DE102010048819A1 - High-speed long-distance traffic system for transporting person or load with rail-guided transport medium, has rail-guided contact-free flying unit provided with drive and suspended load unit established by magnetic fields - Google Patents

Abstract

The high-speed long-distance traffic system has a rail-guided contact-free flying unit (1) provided with a drive and a suspended load unit established by magnetic fields. A rail line is formed as guide path, where the rail line is subdivided in a section for starting or braking the flying unit and a section for guiding through-flying of the section with the flying unit.

Description

The invention relates to a high-speed long-distance transport system for transporting people and / or loads with a track-guided transport.

State of the art

The classic wheel-rail technology of the railroad has reached its economic limit also for high-performance trains such as Transrapid, ICE, TGV, Sabsan etc. at speeds of 300 km / h.

The magnetic track of the Transrapid, developed in Germany in 1979, is based on a drive with long-stator linear motors in which three-phase current flows through windings along the track. This drive concept is characterized by a non-contact thrust generation in a floating state, which, although mechanical transmission elements are no longer required, but the linear motors require input converter, braking resistors and track cables, which can be operated only with losses ( V. Gollnick, "Investigations for the evaluation of the transport efficiency of different means of transport", dissertation, TU Munich 2003, P. 111 to 112 ).

In addition, the Transrapid is needed to maintain the limbo state, a base amount of energy that is always applied and is up to a speed of 160 km / h about 80% of the total energy needs (see Johannes Klühspies, "Future Aspects of European Mobility", ksv-Verlag 2nd edition, 2XX0, p. 73 ).

All measures which the prior art has proposed to magnetic webs contain detail improvements that have not changed the fundamental disadvantages listed below ( DE 707 032 C . DE 36 35 258 C1 . DE 39 14 093 A1 . DE 39 17 058 C1 . DE 39 24 486 C1 . DE 39 41 525 C1 . DE 41 15 936 A1 . DE 43 13 847 A1 . DE 195 05 963 A1 . DE 199 19 703 A1 . DE 102 09 319 C1 . DE 102 13 052 A1 . DE 103 21 047 A1 . DE 10 2005 029 547 A1 . DE 10 2007 047 165 A1 . DE 10 2008 023 086 A1 . DE 10 2008 030 609 B4 . DE 699 32 847 T2 . WO 95/29084 A1 . WO 99/19195 A1 ).

The maglev train is a railway that travels on a magnetic field. In doing so, she exceeds the speed limit of 300 km / h for flying without using this performance potential.

The start-up and braking process are not optimally designed energy, because the majority of the energy costs for the limbo is used up. The higher the level of steady-state speed, the more energy has to be expended to overcome the growing aerodynamic drag. As a result, the energy expenditure for overcoming the air resistance over 300 km / h increases convexly non-linearly.

In addition, the chassis and the car are clearly too heavy and have no shape, which ensure a fluidically low CW value.

Aircraft have gained a significant position in the transportation industry overcoming long distances, and the share of aviation in the transport volume continues to grow, which also increases the risk of flying. It takes the start and landing of aircraft complex technology and large-scale facilities such as airports. The individual aircraft is as limited in its transport capacity as the airport. It has a very high energy consumption and thus a significantly lower efficiency compared to the ICE or Transrapid ( V. Gollnick, "Investigations on the Assessment of the Transport Efficiency of Different Vehicles", Dissertation, TU Munich 2003, p. 115 ).

The investment and maintenance costs per unit transported are several times that of a train on airplanes.

In addition, aircraft offer compared to the train comparatively much less comfort.

task

In this prior art, the present invention seeks to provide a high-speed long-distance transport system for transporting people and / or loads with a track-guided means of transport, which closes the performance gap between high-speed train and the aircraft and at the same time significantly reduces the manufacturing costs and energy consumption Transport performance, convenience, safety, availability and environmental friendliness increased over the train and the aircraft.

This object is achieved by a high-speed long-distance transport system having the features of claim 1.

Advantageous embodiments of the road are the dependent claims.

The solution according to the invention combines the advantages of track-bound non-contact transport with those of flying. It is based on the knowledge that an aircraft flies freely from 250 to 300 km / h and that aerodynamics and flight function are extremely important for the movement processes. As long as the aircraft moves with its drive on the runway, the aircraft is a vehicle. If the buoyancy forces exceed the weight of the aircraft, the vehicle becomes an aircraft.

