CN103662034A - Protruding side face interference wave attracted levitation type aircraft catapult sliding rail - Google Patents
Protruding side face interference wave attracted levitation type aircraft catapult sliding rail Download PDFInfo
- Publication number
- CN103662034A CN103662034A CN201210340999.5A CN201210340999A CN103662034A CN 103662034 A CN103662034 A CN 103662034A CN 201210340999 A CN201210340999 A CN 201210340999A CN 103662034 A CN103662034 A CN 103662034A
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- China
- Prior art keywords
- attraction
- attracted
- permanent magnet
- electromagnet
- levitation
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Abstract
The invention discloses a protruding side face interference wave attracted levitation type aircraft catapult sliding rail. The protruding side face interference wave attracted levitation type aircraft catapult sliding rail mainly and structurally comprises a rail installing frame, an attraction traction electromagnet, an attraction levitation movable permanent magnet assembly and the like, wherein an opposite-pole attraction fixed electromagnet is installed on the lower end face of the rail installing frame, the attraction levitation movable permanent magnet assembly is installed at the bottom of the opposite-pole attraction fixed electromagnet, the attraction levitation movable permanent magnet assembly comprises two magnetic blocks, the like poles of the two magnetic blocks are opposite, a magnetizer is further arranged between the two opposite magnetic blocks, a magnetic field of the end face can be led out, and the levitation side face exactly faces the end face of the opposite-pole attraction fixed electromagnet.
Description
Affiliated technical field
The present invention relates to outstanding scattered noise and be attracted floated aircraft and launch dragging track, especially a kind of have magnetizer to draw between magnetic fidle of end combination magnetic field, permanent magnet side and electromagnet the magnetic-levitation structure of extruding mutually.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
Outstanding scattered noise is attracted floated aircraft and launches dragging track, and keystone configuration comprises track erecting frame, attracts tractive electromagnet and the combination of attraction suspended motion permanent magnet etc. partly to form; There is a natural attraction between the sexes, and fixed electromagnet is arranged on the lower surface of track erecting frame; Attract the combination of suspended motion permanent magnet be arranged on electromagnet below; Suspended motion permanent magnet combination is comprised of two relative magnetic patch of homopolarity, and also magnetizer between two relative magnetic patch, can guide out the magnetic field of end face; Suspension side is over against the end face of electromagnet.
The specific embodiment
Outstanding scattered noise is attracted floated aircraft and launches dragging track, and keystone configuration comprises track erecting frame, attracts tractive electromagnet and the combination of attraction suspended motion permanent magnet etc. partly to form; There is a natural attraction between the sexes, and fixed electromagnet is arranged on the lower surface of track erecting frame; Attract the combination of suspended motion permanent magnet be arranged on electromagnet below; Suspended motion permanent magnet combination is comprised of two relative magnetic patch of homopolarity, and also magnetizer between two relative magnetic patch, can guide out the magnetic field of end face; Suspension side is over against the end face of electromagnet.
Claims (1)
1. outstanding scattered noise is attracted floated aircraft and launches dragging track, it is characterized in that: outstanding scattered noise is attracted floated aircraft and launches dragging track, keystone configuration comprises track erecting frame, attracts tractive electromagnet and the combination of attraction suspended motion permanent magnet etc. partly to form; There is a natural attraction between the sexes, and fixed electromagnet is arranged on the lower surface of track erecting frame; Attract the combination of suspended motion permanent magnet be arranged on electromagnet below; Suspended motion permanent magnet combination is comprised of two relative magnetic patch of homopolarity, and also magnetizer between two relative magnetic patch, can guide out the magnetic field of end face; Suspension side is over against the end face of electromagnet.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210340999.5A CN103662034A (en) | 2012-09-16 | 2012-09-16 | Protruding side face interference wave attracted levitation type aircraft catapult sliding rail |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210340999.5A CN103662034A (en) | 2012-09-16 | 2012-09-16 | Protruding side face interference wave attracted levitation type aircraft catapult sliding rail |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103662034A true CN103662034A (en) | 2014-03-26 |
Family
ID=50301033
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210340999.5A Pending CN103662034A (en) | 2012-09-16 | 2012-09-16 | Protruding side face interference wave attracted levitation type aircraft catapult sliding rail |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103662034A (en) |
-
2012
- 2012-09-16 CN CN201210340999.5A patent/CN103662034A/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 |