CN103662005A - Special horizontal ejection rod structure for pulling magnetic ring to return back for aircraft booster - Google Patents
Special horizontal ejection rod structure for pulling magnetic ring to return back for aircraft booster Download PDFInfo
- Publication number
- CN103662005A CN103662005A CN201210340675.1A CN201210340675A CN103662005A CN 103662005 A CN103662005 A CN 103662005A CN 201210340675 A CN201210340675 A CN 201210340675A CN 103662005 A CN103662005 A CN 103662005A
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- CN
- China
- Prior art keywords
- magnetic ring
- magnet ring
- ejection rod
- rod structure
- end stop
- 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.)
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Abstract
The invention provides a special horizontal ejection rod structure for pulling a magnetic ring to return back for an aircraft booster. The special horizontal ejection rod structure mainly comprises a moving bogie bottom plate, the moving magnetic ring, a slide rail, a magnetic ring outer circle, a motor ejection rod, a tail end baffle and the like. The moving magnetic ring is installed on the front portion of the moving bogie bottom plate and moves along the slide rail, the magnetic ring outer circle is used for fixing the magnetic ring, an unmanned plane supporting rod is installed on the upper portion of the moving bogie bottom plate, a middle hole is formed in the middle of the tail end baffle, and the motor ejection rod is fixed to the rear portion of the tail end baffle and pushes the magnetic ring outer circle so that the magnetic ring can disengage from the tail end baffle.
Description
Affiliated technical field
The present invention relates to the horizontal push rod structure that the special-purpose traction of aircraft booster magnet ring returns, especially a kind of slide trolley end permanent magnetism returns to release.Belong to unmanned aerial vehicle ejector technical field.
Background technology
In more than 50 kilograms SUAV (small unmanned aerial vehicle), launch field, the domestic Electromagnetical ejector that is not applicable to this type of unmanned plane, it is reported and only have the U.S. and Israel to have similar unmanned plane boost installation, the bungee ejector of domestic production can only launch 50 kilograms of following unmanned planes of boosting, the unmanned plane of 50 kilograms of above weight can only rely on solid explosive rocket to carry out boosting, dangerous large, and carry and transport very difficult.
Summary of the invention
The horizontal push rod structure that the special-purpose traction of aircraft booster magnet ring returns, keystone configuration comprises that travelling car base plate, mobile magnet ring, slide rail, magnet ring outer ring, motor push rod and end stop etc. partly form; Mobile magnet ring is arranged on the front portion of travelling car base plate, along slide rail, moves, and magnet ring outer ring is used for fixedly magnet ring; Unmanned plane strut bar is arranged on the top of travelling car base plate; In the middle of end stop, have a mesopore, motor push rod is fixed on end stop rear portion, and pushing tow magnet ring outer ring departs from itself and end stop.
The specific embodiment
The horizontal push rod structure that the special-purpose traction of aircraft booster magnet ring returns, keystone configuration comprises that travelling car base plate, mobile magnet ring, slide rail, magnet ring outer ring, motor push rod and end stop etc. partly form; Mobile magnet ring is arranged on the front portion of travelling car base plate, along slide rail, moves, and magnet ring outer ring is used for fixedly magnet ring; Unmanned plane strut bar is arranged on the top of travelling car base plate; In the middle of end stop, have a mesopore, motor push rod is fixed on end stop rear portion, and pushing tow magnet ring outer ring departs from itself and end stop.
Claims (1)
1. the horizontal push rod structure that the special-purpose traction of aircraft booster magnet ring returns, its feature exists: keystone configuration comprises that travelling car base plate, mobile magnet ring, slide rail, magnet ring outer ring, motor push rod and end stop etc. partly form; Mobile magnet ring is arranged on the front portion of travelling car base plate, along slide rail, moves, and magnet ring outer ring is used for fixedly magnet ring; Unmanned plane strut bar is arranged on the top of travelling car base plate; In the middle of end stop, have a mesopore, motor push rod is fixed on end stop rear portion, and pushing tow magnet ring outer ring departs from itself and end stop.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210340675.1A CN103662005A (en) | 2012-09-15 | 2012-09-15 | Special horizontal ejection rod structure for pulling magnetic ring to return back for aircraft booster |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210340675.1A CN103662005A (en) | 2012-09-15 | 2012-09-15 | Special horizontal ejection rod structure for pulling magnetic ring to return back for aircraft booster |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103662005A true CN103662005A (en) | 2014-03-26 |
Family
ID=50301004
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210340675.1A Pending CN103662005A (en) | 2012-09-15 | 2012-09-15 | Special horizontal ejection rod structure for pulling magnetic ring to return back for aircraft booster |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103662005A (en) |
-
2012
- 2012-09-15 CN CN201210340675.1A patent/CN103662005A/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 |