CN111422071A - Novel transportation device - Google Patents

Novel transportation device Download PDF

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Publication number
CN111422071A
CN111422071A CN202010315249.7A CN202010315249A CN111422071A CN 111422071 A CN111422071 A CN 111422071A CN 202010315249 A CN202010315249 A CN 202010315249A CN 111422071 A CN111422071 A CN 111422071A
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CN
China
Prior art keywords
power supply
supply line
electric
line rail
electric airplane
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
CN202010315249.7A
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Chinese (zh)
Inventor
游正广
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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 CN202010315249.7A priority Critical patent/CN111422071A/en
Publication of CN111422071A publication Critical patent/CN111422071A/en
Pending legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60LPROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L9/00Electric propulsion with power supply external to the vehicle
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/24Aircraft characterised by the type or position of power plants using steam or spring force
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00Ground or aircraft-carrier-deck installations
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JCIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J9/00Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting
    • H02J9/04Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source
    • H02J9/06Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source with automatic change-over, e.g. UPS systems
    • H02J9/061Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source with automatic change-over, e.g. UPS systems for DC powered loads
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60LPROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L2200/00Type of vehicles
    • B60L2200/10Air crafts
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Power Engineering (AREA)
  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Transportation (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)

Abstract

The invention discloses a novel traffic transportation device, which comprises an electric airplane, a docking station, a power supply line rail, a control system, an emergency guarantee system and a route switching system, wherein the docking station is used for placing the electric airplane; the invention is suitable for various complex terrains, has relatively low construction cost, relatively low technical requirement, can be widely and frequently used, can intensively cover regional landmarks, has little influence on environment ecology, and is particularly suitable for regions with complex terrains by arranging the structures of the electric airplane, the docking station, the power supply line rail, the control system, the emergency guarantee system, the road changing system and the like.

