal upper end center
On seat, semicircle tab (s) is flexible coupling with 012 both ends of stepping motor being mounted in third pedestal lower end screw rod respectively, computer
05 control stepping motor 012 advances or retreats, to move 011 or so angular dimension of butterfly valve door, accurate quickly control left and right
The spray air flow in direction, cooperation lifting leaf 016, realizes the various directions and movement that air injection aerial vehicle or so flies up and down.
Inside the computer 05 be equipped with dynamic Control, temperature control, structure control, power supply control, posture execute control,
Pressure control, day line traffic control, command receiver, command encoder, shakes and surveys encoder, shakes and survey transmitter, infrared ray orbits controlling
Shake survey encoder, infrared ray night flight instrument, a series of wireless transceiver system etc. the due circuit process of UAVs and
Equipment powers on key and is in hot stand-by duty, remote controler 001 is waited to award the instruction for starting to take off.
The circuit process are as follows: the photovoltaic cell being arranged in above machine leaf 09 charges to battery 013, and battery passes through
Conducting wire is separately connected computer 05, motor 08, stepping motor 012, lifting leaf 016, the first wireless camera 017, the second nothing
Line camera 018, respective supply terminals, hot stand-by duty wait remote controler 001 to award radio contact and instruction of taking off；
Measured information is passed to 05 computer, computer computer by in-flight 017 first wireless camera and 018 second wireless camera
All parts are issued instructions in time after processing rapidly carries out operation operating；Wherein, remote controler 001 is only electric with 05 computer wireless
Connection, transmits mutually information, and computer 05 only receives the stopping of remote controler 001, opens and task object instruction, and is equipped with a key
One close, authorization is authorized to scrambling coding software and program, is conducive to anti-interference and encryption.
The remote controler 001 is a kind of wireless launcher, by modern digital coding, by key information into
Row coding emits light wave by infrared diode, and the infrared receiver of the received machine of light wave turns the infrared signal received
Become electric signal, be decoded into processor, demodulates corresponding instruction and wanted to reach the operation needed for 05 equipment of computer is completed
It asks；Remote controler 001 or mobile terminal or center controlling platform are equipped with wireless transmitter circuit, command encoder, authorization
Program etc., random after authorizing to generate accessed password, a machine one control does not receive other any instructions and control in the hope of secrecy peace
Entirely；It is encrypted by the way of the concealed that a key one close moment generates, piggybacking WiMAX channel or the channel fifi or Beidou
Navigation channel carries out information transmitting；Aircraft is a kind of high high-tech product of the risk of precision, and producer must obey
International regulations carry out within the limits prescribed, do from remote controlled model plane aircraft of the work in 5.8GHz frequency range, step by step deep
Enter.
The utility model has the advantages that being restricted for a long time by temperature rise heat compared with prior art, the present invention solving, aeroplane motor
It is unable to jet, cannot be made a silk purse out of a sow's ear to small size, high revolving speed, light-weight, high power development difficulty, proposition will be in motor
Portion's heat is converted to vacuum jet power, significantly saves raw material, realizes small in size, amount heavy and light, at low cost, high-efficient new
Scheme；It is the original breakthrough that jet-propelled motor aircraft replaces internal combustion engine aircraft, is that modern electric jet aircraft is gone through
The ground zero of history.
Detailed description of the invention
A kind of schematic cross-sectional view of the jet-propelled Electric aircraft 1 of attached drawing 1, double wind wheel.
Attached drawing 2, a kind of schematic cross-sectional view of jet-propelled Electric aircraft 2.
Attached drawing 3, a kind of overlooking structure diagram of jet-propelled Electric aircraft 3.
Attached drawing 4, a kind of schematic cross-sectional view of construction of wind tunnel.
The internal-rotor stacking adding type motor schematic cross-sectional view of attached drawing 5, a kind of jet-propelled Electric aircraft.
The electric appliance functional-block diagram of attached drawing 6, jet-propelled Electric aircraft.
Specific embodiment
Following embodiment, which is not constituted, places restrictions on any of the scope of the present invention.
A kind of embodiment: the schematic cross-sectional view of the jet-propelled Electric aircraft 1 of attached drawing 1, double wind wheel.
