CN103662037A - Omnilateral magnetic field permanent magnet attraction suspended type aircraft ejection sliding track - Google Patents

Omnilateral magnetic field permanent magnet attraction suspended type aircraft ejection sliding track Download PDF

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Publication number
CN103662037A
CN103662037A CN201210341098.8A CN201210341098A CN103662037A CN 103662037 A CN103662037 A CN 103662037A CN 201210341098 A CN201210341098 A CN 201210341098A CN 103662037 A CN103662037 A CN 103662037A
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CN
China
Prior art keywords
permanent magnet
magnetizes
magnetic field
side direction
magnetic patch
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
Application number
CN201210341098.8A
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Chinese (zh)
Inventor
卓向东
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Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN201210341098.8A priority Critical patent/CN103662037A/en
Publication of CN103662037A publication Critical patent/CN103662037A/en
Pending legal-status Critical Current

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Abstract

The invention discloses an omnilateral magnetic field permanent magnet attraction suspended type aircraft ejection sliding track mainly and structurally comprising a track installation frame, a lateral magnetizing fixed magnetic block, a lateral magnetizing suspended magnetic block and the like. The lateral magnetizing fixed magnetic block is installed on the track installation frame; the lateral magnetizing suspended magnetic block is opposite to the lateral magnetizing fixed magnetic block in magnetizing direction, and is suspended on the track installation frame.

Description

Full side magnetic field permanent magnet is inhaled mutually floated aircraft and is launched dragging track
Affiliated technical field
The present invention relates to full side magnetic field permanent magnet inhales mutually floated aircraft and launches dragging track, the magnetic-levitation structure that magnetic field, especially a kind of two magnetic patch homopolarity sides is pushed mutually.Belong to unmanned aerial vehicle ejector technical 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
Full side magnetic field permanent magnet is inhaled mutually floated aircraft and is launched dragging track, and keystone configuration comprises track erecting frame, side direction magnetic patch and the side direction suspension magnetic patch etc. that magnetizes that magnetizes fixedly; The side direction fixedly magnetic patch that magnetizes is arranged on track erecting frame, and the side direction suspension magnetic patch that magnetizes magnetizes with side direction that fixedly magnetic patch magnetizing direction is contrary, is suspended on track erecting frame.
The specific embodiment
Full side magnetic field permanent magnet is inhaled mutually floated aircraft and is launched dragging track, and keystone configuration comprises track erecting frame, side direction magnetic patch and the side direction suspension magnetic patch etc. that magnetizes that magnetizes fixedly; The side direction fixedly magnetic patch that magnetizes is arranged on track erecting frame, and the side direction suspension magnetic patch that magnetizes magnetizes with side direction that fixedly magnetic patch magnetizing direction is contrary, is suspended on track erecting frame.

Claims (1)

1. full side magnetic field permanent magnet is inhaled mutually floated aircraft and is launched dragging track, it is characterized in that: keystone configuration comprises track erecting frame, side direction magnetic patch and the side direction suspension magnetic patch etc. that magnetizes that magnetizes fixedly; The side direction fixedly magnetic patch that magnetizes is arranged on track erecting frame, and the side direction suspension magnetic patch that magnetizes magnetizes with side direction that fixedly magnetic patch magnetizing direction is contrary, is suspended on track erecting frame.
CN201210341098.8A 2012-09-16 2012-09-16 Omnilateral magnetic field permanent magnet attraction suspended type aircraft ejection sliding track Pending CN103662037A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201210341098.8A CN103662037A (en) 2012-09-16 2012-09-16 Omnilateral magnetic field permanent magnet attraction suspended type aircraft ejection sliding track

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201210341098.8A CN103662037A (en) 2012-09-16 2012-09-16 Omnilateral magnetic field permanent magnet attraction suspended type aircraft ejection sliding track

Publications (1)

Publication Number Publication Date
CN103662037A true CN103662037A (en) 2014-03-26

Family

ID=50301036

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201210341098.8A Pending CN103662037A (en) 2012-09-16 2012-09-16 Omnilateral magnetic field permanent magnet attraction suspended type aircraft ejection sliding track

Country Status (1)

Country Link
CN (1) CN103662037A (en)

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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