Description

Novel transportation device
Technical Field
The invention relates to the field of traffic, in particular to a novel traffic transportation device.
Background
At the present stage, there are already numerous types of vehicles with various features and some mechanical devices not belonging to vehicles but used for transport and delivery. For example, automobiles and trains are widely used and are the main force of land passenger and cargo transportation, but long and winding roads need to be laid, large bridges need to be erected by communicating tunnels, land occupation and forest destruction are achieved, the construction cost is high, the construction difficulty in areas with complex terrains is high, and automobile exhaust is an important source of air pollution. For example, an airplane can realize the operation across the terrain and in a relatively long range, but is often only suitable for the transportation between distant provinces and international landmarks, or like a helicopter, a fighter plane and the like, and is only suitable for special purposes due to high manufacturing cost and technical requirements, and cannot be popularized and used. For example, a ship is convenient to use and low in cost, but is only suitable for water channel operation.
The transportation device can cross various terrains (such as mountains, canyons, rivers, straits, plateau, deserts and even the interior of cities) like an airplane, is easy to manufacture and generally applicable (even can realize the communication between villages and villages) like an automobile, has low road laying cost, small land occupation and forest destruction, less environment destruction and light energy consumption, is cheap and clean in locomotive operation energy, and has no tail gas emission, and is in urgent need of development.
Disclosure of Invention
In order to solve the technical problems, the technical scheme provided by the invention is as follows: a novel transportation device comprises an electric airplane, a docking station, a power supply line rail, a control system, an emergency guarantee system and a road changing system, wherein the docking station is used for docking the electric airplane, the power supply line rail consists of a plurality of sections of power supply lines, an electric tower for connecting the power supply lines and other line fixing or supporting facilities in any form (for example, the power supply line rail crossing a strait can provide supporting force for the middle section of the line by a hydrogen balloon), is used as a main power source and a running track of the electric airplane, and can be erected in any places such as mountainous regions, valleys, deserts, straits, urban roofs and houses; the power supply line rail and the electric plane are movably and electrically connected (such as brushes) to realize electric energy conduction and relative movement, and the electric plane can fly in any direction near the power supply line rail; the control system is electrically connected with the electric airplane, the docking station and the power supply line rail or is connected with the electric airplane by a wireless network to realize condition monitoring and control signal transmission, and is used for controlling the running state of the electric airplane in the flying process and processing various emergency situations;
the electric airplane is a flying device in any form and in any size and takes electric energy as a power source;
the emergency guarantee system is mainly used for handling various accidents and emergency situations, including emergency battery packs, temporary stopping points, parachutes and the like; the switching system is mainly used as a switching power supply line rail of an electric airplane in operation.
The emergency battery pack is electrically connected with the power supply line rail, and the electric brush is used for connecting the electric airplane with the power supply line rail.
Further, the emergency battery pack is used for temporary power-off of the power supply line rail.
Further, the electric tower is arranged below the power supply line rail.
Further, the electric aircraft takes a power supply line as an operation track.
Further, the electric aircraft takes a power supply line as a main power source.
Further, the electric airplane can use any flat vacant ground along the power supply line as a stop point, and the temporary stop point can be any flat vacant ground along the power supply line rail.
Further, the electric airplane flies at any position near the operation orbit.
Further, the electric aircraft may be parked to any open ground along the power rail under the power of the emergency battery pack.
Further, the electric aircraft mainly flies near the ground at low altitudes where power supply rails can be erected.
Further, the locomotive running track can span various complex terrains without tunnel bridges and the like.
Compared with the prior art, the invention has the advantages that: the invention is suitable for various complex terrains, has relatively low construction cost, relatively low technical requirement, can be widely and frequently used, can intensively cover regional landmarks, has cheap and clean locomotive operation energy sources and extremely small influence on environment ecology, and is particularly suitable for regions with complex terrains by arranging the structures of the electric aircraft, the docking station, the power supply line rail, the control system, the emergency guarantee system, the road changing system and the like.
Drawings
Fig. 1 is a schematic structural diagram of a novel transportation device.
As shown in the figure: 1. electric airplane, 2, electric tower, 3, power supply line rail.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings.
The present invention will be described in detail with reference to the accompanying drawings.
The invention provides a novel transportation device in specific implementation, which comprises an electric airplane 1, a parking platform, a power supply line rail 3, a control system, an emergency guarantee system and a route switching system, wherein the parking platform is used for placing the electric airplane 1, the power supply line rail 3 consists of a plurality of sections of power supply lines and an electric tower 2 connected with the lines, the power supply line rail 3 is used for running as a track of the electric airplane 1, and the control system is electrically connected with the electric airplane 1, the parking platform and the power supply line rail 3 and is used for controlling the running state of the electric airplane 1 in the flying process and processing various emergency situations;
the emergency battery pack is electrically connected with the power supply line rail 3, and the electric brush is used for connecting the electric airplane 1 with the power supply line rail 3. In use of the invention, the electric aircraft 1 may be any flight device driven by electricity, such as a helicopter driven by an electric motor, a small flight device driven by a battery, etc. Because the manufacturing cost of the motor is far lower than that of an aero-engine, the motor is easy to manufacture and obtain, and cheap electric energy is used as energy, the construction cost of the electric airplane is very low compared with that of a common airplane. The electric airplane has any size and scale, can be shaped at will, and can be operated quickly or slowly. The electric airplane is a flying device in any form and in any size and takes electric energy as a power source;
as a further illustration of the invention, the docking station is a place for the electric airplane to dock, and can be established in any vacant land, including urban roofs, village vacant lands and mountain flat lands.
As a further elaboration of the invention, the control system can effectively avoid the derailment of the electric airplane in the flying process, avoid the line conflict, reduce the occurrence of the emergency, save the energy and the like.
As a further elaboration of the present invention, the emergency safeguard system is responsible for handling various emergency situations, including rainstorm, lightning strike, rail collapse interruption, power failure, impact, etc.
As a further elaboration of the invention, the diversion system is used when the electric aircraft is to be switched from one supply line rail to another supply line rail.
As a further elaboration of the invention, the emergency battery pack is used for temporary power-off of the supply rail 3 or temporary parking of the electric aircraft along the supply rail.
As a further elaboration of the invention, the electric tower 2 is arranged below the supply line rail 3.
The present invention and its embodiments have been described above, and the description is not intended to be limiting, and the drawings are only one embodiment of the present invention, and the actual structure is not limited thereto. In summary, those skilled in the art should appreciate that they can readily use the disclosed conception and specific embodiments as a basis for designing or modifying other structures for carrying out the same purposes of the present invention without departing from the spirit and scope of the invention as defined by the appended claims.

