CN108116425A - Ground magnetic suspension annulus aircraft - Google Patents
Ground magnetic suspension annulus aircraft Download PDFInfo
- Publication number
- CN108116425A CN108116425A CN201711247005.4A CN201711247005A CN108116425A CN 108116425 A CN108116425 A CN 108116425A CN 201711247005 A CN201711247005 A CN 201711247005A CN 108116425 A CN108116425 A CN 108116425A
- Authority
- CN
- China
- Prior art keywords
- aircraft
- magnetic
- orbit slot
- propeller
- magnetic suspension
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B61—RAILWAYS
- B61B—RAILWAY SYSTEMS; EQUIPMENT THEREFOR NOT OTHERWISE PROVIDED FOR
- B61B13/00—Other railway systems
- B61B13/08—Sliding or levitation systems
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L13/00—Electric propulsion for monorail vehicles, suspension vehicles or rack railways; Magnetic suspension or levitation for vehicles
- B60L13/04—Magnetic suspension or levitation for vehicles
- B60L13/06—Means to sense or control vehicle position or attitude with respect to railway
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Power Engineering (AREA)
- Magnetic Bearings And Hydrostatic Bearings (AREA)
Abstract
Proposed by the present invention is ground magnetic suspension annulus aircraft.Aircraft is placed on magnetic orbit slot, and propeller is housed in aircraft aft；Magnetic orbit slot is semicircular arc, lower part above is provided with magnetic railway body, electric slide is respectively fixed with along both sides on magnetic orbit slot, electric slide is connected by idler wheel and electric conductor with aircraft, and the aircraft lower part opposite with magnetic railway body is equipped with aircraft magnetic substance.The present invention can embody the effect of flight on land, have recreational.Suitable for being used as land magnetic suspension annulus aircraft.
Description
Technical field
Proposed by the present invention is the aircraft of transport field, specifically ground magnetic suspension annulus aircraft.
Background technology
Aircraft usually middle flight on high, and the vehicle of resistance operation is overcome using magnetic suspension, it is impossible to reach flight speed
Degree, and the track used can only back and forth run for rectilinear orbit.
For the aircraft that amusement uses, existing aircraft cannot be used directly.
The content of the invention
In order to realize that aircraft is run on ring ring, the present invention provides ground magnetic suspension annulus aircraft.This flies
Row device solves aircraft magnetic suspension and run on ring ring the technical issues of by being run on annulus magnetic orbit.
Scheme is used by the present invention solves technical problem：
Aircraft is placed on magnetic orbit slot, and propeller is housed in aircraft aft；
Magnetic orbit slot is semicircular arc, and lower part above is provided with magnetic railway body, along both sides point on magnetic orbit slot
Electric slide is not fixed with, and electric slide is connected by idler wheel and electric conductor with aircraft, the aircraft opposite with magnetic railway body
Lower part is equipped with aircraft magnetic substance.
Good effect, the present invention can embody the effect of flight on land, have recreational.Suitable for as land magnetcisuspension
Floating annulus aircraft uses.
Description of the drawings
Fig. 1 is schematic structural view of the invention.
Fig. 2 sets state diagram for magnetic orbit of the present invention and aircraft.
In figure, 0. magnetic orbit slot, 1. electric slides, 1.1. magnetic railway bodies, 1.2. electric conductors, 2. aircraft, 2.1. flies
Row device magnetic substance, 3. propellers.
Specific embodiment
According to the figure, aircraft 2 is placed on magnetic orbit slot 0, and propeller 3 is housed in aircraft aft；
Magnetic orbit slot is semicircular arc, lower part above is provided with magnetic railway body 1.1, along both sides on magnetic orbit slot
Electric slide 1 is respectively fixed with, electric slide is connected by idler wheel and electric conductor 1.2 with aircraft, opposite with magnetic railway body
Aircraft lower part is equipped with aircraft magnetic substance 2.1.
The propeller is screw propeller.
The magnetic railway body and aircraft magnetic substance are permanent magnet.
