CN201712792U - Airplane taking-off and landing platform - Google Patents
Airplane taking-off and landing platform Download PDFInfo
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- CN201712792U CN201712792U CN2009202693038U CN200920269303U CN201712792U CN 201712792 U CN201712792 U CN 201712792U CN 2009202693038 U CN2009202693038 U CN 2009202693038U CN 200920269303 U CN200920269303 U CN 200920269303U CN 201712792 U CN201712792 U CN 201712792U
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Abstract
An airplane taking-off and landing platform is an intelligent, safe and efficient airplane taking-off and landing facility which is built in accordance with the principle on the composition of velocities and used in an aircraft carrier and the like. The taking-off and landing platform comprises a taking-off and landing switch, a velometer, a controlling computer, a frequency regulator, a motor, a speed reducer, a rotating platform which is wider and firmer than a conveying belt or a crawler belt, a cornice platform and the like. When an airplane is about to take off and the sum of the starting speed of the airplane and the reverse speed of the rotating platform is just equal to or slightly larger than the taking-off speed of the airplane, the airplane takes off; or when the airplane is about to land, the landing speed of the airplane is just opposite to the reverse speed of the rotating platform, and the transverse velocity and the like, namely, the resultant velocity is zero, so that the airplane stops running.
Description
Technical field: the invention belongs to the military aviation special facilities.
Background technology: the world today, aircraft that can vertical takeoff and landing except autogyro and minority need not the runway, and general aircraft all must landing on runway, and not only resource cost is many, also has some safety problems.And on aircraft carrier, have only to have equipped and launch or the sliding device of jumping just can take off, mirror, arrester wires, angled deck, elevator etc. fall but must use to help during landing.
Summary of the invention: purpose of the present invention will change conventional airplane landing pattern exactly, builds a kind of modern intelligent landing platform, makes landing platform on the aircraft one, just can fast and safely take off or stop row.The technical characterictic of landing platform is: the landing platform is by the landing switch, form than belt conveyor or the roomy crash-resistant turntable of crawler belt, velometer, regulation and control computer, frequency-shift keying, motor, reductor, eaves platform etc.; The landing switch links to each other with power supply, and velometer links to each other with the regulation and control computer by transmission circuit, and the regulation and control computer links to each other with frequency-shift keying, and frequency-shift keying links to each other with motor, and motor links to each other with reductor, and reductor links to each other with turntable; At turntable one end, be link to each other with runway, with the abundant close eaves platform of turntable.When aircraft need take off or land, press and take off or the switch that lands, just on demand direction running of turntable; When the aircraft that takes off or land enters the eaves platform, velometer on the eaves platform records the instantaneous velocity of aircraft, and the instantaneous velocity signal passed to the regulation and control computer, the regulation and control computer is regulated the frequency of frequency-shift keying according to the instantaneous velocity of aircraft, frequency-shift keying is promptly regulated rotating speed of motor, motor is regulated the rotating speed of reductor, and reductor is regulated the rotating speed of turntable; When the speed of turntable adds that the speed of boarding a plane just in time equals or when being slightly larger than the takeoff speed of aircraft
Then take off, or the inverted speed of turntable just in time equals the instantaneous velocity of aircraft, the relative velocity of the aircraft that then lands will be zero to stop row
Take off or fall latent after, the landing switch is cut off the electricity supply.
Description of drawings: accompanying drawing is a scheme drawing of the present utility model, wherein (1) motor; (2) reductor; (3) turntable; (4) pulley; (5) eaves platform; (6) velometer.
The specific embodiment: a kind of takeoff and landing platform, the landing platform is by landing switch, this belt conveyor or cover the big crash-resistant turntable 3 of bandwidth, velometer 6, compositions such as regulation and control computer, frequency-shift keying, motor 1, reductor 2, eaves platform 5; The landing switch links to each other with power supply, and velometer links to each other with the regulation and control computer by transmission circuit, and the regulation and control computer links to each other with frequency-shift keying, and frequency-shift keying links to each other with motor, and motor links to each other with reductor, and reductor links to each other with turntable; At an end of turntable, have with runway link to each other, with the abundant close eaves platform of turntable.In order to utilize the landing platform better, runway add the eaves platform length should about 30 meters, the length of turntable is advisable about 20 meters.Consider takeoff and landing efficient, aircraft carrier generally can be arranged two landing platforms in the horizontal, vertically goes up and arranges 3 to 4 groups of landing platforms.In case of necessity, also the landing platform can be installed, supply military so that the civil aircraft landing on land; At some confidential departments and some special road sections, also the landing platform can be installed, stop row to force vehicle.
