CN204323705U - The ultrashort runway of conveyor type - Google Patents
The ultrashort runway of conveyor type Download PDFInfo
- Publication number
- CN204323705U CN204323705U CN201420389011.9U CN201420389011U CN204323705U CN 204323705 U CN204323705 U CN 204323705U CN 201420389011 U CN201420389011 U CN 201420389011U CN 204323705 U CN204323705 U CN 204323705U
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- CN
- China
- Prior art keywords
- runway
- aircraft
- speed
- conveyor type
- ultrashort
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- Expired - Fee Related
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Abstract
The ultrashort runway of a kind of conveyor type.When taking off, conveyor type runway constantly accelerates the speed that the aircraft of balancing out motions backward moves ahead, aircraft constantly accelerates in original place, stop the motion of conveyor type runway when speed reaches takeoff speed, aircraft goes ahead punching under momentum, as long as ceaselessly acceleration just can be taken off successfully.During aircraft landing, runway is to rear, aircraft flight direction high-speed motion, as long as aircraft drops to runway zone, runway is movement proal speed after counteracting aircraft landing backward, allows aircraft slow down gradually and stop.The utility model shortens to be taken off and landing runway length, and manufacturing process and technical requirements are not high, low cost of manufacture, and aviator easily masters a skill main points, and the aircraft carrier Miniaturizable manufactured by this technology, maneuverability, is not easily found.
Description
Technical field
The utility model relates to the runway of a kind of aircraft short field take-off and landing, particularly relates to the ultrashort runway of a kind of conveyor type.
Background technology
Current aircraft flight speed goes is fast, and take off and the runway all needing to grow very much that lands, long runway is easily subject to the destruction of enemy in war, and fighting capacity is reduced greatly.Aircraft carrier with launch to solve with check cable method take off and land in the problem that falls short of of runway, but in device fabrication complex process, in using to pilot psychological's quality and technical requirements high-leveled and difficult to grasp.
Utility model content
For overcome above-mentioned prior art once deficiency, the utility model provides a kind of conveyor type ultrashort runway.
The utility model is realized by following scheme: the ultrashort runway of a kind of conveyor type, the conveyor type runway of cycle rotation comprising roller and driven by roller and support, ultrashort runway when taking off and land under computer to the direction motion that aircraft moves ahead contrary.
Advantage of the present utility model: 1, shortening is taken off and landing runway length greatly.2, manufacturing process and technical requirements are not high, low cost of manufacture.3, aviator easily masters a skill main points.4, the situation that aircraft carrier, air-raid shelter formula hangar etc. require dash road is practically applicable to.5, with the aircraft carrier Miniaturizable that this technology manufactures, maneuverability, is not easily found.
Accompanying drawing explanation
Accompanying drawing is the ultrashort runway schematic diagram of conveyor type, and 1 is roller, and 2 is conveyor type runway, and 3 is the aircraft of landing, and 4 is the fixing runways that conveyor type runway connects.
Detailed description of the invention
If Aircraft Quality is m, the aircraft speed that can rise when flying up into the sky is v
rise, the aircraft momentum that can rise when flying up into the sky is then P
rise=mv
rise.Generally take off hourly velocity from v
0start to v
riseslide a period of time and a segment distance.When aircraft takes off on the ultrashort runway of conveyor type, the ultrashort runway of conveyor type constantly accelerates the speed that the aircraft of balancing out motions backward moves ahead under computer equipment controls under roller drives, now aircraft be equivalent to a people run on a treadmill the same remaining where one is always do not advance but speed in increase, when speed close to or reach v
risethe momentum of Shi Feiji close to or reach the requirement of taking off, just do not advance and can't to take off on aerodynamics.At this moment stop the motion of the ultrashort runway of conveyor type, the momentum of aircraft reaches mv
risecannot stop the punching that can go ahead, as long as aircraft ceaselessly accelerates just can take off successfully.Speed just can not be dropped to v once by the ultrashort runway of conveyor type
0, speed is from v
risedrop to v
0process can give one, aircraft buffering, than use electromagnetic launch and steam ejection air speed from v
0reach v quickly
risein time, damage less to aircraft and aviator.Because the ultrashort runway of conveyor type is that circulation rotating is not stopped transport dynamic, the length of 50 meters can be equivalent to thousands of meters of length, takes off hourly velocity from v
0start to accelerate, aviator more easily grasps.
