CN104554759A - More-than-twice boosting type double-rail unmanned aerial vehicle catapult boosting system - Google Patents
More-than-twice boosting type double-rail unmanned aerial vehicle catapult boosting system Download PDFInfo
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- CN104554759A CN104554759A CN201310494449.3A CN201310494449A CN104554759A CN 104554759 A CN104554759 A CN 104554759A CN 201310494449 A CN201310494449 A CN 201310494449A CN 104554759 A CN104554759 A CN 104554759A
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- slide rail
- slide
- boosting
- aerial vehicle
- unmanned aerial
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Abstract
The invention relates to a more-than-twice boosting type double-rail unmanned aerial vehicle catapult boosting system. The system mainly structurally comprises a bottom plate, a slide rail base, slide rails, four sliders, a sliding trolley, a primary catapult structure, a secondary catapult structure and the like. The slide rails are mounted on the slide rail base which is mounted on the bottom plate, and the most upper portion of the slide rail base is provided with circular grooves used for mounting the slide rails; the four sliders are mounted on the slide rails in a linearly sliding manner; a bottom plate of the sliding trolley is mounted on the four sliders; the first catapult structure is mounted at the most front end, and the second catapult structure is mounted at a position 50% length of the slide rails.
Description
Art
The present invention relates to more than twice assisted double track unmanned aerial vehicle ejecting assist system, the especially a kind of multi-stage sliding car of double track in same level of small aircraft ejection boosting device.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
More than twice assisted double track unmanned aerial vehicle ejecting assist system, keystone configuration comprises the part compositions such as base plate, slide rail pedestal, slide rail, slide block, slide trolley, one-level ejection structure, secondary ejection structure; Slide rail pedestal is arranged on base plate, and slide rail is arranged on slide rail impact faces, and the topmost of slide rail pedestal has circular groove, for installing slide rail; Four slide blocks are arranged on slide rail in line sliding mode; Cart base plate is arranged on four slide blocks; Foremost first order ejection structure is installed, at the installation second stage, the position ejection structure of slide rail length 50%.
Detailed description of the invention
More than twice assisted double track unmanned aerial vehicle ejecting assist system, keystone configuration comprises the part compositions such as base plate, slide rail pedestal, slide rail, slide block, slide trolley, one-level ejection structure, secondary ejection structure; Slide rail pedestal is arranged on base plate, and slide rail is arranged on slide rail impact faces, and the topmost of slide rail pedestal has circular groove, for installing slide rail; Four slide blocks are arranged on slide rail in line sliding mode; Cart base plate is arranged on four slide blocks; Foremost first order ejection structure is installed, at the installation second stage, the position ejection structure of slide rail length 50%.
Claims (1)
1. more than twice assisted double track unmanned aerial vehicle ejecting assist system, is characterized in that: keystone configuration comprises the part compositions such as base plate, slide rail pedestal, slide rail, slide block, slide trolley, one-level ejection structure, secondary ejection structure; Slide rail pedestal is arranged on base plate, and slide rail is arranged on slide rail impact faces, and the topmost of slide rail pedestal has circular groove, for installing slide rail; Four slide blocks are arranged on slide rail in line sliding mode; Cart base plate is arranged on four slide blocks; Foremost first order ejection structure is installed, at the installation second stage, the position ejection structure of slide rail length 50%.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310494449.3A CN104554759A (en) | 2013-10-21 | 2013-10-21 | More-than-twice boosting type double-rail unmanned aerial vehicle catapult boosting system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310494449.3A CN104554759A (en) | 2013-10-21 | 2013-10-21 | More-than-twice boosting type double-rail unmanned aerial vehicle catapult boosting system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104554759A true CN104554759A (en) | 2015-04-29 |
Family
ID=53072026
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310494449.3A Pending CN104554759A (en) | 2013-10-21 | 2013-10-21 | More-than-twice boosting type double-rail unmanned aerial vehicle catapult boosting system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104554759A (en) |
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2013
- 2013-10-21 CN CN201310494449.3A patent/CN104554759A/en active Pending
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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 |