Preferably, in attached drawing 1: 02. wind-tunnel, 022. wind-tunnel shell, 08. high-speed motor, 09. machine leaf, above machine leaf
If photovoltaic cell, 015. landing gear, 016. lifting leaf, wherein crane includes 4 pressure liftable legs automatically controlled by computer
And wheel；In figure, arrow indicates airflow direction.
A kind of embodiment: the schematic cross-sectional view of the jet-propelled Electric aircraft 2 of attached drawing 2, double wind wheel.
Preferably, in attached drawing 2: 01. main shaft, 02. wind-tunnel, 03. first wind wheel are made of 2 turbine fans, and 04. is unidirectional
Pressure breathing valve, 05. computer, 06. first circle bracket, 07. battery, 08. high-speed motor, 09. machine leaf install light on machine leaf
Lie prostrate battery be used as solar power generation, 010. second justify bracket, 011. butterfly valve door, 012. stepper motor, 014. one-way exhaust valve,
015. landing gear, 016. lifting leaf, 020. air duct, 022. wind-tunnel shell, wherein key power switch is set above battery；It rises
Dropping platform 016 includes 4 pressure liftable legs and wheel automatically controlled by computer or baroceptor, electronic one-way exhaust valve 014
360 ° of degree mean allocations of the area of a circle are pressed for 6, are arranged in the second end cover of motor 08.
Embodiment: attached drawing 3, a kind of schematic top plan view of jet-propelled Electric aircraft 3.
Preferably, in attached drawing 3: 01. main shaft, 02. wind-tunnel, wind-tunnel mouth are equipped with stainless steel mesh enclosure, 09. machine leaf and the sun
Can generate electricity pond, 011 butterfly valve door, 012. stepper motor, 015. landing gear, 016. lifting leaf, 017. first wireless camera, and 018.
Second wireless camera, arrow indicates air-flow jet direction in figure.
Embodiment: attached drawing 4, a kind of schematic cross-sectional view of construction of wind tunnel.
Preferably, in attached drawing: 01. main shaft, 022. shell, shell be equipped with stainless steel mesh enclosure, 03. first wind wheel, 04.
Uniaxial pressure intake valve, 05. computer, 06. first circle bracket, 07. battery, 08. high-speed motor, 010. second circle bracket,
011. butterfly valve door, 012. stepper motor, 013. second wind wheel, 014. one-way exhaust valve, 020. air duct, 021. third bracket, figure
Arrow indicates air-flow jet direction in mark.
A kind of embodiment: the internal-rotor stacking adding type motor schematic cross-sectional view of attached drawing 5, jet-propelled Electric aircraft.
Preferably, in attached drawing: 1. first end covers, 2. rotors, the turntable of rotor, 3. magnetic guiding loops, 04. uniaxial pressure air inlet
Valve, 5. stator winding, 6. stators, 7. bearings, 01. main shaft, 9. reinforcing ribs, 10. permanent magnets, 11. bolts, 12. air gaps, 13. peaces
Full valve, 014. one-way exhaust valve, 14. inner oil seal lids, 15. outer oil seal lids, 16. ripple compensation sets, 17. maintenance screw holes, 18. wind
Leaf, 19. conducting wires, 20. flat keys, 21. sensors, 22. magnet rings, 23. follower bolts, 101. second end covers, 201. superimposed type turntables,
601 superimposed type stators, the superimposed type stator that can be matched with superimposed type turntable 201, to expand motor power (output), Section line in figure
The quantity that increase matched superimposed type turntable and superimposed type stator is indicated with dotted line, expands motor power (output) in which can be convenient, and makes
Make large-scale superimposed type motor, wherein bearing is that magnetic is floating or high-speed bearing, follower bolt 23 are positioned by pressing plate by all turns
Disk is respectively fixed together with main shaft, constitutes internal rotor, and uniaxial pressure intake valve and one-way exhaust valve are respectively 6, setting
Safety valve 13 is to prevent accident.
Embodiment: the electric appliance functional-block diagram of attached drawing 6, jet-propelled Electric aircraft.
