CN103662046A - Secondary accelerating high-speed jointing device for aircraft projection accelerator - Google Patents
Secondary accelerating high-speed jointing device for aircraft projection accelerator Download PDFInfo
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- CN103662046A CN103662046A CN201210354232.8A CN201210354232A CN103662046A CN 103662046 A CN103662046 A CN 103662046A CN 201210354232 A CN201210354232 A CN 201210354232A CN 103662046 A CN103662046 A CN 103662046A
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- magnet ring
- traction magnetic
- magnetic patch
- fixed
- speed
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Abstract
The invention relates to a secondary accelerating high-speed jointing device for an aircraft projection accelerator. The secondary accelerating high-speed jointing device mainly comprises a base plate, a movable traction magnetic block, a fixed traction magnetic block, a fixed magnetic ring sleeve, a magnetic ring sleeve with a spring and the like. The movable traction magnetic block is arranged on the front portion of the base plate, the fixed traction magnetic block is sleeved on the inner side of the fixed magnet ring sleeve, two wing structures are arranged on two sides of the fixed magnetic ring sleeve, and a thrust sliding device with a spring is arranged on the wing structures.
Description
Affiliated technical field
The present invention relates to accelerate high speed connecting device, the permanent magnetism latch-up structure in especially a kind of high speed slide process of small aircraft ejection boosting device for the secondary of aircraft projection accelerator.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
Secondary for aircraft projection accelerator accelerates high speed connecting device, and keystone configuration comprises base plate, mobile traction magnetic patch, fixed traction magnetic patch, fixing magnet ring cover and with the composition partly such as the magnet ring cover of spring; Mobile traction magnetic patch is arranged on the front portion of base plate; Fixed traction magnetic patch is enclosed within fixedly magnet ring cover inner side, and there are two wings the both sides that fixedly magnet ring overlaps, needs the thrust skid of spring in wings.
The specific embodiment
Secondary for aircraft projection accelerator accelerates high speed connecting device, and keystone configuration comprises base plate, mobile traction magnetic patch, fixed traction magnetic patch, fixing magnet ring cover and with the composition partly such as the magnet ring cover of spring; Mobile traction magnetic patch is arranged on the front portion of base plate; Fixed traction magnetic patch is enclosed within fixedly magnet ring cover inner side, and there are two wings the both sides that fixedly magnet ring overlaps, needs the thrust skid of spring in wings.
Claims (1)
1. the secondary for aircraft projection accelerator accelerates high speed connecting device, it is characterized in that: keystone configuration comprises base plate, mobile traction magnetic patch, fixed traction magnetic patch, fixing magnet ring cover and with the composition partly such as the magnet ring cover of spring; Mobile traction magnetic patch is arranged on the front portion of base plate; Fixed traction magnetic patch is enclosed within fixedly magnet ring cover inner side, and there are two wings the both sides that fixedly magnet ring overlaps, needs the thrust skid of spring in wings.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210354232.8A CN103662046A (en) | 2012-09-21 | 2012-09-21 | Secondary accelerating high-speed jointing device for aircraft projection accelerator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210354232.8A CN103662046A (en) | 2012-09-21 | 2012-09-21 | Secondary accelerating high-speed jointing device for aircraft projection accelerator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103662046A true CN103662046A (en) | 2014-03-26 |
Family
ID=50301045
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210354232.8A Pending CN103662046A (en) | 2012-09-21 | 2012-09-21 | Secondary accelerating high-speed jointing device for aircraft projection accelerator |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103662046A (en) |
-
2012
- 2012-09-21 CN CN201210354232.8A patent/CN103662046A/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 |