• a mindestens eine spurgebundene berührungslose mit einer auf Magnetfelder beruhende Antriebs- und Schwebeeinrichtung versehene Flugeinrichtung, die mindestens aus einem Rumpf, Tragflügeln zum Erzeugen eines Auftriebs und einem Fahrwerk gebildet ist, und
• b eine als Führungsbahn ausgebildete Schienenstrecke, die mindestens in einen Abschnitt zum Anfahren oder Bremsen der Flugeinrichtung und einen Abschnitt zum geführten Durchfliegen des Abschnitts mit der Flugeinrichtung unterteilt ist, wobei der durch die Tragflügel resultierende Auftrieb beim Fliegen die magnetischen Kräfte der Schwebeeinrichtung und das Gewicht der Flugeinrichtung im Gleichgewicht stehen, so dass die Flugeinrichtung während des Fliegens in einer schwebenden Lage spurgeführt gehalten ist.

The application of this knowledge is achieved by comprising the high-speed system according to the invention

• a at least one track-bound non-contact with a magnetic field based propulsion and levitation device provided flying device, which is at least formed of a fuselage, wings for generating a buoyancy and a chassis, and
• b is formed as a guideway rail track, which is subdivided into at least a portion for starting or braking of the flying device and a portion for guided flying through the portion with the flying device, wherein the lift resulting from the wings when flying the magnetic forces of the levitation device and the weight of Flight equipment are in equilibrium, so that the flying device is kept track guided while flying in a floating position.

In a further advantageous embodiment of the invention, the flying device is provided with different levitation devices, such that the levitation device for the starting or braking section is a superconducting magnetic levitation device or an electromagnetic levitation device and the levitation device for the flight section is an electromagnetic levitation device.

But it is also possible, without departing from the invention, that the flying device for the starting or braking section and the flight section has a common levitation device, such that the levitation device is a Elektromagnetschwebeeinrichtung.

Particularly advantageous for the embodiment of the invention, when the chassis is part of the superconducting magnetic levitation device, so that the superconductor and the cooling device is retractable immediately after the beginning of the flight phase in the fuselage of the aircraft, whereby cold losses can be avoided and the air resistance is reduced.

The permanent magnets belonging to the superconducting magnetic levitation device are advantageously laid directly on the rails.

It is of particular advantage that the flying device contains a streamlined head unit with a tip and bead for reducing the air resistance, at least one transport unit for accommodating cabins of seats for persons and / or transport containers for goods and a tail unit which is designed in its shape in that a disruption of the air flow is clearly counteracted.

In a preferred embodiment, the head unit has a crumple zone to increase safety and in the top lights, cameras for distance, wide angle and night vision are arranged, which are centrally monitored so that the flying device can be controlled without a driver. It is also useful if the rear unit has a large-scale Entladeluke for loading and unloading large and long goods.

The particular suitability for spargeführt flying the high-speed rail system according to the invention in the suspended section of the rail track results from the fact that the wings of primary wings and optional secondary wings and side wings are formed, the primary wing on the roof of the fuselage one behind the other at a distance from each other at different heights, the secondary wing are arranged behind the primary wings and the side wings at the lower part of the fuselage such that the flying device uniformly floats on reaching the critical airspeed over the length of the magnetic field generated by the levitation device.

Due to the buoyancy generated by the wings during propulsion of the flying device has the particular advantage that the buoyancy forces generated counteract the vehicle load and lead to significant reduction in energy requirements for the generation of the electromagnetic limbo.

In a further advantageous embodiment of the wing is provided that the primary wings have delta shape and are designed to change the buoyancy and braking forces adjustable.

According to a further advantageous embodiment of the invention, the flying device consists of carbon fiber or glass fiber reinforced plastic with or without metal inserts and has a derived from the aircraft oval basic shape, whereby the vehicle weight drops significantly and the air resistance, especially at high Speed range is reduced, which also contributes to reducing energy consumption.

In a preferred embodiment of the invention, the permanent magnets of the superconducting magnetic levitation device along the start-up and braking section are arranged on the rails, wherein the generated magnetic field between the permanent magnet and superconductor keeps the flying device at rest in the floating state.

This has the extraordinary advantage that the flying device no further energy to maintain its position in the magnetic field must be supplied.

According to a further advantageous embodiment of the invention, the drive and levitation device for guiding, holding and driving the flying device from a arranged along the flight section synchronous long stator linear motor, the stator of the rails of the flight section and the rotor of the flying device is assigned.