Preferably, the circuit process in attached drawing are as follows: 09. solar power generation cell charges to 07. battery, and battery is logical
It crosses conducting wire and is separately connected 05. computer, 08. motor, 012. stepping motor, 016. lifting leaf, 017. first wireless camera,
018. second wireless camera, respective supply terminals, hot stand-by duty wait remote controler 001 to award radio contact and rise
Fly instruction；017. first wireless camera and 018. second wireless camera, measured information is passed in nolo flight
05. computer, computer computer issue instructions to all parts after handling rapidly in time and carry out operation running；Wherein, remote controler
001 with 05. computer wireless electrical communication, transmit information mutually, computer only receives the stopping of the sending of remote controler 001, opens and task mesh
The instruction of mark property, routine matter is unified to be executed by brain, and is equipped with that a key is one close, authorization, is authorized to scrambling coding software and journey
Sequence is conducive to anti-interference and encryption；Spare socket one is set in figure.
Claims (10)
1. a kind of jet-propelled Electric aircraft, comprising: wind-tunnel (02) and wind-tunnel shell (022), in wind-tunnel hull outside fitting machine
Leaf (09), lifting leaf (016), landing gear (015) and remote controler (001) are constituted: being characterized in: using wind-tunnel (02) as jet
Propeller power is equipped with automatic vacuum jet high-speed motor (08) in wind-tunnel, as long as medium reaches setting in vacuum
Boiling point can transmit heat moment and spray radiating airflow outward with supersonic velocity, in conjunction with the dual of the first wind wheel and the second wind wheel
Accelerate, aircraft is further pushed to accelerate to advance, in unmanned middle computer (05) according to the first wireless camera (017) and the
Two wireless cameras (018) or the information of radar antenna transmitting, the mobile butterfly valve door of rapid process instruction stepper motor (012)
(011) angular dimension, is precisely controlled left and right spray air flow, and safe galloping is realized in cooperation lifting leaf (016)；Change, which is given up, is
Treasured is solved and is restricted for a long time by temperature rise heat, motor cannot replace internal combustion engine as jet high-speed propeller it is winged on
The difficulty in blue sky installs several wind-tunnel side by side, as long as jet direction is consistent, enhances power, makes flying speed faster.
2. a kind of jet-propelled Electric aircraft according to claim 1, is characterized in: the motor (08) is to turn in jet-propelled
Sub- high-speed motor, comprising: two turntables (2) or X superimposed type turntable (201) are fixed with flat key and follower bolt (23) respectively
In the convex shelves backer two sides of main shaft (01), magnetic guiding loop (3), permanent magnetism are each provided in turntable (2) or X superimposed type turntable (201)
Body (10), fan blade (18) or reinforcing rib (9)；Main shaft (01) both ends pass through bearing (7) connection first end cover (1) and second end respectively
The outer nose circle for covering (101) two end caps is tightly connected each by bolt (11) and stator (6) or S superimposed type stator (601),
Gap (12), sensor (21) are equipped between stator and plane of rotor disc, by conducting wire after the terminal block and seal stator in terminal box
(19) it draws；The difference is that: winding is made by double-sided printed-circuit board in stator (6) or S superimposed type stator (601)
(5), under high vacuum ultra low temperature state, with non-magnetic metal packing sealed package, with powder metallurgic method, vacuum high-temperature pressure
It makes, be sintered, winding (5) is made to keep high vacuum state and ultralow temperature and high temperature traces of memory forever in stator, it is ultra-thin
The magnet ring (22) being arranged in type stator and permanent magnet (10) cooperation generate the floating effect of magnetic, and control gap (12) is arrived minimum, made
Electric efficiency is up to 95% or more, carries out jet heat dissipation in conjunction with motor automatic vacuum-pumping apparatus, automatic vacuum-pumping apparatus includes: dynamic
It state seal member and several uniaxial pressure intake valves (04) being located on first end cover (1) and is located on second end cover (101)
Several one-way exhaust valves (014) and the fan blade (18) that is located on turntable constitute；Fan blade promotes inside when motor rotates
Heat and air-flow are discharged rapidly from one-way exhaust valve, since the vacuum degree that uniaxial pressure intake valve will arrive setting can just be opened, institute
To cause negative pressure of vacuum operating status, as long as medium has reached the boiling point of setting in vacuum, moment can absorb a large amount of heat, with
The speed of ultrasonic sound transmits heat to distal end, so that the heat eliminating medium recycled in gap (12) is undergone phase transition generation " superconduction " first existing
As, a large amount of heat of transient absorption is radiated with ultrasonic speed from one-way exhaust valve jet, meanwhile, uniaxial pressure intake valve and list
To interaction is generated between exhaust valve, frequency realizes resonance close to synchronous, and since jet heat dissipation flow velocity is fast, inner wall generates refrigeration effect
Answer, contained that the temperature of stator winding (5) and permanent magnet (10) rises, band played in high-intensity magnetic field and vacuum with winding superconduction or
The load-bearing capacity of motor is greatly improved in sub- superconductivity effects, makes the volume and weight of motor than the biography with Same Efficieney
Silicon steel sheet motor of uniting compares 10 times of volume-diminished, converts jet power for damaging heat inside motor, and utilization efficiency is higher,
It especially adapts to use in aircraft, wherein X or S is natural number.
