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Everything should be as simple as possible, but not simpler than that. |
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his page describes the FLYWAY® propulsion car. Let us start by defining our terminology. The propulsion car is the controlling and driving unit for every vehicle. It is the "invisible" part that is inside the hollow beam.
The carriage is the part that hangs underneath the beam and is transported along by the propulsion carriage. |
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he FLYWAY® propulsion car (figures 1 and 2) can have the following attributes and equipment:
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Figure 1:1: Cross-sectional view of beam and propulsion car |
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![]() Figure 1:2The FLYWAY propulsion car is longer than is strictly necessary, and has a slimmed waist (see figure 1:2 above) which is also flexibly jointed. The purpose is of course to:
The FLYWAY® propulsion cars rely on radar signals and on detectors in the beam to alert them about obstacles. The FLYWAY cabins for PRT-operation are not planned to be longer than about 6 meters. Cabins of 10 meters or more in length (for GRT-operation) might need 2 beam attachments (and thus 2 propulsion cars) in order to keep the cabin properly balanced, as shown to the left in figure 3:1 below. This arrangement makes it trickier to keep the cabin level when the beam slopes. |
![]() Figure 1:3 |
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This is a (incomplete) list of controls and measures that has to be programmed into the propulsion car.
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here could be 2 situations when the propulsion cars need to be coupled together (and please note that we are talking about the propulsion cars here, not the beam vehicles):
Long cars might, for stability reasons, need two suspension points, each controlled by a propulsion vehicle. The reasons why those propulsion cars should be joined together inside the beam are mainly two: |
Regarding the train situation, the same two reasons would apply. In addition, one could conceive of a situation where one car pulls some other cars that are not equipped with proper propulsion engines. The reason for that might be economics; such cars would be cheaper to manufacture. |
While the connection point at A in the figure above is permanent, the connection at B should be automatically controlled by the cars' computers. There would have to be strain indicators mounted at those connection points, signalling whether a proper connection has been attained or the connection has been disengaged, as the case may be. When passageways for passengers are used between the cabins, as in the illustration, the same kind of safety measures would have to apply there. As a rule, however, when there are no passageways between cars, the cabins should not come within touching distance of one another. Another safety aspect comes into play if these cars are equipped with elevators to lower them to the ground. Then, obviously, all elevators have to operate in concert with one another. This would have to be closely monitored, with safety mechanisms to stop the operation of the elevators if they should get out of synchronization. |
The demands on this motor are:
The beamcar engines are required to vary their speeds all the time during travel. To use gears between the motor and the wheels degrade efficiency, but might have to be used in FLYWAY anyway. What is really needed is a supply voltage that varies it frequency in tune with the motor´s rotational speed, so much so that the motor can cover the whole range of speeds for the vehicle without having to use gears. Inverted rectifiers for speed regulation have been around for some time. But the technology for integrating this frequency regulation with the motor in a small and handy format has been available only since 1997. VFD (Variable-Frequency Drives) units are relatively expensive, but unit size reduction and mass production are gradually lowering costs. Modern VFDs produce the variable frequency output by a process called Pulse Width Modulation (PWM). It converts intermediate DC voltage to the synthesized AC voltage that drives the motor. Unfortunately, it is tricky to digitally produce perfect sinus waves. The PWM wave does not come anywhere near resembling a sinus wave, as can be seen in figure 4:1. The Amplitude (A) is adapted to the motor´s requirements, and the pulse width (W) is varied according to the speed requirements of the motor, and that´s it! Feeding the motor this kind of current causes great strain to the motor, and has other drawbacks as well. Digital components can of course produce sinus waves, but it is difficult to make them perfect. They generate radio frequency electrical energy because of their "jagged" appearance, as can be seen in A in figure 4:2. Radio Frequency Interference (RFI) along the cable from the VFD to the motor may exceed FCC requirements for digital equipment, especially if the installation is not carefully balanced and grounded. Imperfect sinus waves also cause strain on electrical components and wear down the insulation of motor wirings. |