In a particularly advantageous embodiment of the Elektromagnetschwebeeinrichtung the juxtaposed rails are arranged at an angle deviating from zero degrees to each other, resulting in an oblique arrangement of the magnetic fields, which is able to simultaneously absorb forces in two load directions and compensate for deviations accordingly.

According to a variant of the invention, it is particularly advantageous to mount one or more rail sections on a multi-functional track construction.

The material for the track construction consists of a reinforced concrete pipe produced by the centrifugal process, the interior of which serves as an infrastructure channel for supply and disposal facilities, walk-in ducts, lines for gas, oil, electricity, water, etc. This has the extraordinary advantage of ensuring the energy supply of the high-speed long-distance transport system and at the same time the route structure for the passage of other media such as oil and / or gas, power or information lines with significant savings in floor space, effort, material and costs and the improvement of environmental protection use.

Another advantage is that the rails are designed as solid concrete rails, which are firmly connected to each other, preferably by concrete rocker, the rails are mounted directly on the train construction or the infrastructure channel with the interposition of a elastoviskosen intermediate layer. The intermediate layer fulfills tasks of vibration damping and fine adjustment of the rails.

Of course, it also belongs to the invention when the rails and the concrete rocker are integral, d. H. to form a common massive part.

In a further embodiment of the invention, the rail routes are interconnected by stations, in each of which the starting or braking section is arranged.

The solution according to the invention is characterized in that the total energy consumption of the high-speed long-distance transport system according to the invention is significantly lower than the energy consumption of existing high-speed systems such as Transrapid, Maglev, ICE, etc., and at the same time offers higher safety, better comfort and greater environmental compatibility.

Further advantages and details will become apparent from the following description with reference to the accompanying drawings.

embodiment

The invention will be explained in more detail below using an exemplary embodiment.

Show it

1 a top view of the flying device of the high-speed rail system according to the invention,

2 a side view of the flying device of the high-speed rail system according to the invention,

3 a section through the flying device along the line AA of 1 .

4 a schematic representation of the rail route of the high-speed system according to the invention between two stations,

5 the arrangement of the flying device on a route in sectional view,

6 the concrete rails connected by concrete sleepers in a schematic representation,

7 a schematic representation of the holding and guiding function on the concrete rail,

8th a section through an elevated infrastructure route at a breakpoint,

9 the connection of the infrastructure route and flight facility for persons to a station on average and

10 the connection of the infrastructure route and aircraft for goods to a station on average.

The 1 to 3 show the basic structure of the aircraft 1 the high-speed long-distance transport system according to the invention, for speeds above 500 km / h on a railway line 2 is designed. The flying device 1 consists of a streamlined head unit 3 , several, for example, six consecutively arranged transport units 4.1 to 4.6 and a tail unit 5 together.

The head unit 3 that a bit 6 and a bead 7 To reduce the air resistance similar to an aircraft, a crash box picks up and is equipped with lights 9 as well as cameras 10 provided for distance vision, wide angle and night vision. The lights 9 and cameras 10 are centrally monitored together with all functions and operating parameters, so that the flight device 1 can be controlled without driver.

In the transport units 4.1 to 4.6 Different cabin types, for example, a seating 11 for passenger transport or container pickup 12 for goods transport or open spaces 13 for vehicles, such as cars (see also 9 and 10 ) are used.

On the roof 14 each transport unit 4.1 to 4.6 are the wings as the primary wing 15 , Secondary wing 17 and at the side of the hull 16 every transport unit 4.1 , to 4.6 wing 18 assembled. The primary wings 15 have delta shape and are arranged behind each other at a distance from each other at different heights.

Primary and secondary wings 15 respectively. 17 as well as the side wings 18 are spaced from each other so that they can only slightly influence each other and ensure even lift over their entire length of the flying device as soon as the critical speed is overcome by the buoyancy when entering the flight phase. The wings of the primary and secondary wings 15 respectively. 17 as well as side wings 18 are designed so that the lift generated only a part of the weight of the aircraft 1 compensated, so that a residual weight for the tracking by the magnetic field and thus for the control of the magnetic field gap for the start-up or braking phase and the flight phase is ready. To change the buoyancy and braking forces, for example, the primary wings 15 be designed adjustable.

Most of the buoyancy force is due to the primary and secondary wings 15 respectively. 17 generated. The wing potential can reach, for example, with a length of the flying device of 250 m and a width of the flying device of 5.2 m, a wing of 1300 m ² .