3. a kind of jet-propelled Electric aircraft according to claim 1, is characterized in: the wind-tunnel shell (022) is by titanium aluminium
Barrel shape is made in alloy material, and each one circle boss slot of rolling, solid for the first circle bracket (06) and the second circle bracket (010) up and down
Determine motor (08) to use, wind-tunnel shell (022) front end setting shield, outside left and right settings machine leaf (09), on machine leaf (09)
Photovoltaic power generation battery is set and supplements power supply to battery (07), wind-tunnel shell inner periphery is equipped with air duct (020).
4. a kind of jet-propelled Electric aircraft according to claim 2, is characterized in: the motor main shaft (01) is by Ovshinsky
Body heavy wall stainless steel tube or round steel are made, and the convex shelves being arranged in main shaft choose convex as the backer fixed between two turntables
Shelves thickness is assured that between two turntables that there are the size of gap (12), gaps between permanent magnet (10) and stator plane
(12) distance can be selected in the range of 0.02~4.5mm depending on motor power (output) size, and main shaft is equipped with peace
The sealing shelves for filling dynamic sealing component, the external diameter surface roughness requirements for sealing shelves are≤0.004mm, seal the diameter of axle straight line of shelves
Degree and circularity require 0.002 へ 0.004mm, are adapted to the automatic compensation gap in -50 DEG C~300 DEG C temperature ranges, and dynamic
State seal member constitutes good dynamic sealing together；The setting of main shaft (01) top is greater than the cone of major axis diameter convenient for high speed
Concentricity is kept in rotation.
5. a kind of jet-propelled Electric aircraft according to claim 2, is characterized in: it is described by double-sided printed-circuit board be made around
Group (5), be made according to the plane product and shape of permanent magnet (10) in rotor all stay in end to end it is several on the outside of copper foil windings
A coil, number of coils is identical as the quantity of permanent magnet in rotor (10) to form a circle, the company of series connection between each coil and coil
It connects, is then shaped into a phase monolithic winding with spraying nanometer coatings bonding under high vacuum state, then by tri- groups of lists of a, b, c
Piece winding is sprayed high temperature resistant under high vacuum low-temperature condition and received by 120 ° of phase shift angle stacking positioning by vacuum drying treatment
Rice insulating coating, unified sizing bonding are made three-phase windings (5) or six groups of monolithic windings and positioning are laminated by 60 ° of phase shift angles,
Six phase windings (5) are made in bonding, and magnetic floating ring (22) are arranged in winding periphery.
6. a kind of jet-propelled Electric aircraft according to claim 1, is characterized in: first wind wheel (03) and the second wind wheel
(013) it is high-speed turbine fan or centrifugal vortex wind wheel, is made of no magnetic metal material, in the hope of big wind-force, high revolving speed, low throat
Sound.
7. a kind of jet-propelled Electric aircraft according to claim 1, is characterized in: the butterfly valve door (011), by aluminium alloy
2 semicircle tab (s) are made in material, are movably arranged in the center seat of third pedestal upper end, semicircle tab (s) respectively with installation
Stepping motor (012) in third pedestal lower end screw rod is flexible coupling, computer (05) control stepping motor (012) advance or
Person retreats, to move butterfly valve door (011) left and right angular dimension, the spray air flow of accurate quickly control left and right directions, and cooperation lifting
Leaf (016) realizes various directions and movement that air injection aerial vehicle or so flies up and down.
