CN107869100A - A kind of electromagnetic runway system - Google Patents
A kind of electromagnetic runway system Download PDFInfo
- Publication number
- CN107869100A CN107869100A CN201711312070.0A CN201711312070A CN107869100A CN 107869100 A CN107869100 A CN 107869100A CN 201711312070 A CN201711312070 A CN 201711312070A CN 107869100 A CN107869100 A CN 107869100A
- Authority
- CN
- China
- Prior art keywords
- electromagnet
- runway
- wing aircraft
- electromagnetic
- inductor
- 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
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 4
- 229910052742 iron Inorganic materials 0.000 claims description 2
- 230000001133 acceleration Effects 0.000 abstract description 4
- 239000000725 suspension Substances 0.000 abstract description 2
- 230000005611 electricity Effects 0.000 description 5
- 239000000463 material Substances 0.000 description 2
- 244000025254 Cannabis sativa Species 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000002689 soil Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- E—FIXED CONSTRUCTIONS
- E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
- E01C—CONSTRUCTION OF, OR SURFACES FOR, ROADS, SPORTS GROUNDS, OR THE LIKE; MACHINES OR AUXILIARY TOOLS FOR CONSTRUCTION OR REPAIR
- E01C9/00—Special pavings; Pavings for special parts of roads or airfields
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/04—Ground or aircraft-carrier-deck installations for launching aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
A kind of electromagnetic runway system, belongs to technical field of aerospace, including fixed wing aircraft and electromagnetic runway, and fixed-wing includes head, fuselage, wing, empennage, the first electromagnet, control system and battery；Electromagnetic runway includes inductor, the second electromagnet, controller and battery.Operation principle is：After controller controls the second electromagnet to be powered, the magnetic pole of electromagnet has been confirmed, inductor starts to sense the magnetic pole of the first electromagnet；Control system controls the magnetic pole of the first electromagnet identical with the pole orientation of the second electromagnet, fixed wing aircraft just can suspend, the fixed wing aircraft to get up suspend almost without the resistance on ground, so resistance very little when starting, the acceleration time of the takeoff speed reached is shorter, the runway needed is shorter, realizes the short field take-off of fixed wing aircraft.The resistance when present invention takes full advantage of the magnetic suspension of the device is small, can shorten the distance of taking off of fixed wing aircraft, saves the fixed-wing departure time, improves the utilization rate of the energy.
Description
Technical field
A kind of electromagnetic runway system, belong to technical field of aerospace, more particularly to a kind of electromagnetic runway system.
Background technology
Traditional runway can be pitch or concrete using material, or grass, soil or the rubble flattened
Face or the water surface, but the runway of these material construction is all only used for the place of takeoff and landing, can not be aircraft
Take off provide power.
The content of the invention
The purpose of the present invention is to provide power on runway for aircraft, invents a kind of electromagnetic runway system.
A kind of electromagnetic runway system, including fixed wing aircraft and electromagnetic runway, described fixed-wing include head, fuselage,
Wing, empennage, the first electromagnet, control system and battery, wing and the fuselage lower section is provided with the first electromagnet, described
Control system is located at fuselage interior, for controlling the power on/off and magnetic direction of the first electromagnet；Described battery is control
System and the power supply of the first electromagnet；Described electromagnetic runway includes inductor, the second electromagnet, controller and battery；Described
Inductor is used for the changes of magnetic field for sensing the first electromagnet, and feeds back to controller, in electromagnetic runway；Described controller
For controlling the power on/off and magnetic direction of the second electromagnet, and the letter that inductor provides can be received, positioned at electromagnetic runway
It is internal；Described electromagnetism is inductor, the second electromagnet and controller power supply.
Preferably, the first described electromagnet can also use permanent magnet.
Preferably, described fixed wing aircraft also carries undercarriage and GPS.
A kind of described electromagnetic runway system, operation principle are：When fixed wing aircraft needs to take off, the electricity of electromagnetic runway
Magnetic starts to power for the second electromagnet, controller, inductor, after controller controls the second electromagnet to be powered, has confirmed electromagnet
Magnetic pole, inductor start sense the first electromagnet magnetic pole；Meanwhile the battery of fixed wing aircraft also for the first electromagnet and
Control system is powered, and control system controls the magnetic pole of the first electromagnet identical with the pole orientation of the second electromagnet, at this time solid
Determining wing aircraft can just suspend, because the fixed wing aircraft to suspend is almost without the resistance on ground, so when starting
Resistance very little, accelerate it is faster, the acceleration time of the takeoff speed reached it is shorter, it is necessary to runway it is shorter, realize that fixed-wing flies
The short field take-off of machine.
The resistance when present invention takes full advantage of the magnetic suspension of the device is small, can shorten fixed wing aircraft take off away from
From saving the fixed-wing departure time, improve the utilization rate of the energy.
Brief description of the drawings
Fig. 1 is a kind of axle side schematic diagram of electromagnetic runway system.
In figure, 1- fixed wing aircrafts, 2- electromagnetic runways, 11- heads, 12- fuselages, 13- wings, 14- empennages, 15- first
Electromagnet, 16- control systems, 21- inductors, the electromagnet of 22- second, 23- controllers.