The operation of the present invention：
There is a track magnetic substance magnetic orbit slot semicircular arc groove is built-in, and the lower part circular arc protruding portion of aircraft is equipped with flight
Device magnetic substance, the magnetic railway body is identical with aircraft magnetic substance magnetic pole, generates phase holding force between the two, aircraft is suspended
Get up, meanwhile, electric conductor is respectively equipped in the both sides of aircraft with idler wheel and the electric slide with being located at magnetic orbit slot both sides connects
Touch connection.
After electric conductor is powered, the propeller rotation of aircraft under the action of screw propeller rotary force, makes flight
Device travels forward, while the electrical appliance normal use in aircraft.
Due to being respectively provided with magnetic substance between aircraft and magnetic orbit slot, make to hang between aircraft and magnetic orbit slot
It is floating, therefore without using wheel, and frictional force very little, partial frictional resistance is overcome, aircraft is in floating state.
Since magnetic orbit slot is annulus state setting, so aircraft can only again and again be transported on ring ring
Row, escapes the limitation of not errant, so safer.Certainly also can back and forth be run on rectilinear orbit.
The present invention uses suitable for embodying the aircraft of flight for people as large-scale public place of entertainment, can realize safety, quickly
It flies on ground.
When stopping aircraft operation, by turning off the power supply of propeller, propeller stalling is realized.
Such as airflight effect when the present invention takes.
Claims (3)
1. ground magnetic suspension annulus aircraft, aircraft（2）It is placed in magnetic orbit slot（0）On,
It is characterized in that：
Propeller is housed in aircraft aft（3）；
Magnetic orbit slot is semicircular arc, and lower part above is provided with magnetic railway body（1.1）, along two on magnetic orbit slot
Side is respectively fixed with electric slide（1）, electric slide passes through idler wheel and electric conductor（1.2）It is connected with aircraft, with magnetic railway body
Opposite aircraft lower part is equipped with aircraft magnetic substance（2.1）.
2. magnetic suspension annulus aircraft in ground according to claim 1, it is characterised in that：The propeller pushes away for propeller
Into device.
3. magnetic suspension annulus aircraft in ground according to claim 1, it is characterised in that：The magnetic railway body and flight
Device magnetic substance is permanent magnet.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711247005.4A CN108116425A (en) | 2017-12-01 | 2017-12-01 | Ground magnetic suspension annulus aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711247005.4A CN108116425A (en) | 2017-12-01 | 2017-12-01 | Ground magnetic suspension annulus aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108116425A true CN108116425A (en) | 2018-06-05 |
Family
ID=62228875
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711247005.4A Pending CN108116425A (en) | 2017-12-01 | 2017-12-01 | Ground magnetic suspension annulus aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108116425A (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2371033A (en) * | 2001-01-10 | 2002-07-17 | Norman George Hannaford | Magnetic levitation transport system |
| CN101274631A (en) * | 2008-04-10 | 2008-10-01 | 内蒙古麦格磁投资管理有限公司 | Transportation pipeline unit for electromagnetic pipeline transportation system |
| US20100192799A1 (en) * | 2009-02-02 | 2010-08-05 | Miller Arnold R | Supersonic Hydrogen Tube Vehicle |
| CN102910087A (en) * | 2012-10-22 | 2013-02-06 | 北京工业大学 | Propeller-driven permanent magnetic levitation vehicle |
-
2017
- 2017-12-01 CN CN201711247005.4A patent/CN108116425A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2371033A (en) * | 2001-01-10 | 2002-07-17 | Norman George Hannaford | Magnetic levitation transport system |
| CN101274631A (en) * | 2008-04-10 | 2008-10-01 | 内蒙古麦格磁投资管理有限公司 | Transportation pipeline unit for electromagnetic pipeline transportation system |
| US20100192799A1 (en) * | 2009-02-02 | 2010-08-05 | Miller Arnold R | Supersonic Hydrogen Tube Vehicle |
| CN102910087A (en) * | 2012-10-22 | 2013-02-06 | 北京工业大学 | Propeller-driven permanent magnetic levitation vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180605 |
|
| RJ01 | Rejection of invention patent application after publication |