8. a kind of jet-propelled Electric aircraft according to claim 1, is characterized in: being equipped with power inside the computer (05)
Control, temperature control, structure control, power supply control, posture execute control, orbits controlling, day line traffic control, command receiver, refer to
Encoder is enabled, is shaken and is surveyed encoder, shakes to survey transmitter, infrared ray and shake and survey encoder, infrared ray night flight instrument, wireless transceiver system, one
The due circuit process of serial UAV and equipment power on key and are in hot stand-by duty, wait remote controler
(001) instruction for starting to take off is awarded.
9. a kind of jet-propelled Electric aircraft according to claim 1, is characterized in: the remote controler (001) is a kind of wireless
Emitter is encoded key information by modern digital coding, emits light wave by infrared diode,
The infrared signal received is transformed into electric signal by the infrared receiver of the received machine of light wave, is decoded into processor, demodulation
Corresponding instruction requires out to reach the operation needed for computer (05) equipment is completed；Remote controler (001) or mobile terminal
Or center controlling platform, it is equipped with wireless transmitter circuit, command encoder, authoring program, random generation is accessed after authorizing
Password, a machine one control do not receive other any instructions and control in the hope of secret and safe；The stealth generated using the close moment of a key one
The mode of password encrypts, and piggybacking WiMAX channel or the channel fifi or Beidou satellite navigation channel carry out information transmitting；From work
The remote controlled model plane aircraft made in 5.8GHz frequency range is done.
10. a kind of jet-propelled Electric aircraft according to claim 8, is characterized in: the circuit process are as follows: be arranged in machine
The photovoltaic cell of leaf (09) above charges to battery (07), and battery is separately connected computer (05), motor by conducting wire
(08), stepping motor (012), lifting leaf (016), the first wireless camera (017), the second wireless camera (018), respectively
Supply terminals, hot stand-by duty waits remote controler (001) to award radio contact and take off instruction；In-flight first is wireless
Measured information is passed to computer (05) by camera (017) and the second wireless camera (018), and computer computer is handled rapidly
Issuing instructions to all parts in time carries out operation operating later；Wherein, remote controler (001) and (05) computer wireless Electricity Federation
System, transmits mutually information, and computer (05) only receives the stopping of remote controler (001), opens and task object instruction, and is equipped with one
Key one is close, authorization, is authorized to scrambling coding software and program, is conducive to anti-interference and encryption.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811035797.3A CN109018381A (en) | 2018-08-23 | 2018-08-23 | Jet-propelled Electric aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811035797.3A CN109018381A (en) | 2018-08-23 | 2018-08-23 | Jet-propelled Electric aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109018381A true CN109018381A (en) | 2018-12-18 |
Family
ID=64624307
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811035797.3A Pending CN109018381A (en) | 2018-08-23 | 2018-08-23 | Jet-propelled Electric aircraft |
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| Country | Link |
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| CN (1) | CN109018381A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113091857A (en) * | 2021-04-30 | 2021-07-09 | 中水东北勘测设计研究有限责任公司 | Emergency response equipment for dealing with flood burst |
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| CN103158880A (en) * | 2013-03-04 | 2013-06-19 | 陆建收 | Aerospace motor-driven helicopter |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1289705A (en) * | 2000-11-10 | 2001-04-04 | 贾龙 | Flying method and equipment |
| CN1520632A (en) * | 2001-06-26 | 2004-08-11 | �Ƚ�ת��ϵͳ���Ϲ�˾ | Brushless DC electric motor |
| CN2528706Y (en) * | 2002-01-25 | 2003-01-01 | 王保平 | Manned craft |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN113091857A (en) * | 2021-04-30 | 2021-07-09 | 中水东北勘测设计研究有限责任公司 | Emergency response equipment for dealing with flood burst |
| CN113091857B (en) * | 2021-04-30 | 2024-04-26 | 中水东北勘测设计研究有限责任公司 | Emergent response equipment of reply flood burst |
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Effective date of registration: 20200701 Address after: Xiaoshan District of Hangzhou City, Zhejiang province 311258 Wenyan Hunan No. 1711, building 12, Ai Wei Innovation Park Applicant after: HANGZHOU AIVISI ELECTRONICS CO.,LTD. Address before: Room 77-3-201, Gaoqiao community, Chengxiang street, Xiaoshan District, Hangzhou City, Zhejiang Province Applicant before: Chen Guobao Applicant before: HANGZHOU TIANHANG GUOFA TECHNOLOGY CO.,LTD. |
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Application publication date: 20181218 |
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