CN104554763A - Magnetic suspension boosting structure with included angle formed between sliding track and sliding trolley - Google Patents
Magnetic suspension boosting structure with included angle formed between sliding track and sliding trolley Download PDFInfo
- Publication number
- CN104554763A CN104554763A CN201310494474.1A CN201310494474A CN104554763A CN 104554763 A CN104554763 A CN 104554763A CN 201310494474 A CN201310494474 A CN 201310494474A CN 104554763 A CN104554763 A CN 104554763A
- Authority
- CN
- China
- Prior art keywords
- sliding
- trolley
- magnetic suspension
- included angle
- boosting structure
- 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
- Toys (AREA)
Abstract
The invention provides a magnetic suspension boosting structure with an included angle formed between a sliding track and a sliding trolley. The magnetic suspension boosting structure mainly comprises a supporting frame, the sliding track, the sliding trolley, an aircraft support and the like, wherein the sliding track is arranged on the supporting frame; the sliding trolley is arranged on the track; the aircraft support is arranged on the sliding trolley; and an included angle is formed between the aircraft support and the sliding trolley and is smaller than 5 degrees.
Description
Art
The present invention relates to the magnetic suspension boosting structure having angle between dragging track and slide trolley, between especially a kind of unmanned slide truck system and aircraft support frame, have the ejector of angle.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
Have the magnetic suspension boosting structure of angle between dragging track and slide trolley, keystone configuration comprises the part compositions such as bracing frame, dragging track, slide trolley and aircraft parking stand; Dragging track is arranged on bracing frame, and slide trolley is installed in orbit, and aircraft parking stand is arranged on slide trolley, has angle between aircraft parking stand and slide trolley, and the angle number of degrees are less than 5 °.
Detailed description of the invention
Have the magnetic suspension boosting structure of angle between dragging track and slide trolley, keystone configuration comprises the part compositions such as bracing frame, dragging track, slide trolley and aircraft parking stand; Dragging track is arranged on bracing frame, and slide trolley is installed in orbit, and aircraft parking stand is arranged on slide trolley, has angle between aircraft parking stand and slide trolley, and the angle number of degrees are less than 5 °.
Claims (1)
1. there is the magnetic suspension boosting structure of angle between dragging track and slide trolley, it is characterized in that: keystone configuration comprises the part compositions such as bracing frame, dragging track, slide trolley and aircraft parking stand; Dragging track is arranged on bracing frame, and slide trolley is installed in orbit, and aircraft parking stand is arranged on slide trolley, has angle between aircraft parking stand and slide trolley, and the angle number of degrees are less than 5 °.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201310494474.1A CN104554763A (en) | 2013-10-21 | 2013-10-21 | Magnetic suspension boosting structure with included angle formed between sliding track and sliding trolley |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201310494474.1A CN104554763A (en) | 2013-10-21 | 2013-10-21 | Magnetic suspension boosting structure with included angle formed between sliding track and sliding trolley |
Publications (1)
Publication Number | Publication Date |
---|---|
CN104554763A true CN104554763A (en) | 2015-04-29 |
Family
ID=53072030
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201310494474.1A Pending CN104554763A (en) | 2013-10-21 | 2013-10-21 | Magnetic suspension boosting structure with included angle formed between sliding track and sliding trolley |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN104554763A (en) |
-
2013
- 2013-10-21 CN CN201310494474.1A patent/CN104554763A/en active Pending
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN104554763A (en) | Magnetic suspension boosting structure with included angle formed between sliding track and sliding trolley | |
CN103661987A (en) | Magnetic force catapulting booster with included angle formed between aircraft and sliding bogie | |
CN104554788A (en) | Unmanned aerial vehicle carrying sliding trolley capable of running on two layers of tracks | |
CN103661986A (en) | Magnetic flight booster with elevation angle between movement body and sliding track | |
CN104554767A (en) | Magnetic levitation booster with included angles between tracks and takeoff paths of fixed-wing aircrafts | |
CN104554752A (en) | Loosening device of UAV (unmanned aerial vehicle) boost system | |
CN103662064A (en) | Aircraft booster used for disengaging aircraft through tail end lifting structure | |
CN104554800A (en) | Double-layer track catapult boosting device of fixed-wing aircraft catapult | |
CN104554778A (en) | Slide cart braking device at tail end of ejection booster | |
CN103661993A (en) | Magnetic flight booster with automatic sliding rail lubrication structure | |
CN104554796A (en) | Ejection booster with single double-shaft track for unmanned aerial vehicle | |
CN103661985A (en) | Booster disengagement device with elevation angle formed between aircraft and sliding rail | |
CN104554791A (en) | Tail end vertical ejector rod structure of magnetic suspension fixed wing aircraft booster | |
CN103661992A (en) | Tail end brake device of sliding bogie of aircraft booster | |
CN103662017A (en) | Sliding trolley suitable for double-layer and double-track structure | |
CN104554759A (en) | More-than-twice boosting type double-rail unmanned aerial vehicle catapult boosting system | |
CN103660963A (en) | Like-pole repelling brake device specially used at tail end of roll booster sliding trolley | |
CN103662008A (en) | Ejection boosting device with double rails on same horizontal plane | |
CN103662081A (en) | Sliding track active cleaner special for aircraft dropping device | |
CN104555302A (en) | Spring braking device on magnetic levitation automobile production line sliding rail | |
CN104554762A (en) | Permanent magnetic brake device for high-speed catapulting of slide trolley of catapult of UAV (unmanned aerial vehicle) | |
CN103662012A (en) | Unmanned aerial vehicle ejection boosting system with double layers of tracks | |
CN103661983A (en) | Catapult scooter with fixing lock | |
CN104554777A (en) | Electromagnetic glide-cart brake device arranged at the tail end of fixed-wing aircraft catapult | |
CN103662052A (en) | Multistage double-track ejection boosting device on same horizontal level |
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 |