CN103662016A - Glider catapult booster system with multi-layer tracks and multi-stage catapults - Google Patents
Glider catapult booster system with multi-layer tracks and multi-stage catapults Download PDFInfo
- Publication number
- CN103662016A CN103662016A CN201210340744.9A CN201210340744A CN103662016A CN 103662016 A CN103662016 A CN 103662016A CN 201210340744 A CN201210340744 A CN 201210340744A CN 103662016 A CN103662016 A CN 103662016A
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- Prior art keywords
- magnet ring
- track
- sliding
- glider
- slide
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Abstract
The invention provides a glider catapult booster system with multi-layer tracks and multi-stage catapults. The glider catapult booster system mainly and structurally comprises a support frame, a powered slide track, an aircraft sliding track, a starting magnet ring, a sliding trolley, a sliding magnet ring, a traction magnet ring and a bottom plate. The powered slide track is installed in the middle of the support frame. The aircraft sliding track is installed on the upper portion of the support frame. The sliding trolley is arranged on the aircraft sliding track. The starting magnet ring is sleeved with the sliding magnet ring which slides along the aircraft sliding track. The sliding trolley is pushed by the sliding magnet ring to advance. The traction magnet ring is installed on the bottom plate and located at the tail end of the aircraft sliding track to pull the sliding trolley.
Description
Affiliated technical field
The present invention relates to multilayer track and the multistage glider catapulting assist system launching, part is launched in especially a kind of startup and aircraft taxi dolly is sentenced respectively two-layer track, launches and draw the ejector of also sentencing two-layer track.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
Have multilayer track and the multistage glider catapulting assist system launching, keystone configuration comprises bracing frame, power slide rail, aircraft taxi track, starts magnet ring, slide trolley, slides magnet ring, draws the partly composition such as magnet ring and base plate; Power slide rail is arranged on the middle part of support; Aircraft taxi track is arranged on the top of support; Slide trolley is arranged on aircraft taxi track; Slide magnet ring and be enclosed within the outside that starts magnet ring; Sliding magnet ring slides along track; Slide trolley is slided magnet ring and promotes to advance; Traction magnet ring is arranged on base plate; Be positioned at the end of aircraft taxi track, traction slide dolly.
The specific embodiment
Have multilayer track and the multistage glider catapulting assist system launching, keystone configuration comprises bracing frame, power slide rail, aircraft taxi track, starts magnet ring, slide trolley, slides magnet ring, draws the partly composition such as magnet ring and base plate; Power slide rail is arranged on the middle part of support; Aircraft taxi track is arranged on the top of support; Slide trolley is arranged on aircraft taxi track; Slide magnet ring and be enclosed within the outside that starts magnet ring; Sliding magnet ring slides along track; Slide trolley is slided magnet ring and promotes to advance; Traction magnet ring is arranged on base plate; Be positioned at the end of aircraft taxi track, traction slide dolly.
Claims (1)
1. have multilayer track and the multistage glider catapulting assist system launching, its feature exists: keystone configuration comprises bracing frame, power slide rail, aircraft taxi track, starts magnet ring, slide trolley, slides magnet ring, draws the partly composition such as magnet ring and base plate; Power slide rail is arranged on the middle part of support; Aircraft taxi track is arranged on the top of support; Slide trolley is arranged on aircraft taxi track; Slide magnet ring and be enclosed within the outside that starts magnet ring; Sliding magnet ring slides along track; Slide trolley is slided magnet ring and promotes to advance; Traction magnet ring is arranged on base plate; Be positioned at the end of aircraft taxi track, traction slide dolly.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210340744.9A CN103662016A (en) | 2012-09-15 | 2012-09-15 | Glider catapult booster system with multi-layer tracks and multi-stage catapults |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210340744.9A CN103662016A (en) | 2012-09-15 | 2012-09-15 | Glider catapult booster system with multi-layer tracks and multi-stage catapults |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103662016A true CN103662016A (en) | 2014-03-26 |
Family
ID=50301015
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210340744.9A Pending CN103662016A (en) | 2012-09-15 | 2012-09-15 | Glider catapult booster system with multi-layer tracks and multi-stage catapults |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103662016A (en) |
-
2012
- 2012-09-15 CN CN201210340744.9A patent/CN103662016A/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 |