CN201254294Y - Novel flying saucer - Google Patents
Novel flying saucer Download PDFInfo
- Publication number
- CN201254294Y CN201254294Y CNU2008201274600U CN200820127460U CN201254294Y CN 201254294 Y CN201254294 Y CN 201254294Y CN U2008201274600 U CNU2008201274600 U CN U2008201274600U CN 200820127460 U CN200820127460 U CN 200820127460U CN 201254294 Y CN201254294 Y CN 201254294Y
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Abstract
Disclosed is a novel flying disk which is provided with two vertical engines. Rotors of the vertical engines surround stators; fan blades are evenly distributed on outer peripheries of the rotors; permanent magnets are arranged in the rotors; the stators are provided with coils; the rotors and the stators are connected with each other by magnetic bearings; the rotors, stators and the magnetic bearings for a special motor. The start, the halt, the rotation speed and the rotation direction of the motor can be controlled; the upper ends of the stators are coaxially fixed with stream-line upper cabins with round disks; horizontal thrusting engines with controllable rotation, halt and rotation speed are arranged in the upper cabins along the length direction of the cabins; the left sides and the right sides of the middle part and the tail part of the cabins are provided with compressed air spray openings; and the compressed air is guided from the horizontal thrusting engines through control valves to the gas spray openings. The vertical engines cause the flying disk to ascend and descend, the horizontal thrusting engines cause the flying disk to fly, and the flying direction of the flying disk is realized by controlling the spray of compressed air towards the air spray openings. The flying speed of the flying disk is high, and the fly is economical, convenient, safe and environment friendly.
Description
Technical field
The utility model relates to a kind of aircraft, particularly a kind of novel flying saucer.
Background technology
Have now and go straight up to the function vertical takeoff and landing and hover, but capacity weight and aircraft overall dimensions ratio are little, it is bigger to take up space, and flying speed (being no more than 370km/h) is low, turn to underaction, and energy consumption is big.
Summary of the invention
The utility model discloses a kind of novel flying saucer, is intended to overcome existing helicopter defective, improves capacity weight and aircraft overall dimensions ratio, and flying speed is higher, turns to more flexibly, and the lifting power consumption is little, fly economy, safety, environmental protection.
The utility model is realized by following technical scheme.
Show as Fig. 1 to Fig. 4.Stator cylinder 18, stator coil and iron core 17, magnetic suspension bearing inner ring 5 and 11 fixed composition stators; The annulus 9 that permanent magnet and magnetizer and non magnetic insulator combine, end plate 7 and 8, cylinder 13, be connected in fan, magnetic suspension shaft bearing outer-ring 6 and 10 that the blade 16 on cylinder 13 cylindricals is formed, these parts constitute rotor, described stator and rotor constitute special machines, vertical driving engine promptly of the present utility model; Vertical driving engine is provided with two along vertical, and vertical driving engine changes and stops and controllable rotation speed; Vertical cylinder 18 coaxial hearts are fixed on the disk 14; Cabin 1 on the stream line pattern of the upper end of vertical cylinder 18 coaxial heart clamping band disk, in last cabin 1 along on the cabin length direction be provided with and change the horizontal propelling motor stop with controllable rotation speed, horizontal propelling motor band turbine 20, engine body 25 usefulness ring supports 24 and horizontal stator 23 are supported in the interior circle of cylindrical casing 3, and the effect of horizontal stator 23 is the air-flow of turbine 20 spinning to be led help axial flow.Connect collector ring 15 at the cylindrical of disk 14 and tooth 22 tops of last cabin 1 lower disc; Some vertical stators (vertically-guided air-flow blade) 27 and 26 are set between two vertical driving engines and below the vertical driving engine of bottom, vertical stator 27 and 26 roots are fixed on vertical cylinder 18 cylindricals, and vertical stator 27 and 26 tops are fixed on circle in the collector ring 15; Dividing plate 21 connects with last cabin 1 inwall; Pressure gas air nozzle (drawing among the figure) is arranged about the middle part in last cabin and afterbody, from horizontal propelling motor impulse contract gas through by-pass valve control to described air nozzle.Driving compartment and crew module are 2, cabin the 4,19, the 12nd, the cabin of airborne equipment, instrument, battery or fuel and goods.
When novel flying saucer takes off or hovers, start vertical driving engine, and make the rotor rotation direction of a vertical driving engine opposite, to eliminate counter torque stator with the rotor rotation direction of a vertical driving engine.Their fan blade rotation, under aerodynamic effect, novel flying saucer vertical uplift can be hovered to the height of desiring to reach; When flying before wanting, start horizontal propelling motor, novel flying saucer also can start horizontal propelling motor along continuous straight runs when rising quickens, when rising to the height of desiring to reach, control the rotating speed of vertical driving engine, keep height, and the horizontal velocity flight reaching.
