CN201633925U - Magnetic suspension type lifting device of airplane - Google Patents
Magnetic suspension type lifting device of airplane Download PDFInfo
- Publication number
- CN201633925U CN201633925U CN2010201581979U CN201020158197U CN201633925U CN 201633925 U CN201633925 U CN 201633925U CN 2010201581979 U CN2010201581979 U CN 2010201581979U CN 201020158197 U CN201020158197 U CN 201020158197U CN 201633925 U CN201633925 U CN 201633925U
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- Prior art keywords
- airplane
- lifting device
- aircraft
- electromagnets
- suspension type
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- 239000000725 suspension Substances 0.000 title abstract description 9
- 238000005339 levitation Methods 0.000 claims description 10
- 238000000034 method Methods 0.000 abstract description 2
- 206010000369 Accident Diseases 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000002950 deficient Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
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Abstract
The utility model discloses a lifting device of an airplane, in particular to a magnetic suspension type lifting device of an airplane. The magnetic suspension type lifting device of the airplane comprises an airplane and an airfield runway and is characterized in that a plurality of lightweight electromagnets are arranged at the bottom end of the airplane; a plurality of electromagnets are arranged on the airfield runway; and after the lightweight electromagnets are electrified, the upper ends of the lightweight electromagnets and the upper ends of the electromagnets respectively become like magnetic poles which mutually repel. By using the suspension principle of a magnetically levitated train, the magnetic suspension type lifting device of the airplane ensures that the airplane can not directly contact the airfield runway in the taking-off or landing process, reduces the chance of the collision and the friction and improves the safety coefficient of the airplane.
Description
(1) technical field
The utility model relates to a kind of aircraft lifting and landing device, particularly a kind of electromagnetic levitation type aircraft lifting and landing device.
(2) background technology
Aircraft has become a kind of vehicle the most efficiently at present, but the safety factor of aircraft is not high, both at home and abroad there is the problem of airplane fault to take place all the time, cast aside the influence of environmental factor such as thunderstorm etc., airplane fault be mostly owing to when taking off or land and runway huge collision taking place or produces fire by friction causes, not only jeopardize passenger's personal safety, and can cause enormous economic loss.
(3) summary of the invention
The utility model provides a kind of aircraft safety high electromagnetic levitation type aircraft lifting and landing device in order to remedy the defective of prior art.
The utility model is achieved by the following technical solution:
A kind of electromagnetic levitation type aircraft lifting and landing device, comprise aircraft and airfield runway, it is characterized in that: the bottom of aircraft is equipped with a plurality of lightweight electromagnet, and the airfield runway mounted on surface has a plurality of electromagnet, and the lower end of energising back lightweight electromagnet and the upper end of electromagnet become the like pole of mutual repulsion respectively.
The beneficial effects of the utility model are: this electromagnetic levitation type aircraft lifting and landing device, utilize the suspension theory of magnetic suspension train, aircraft has been avoided in the process of taking off or landing and the runway direct contact, reduced collision and rubbing machine meeting, improved the aircraft safety coefficient.
(4) description of drawings
Below in conjunction with accompanying drawing the utility model is further described.
Accompanying drawing 1 is the structural representation of the utility model electromagnetic levitation type aircraft lifting and landing device.
Accompanying drawing 2 is the fundamental diagram of the utility model electromagnetic levitation type aircraft lifting and landing device.
Among the figure, 1 aircraft, 2 airfield runways, 3 lightweight electromagnet, 4 electromagnet.
(5) specific embodiment
Accompanying drawing is a kind of specific embodiment of the present utility model.This electromagnetic levitation type aircraft lifting and landing device, comprise aircraft 1 and airfield runway 2, it is characterized in that: the bottom of aircraft 1 is equipped with a plurality of lightweight electromagnet 3, airfield runway 2 mounted on surface have a plurality of electromagnet 4, and the lower end of energising back lightweight electromagnet 3 and the upper end of electromagnet 4 become the like pole of mutual repulsion respectively.
This electromagnetic levitation type aircraft lifting and landing device, mainly used the suspension theory of magnetic suspension train, when aircraft 1 takes off or lands, apply huge voltage for the electromagnet 4 on airfield runway 2 surfaces by the airport, the aircraft 1 inner lightweight electromagnet 3 of giving applies huge voltage, make lightweight electromagnet 3 and electromagnet 4 all produce strong magnetic field, at this moment, airfield runway 2 just is equal to two blocks of magnet that homopolarity is relative with aircraft 1, repulsion suspends aircraft 1, avoid aircraft 1 and airfield runway 2 direct contacts in the past, can reduce the generation of aircraft accident.