Embodiment
The present invention is illustrated in conjunction with accompanying drawing：A kind of electromagnetic runway system, including fixed wing aircraft 1 and electromagnetism
Runway 2, described fixed-wing include head 11, fuselage 12, wing 13, empennage 14, the first electromagnet 15, control system 16 and electricity
Pond, the lower section of wing 13 and fuselage 12 are provided with the first electromagnet 15, and described control system 16 is located inside fuselage 12, uses
In the power on/off and magnetic direction that control the first electromagnet 15；Described battery is that the electromagnet 15 of control system 16 and first supplies
Electricity；Described electromagnetic runway 2 includes inductor 21, the second electromagnet 22, controller 23 and battery；Described inductor 21 is used for
Sense the changes of magnetic field of the first electromagnet 15, and feed back to controller 23, in electromagnetic runway 2；Described controller 23 is used
In the power on/off and magnetic direction of the second electromagnet 22 of control, and the letter that inductor 21 provides can be received, be run positioned at electromagnetism
Inside road 2；Described electromagnetism is that inductor 21, the second electromagnet 22 and controller 23 are powered.
Described fixed wing aircraft 1 also carries undercarriage and GPS.
A kind of described electromagnetic runway system, operation principle are：When fixed wing aircraft 1 needs to take off, electromagnetic runway 2
Electromagnetism starts to power for the second electromagnet 22, controller 23, inductor 21, after controller 23 controls the second electromagnet 22 to be powered,
The magnetic pole of electromagnet is confirmed, inductor 21 starts to sense the magnetic pole of the first electromagnet 15；Meanwhile the electricity electricity of fixed wing aircraft 1
Pond also powers for the first electromagnet 15 and control system 16, and control system 16 controls the magnetic pole and the second electromagnetism of the first electromagnet 15
The pole orientation of iron 22 is identical, and at this time fixed wing aircraft 1 just can suspend, due to the fixed wing aircraft more than 1 to suspend
Without the resistance on ground, so resistance very little when starting, acceleration is faster, and the acceleration time of the takeoff speed reached gets over
It is short, it is necessary to runway it is shorter, realize the short field take-off of fixed wing aircraft 1.
Claims (3)
- A kind of 1. electromagnetic runway system, it is characterised in that：Including fixed wing aircraft（1）And electromagnetic runway（2）, described fixed-wing Including head（11）, fuselage（12）, wing（13）, empennage（14）, the first electromagnet（15）, control system（16）And battery, institute State wing（13）And fuselage（12）Lower section is provided with the first electromagnet（15）, described control system（16）Positioned at fuselage interior, For controlling the first electromagnet（15）Power on/off and magnetic direction；Described battery is control system（16）With the first electromagnetism Iron（15）Power supply；Described electromagnetic runway（2）Including inductor（21）, the second electromagnet（22）, controller（23）And battery；Institute The inductor stated（21）For sensing the first electromagnet（15）Changes of magnetic field, and feed back to controller（23）, run positioned at electromagnetism Road（2）It is interior；Described controller（23）For controlling the second electromagnet（22）Power on/off and magnetic direction, and can receive Inductor（21）The letter provided, positioned at electromagnetic runway（2）It is internal；Described electromagnetism is inductor（21）, the second electromagnet（22） And controller（23）Power supply.
- A kind of 2. electromagnetic runway system according to claim 1, it is characterised in that：The first described electromagnet（15）May be used also With using permanent magnet.
- A kind of 3. electromagnetic runway system according to claim 1 or 2, it is characterised in that：Described fixed wing aircraft（1）Also With undercarriage and GPS.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711312070.0A CN107869100A (en) | 2017-12-12 | 2017-12-12 | A kind of electromagnetic runway system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711312070.0A CN107869100A (en) | 2017-12-12 | 2017-12-12 | A kind of electromagnetic runway system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107869100A true CN107869100A (en) | 2018-04-03 |
Family
ID=61755477
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711312070.0A Pending CN107869100A (en) | 2017-12-12 | 2017-12-12 | A kind of electromagnetic runway system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107869100A (en) |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ES8707459A1 (en) * | 1985-07-02 | 1987-08-01 | Leduc Rene | TRAINING AND LEARNING DEVICE TO PILOT A CAPTIVE AIRCRAFT |
| CN101671988A (en) * | 2008-09-11 | 2010-03-17 | 上海市建青实验学校 | electromagnetic runway |
| CN202193207U (en) * | 2011-06-22 | 2012-04-18 | 曾彬 | Magnetic levitation airplane lifting runway |
-
2017
- 2017-12-12 CN CN201711312070.0A patent/CN107869100A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ES8707459A1 (en) * | 1985-07-02 | 1987-08-01 | Leduc Rene | TRAINING AND LEARNING DEVICE TO PILOT A CAPTIVE AIRCRAFT |
| CN101671988A (en) * | 2008-09-11 | 2010-03-17 | 上海市建青实验学校 | electromagnetic runway |
| CN202193207U (en) * | 2011-06-22 | 2012-04-18 | 曾彬 | Magnetic levitation airplane lifting runway |
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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: 20180403 |
|
| RJ01 | Rejection of invention patent application after publication |