CN103661987A - Magnetic force catapulting booster with included angle formed between aircraft and sliding bogie - Google Patents
Magnetic force catapulting booster with included angle formed between aircraft and sliding bogie Download PDFInfo
- Publication number
- CN103661987A CN103661987A CN201210340592.2A CN201210340592A CN103661987A CN 103661987 A CN103661987 A CN 103661987A CN 201210340592 A CN201210340592 A CN 201210340592A CN 103661987 A CN103661987 A CN 103661987A
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- CN
- China
- Prior art keywords
- aircraft
- booster
- magnetic force
- included angle
- sliding
- 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
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- Control Of Vehicles With Linear Motors And Vehicles That Are Magnetically Levitated (AREA)
Abstract
The invention provides a magnetic force catapulting booster with an included angle formed between an aircraft and a sliding bogie. The booster mainly comprises a supporting frame, a sliding rail, the sliding bogie, an aircraft support and the like. The sliding rail is installed on the supporting frame, the sliding bogie is installed on the rail, the aircraft support is installed on the sliding bogie, and the included angle is formed between the aircraft support and the sliding bogie and is less than 5 degrees.
Description
Affiliated technical field
The present invention relates to has the magnetic force of angle to launch booster between aircraft and slide trolley, has the ejector of angle between especially a kind of unmanned slide truck system and aircraft bracing frame.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
Between aircraft and slide trolley, have the magnetic force of angle to launch booster, keystone configuration comprises that bracing frame, dragging track, slide trolley and aircraft parking stand etc. partly form; Dragging track is arranged on bracing frame, and slide trolley is installed in orbit, and aircraft parking stand is arranged on slide trolley, between aircraft parking stand and slide trolley, has angle, and the angle number of degrees are less than 5 °.
The specific embodiment
Between aircraft and slide trolley, have the magnetic force of angle to launch booster, keystone configuration comprises that bracing frame, dragging track, slide trolley and aircraft parking stand etc. partly form; Dragging track is arranged on bracing frame, and slide trolley is installed in orbit, and aircraft parking stand is arranged on slide trolley, between aircraft parking stand and slide trolley, has angle, and the angle number of degrees are less than 5 °.
Claims (1)
1. between aircraft and slide trolley, there is the magnetic force of angle to launch booster, it is characterized in that: keystone configuration comprises that bracing frame, dragging track, slide trolley and aircraft parking stand etc. partly form; Dragging track is arranged on bracing frame, and slide trolley is installed in orbit, and aircraft parking stand is arranged on slide trolley, between aircraft parking stand and slide trolley, has angle, and the angle number of degrees are less than 5 °.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210340592.2A CN103661987A (en) | 2012-09-15 | 2012-09-15 | Magnetic force catapulting booster with included angle formed between aircraft and sliding bogie |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210340592.2A CN103661987A (en) | 2012-09-15 | 2012-09-15 | Magnetic force catapulting booster with included angle formed between aircraft and sliding bogie |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103661987A true CN103661987A (en) | 2014-03-26 |
Family
ID=50300986
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210340592.2A Pending CN103661987A (en) | 2012-09-15 | 2012-09-15 | Magnetic force catapulting booster with included angle formed between aircraft and sliding bogie |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103661987A (en) |
-
2012
- 2012-09-15 CN CN201210340592.2A patent/CN103661987A/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 |