The ultrashort runway of conveyor type that during aircraft landing, roller drives is under computer to rear, aircraft flight direction high-speed motion, as long as aircraft drops to tens meters of long runway regions, the ultrashort runway of conveyor type is movement proal speed after counteracting aircraft landing backward, being equivalent to the long runway of thousands of rice can allow aircraft slow down gradually, than with check cable by force reduction of speed safely many.
Claims (1)
1. the ultrashort runway of conveyor type, is characterized in that: the conveyor type runway of cycle rotation comprising roller and driven by roller and support, ultrashort runway when taking off and land under computer to the direction motion that aircraft moves ahead contrary.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420389011.9U CN204323705U (en) | 2014-07-15 | 2014-07-15 | The ultrashort runway of conveyor type |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420389011.9U CN204323705U (en) | 2014-07-15 | 2014-07-15 | The ultrashort runway of conveyor type |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204323705U true CN204323705U (en) | 2015-05-13 |
Family
ID=53160089
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420389011.9U Expired - Fee Related CN204323705U (en) | 2014-07-15 | 2014-07-15 | The ultrashort runway of conveyor type |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204323705U (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105292512A (en) * | 2015-10-27 | 2016-02-03 | 林国强 | Airplane lander and landing system thereof |
| CN106628221A (en) * | 2016-11-08 | 2017-05-10 | 黄延庆 | Novel airplane runway |
| CN106904289A (en) * | 2017-03-21 | 2017-06-30 | 张宏 | Aircraft elevation angle ejector |
| CN108408075A (en) * | 2017-02-09 | 2018-08-17 | 陈云桥 | Aircraft carrier landing high-speed annular mobile device |
| CN108502199A (en) * | 2018-04-03 | 2018-09-07 | 东华大学 | A kind of novel warship method applied to aircraft carrier |
| CN108820236A (en) * | 2018-03-10 | 2018-11-16 | 乔华兵 | Aircraft carrier opportunity of combat landing platform |
| CN110723305A (en) * | 2019-10-15 | 2020-01-24 | 西京学院 | Relatively stationary aircraft landing gear and control method thereof |
| CN113386969A (en) * | 2021-07-13 | 2021-09-14 | 大连大学 | Take-off combined runway of carrier-based aircraft of aircraft carrier |
-
2014
- 2014-07-15 CN CN201420389011.9U patent/CN204323705U/en not_active Expired - Fee Related
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105292512A (en) * | 2015-10-27 | 2016-02-03 | 林国强 | Airplane lander and landing system thereof |
| CN106628221A (en) * | 2016-11-08 | 2017-05-10 | 黄延庆 | Novel airplane runway |
| CN108408075A (en) * | 2017-02-09 | 2018-08-17 | 陈云桥 | Aircraft carrier landing high-speed annular mobile device |
| CN106904289A (en) * | 2017-03-21 | 2017-06-30 | 张宏 | Aircraft elevation angle ejector |
| CN108820236A (en) * | 2018-03-10 | 2018-11-16 | 乔华兵 | Aircraft carrier opportunity of combat landing platform |
| CN108502199A (en) * | 2018-04-03 | 2018-09-07 | 东华大学 | A kind of novel warship method applied to aircraft carrier |
| CN110723305A (en) * | 2019-10-15 | 2020-01-24 | 西京学院 | Relatively stationary aircraft landing gear and control method thereof |
| CN113386969A (en) * | 2021-07-13 | 2021-09-14 | 大连大学 | Take-off combined runway of carrier-based aircraft of aircraft carrier |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150513 Termination date: 20150715 |
|
| EXPY | Termination of patent right or utility model |