Claims (1)
1. takeoff and landing platform is characterized in that: the landing platform is by the landing switch, form than belt conveyor or the roomy crash-resistant turntable of crawler belt, velometer, regulation and control computer, frequency-shift keying, motor, reductor, eaves platform; The landing switch links to each other with power supply, and velometer links to each other with the regulation and control computer by transmission circuit, and the regulation and control computer links to each other with frequency-shift keying, and frequency-shift keying links to each other with motor, and motor links to each other with reductor, and reductor links to each other with turntable; At an end of turntable, have with runway link to each other, with the abundant close eaves platform of turntable.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009202693038U CN201712792U (en) | 2009-10-19 | 2009-10-19 | Airplane taking-off and landing platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009202693038U CN201712792U (en) | 2009-10-19 | 2009-10-19 | Airplane taking-off and landing platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201712792U true CN201712792U (en) | 2011-01-19 |
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ID=43458791
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009202693038U Expired - Fee Related CN201712792U (en) | 2009-10-19 | 2009-10-19 | Airplane taking-off and landing platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201712792U (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102514721A (en) * | 2011-12-18 | 2012-06-27 | 张康德 | Aircraft (or rocket or guided missile) take-off (launching) and landing aid |
| CN102826232A (en) * | 2011-06-17 | 2012-12-19 | 航天信息股份有限公司 | Airplane short-distance sliding take-off and landing system based on RFID (Radio Frequency Identification) technology |
| CN103010475A (en) * | 2011-09-26 | 2013-04-03 | 陈新康 | Device for transmitting, boosting and lifting runway by multistage motive unit |
| CN103587711A (en) * | 2013-04-28 | 2014-02-19 | 叶元华 | Arresting device and runway being provided with arresting device |
| CN104002983A (en) * | 2014-05-30 | 2014-08-27 | 陈亮 | Aircraft take-off and landing device |
| CN105667822A (en) * | 2016-03-30 | 2016-06-15 | 代翔 | Aircraft cyclic transfer traction system |
| CN107813957A (en) * | 2017-11-27 | 2018-03-20 | 郭俭 | A kind of carrier-borne aircraft on aircraft carrier the method for warship |
| CN108408075A (en) * | 2017-02-09 | 2018-08-17 | 陈云桥 | Aircraft carrier landing high-speed annular mobile device |
| CN109159907A (en) * | 2018-08-23 | 2019-01-08 | 程帅奇 | Crawler type lifting gear |
-
2009
- 2009-10-19 CN CN2009202693038U patent/CN201712792U/en not_active Expired - Fee Related
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102826232A (en) * | 2011-06-17 | 2012-12-19 | 航天信息股份有限公司 | Airplane short-distance sliding take-off and landing system based on RFID (Radio Frequency Identification) technology |
| CN102826232B (en) * | 2011-06-17 | 2015-04-22 | 航天信息股份有限公司 | Airplane short-distance sliding take-off and landing system based on RFID (Radio Frequency Identification) technology |
| CN103010475A (en) * | 2011-09-26 | 2013-04-03 | 陈新康 | Device for transmitting, boosting and lifting runway by multistage motive unit |
| CN102514721A (en) * | 2011-12-18 | 2012-06-27 | 张康德 | Aircraft (or rocket or guided missile) take-off (launching) and landing aid |
| CN103587711A (en) * | 2013-04-28 | 2014-02-19 | 叶元华 | Arresting device and runway being provided with arresting device |
| CN104002983A (en) * | 2014-05-30 | 2014-08-27 | 陈亮 | Aircraft take-off and landing device |
| CN105667822A (en) * | 2016-03-30 | 2016-06-15 | 代翔 | Aircraft cyclic transfer traction system |
| CN105667822B (en) * | 2016-03-30 | 2018-07-27 | 成都天空营地科技有限公司 | A kind of aircraft cyclic transfer trailer system |
| CN108408075A (en) * | 2017-02-09 | 2018-08-17 | 陈云桥 | Aircraft carrier landing high-speed annular mobile device |
| CN107813957A (en) * | 2017-11-27 | 2018-03-20 | 郭俭 | A kind of carrier-borne aircraft on aircraft carrier the method for warship |
| CN109159907A (en) * | 2018-08-23 | 2019-01-08 | 程帅奇 | Crawler type lifting gear |
| CN109159907B (en) * | 2018-08-23 | 2024-02-27 | 程帅奇 | Crawler-type lifting device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20110119 Termination date: 20121019 |