The cross section through the transport units 4.1 to 4.2 Like the fuselage of the aircraft, it has an oval basic shape to minimize air resistance (see 3 ).

The outer skin of head unit 3 , Transport units 4.1 to 4.6 , Rear unit 5 , Primary and secondary wings 15 respectively. 17 and side wings 18 are made of carbon fiber or glass fiber reinforced plastic with or without metal inserts, reducing the weight of the flying device 1 significantly decreases and the air resistance is reduced, especially in the high speed range, which significantly contributes to the reduction of energy consumption.

4 shows the basic structure of the high-speed long-distance transport system according to the invention between two stations 19.1 and 19.2 , The rail routes 20 and 21 are each in a starting or braking section 20.1 respectively. 21.1 and a flight section 20.2 and 21.2 divided up.

The starting or braking sections 20.1 respectively. 21.1 are for example in the area of the stations 19.1 and 19.2 designed so that they have a length of at least 1.6 km.

The flying device 1 preferably has two different levitation devices, for the starting or braking section 20.1 respectively. 21.1 a superconducting magnetic levitation device and for the flight section 20.2 respectively. 21.2 an electromagnetic levitation device. Both levitation devices are well known and tested, so that dispenses with a more detailed description of the function of these facilities and on the relevant sources (for example, in Johannes Klühspies, "Future Aspects of European Mobility", ksv-Verlag 2nd edition, 2010 , or R. Schach, P. Jehle, R. Naumann, "Transrapid and Wheel-Rail High-Speed Rail", Springer-Verlag, 2005 ) can be referenced

The superconducting magnetic levitation device is made up of permanent magnets arranged along the start-up and braking sections on the rails and at least in the chassis of each transport unit 4.1 to 4.6 arranged superconductors with cooling device together. The generated magnetic field keeps the flying device 1 over her entire Length in limbo. This has the extraordinary advantage that the flying device no further energy to maintain its position in the magnetic field must be supplied.

Once the flying device 1 after approaching the starting section 20.1 respectively. 21.1 leaves, the suspension is retracted with the superconductor including cooling device and the electromagnetic drive and levitation device for the flight section 20.2 respectively. 21.2 effective. By retracting the landing gear, the cold losses and air resistance at the flying device are significantly reduced.

The drive for the flight phase of the flying device 1 consists of one along the flight section 20.2 respectively. 21.2 arranged synchronous long-stroke linear motor whose stator is assigned to the rails of the flight section and the rotor of the flying device.

The rail route 20 respectively. 21 are like 5 shows - on a multifunctional road construction 22 mounted, at ground level or in stand construction (see 8th ) can be executed.

The material for the route construction, for example, consists of a reinforced concrete pipe produced by the centrifugal process, the interior of which is an infrastructure channel 23 for supply and disposal facilities 24 , walk-in ducts 25 , Cables 26 for gas, oil, electricity, water etc. ( 8th ).

This has the extraordinary advantage of ensuring the energy supply of the high-speed long-distance transport system and at the same time the route structure for the passage of other media such as oil and / or gas, power or information lines with significant savings in floor space, effort, material and costs and the improvement of environmental protection use. Furthermore, such reinforced concrete pipes not only have an extraordinary rigidity, but the hurled concrete is also at temperatures between -40 and + 40 ° C resistant.

The rails 27 the railways 20 respectively. 21 can be designed as solid concrete rails that intersect each other by concrete rocker 28 are connected, with the rails directly on the track structure 22 or the infrastructure channel 23 with the interposition of a elastoviskosen liner 29 are mounted (see 6 ). Any sound emissions or other vibrations can be minimized.

In 7 is the guiding and holding function on the rail 27 clarified. The requirements for the geometric accuracy of the railway line 20 respectively. 21 of the high-speed long-distance transport system according to the invention increase with increasing speed.

As a holder for the permanent magnets of the superconducting magnetic levitation device and for the stators of the electromagnetic levitation therefore serve solid concrete rails 27 , which can be fine-adjusted on the track structure 22 rest.

Due to the particular inclination of the magnetic fields of the permanent magnets and the stators on both rails 27 at an angle α deviating from zero, the generated magnetic fields can absorb forces simultaneously in two load directions. The lateral guidance as required by the Transrapid can be omitted. Deviations can be determined as before by gap sensors and compensated by control, so that the predetermined gap width of about 10 mm is maintained.

