CN101633408A

CN101633408A - Flying disk

Info

Publication number: CN101633408A
Application number: CN200810132270A
Authority: CN
Inventors: 刘新广
Original assignee: Individual
Current assignee: Individual
Priority date: 2008-07-23
Filing date: 2008-07-23
Publication date: 2010-01-27

Abstract

The invention discloses a flying disk, which is provided with two vertical motors. Rotors of the motors are arranged around stators, fan blades are evenly distributed on the periphery of the rotors, permanent magnets are arranged on internal circles of the rotors, the stators are provided with coils, the rotors and the stators are connected by magnetic bearings, and the rotors, the stators and the magnetic bearings form the special motors; the start/stop, rotating speed and turning of the motors are controllable; the upper end of the stator is coaxially fixed with a streamline upper engine room with a disk, a horizontal propelling motor with controllable halt and rotating speed is arranged in the upper engine room along the length direction of the upper engine room, the left and right of the middle part and the tail part of the engine room are provided with compressed gas nozzles, and compressed gas is guided to the nozzles through a control valve from the horizontal propelling motor. The flying disk rises and falls through the vertical motors, the flying disk flies by horizontal propelling motor, and the flying direction of the flying disk is realized by controlling the compressed gas sprayed to the nozzles. The flying disk has high flying speed, and is economic, convenient, safe and environment-friendly to fly.

Description

Flying saucer

Technical field

The present invention relates to a kind of aircraft, particularly a kind of 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 present invention discloses a kind of 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 present invention realizes 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 invention; 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 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, the flying saucer vertical uplift can be hovered to the height of desiring to reach; When flying before wanting, start horizontal propelling motor, flying saucer also can start horizontal propelling motor along continuous straight runs when rising quickens, and when rising to the height of desiring to reach, controls the rotating speed of vertical driving engine, keeps height, and the horizontal velocity flight reaching.

During the flying saucer landing, 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 flying saucer is controlled to air nozzle ejection pressure gas by control.

The effect that the present invention is useful is:

1, vertical driving engine of the present invention 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 flying saucer, flying saucer also can be done " cushioning effect " flight, increases upper pulling force (buoyancy), cuts down the consumption of energy;

6, in the described flying saucer landing process, renewable generating, recuperated energy;

7, the vertical driving engine of the present invention 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 flying saucer air nozzle, can make flying saucer translation to the left or to the right, by the air nozzle ejection pressure gas of control to the afterbody in the cabin of flying saucer, can make the flying saucer pivot stud, so the flying saucer dogled is very flexible, other kind of aircraft is incomparable;

9, owing to above advantage, flying saucer flight economy, convenience, safety, environmental protection.

Description of drawings

Fig. 1 is a structural representation of the present invention;

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 invention; 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

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 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. a 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.