When novel flying saucer lands, horizontal propelling motor is slowed down, make vertical engine retard again, in this process, the airplane nose down landing, when horizontal velocity is kept to zero, but just vertical landing; Certainly, also can reduce horizontal velocity component gradually near zero the time, vertical landing again.In the landing process, can utilize the up current drive fan to drive described motor regenerative electric power, recuperated energy, this process fan plays the effect of parachute.
Fan blade drives that air forms rotation and along the air-flow of catenary motion, and the effect of stator is that the rotational component that air is driven formation by fan blade is dredged vertical (axially) along vertical driving engine, improves the efficient of vertical driving engine.
The heading of novel flying saucer is controlled to air nozzle ejection pressure gas by control.
The effect that the utility model is useful is:
1, vertical driving engine of the present utility model is the ducted fan driving engine, promptly at the driving engine of a cylinder of fan blade overcoat.Compare with separate propellers, advantage such as the ducted fan aeroperformance is good, size is little and safety is good sees relevant documents and materials for details;
2, capacity weight and aircraft overall dimensions ratio are big, and it is little to take up space, convenient parking;
3, because induced drag and useless resistance are little, thereby flying speed is higher, high efficiency;
4, if control the flying height of novel flying saucer, novel flying saucer also can be done " cushioning effect " flight, increases upper pulling force (buoyancy), cuts down the consumption of energy;
6, in the described novel flying saucer landing process, renewable generating, recuperated energy;
7, the vertical driving engine of the utility model adopts the electromagnetic levitation type motor, and have many good qualities: energy consumption is little, do not produce pernicious gas, vibration is little, noise is little, heating is less, loss is little, efficient is high, weight is little, overhaul maintain easy, the lifting flight control is good;
8, spray pressure gas by control to the left and right sides at the middle part in the cabin of novel flying saucer air nozzle, can make the translation to the left or to the right of novel flying saucer, by the air nozzle ejection pressure gas of control to the afterbody in the cabin of novel flying saucer, can make novel flying saucer pivot stud, so novel flying saucer dogled is very flexible, other kind of aircraft is incomparable;
9, owing to above advantage, novel flying saucer flight economy, convenience, safety, environmental protection.
Description of drawings
Fig. 1 is a structural representation of the present utility model;
Fig. 2 is the birds-eye view of Fig. 1;
Fig. 3 is the left view of Fig. 1;
Fig. 4 is the A-A cutaway view of Fig. 1.
The specific embodiment
Embodiment: show as Fig. 1 to Fig. 4.Stator cylinder 18, stator coil and iron core 17, magnetic suspension bearing inner ring 5 and 11 fixed composition stators; The annulus 9 that permanent magnet and magnetizer and non magnetic insulator combine, end plate 7 and 8, cylinder 13, be connected in fan, magnetic suspension shaft bearing outer-ring 6 and 10 that the blade 16 on cylinder 13 cylindricals is formed, these parts constitute rotor, described stator and rotor constitute special machines, vertical driving engine promptly of the present utility model; Vertical driving engine is provided with two along vertical, and vertical driving engine changes and stops and controllable rotation speed; Vertical cylinder 18 coaxial hearts are fixed on the disk 14; Cabin 1 on the stream line pattern of the upper end of vertical cylinder 18 coaxial heart clamping band disk, in last cabin 1 along on the cabin length direction be provided with and change the horizontal propelling motor stop with controllable rotation speed, horizontal propelling motor band turbine 20, engine body 25 usefulness ring supports 24 and horizontal stator 23 are supported in the interior circle of cylindrical casing 3, and the effect of horizontal stator 23 is the air-flow of turbine 20 spinning to be led help axial flow.Connect collector ring 15 at the cylindrical of disk 14 and tooth 22 tops of last cabin 1 lower disc; Some vertical stators (vertically-guided air-flow blade) 27 and 26 are set between two vertical driving engines and below the vertical driving engine of bottom, vertical stator 27 and 26 roots are fixed on vertical cylinder 18 cylindricals, and vertical stator 27 and 26 tops are fixed on circle in the collector ring 15; Dividing plate 21 connects with last cabin 1 inwall; Pressure gas air nozzle (drawing among the figure) is arranged about the middle part in last cabin and afterbody, from horizontal propelling motor impulse contract gas through by-pass valve control to described air nozzle.Driving compartment and crew module are 2, cabin the 4,19, the 12nd, the cabin of airborne equipment, instrument, battery or fuel and goods.
Described vertical start function to be used as to do rocket or space shuttle or aerospace plane emission initial propulsion device, earlier onto certain speed will be shifted on the missile with described vertical driving engine, refire solid or liquid fuel propelling unit, take off vertical driving engine simultaneously and reclaim it, can reduce launch cost greatly like this.
The driving engine of described novel flying saucer adopts sealing drive technology and correlation technique, just becomes the water air flying disc, can dive under water, and can park on the water and landing, lifting aloft, hovers, flies.