The 8th to 10 show examples of the connection of the multifunctional road construction 22 the high-speed long-distance transport system according to the invention at stops and stations. Side by side guided pipes of the route construction 22 can preferably be connected by walk-in and passable channels, which can also serve to accommodate cables of any kind and service. It is also possible to connect the space of the adjacent tubes through a central part, which is guided over the entire route or only over a section of the route, which makes maintenance and repair much easier.

Thanks to the multi-functionality, considerable investment and maintenance costs are saved and ecological effects achieved, especially when overcoming long distances. The infrastructure route 22 Fulfills connection functions, development and supply functions for urban and industrial areas alike.

When entering a station or a breakpoint, the carrying principle changes from electromagnetic carrying (hovering) to carrying through a magnetic field of a superconductor.

LIST OF REFERENCE NUMBERS

1

flight equipment

2

railway line

3

head unit

4, 4.1-4.6

transport unit

5

rear unit

6

Tip of 3

7

Bead of 3

9

to shine

10

cameras

11

seating

12

container spreader

13

open space

14

Roof of 1

15

primary wing

16

Hull of 1

17

secondary wing

18

wing

19.1, 19.2

stations

20, 21

Rail routes between stations

20.1, 21.1

Starting or braking section

20.2, 21.2

flight segment

22

route structure

23

Infrastructure channel in 22

24

Supply and disposal facility

25

Walk-in ducts

26

cables

27

rails

28

concrete sill

29

liner

α

Angle of inclination of the magnetic fields

QUOTES INCLUDE IN THE DESCRIPTION

This list of the documents listed by the applicant has been generated automatically and is included solely for the better information of the reader. The list is not part of the German patent or utility model application. The DPMA assumes no liability for any errors or omissions.

Cited patent literature

• DE 707032 C [0005]
• DE 3635258 C1 [0005]
• DE 3914093 A1 [0005]
• DE 3917058 C1 [0005]
• DE 3924486 C1 [0005]
• DE 3941525 C1 [0005]
• DE 4115936 A1 [0005]
• DE 4313847 A1 [0005]
• DE 19505963 A1 [0005]
• DE 19919703 A1 [0005]
• DE 10209319 C1 [0005]
• DE 10213052 A1 [0005]
• DE 10321047 A1 [0005]
• DE 102005029547 A1 [0005]
• DE 102007047165 A1 [0005]
• DE 102008023068 A1 [0005]
• DE 102008030609 B4 [0005]
• DE 69932847 T2 [0005]
• WO 95/29084 A1 [0005]
• WO 99/19195 A1 [0005]

Cited non-patent literature

• V. Gollnick, "Investigations on the Assessment of the Transport Efficiency of Different Vehicles", Dissertation, TU Munich 2003, pp. 111 to 112 [0003]
• Johannes Klühspies, "Future Aspects of European Mobility", ksv-Verlag 2nd edition, 2XX0, p. 73 [0004]
• V. Gollnick, "Investigations for the Assessment of the Transport Efficiency of Different Vehicles", Dissertation, TU Munich 2003, p. 115 [0009]
• Johannes Klühspies, "Future Aspects of European Mobility", ksv-Verlag 2nd edition, 2010 [0060]
• R. Schach, P. Jehle, R. Naumann, "Transrapid and Wheel-Rail High-Speed Rail", Springer-Verlag, 2005 [0060]

Claims (22)

