CN101269660A - Electric flying apparatus - Google Patents
Electric flying apparatus Download PDFInfo
- Publication number
- CN101269660A CN101269660A CNA2007100899188A CN200710089918A CN101269660A CN 101269660 A CN101269660 A CN 101269660A CN A2007100899188 A CNA2007100899188 A CN A2007100899188A CN 200710089918 A CN200710089918 A CN 200710089918A CN 101269660 A CN101269660 A CN 101269660A
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- electric
- flying apparatus
- electric flying
- conductive casters
- vehicle body
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- Current-Collector Devices For Electrically Propelled Vehicles (AREA)
Abstract
The invention relates to an electric flying vehicle which uses fixed wire electric power and an overhead wire as a traveling track, in particular to a traffic tool flying in the sky. The electric flying vehicle is an optimal combination of a motorcar and a plane, and comprises a left and a right drivers, a left and a right conductive casters, a left and a right balance wings, an electric power control system and a vehicle body. The electric flying vehicle has high speed per hour, no need of ground, simple structure, zero pollution, flexible performance, security, power conservation and low cost.
Description
Technical field
The present invention relates to a kind of technological improvement of trunk-line traffic instrument, especially have greatly improved to the pollution of atmosphere with to the utilization of the energy.
Background technology
At present, known vehicle environmental pollution is very big, energy consumption is high, moving velocity is slow, deadweight has surpassed load carrying ability and make complicated.Just can finish transportation in travels down, most energy are consumed by own wt, and the investment of road construction is huge, again land occupation.Bring great negative effect to saving energy and reduce the cost.
Summary of the invention
The deficiency that can not use wired electric energy in order to overcome existing long, rely on road driving, self is overweight and moving velocity is slow, the invention provides a kind of electric flying apparatus, this electric flying apparatus can not only use wired electric energy and need not road fully, and quick again from heavy and light.
For realizing that technical scheme of the present invention is: electric flying apparatus is made up of left and right sides balance wing, left and right sides pusher, electric energy control system, left and right sides conductive casters and vehicle body etc.The driving road adopts the principle of aerial line, and line footpath bar is directly strengthened, and pole clearance is little, and it is big to put up the little camber of the gradient, is that supply line travels.
For better realizing scalable driving balanced system being arranged above-mentioned purpose on the balance wing, pusher is installed on the balance wing, and pusher is made up of purpose made motor and fan blade etc.Four conductive casterses are equipped with on the vehicle body both sides, are used for sliding support electric flying apparatus and conduction.
Because the present invention has taked electric flying apparatus to utilize aerial line and travelled, so the requirement of strength of electric flying apparatus is not high, can be controlled at the deadweight of electric flying apparatus about 500 kilograms, accurate carrying capacity is established 10 or 1000 kilograms, can reach from the fireballing purpose of heavy and light.
The invention has the beneficial effects as follows: without road, simple in structure, zero pollute, at the bottom of flexible, quick and easy, the energy-conservation and laid down cost.Because coming and going all is independently to travel, the center of gravity of driving below travelling, so more safer than the existing vehicle, it the time about 300 kilometers of scooters.
Description of drawings
The present invention is further described below in conjunction with accompanying drawing.
Fig. 1 is electric flying apparatus one an embodiment organigram.
Fig. 2 is that electric flying apparatus one embodiment comes and goes the scheme drawing that travels.
The specific embodiment
In Fig. 1, the vehicle body of electric flying apparatus (13) adopts light material to make, and pusher (3,7) utilizes wired electric energy to finish acting.Conductive casters (2,6,10,11) is installed in above the center of gravity on vehicle body both sides, is used for supporting electric flying apparatus and slides conduction.Balance wing (5,9) is the balance vehicle body and supports pusher that it is fixed on the vehicle body both sides.
In embodiment illustrated in fig. 2, conductor wire (A, B) utilizes high strength and the strong material of conduction to synthesize, and the available pair of bar in every place or many bridges sky form, and establish to come and go or many tracks, and each track is that A line and B line are formed.Left front conductive casters (2) contacts with the A circuit with left back conductive casters (6) electric flying apparatus and conduct electricity in that drawing lines is up when sailing, right front conductive casters (10) contacts with the B circuit with right back conductive casters (11) and conducts electricity, institute's power taking can be by electrical apparatus control system, supply with left and right sides pusher operation, produce pneumatic power and promote driving and travel.
The present invention can be used for present micro-computer technology the control of driving, can realize remote driving.In a word, utilize wired electricity to make energy, the built on stilts supply line of employing the long of moving traffic lane, all within the scope of the present invention.
Claims (3)
1. electric flying apparatus comprises that left and right sides pusher, left and right sides conductive casters, left and right sides balance wing and vehicle body in one, is characterized in that: electric flying apparatus travels on built on stilts circuit, provides electric energy by this circuit again.
2. electric flying apparatus according to claim 1 is characterized in that: pusher utilizes wired electric energy acting, is rolled to slide by conductive casters and conductor wire and transmits electric energy.
3. according to claim 1,2 described electric flying apparatus, it is characterized in that: conductive casters is contained in above the center of gravity on vehicle body both sides, is supporting travelling of electric flying apparatus.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2007100899188A CN101269660A (en) | 2007-03-19 | 2007-03-19 | Electric flying apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2007100899188A CN101269660A (en) | 2007-03-19 | 2007-03-19 | Electric flying apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN101269660A true CN101269660A (en) | 2008-09-24 |
Family
ID=40003964
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNA2007100899188A Pending CN101269660A (en) | 2007-03-19 | 2007-03-19 | Electric flying apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN101269660A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103318203A (en) * | 2012-10-12 | 2013-09-25 | 北京航空航天大学 | Lightweight composite-material carriage structure of aerodynamic aerotrain with imitated wings |
| RU2549728C2 (en) * | 2012-12-11 | 2015-04-27 | Александр Афанасьевич Нарижный | Passengers and cargoes air transportation and system to this end |
| CN108423012A (en) * | 2018-05-09 | 2018-08-21 | 安徽江淮汽车集团股份有限公司 | A kind of sky rail train and its control method |
-
2007
- 2007-03-19 CN CNA2007100899188A patent/CN101269660A/en active Pending
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103318203A (en) * | 2012-10-12 | 2013-09-25 | 北京航空航天大学 | Lightweight composite-material carriage structure of aerodynamic aerotrain with imitated wings |
| CN103318203B (en) * | 2012-10-12 | 2015-09-23 | 北京航空航天大学 | With the Lightweight composite-material carriage structure of the aerodynamic force aerotrain of imitative wing |
| RU2549728C2 (en) * | 2012-12-11 | 2015-04-27 | Александр Афанасьевич Нарижный | Passengers and cargoes air transportation and system to this end |
| CN108423012A (en) * | 2018-05-09 | 2018-08-21 | 安徽江淮汽车集团股份有限公司 | A kind of sky rail train and its control method |
| CN108423012B (en) * | 2018-05-09 | 2020-05-19 | 安徽江淮汽车集团股份有限公司 | Air rail train and control method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C12 | Rejection of a patent application after its publication | ||
| RJ01 | Rejection of invention patent application after publication |
Open date: 20080924 |