CN104554817A - High-speed slide cart special for permanent magnet ejection acceleration ejector - Google Patents
High-speed slide cart special for permanent magnet ejection acceleration ejector Download PDFInfo
- Publication number
- CN104554817A CN104554817A CN201310500196.6A CN201310500196A CN104554817A CN 104554817 A CN104554817 A CN 104554817A CN 201310500196 A CN201310500196 A CN 201310500196A CN 104554817 A CN104554817 A CN 104554817A
- Authority
- CN
- China
- Prior art keywords
- aircraft
- magnet ring
- ejector
- speed slide
- base plate
- 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
Links
Landscapes
- Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
Abstract
The invention relates to a high-speed slide cart special for a permanent magnet ejection acceleration ejector. The high-speed slide cart mainly structurally comprises four sliders, a baseplate, an aircraft support, a rear fixed magnet ring, a front ejection magnet ring, a front fixed pin, a pin loosening structure and the like. The sliders are mounted on the lower portion of the baseplate, the aircraft support is mounted on the baseplate, the rear fixed magnet ring and the front ejection magnet ring jointly sleeve the aircraft support, the bottom of an aircraft is mounted in the front of the front ejection magnet ring, and a loose pin is mounted in the front of the bottom of the aircraft so as to fix the aircraft.
Description
Art
The present invention relates to the ejector specialized high-speed slide trolley that permanent magnetism launches acceleration, especially a kind of movable permanent magnet two like magnetic poles repel each other accelerator on unmanned slide car top.Belong to unmanned aerial vehicle ejector technical field.
Background technology
More than 50 kilograms, SUAV (small unmanned aerial vehicle) launches field, the domestic Electromagnetical ejector not being 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 the unmanned plane of boosting less than 50 kilograms, the unmanned plane of more than 50 kilograms weight can only rely on solid explosive rocket to carry out boosting, dangerous large, and carry and transport very difficult.
Summary of the invention
Permanent magnetism launches the ejector specialized high-speed slide trolley of acceleration, and keystone configuration comprises slide block, base plate, aircraft rack, rear fixing magnet ring, frontly launches the part such as magnet ring, front Fixed latches and latch release construction composition; Four slide blocks are arranged on the bottom of base plate, and base plate installs aircraft rack, rear fixing magnet ring and before launch magnet ring and be jointly enclosed within aircraft rack, launch before magnet ring before being arranged on bottom aircraft, the latch that gets loose is arranged on before bottom aircraft, fixes aircraft.
Detailed description of the invention
Permanent magnetism launches the ejector specialized high-speed slide trolley of acceleration, and keystone configuration comprises slide block, base plate, aircraft rack, rear fixing magnet ring, frontly launches the part such as magnet ring, front Fixed latches and latch release construction composition; Four slide blocks are arranged on the bottom of base plate, and base plate installs aircraft rack, rear fixing magnet ring and before launch magnet ring and be jointly enclosed within aircraft rack, launch before magnet ring before being arranged on bottom aircraft, the latch that gets loose is arranged on before bottom aircraft, fixes aircraft.
Claims (1)
1. permanent magnetism launches the ejector specialized high-speed slide trolley of acceleration, it is characterized in that: keystone configuration comprises slide block, base plate, aircraft rack, rear fixing magnet ring, frontly launches the part such as magnet ring, front Fixed latches and latch release construction composition; Four slide blocks are arranged on the bottom of base plate, and base plate installs aircraft rack, rear fixing magnet ring and before launch magnet ring and be jointly enclosed within aircraft rack, launch before magnet ring before being arranged on bottom aircraft, the latch that gets loose is arranged on before bottom aircraft, fixes aircraft.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310500196.6A CN104554817A (en) | 2013-10-23 | 2013-10-23 | High-speed slide cart special for permanent magnet ejection acceleration ejector |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310500196.6A CN104554817A (en) | 2013-10-23 | 2013-10-23 | High-speed slide cart special for permanent magnet ejection acceleration ejector |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104554817A true CN104554817A (en) | 2015-04-29 |
Family
ID=53072084
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310500196.6A Pending CN104554817A (en) | 2013-10-23 | 2013-10-23 | High-speed slide cart special for permanent magnet ejection acceleration ejector |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104554817A (en) |
-
2013
- 2013-10-23 CN CN201310500196.6A patent/CN104554817A/en active Pending
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104554817A (en) | High-speed slide cart special for permanent magnet ejection acceleration ejector | |
| CN103662019A (en) | High-speed taxi-vehicle which is provided with permanent magnetic accelerator and specially used for flight catapult | |
| CN103662069A (en) | Flying object catapult capable of conducting acceleration in high-velocity moving process | |
| CN104554778A (en) | Slide cart braking device at tail end of ejection booster | |
| CN103662046A (en) | Secondary accelerating high-speed jointing device for aircraft projection accelerator | |
| CN104554787A (en) | Gliding trolley for bearing and supporting unmanned plane | |
| CN104554775A (en) | Protection device used for railway logistics and provided with traction structure and disengagement structure simultaneously | |
| CN104554762A (en) | Permanent magnetic brake device for high-speed catapulting of slide trolley of catapult of UAV (unmanned aerial vehicle) | |
| CN104554774A (en) | Parallel-to-track ejection rod structure of pull-back magnet ring special for ejector | |
| CN103661982A (en) | Permanent magnet flight catapult buffer device with like-pole repulsion structure | |
| CN103661981A (en) | Aircraft catapult with permanent magnet midway acceleration function | |
| CN104554791A (en) | Tail end vertical ejector rod structure of magnetic suspension fixed wing aircraft booster | |
| CN103662010A (en) | Two-level launching structure provided with only one sliding track | |
| CN103662070A (en) | Airplane glide boosting frame capable of conducting acceleration multiple times in gliding process | |
| CN104554777A (en) | Electromagnetic glide-cart brake device arranged at the tail end of fixed-wing aircraft catapult | |
| CN103662005A (en) | Special horizontal ejection rod structure for pulling magnetic ring to return back for aircraft booster | |
| CN104554800A (en) | Double-layer track catapult boosting device of fixed-wing aircraft catapult | |
| CN104554780A (en) | Two-stage ejection structure implemented on same layer of track | |
| CN103662007A (en) | Special booster device with dual effects of traction and tail end loosening | |
| CN104554793A (en) | Ejector for realizing double ejection acceleration effects on same track for unmanned aerial vehicle | |
| CN103662013A (en) | Two-level catapult structure with single-layer rails | |
| CN103661978A (en) | Electromagnetic type catapulting buffer device in flight catapult | |
| CN103662071A (en) | Fixing and disengaging structure of high-speed ejector during halfway acceleration | |
| CN103662068A (en) | Spiral parallel insertion ejector rod used for separating opposite-attracting magnetic blocks | |
| CN104554776A (en) | Permanent-magnetic brake structure with like poles repellent at rail end of catapult of UAV (unmanned aerial vehicle) |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20150429 |
|
| WD01 | Invention patent application deemed withdrawn after publication |