High-speed long-distance transport system for transporting people and / or loads by means of a track-guided means of transport, comprising a at least one track-bound non-contact flying device provided with a magnetic field-based drive and levitation device ( 1 ) consisting of at least one hull ( 16 ), Wings ( 15 . 17 . 18 ) is formed for generating a lift, and a chassis, and b is formed as a guideway rail track ( 20 and or 21 ), which are at least in one section ( 20.1 . 21.1 ) for starting or braking the flying device and a section ( 20.2 . 21.2 ) for guided flight of the portion with the flying device, the buoyancy resulting from the wings being in equilibrium with the magnetic forces of the levitation device and the weight of the flying device, so that the flying device is kept track guided while flying in a floating position. High-speed long-distance transport system according to claim 1, characterized in that the flying device ( 1 ) is provided with different levitation devices, such that the levitation device for the starting or braking section ( 20.1 . 21.2 ) a superconducting magnetic levitation device or an electromagnetic levitation device and the levitation device for the flight section ( 20.2 . 21.2 ) is an electromagnetic levitation device. High-speed long-distance transport system according to claim 1, characterized in that the flying device ( 1 ) for the starting or braking section ( 20.1 . 21.1 ) and the flight section ( 20.2 . 21.2 ) has a common levitation device, such that the levitation device is an electromagnetic levitation device. High-speed long-distance transport system according to claim 1 or 2, characterized in that the chassis is part of the superconducting magnetic levitation device having a superconductor with cooling device. High-speed long-distance transport system according to claim 1, characterized in that the flying device ( 1 ) a streamlined head unit ( 3 ) with tip ( 6 ) and bead ( 7 ), at least one transport unit ( 4.1 ) and a tail unit ( 5 ) contains. High-speed long-distance transport system according to claim 5, characterized in that the head unit ( 3 ) has a crumple zone. High-speed long-distance transport system according to claim 5, characterized in that the rear unit ( 5 ) has a large-scale Entladeluke for loading and unloading large and long goods. High-speed long-distance transport system according to claim 1, characterized in that the wings of primary wings ( 15 ), optionally secondary wings ( 17 ) and side wings ( 18 ), the primary wings ( 15 ) on the roof ( 14 ) of the fuselage ( 16 ) one behind the other at a distance from each other at different heights, the secondary wings ( 17 ) behind the primary wings ( 15 ) and the side wings ( 18 ) at the lower part of the fuselage ( 16 ) are arranged such that the flying device uniformly floats on reaching the critical airspeed over the length of the magnetic field generated by the levitation device. High-speed long-distance transport system according to claim 8, characterized in that the primary wings ( 15 ) Have delta shape. High-speed long-distance transport system according to claim 8, characterized in that the primary wings ( 15 ) are adjustable for changing the buoyancy and braking forces. High-speed long-distance transport system according to one of claims 1 to 10, characterized in that the outer skin of the flying device ( 1 ) is made of carbon or glass fiber reinforced plastic with or without metal inserts and has an oval basic shape. High-speed long-distance transport system according to claim 2, characterized in that the permanent magnets of the superconducting magnetic levitation device along the starting and braking section ( 20.1 . 21.1 ) on the rails ( 20 . 21 ) are arranged, and that the magnetic field generated between the permanent magnet and superconductor, the flying device ( 1 ) keeps floating in the dormant state. High-speed long-distance transport system according to claim 1 or 4, characterized in that the landing gear in the fuselage ( 16 ) of the flying device ( 1 ) is formed retractable. High-speed long-distance transport system according to claim 1, characterized in that the drive and levitation device for guiding, holding and driving the flying device from one along the starting or braking section ( 20.1 . 21.1 ) and the flight section ( 20.2 . 21.2 ) on the rails ( 20 . 21 ) installed synchronous long stator linear motor, whose stator is assigned to the rails of the flight section and the rotor of the flying device. High-speed long-distance transport system according to claim 13, characterized in that the side-by-side rails ( 27 ) of the electromagnetic levitation device are arranged at an angle deviating from zero degrees to each other. High-speed long-distance transport system according to one of Claims 1 to 14, characterized in that one or more rail links / n ( 20 . 21 ) on a multifunctional route structure ( 22 ) are arranged. High-speed long-distance transport system according to claim 16, characterized in that the route structure ( 22 ) comprises a tube produced by the centrifugal process, preferably made of reinforced concrete, the interior of which is used as an infrastructure channel ( 23 ) for supply and disposal facilities ( 24 ), walk-in ducts ( 25 ), Cables ( 26 ) for gas, oil, electricity, water or information purposes. High-speed long-distance transport system according to one of claims 1 to 17, characterized in that the rails ( 27 ) are designed as solid concrete rails, which are interconnected by concrete rocker ( 28 ) are connected. High-speed long-distance transport system according to claim 18, characterized in that the rails ( 27 ) and the concrete rocker ( 28 ) are integral, ie form a common solid part. High-speed long-distance transport system according to one of claims 1 to 17, characterized in that the rails ( 27 ) directly on the track structure ( 22 ) or the infrastructure channel ( 23 ) with the interposition of an elastoviscose intermediate layer ( 28 ) are mounted. High-speed long-distance transport system according to one of claims 1 to 20, characterized in that the rail lines ( 20 . 21 ) through stations ( 19.1 . 19.2 ) are connected to each other, in which the starting or braking distance ( 20.1 . 21.1 ) are arranged. High-speed long-distance transport system according to claim 5, characterized in that in the top of the head unit ( 3 ) of the flying device ( 1 ) To shine ( 9 ), Cameras ( 10 ) are arranged for long-distance, wide-angle and night vision, which are monitored centrally.

Images