CN103662026A - Electromagnetism-permanent-magnet mixed type repulsion-attraction combined suspension aircraft catapulting glissade track - Google Patents
Electromagnetism-permanent-magnet mixed type repulsion-attraction combined suspension aircraft catapulting glissade track Download PDFInfo
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- CN103662026A CN103662026A CN201210340991.9A CN201210340991A CN103662026A CN 103662026 A CN103662026 A CN 103662026A CN 201210340991 A CN201210340991 A CN 201210340991A CN 103662026 A CN103662026 A CN 103662026A
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- electromagnet
- track
- permanent magnet
- attraction
- repulsion
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- Control Of Vehicles With Linear Motors And Vehicles That Are Magnetically Levitated (AREA)
Abstract
The invention relates to an electromagnetism-permanent-magnet mixed type repulsion-attraction combined suspension aircraft catapulting glissade track which mainly and structurally comprises an upper track installation frame, a lower track installation frame, an upper opposite-pole attraction fixing electromagnet, a lower same-pole repulsion electromagnet, a suspension motion permanent magnet and the like. The upper opposite-pole attraction fixing electromagnet is installed on the lower end face of the upper track installation frame, and is in opposite-pole attraction with the suspension motion permanent magnet. The lower same-pole repulsion electromagnet is installed on the lower track installation frame and is in same-pole repulsion with the suspension motion permanent magnet.
Description
Affiliated technical field
The present invention relates to the hybrid repulsion phase of electromagnet and permanent magnet and inhale combined suspension aircraft and launch dragging track, especially a kind of permanent magnet repels each other and has the magnetic-levitation structure of suction mutually with two electromagnetic paths are existing.Belong to magnetic levitation technology field.
Background technology
In horizontal magnetic levitation technology field, be divided into several forms of electromagnetic suspension and permanent magnet suspension, the horizontal magnetic suspension in past is mostly two like magnetic poles repel each other magnetic suspension, due to the poor stability of two like magnetic poles repel each other, so the product of producing can not meet the horizontal magnetic suspension requirement of extraordinary circumstances.
Summary of the invention
The hybrid repulsion phase of electromagnet and permanent magnet is inhaled combined suspension aircraft and is launched dragging track, and keystone configuration comprises that the erecting frame that gets on the right track, lower railway erecting frame, upper there is a natural attraction between the sexes fixed electromagnet, lower two like magnetic poles repel each other electromagnet and suspended motion permanent magnet etc. partly form; There is a natural attraction between the sexes, and fixed electromagnet is arranged on the lower surface of track erecting frame, and between motion permanent magnetic iron, realizes that there is a natural attraction between the sexes; Lower two like magnetic poles repel each other electromagnet is arranged on lower railway erecting frame, realizes two like magnetic poles repel each other with suspended motion permanent magnet.
The specific embodiment
The hybrid repulsion phase of electromagnet and permanent magnet is inhaled combined suspension aircraft and is launched dragging track, and keystone configuration comprises that the erecting frame that gets on the right track, lower railway erecting frame, upper there is a natural attraction between the sexes fixed electromagnet, lower two like magnetic poles repel each other electromagnet and suspended motion permanent magnet etc. partly form; There is a natural attraction between the sexes, and fixed electromagnet is arranged on the lower surface of track erecting frame, and between motion permanent magnetic iron, realizes that there is a natural attraction between the sexes; Lower two like magnetic poles repel each other electromagnet is arranged on lower railway erecting frame, realizes two like magnetic poles repel each other with suspended motion permanent magnet.
Claims (1)
1. the hybrid repulsion phase of electromagnet and permanent magnet is inhaled combined suspension aircraft and is launched dragging track, it is characterized in that: keystone configuration comprises that the erecting frame that gets on the right track, lower railway erecting frame, upper there is a natural attraction between the sexes fixed electromagnet, lower two like magnetic poles repel each other electromagnet and suspended motion permanent magnet etc. partly form; There is a natural attraction between the sexes, and fixed electromagnet is arranged on the lower surface of track erecting frame, and between motion permanent magnetic iron, realizes that there is a natural attraction between the sexes; Lower two like magnetic poles repel each other electromagnet is arranged on lower railway erecting frame, realizes two like magnetic poles repel each other with suspended motion permanent magnet.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210340991.9A CN103662026A (en) | 2012-09-16 | 2012-09-16 | Electromagnetism-permanent-magnet mixed type repulsion-attraction combined suspension aircraft catapulting glissade track |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210340991.9A CN103662026A (en) | 2012-09-16 | 2012-09-16 | Electromagnetism-permanent-magnet mixed type repulsion-attraction combined suspension aircraft catapulting glissade track |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103662026A true CN103662026A (en) | 2014-03-26 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210340991.9A Pending CN103662026A (en) | 2012-09-16 | 2012-09-16 | Electromagnetism-permanent-magnet mixed type repulsion-attraction combined suspension aircraft catapulting glissade track |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103662026A (en) |
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2012
- 2012-09-16 CN CN201210340991.9A patent/CN103662026A/en active Pending
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20140326 |