Claims (1)
1. electromagnetic levitation type aircraft lifting and landing device, comprise aircraft (1) and airfield runway (2), it is characterized in that: the bottom of aircraft (1) is equipped with a plurality of lightweight electromagnet (3), airfield runway (2) mounted on surface has a plurality of electromagnet (4), and the lower end of energising back lightweight electromagnet (3) and the upper end of electromagnet (4) become the like pole of mutual repulsion respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010201581979U CN201633925U (en) | 2010-04-14 | 2010-04-14 | Magnetic suspension type lifting device of airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010201581979U CN201633925U (en) | 2010-04-14 | 2010-04-14 | Magnetic suspension type lifting device of airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201633925U true CN201633925U (en) | 2010-11-17 |
Family
ID=43078409
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010201581979U Expired - Fee Related CN201633925U (en) | 2010-04-14 | 2010-04-14 | Magnetic suspension type lifting device of airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201633925U (en) |
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104443419A (en) * | 2014-11-25 | 2015-03-25 | 南京艾凌节能技术有限公司 | Permanent magnet magnetic suspension landing assisting system |
| CN105667768A (en) * | 2015-12-31 | 2016-06-15 | 歌尔科技有限公司 | Unmanned aerial vehicle take-off or landing control system and control method |
| CN105775112A (en) * | 2016-03-21 | 2016-07-20 | 安徽钰龙信息科技有限公司 | Four-shaft unmanned aerial vehicle taking-off and landing device |
| CN106516149A (en) * | 2017-01-03 | 2017-03-22 | 上海量明科技发展有限公司 | Electromagnetic aircraft launch system and method |
| CN106585961A (en) * | 2015-10-14 | 2017-04-26 | 熵零控股股份有限公司 | Fixed-wing aircraft |
| CN106586015A (en) * | 2015-10-14 | 2017-04-26 | 熵零控股股份有限公司 | Taking-off and landing method for fixed-wing aircraft |
| CN107209521A (en) * | 2015-04-30 | 2017-09-26 | 深圳市大疆创新科技有限公司 | Pass through the system and method for magnetic field landing mobile platform |
| CN108058846A (en) * | 2017-12-12 | 2018-05-22 | 佛山市神风航空科技有限公司 | A kind of mobile model electromagnetic runway system |
| CN108058845A (en) * | 2017-12-12 | 2018-05-22 | 佛山市神风航空科技有限公司 | A kind of electromagnetic runway system of aircraft |
| CN108082521A (en) * | 2017-12-12 | 2018-05-29 | 佛山市神风航空科技有限公司 | A kind of electromagnet track systems |
| CN108082520A (en) * | 2017-12-12 | 2018-05-29 | 佛山市神风航空科技有限公司 | A kind of landing electromagnetic runway system of aircraft |
| CN108528651A (en) * | 2018-03-28 | 2018-09-14 | 合肥凯石投资咨询有限公司 | Aircraft electromagnetic runway |
| CN109741673A (en) * | 2019-01-31 | 2019-05-10 | 佛山市神风航空科技有限公司 | A kind of model suspending aircraft |
| CN110356578A (en) * | 2018-04-09 | 2019-10-22 | 姜常勇 | It is a kind of elasticity magnetoelectricity ejection and magnetic float soft landing control device |
-
2010
- 2010-04-14 CN CN2010201581979U patent/CN201633925U/en not_active Expired - Fee Related
Cited By (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104443419B (en) * | 2014-11-25 | 2016-05-18 | 南京艾凌节能技术有限公司 | A kind of permanent magnetism magnetic suspension helps the system of falling |
| CN104443419A (en) * | 2014-11-25 | 2015-03-25 | 南京艾凌节能技术有限公司 | Permanent magnet magnetic suspension landing assisting system |
| CN107209521A (en) * | 2015-04-30 | 2017-09-26 | 深圳市大疆创新科技有限公司 | Pass through the system and method for magnetic field landing mobile platform |