Claims (1)
1. a novel flying saucer is characterized in that: stator cylinder (18), stator coil and iron core (17), magnetic suspension bearing inner ring (5) and (11) fixed composition stator; The annulus (9) that permanent magnet and magnetizer and non magnetic insulator combine, end plate (7) and (8), cylinder (13), be connected in fan that the blade (16) on cylinder (13) cylindrical forms, magnetic suspension shaft bearing outer-ring (6) and (10), these parts constitute rotor, described stator and rotor constitute special machines, vertical driving engine promptly of the present utility model; Vertical driving engine is provided with two along vertical, and vertical driving engine changes and stops and controllable rotation speed; The coaxial heart of vertical cylinder (18) is fixed on the disk (14); On the stream line pattern of the upper end of vertical cylinder (18) coaxial heart clamping band disk cabin (1), in last cabin (1), be provided with and change the horizontal propelling motor stop with controllable rotation speed along last cabin length direction, horizontal propelling motor band turbine (20), engine body (25) is supported in the interior circle of cylindrical casing (3) with ring support (24) and horizontal stator (23), and the effect of horizontal stator (23) is the air-flow of turbine (20) spinning to be led help axial flow; Connect collector ring (15) at the cylindrical of disk (14) and tooth (22) top of last cabin (1) lower disc; Some vertical stators (27) and (26) are set between two vertical driving engines and below the vertical driving engine of bottom, vertical stator (27) and (26) root are fixed on vertical cylinder (18) cylindrical, and vertical stator (27) and (26) top are fixed on circle in the collector ring (15); Dividing plate (21) connects with last cabin (1) inwall; About the middle part in last cabin and afterbody, the pressure gas air nozzle is arranged, from horizontal propelling motor impulse contract gas through by-pass valve control to described air nozzle; Driving compartment and crew module are (2), and cabin (4), (19), (12) are the cabins of airborne equipment, instrument, battery or fuel and goods.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008201274600U CN201254294Y (en) | 2008-07-23 | 2008-07-23 | Novel flying saucer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008201274600U CN201254294Y (en) | 2008-07-23 | 2008-07-23 | Novel flying saucer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201254294Y true CN201254294Y (en) | 2009-06-10 |
Family
ID=40737610
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2008201274600U Expired - Fee Related CN201254294Y (en) | 2008-07-23 | 2008-07-23 | Novel flying saucer |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201254294Y (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101633408A (en) * | 2008-07-23 | 2010-01-27 | 刘新广 | Flying disk |
| WO2011050594A1 (en) * | 2009-10-30 | 2011-05-05 | 北京工业大学 | Magnetic suspension electric rotor flying saucer |
| WO2019204493A1 (en) | 2018-04-17 | 2019-10-24 | The Maglev Aero Co. | Systems and methods for vertical takeoff and landing using magnetic levitation |
| CN112407248A (en) * | 2020-11-23 | 2021-02-26 | 刘国 | Coaxial magnetic suspension rotary wing type ducted propeller fan |
-
2008
- 2008-07-23 CN CNU2008201274600U patent/CN201254294Y/en not_active Expired - Fee Related
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101633408A (en) * | 2008-07-23 | 2010-01-27 | 刘新广 | Flying disk |
| WO2011050594A1 (en) * | 2009-10-30 | 2011-05-05 | 北京工业大学 | Magnetic suspension electric rotor flying saucer |
| US8752787B2 (en) | 2009-10-30 | 2014-06-17 | Beijing University Of Technology | Electrical driven flying saucer based on magnetic suspension |
| WO2019204493A1 (en) | 2018-04-17 | 2019-10-24 | The Maglev Aero Co. | Systems and methods for vertical takeoff and landing using magnetic levitation |
| EP3781790A4 (en) * | 2018-04-17 | 2022-01-19 | The Maglev Aero Co. | Systems and methods for vertical takeoff and landing using magnetic levitation |
| US11292592B2 (en) | 2018-04-17 | 2022-04-05 | Maglev Aero Inc. | Systems and methods for independent pitch control of rotor blades of rotor assembly to achieve directional control |
| US11541997B2 (en) | 2018-04-17 | 2023-01-03 | Maglev Aero Inc. | Systems and methods for improved rotor assembly for use with a stator |
| US11541998B2 (en) | 2018-04-17 | 2023-01-03 | Maglev Aero Inc. | Systems and methods for controlling lift using contra-rotating rotors |
| US11591080B2 (en) | 2018-04-17 | 2023-02-28 | Maglev Aero Inc. | Systems and methods for drive control of a magnetically levitated rotor |
| US11958596B2 (en) | 2018-04-17 | 2024-04-16 | Maglev Aero Inc. | Systems and methods for reducing noise based on effective rotor area relative to a center of rotation |
| CN112407248A (en) * | 2020-11-23 | 2021-02-26 | 刘国 | Coaxial magnetic suspension rotary wing type ducted propeller fan |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20090610 Termination date: 20100723 |