CN102040003A - Orbiter - Google Patents

Orbiter Download PDF

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Publication number
CN102040003A
CN102040003A CN2010106124550A CN201010612455A CN102040003A CN 102040003 A CN102040003 A CN 102040003A CN 2010106124550 A CN2010106124550 A CN 2010106124550A CN 201010612455 A CN201010612455 A CN 201010612455A CN 102040003 A CN102040003 A CN 102040003A
Authority
CN
China
Prior art keywords
orbiter
ground
power source
power supply
portable power
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
Application number
CN2010106124550A
Other languages
Chinese (zh)
Inventor
吴倌熹
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN2010106124550A priority Critical patent/CN102040003A/en
Publication of CN102040003A publication Critical patent/CN102040003A/en
Pending legal-status Critical Current

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Abstract

The invention relates to an orbiter, in particular to an orbiter of which a power source is provided by an orbit, belonging to the technical field of vehicles. The technical scheme is as follows: an orbit on which a mobile power supply can move is laid on the ground, the orbiter is connected with the mobile power supply through a cable, and the mobile power supply is powered by the ground orbit. The aerial orbiter is powered by the ground power supply, thereby greatly saving ineffective energy consumption and greatly increasing the effective load; and in addition, since the consumption of fossil energy is reduced, the quality of our living environment is further improved.

Description

Orbiter
Technical field
The present invention relates to technical field of transportation means, refer in particular to a kind of flying instrument that utilizes track that propulsion source is provided.
Background technology
Progress along with society, it is frequent day by day that people carry out comings and goings by means of the vehicle, oneself becomes the people's life or the indispensable instrument of working the vehicle, and along with the quickening of work rhythm, the speed of the vehicle is also in speed-raising, from the most original ox cart, bicycle, progressively carry out the transition to high speed train, the aircraft of today.We know that today, the fastest vehicle were aircrafts, yet it is to carry a large amount of fuel oils in flight course, and the application of these fuel oils mainly consumes for the deadweight of carrying aircraft, ccasual various items.But, also having a most important consumption source, that is exactly the deadweight of fuel oil.Flight each time, aircraft all will carry tens tons fuel oil, not only because deadweight consumes great amount of fuel oil, also gives our earth, has caused huge pollution.
Summary of the invention
The objective of the invention is to overcome above-mentioned weak point of the prior art, and a kind of orbit aerocraft that has that utilizes ground rail that propulsion source is provided is provided.
The present invention is achieved through the following technical solutions: lay the track that can supply portable power source to move on ground, aircraft and portable power source are by cable connection, and portable power source provides electric power by ground rail.
The present invention has save the effective consumption of the energy greatly because the employing ground power supply provides the power of airborne aircraft, and capacity weight is greatly improved; Moreover, because the reduction that fossil energy consumes, also make to be further improved our living environment quality.
Description of drawings
Accompanying drawing is a structural representation of the present invention.
The specific embodiment
See accompanying drawing, the present invention mainly is made up of track 1, aircraft 2, cable 3 and portable power source 4.Lay the track 1 that can supply portable power source 4 to move on ground, aircraft 2 is connected by cable 3 with portable power source 4, and portable power source 4 provides electric power by ground rail 1.
When application is of the present invention, offer portable power source 4 electric power by being laid on ground track 1, portable power source 4 provides sufficient electric power for aircraft 2 by cable 3, portable power source 4 and aircraft 2 advanced in unison, can offer user's fast speed vehicle, and can not pollute to environment; If track 1 usefulness magnetic-levitation is substituted, then can obtain as the rapid advance speed as the aircraft.
Because portable power source 4 is very light objects, so the track 1 that carries it is also required lower, the cost cost is significantly less than existing track; Also can adopt the form of aerial conveyor, more can save a large amount of land resources, have the effect of well preserving the ecological environment.

Claims (1)

1. orbiter, mainly formed by track (1), aircraft (2), cable (3) and portable power source (4), it is characterized in that: lay the track (1) that can supply portable power source (4) to move on ground, aircraft (2) is connected by cable (3) with portable power source (4), and portable power source (4) provides electric power by ground rail (1).
CN2010106124550A 2010-12-30 2010-12-30 Orbiter Pending CN102040003A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2010106124550A CN102040003A (en) 2010-12-30 2010-12-30 Orbiter

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2010106124550A CN102040003A (en) 2010-12-30 2010-12-30 Orbiter

Publications (1)

Publication Number Publication Date
CN102040003A true CN102040003A (en) 2011-05-04

Family

ID=43906622

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2010106124550A Pending CN102040003A (en) 2010-12-30 2010-12-30 Orbiter

Country Status (1)

Country Link
CN (1) CN102040003A (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1113869A (en) * 1994-05-26 1995-12-27 刘奥宇 Cabled motor-driven air-cushion air craft
CN1446729A (en) * 2002-03-26 2003-10-08 刘毅 Low altitude aircraft with power supplied by wired electricity
CN101385903A (en) * 2007-09-14 2009-03-18 北京德庐影像技术有限责任公司 Hitching type electric self-service helicopter and system thereof
CN201494622U (en) * 2009-12-18 2010-06-02 杨礼诚 Wired electric flying and floating aircraft

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1113869A (en) * 1994-05-26 1995-12-27 刘奥宇 Cabled motor-driven air-cushion air craft
CN1446729A (en) * 2002-03-26 2003-10-08 刘毅 Low altitude aircraft with power supplied by wired electricity
CN101385903A (en) * 2007-09-14 2009-03-18 北京德庐影像技术有限责任公司 Hitching type electric self-service helicopter and system thereof
CN201494622U (en) * 2009-12-18 2010-06-02 杨礼诚 Wired electric flying and floating aircraft

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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
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20110504