| US11378982B2 (en) | 2015-04-30 | 2022-07-05 | SZ DJI Technology Co., Ltd. | System and method for landing a mobile platform via a magnetic field |
| US10509416B2 (en) | 2015-04-30 | 2019-12-17 | SZ DJI Technology Co., Ltd. | System and method for landing a mobile platform via a magnetic field |
| CN106585961A (en) * | 2015-10-14 | 2017-04-26 | 熵零控股股份有限公司 | Fixed-wing aircraft |
| CN106586015A (en) * | 2015-10-14 | 2017-04-26 | 熵零控股股份有限公司 | Taking-off and landing method for fixed-wing aircraft |
| US10287033B2 (en) | 2015-12-31 | 2019-05-14 | Goertek Technology Co., Ltd. | Unmanned aerial vehicle take-off and landing control system and control method |
| CN105667768A (en) * | 2015-12-31 | 2016-06-15 | 歌尔科技有限公司 | Unmanned aerial vehicle take-off or landing control system and control method |
| CN105775112A (en) * | 2016-03-21 | 2016-07-20 | 安徽钰龙信息科技有限公司 | Four-shaft unmanned aerial vehicle taking-off and landing device |
| CN106516149A (en) * | 2017-01-03 | 2017-03-22 | 上海量明科技发展有限公司 | Electromagnetic aircraft launch system and method |
| CN108058846A (en) * | 2017-12-12 | 2018-05-22 | 佛山市神风航空科技有限公司 | A kind of mobile model electromagnetic runway system |
| CN108082520A (en) * | 2017-12-12 | 2018-05-29 | 佛山市神风航空科技有限公司 | A kind of landing electromagnetic runway system of aircraft |
| CN108082521A (en) * | 2017-12-12 | 2018-05-29 | 佛山市神风航空科技有限公司 | A kind of electromagnet track systems |
| CN108058845A (en) * | 2017-12-12 | 2018-05-22 | 佛山市神风航空科技有限公司 | A kind of electromagnetic runway system of aircraft |
| CN108528651A (en) * | 2018-03-28 | 2018-09-14 | 合肥凯石投资咨询有限公司 | Aircraft electromagnetic runway |
| CN108528651B (en) * | 2018-03-28 | 2020-05-01 | 合肥凯石投资咨询有限公司 | Electromagnetic runway of aircraft |
| CN110356578A (en) * | 2018-04-09 | 2019-10-22 | 姜常勇 | It is a kind of elasticity magnetoelectricity ejection and magnetic float soft landing control device |
| CN109741673A (en) * | 2019-01-31 | 2019-05-10 | 佛山市神风航空科技有限公司 | A kind of model suspending aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| ASS | Succession or assignment of patent right |
Owner name: SHENZHEN SENGANG HEAVY STEEL STRUCTURAL ENGINEERIN Free format text: FORMER OWNER: ZENG BIN Effective date: 20110519 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| C53 | Correction of patent of invention or patent application | ||
| CB03 | Change of inventor or designer information |
Inventor after: Huang Zihao Inventor before: Zeng Bin |
|
| COR | Change of bibliographic data |
Free format text: CORRECT: INVENTOR; FROM: ZENG BIN TO: HUANG ZIHAO Free format text: CORRECT: ADDRESS; FROM: 250000 NO. 2 (MBA CLASS 2, SHANDONG YINGCAI UNIVERSITY), YINGCAI ROAD, LICHENG HIGH-TECH. INDUSTRIAL DEVELOPMENT ZONE, JI'NAN CITY, SHANDONG PROVINCE TO: 518103 BUILDING 3, SENGANG INDUSTRIAL PARK, TIANFU ROAD, QIAOTOU COMMUNITY, FUYONG SUBDISTRICT, BAO'AN DISTRICT, SHENZHEN CITY, GUANGDONG PROVINCE |
|
| TR01 | Transfer of patent right |
Effective date of registration: 20110519 Address after: 518103 Guangdong city of Shenzhen province Baoan District Fuyong Qiaotou street community Sengang Fuk Road Industrial Park building third Patentee after: Shenzhen Sengang Heavy Steel Structural Engineering Co., Ltd. Address before: 250000, No. 2, excellence Road, Licheng hi tech Industrial Development Zone, Shandong, Ji'nan (2 classes of business administration, Shandong Yingcai University) Patentee before: Zeng Bin |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20101117 Termination date: 20170414 |