Claims (3)

1. The utility model provides a novel transportation device which characterized in that: the emergency protection system comprises an electric airplane, a docking station, a power supply line rail, a control system, an emergency guarantee system and a route changing system, wherein the docking station is used for placing the electric airplane, the power supply line rail consists of a plurality of power supply lines and an electric tower connected with the power supply lines, the power supply line rail is used for operating as an electric airplane rail, and the control system is electrically connected with the electric airplane, the docking station and the power supply line rail and is used for controlling the operating state of the electric airplane in the flying process and processing various emergency situations;
the emergency battery pack is electrically connected with the power supply line rail, and the electric brush is used for connecting the electric airplane with the power supply line rail.
2. The new transportation device as claimed in claim 1, wherein: the emergency battery pack is used for temporarily powering off the power supply line rail.
3. The new transportation device as claimed in claim 1, wherein: the electric tower is arranged below the power supply line rail.
CN202010315249.7A 2020-04-21 2020-04-21 Novel transportation device Pending CN111422071A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202010315249.7A CN111422071A (en) 2020-04-21 2020-04-21 Novel transportation device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010315249.7A CN111422071A (en) 2020-04-21 2020-04-21 Novel transportation device

Publications (1)

Publication Number Publication Date
CN111422071A true CN111422071A (en) 2020-07-17

Family

ID=71558194

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202010315249.7A Pending CN111422071A (en) 2020-04-21 2020-04-21 Novel transportation device

Country Status (1)

Country Link
CN (1) CN111422071A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112070427A (en) * 2020-07-30 2020-12-11 辽宁立洲科技有限公司 Transmission tower Internet of things

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1084818A (en) * 1993-03-12 1994-04-06 刘奥宇 Wire control electric airplane
CN102310862A (en) * 2010-07-09 2012-01-11 侯卫平 Low-altitude and high-speed rail, namely, integral regional low-altitude and high-speed traffic transportation equipment and method
CA2895874A1 (en) * 2012-12-21 2014-06-26 European Aeronautic Defence And Space Company Eads France In-flight refuelling device for electric storage system and aircraft equipped with such a device
CN106274506A (en) * 2016-08-08 2017-01-04 蒋汉杰 A kind of urban air public transportation system
CN206067739U (en) * 2016-07-01 2017-04-05 何瑞根 Solar energy and hydrodynamic air transport device
CN209305857U (en) * 2018-10-26 2019-08-27 高洪江 Fixed-wing electric airplane co-axial contra rotating propeller dynamical system and fixed-wing electric airplane

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1084818A (en) * 1993-03-12 1994-04-06 刘奥宇 Wire control electric airplane
CN102310862A (en) * 2010-07-09 2012-01-11 侯卫平 Low-altitude and high-speed rail, namely, integral regional low-altitude and high-speed traffic transportation equipment and method
CA2895874A1 (en) * 2012-12-21 2014-06-26 European Aeronautic Defence And Space Company Eads France In-flight refuelling device for electric storage system and aircraft equipped with such a device
CN206067739U (en) * 2016-07-01 2017-04-05 何瑞根 Solar energy and hydrodynamic air transport device
CN106274506A (en) * 2016-08-08 2017-01-04 蒋汉杰 A kind of urban air public transportation system
CN209305857U (en) * 2018-10-26 2019-08-27 高洪江 Fixed-wing electric airplane co-axial contra rotating propeller dynamical system and fixed-wing electric airplane

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112070427A (en) * 2020-07-30 2020-12-11 辽宁立洲科技有限公司 Transmission tower Internet of things
WO2022020978A1 (en) * 2020-07-30 2022-02-03 辽宁立洲科技有限公司 Power transmission tower internet of things

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