CN103662048A - Sliding rail car with more than two times of sliding acceleration function and for directional aircraft - Google Patents
Sliding rail car with more than two times of sliding acceleration function and for directional aircraft Download PDFInfo
- Publication number
- CN103662048A CN103662048A CN201210354236.6A CN201210354236A CN103662048A CN 103662048 A CN103662048 A CN 103662048A CN 201210354236 A CN201210354236 A CN 201210354236A CN 103662048 A CN103662048 A CN 103662048A
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- aircraft
- sliding
- acceleration function
- magnetic patch
- fixed link
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Abstract
The invention provides a sliding rail car with more than two times of sliding acceleration function and for a directional aircraft. The sliding rail car mainly comprises four sliding blocks, a car base plate, an aircraft fixing rod, hoisting holes, an upper layer of magnetic blocks, a lower layer of magnetic blocks and the like; the four sliding blocks are arranged at the bottom of the car base plate and the openings of the four sliding blocks are downward; the aircraft fixing rod is arranged in the middle of the front portion of the base plate; the hoisting holes are formed in the bilateral sides of the aircraft fixing rod arranged on the front portion; the hoisting holes and the upper layer of magnetic blocks protrude the lower layer of magnetic blocks, wherein the bottoms of the upper layer of magnetic blocks are fixed together.
Description
Affiliated technical field
The present invention relates to have twice above direction that slides acceleration function and remove aircraft dragging track car, the multistage scooter that launches that especially a kind of upper drive small aircraft of ejection boosting device slides fast.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 twice above direction that slides acceleration function and remove aircraft dragging track car, keystone configuration comprises that four slide blocks, little car bottom plate, aircraft fixed link, lifting hole and upper and lower two-layer magnetic patch etc. partly form; Four slide blocks are arranged on the bottom of little car bottom plate, and Open Side Down, and aircraft fixed link is arranged on the anteriomedial position of base plate, and lifting hole designs in the both sides of anterior aircraft fixed link, and the upper strata magnetic patch being fixed together with bottom protrudes from lower floor's magnetic patch.
The specific embodiment
Have twice above direction that slides acceleration function and remove aircraft dragging track car, keystone configuration comprises that four slide blocks, little car bottom plate, aircraft fixed link, lifting hole and upper and lower two-layer magnetic patch etc. partly form; Four slide blocks are arranged on the bottom of little car bottom plate, and Open Side Down, and aircraft fixed link is arranged on the anteriomedial position of base plate, and lifting hole designs in the both sides of anterior aircraft fixed link, and the upper strata magnetic patch being fixed together with bottom protrudes from lower floor's magnetic patch.
Claims (1)
1. there is twice above direction that slides acceleration function and remove aircraft dragging track car, it is characterized in that: keystone configuration comprises that four slide blocks, little car bottom plate, aircraft fixed link, lifting hole and upper and lower two-layer magnetic patch etc. partly form; Four slide blocks are arranged on the bottom of little car bottom plate, and Open Side Down, and aircraft fixed link is arranged on the anteriomedial position of base plate, and lifting hole designs in the both sides of anterior aircraft fixed link, and the upper strata magnetic patch being fixed together with bottom protrudes from lower floor's magnetic patch.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210354236.6A CN103662048A (en) | 2012-09-21 | 2012-09-21 | Sliding rail car with more than two times of sliding acceleration function and for directional aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210354236.6A CN103662048A (en) | 2012-09-21 | 2012-09-21 | Sliding rail car with more than two times of sliding acceleration function and for directional aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103662048A true CN103662048A (en) | 2014-03-26 |
Family
ID=50301047
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210354236.6A Pending CN103662048A (en) | 2012-09-21 | 2012-09-21 | Sliding rail car with more than two times of sliding acceleration function and for directional aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103662048A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107804472A (en) * | 2017-10-06 | 2018-03-16 | 廖忠民 | Express locomotive assist system |
-
2012
- 2012-09-21 CN CN201210354236.6A patent/CN103662048A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107804472A (en) * | 2017-10-06 | 2018-03-16 | 廖忠民 | Express locomotive assist system |
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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 |