![]() Figure 4:1![]() Figure 4:2
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he FLYWAY beamcars can be propelled by 3 alternative means:
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Traction, then, is only a limiting factor in the first case, i.e. when asynchronous motors for propelling the wheels are used. In this case, the slope of the beams are limited to 5o. If linear motors (LIMs) are used, traction is not a limiting factor, and the slope could be increased to 10o, possibly more.Magnetic Levitation is a technology which probably has a great future. It is as yet rather expensive. The FLYWAY® system will include MagLev if customers so desire. In this case, there are a couple of US patents that are quite promising, as regards performance and affordability. |
t is often advantageous to be able to swivel the carriage sideways 90 degrees or maybe even more. Take, for instance, the loading of motorcars at a terminus or along highways (figure 6:1), to allow motorists to hike a few miles towards their destination, while saving gas. It would take a long time of vigorous construction before the beam network reaches everywhere in a metropolitan area. So, motorists will need to take their cars along to carry them the extra miles back and forth, along the roads which the beam network does not cover. |
![]() Figure 6:1 |
Figure 6:1 shows 4 beamcars (depicted in red) lowering, swivelling, and taking on motorcars (blue) in parallel, thus speeding up the loading/unloading process. You can read about its technical functionality on this page. The FLYWAY® system will use a patented technology to swivel the cabins and other types of loads 180 degrees around. Thus, passenger could always travel facing forwards (or backwards) regardless in which direction the propulsion car is travelling. |
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The following factors influence the speed of the beamcar:
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![]() Figure 7:1
The internal radar inside the beam functions as an electronic bumper. It also has a doppler function, enabling the car to calculate the speed of an encountered car by measuring their relative speeds and knowing its own speed. The beamcar then behaves as a human driver; it regulates its own speed so that it keeps a safety distance commensurate with the current speed, i.e. the higher the speed, the longer the required distance to the car up ahead. The doppler function will in all likelihood be implemented by comparing successive measurements. For trunkbeams, we calculate with speeds upwards of 140 km/hour (corresponding to 90 miles/hour). Depending on how the obstacle detection is implemented, it has been calculated that the safety distance for that speed should be at least 120 meters. Generally, this internal radar should be able to see far enough. Long, straight beams should not present any impediment to these 120 meters. |
Figure 7:2 |
urving beams usually means that the speed will have to be reduced, thus lowering the requirements as to how far the radar has to see. Obstacle detection for FLYWAY is examined more in detail on another page.It could be that, as soon as the beam bends, the allowable maximum speed would be reduced to that commensurate with visibility inside the beam. The beamcar could be told by sensors whenever this allowed speed is altered, or the inside of the outer wall of the bending beam segment could have reflectors, telling the car´s radar that the beam is bending, and how far away this is. This speed reduction is a policy matter, however, since there is also an obstacle detction system on the carriages themselves. |
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he beamcar must (of course!) be able to brake, both in order to regulate speed and to stop at stations, and in emergency situations. There are situations such as:
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The ensuing mechanical torque is fed back to the power rail. The propulsion motor should be designed to generate enough braking torque to suffice in most cases. This not only conserves energy (by feeding it back into the power rails) but also saves on the wear of the mechanical brakes. Under certain circumstances, however, the beamcar might be required to brake at maximum force to prevent a possible accident. This "maximum force" has to take due consideration to possible passengers; an empty car could brake even harder. It is stated above about the traction motor that "It should be dimensioned to handle the emergency braking required". This means that if the electrical power is cut altogether, the beamcar will breake at a rate of approximately 2g (= 20 meters/second2). To complement this, there is also a mechanical brake, functioning in principle like the illustration at right, and applied on all four wheels of the propulsion car. |
Figure 8:1: Mechanical brake assembly |
he propulsion car cannot be designed as a rectangular wagon, with a wheel in each corner, as a regular railway bogey car.Because the beam bends and slopes here and there,
One could make 3 general designs for the propulsion car.
The one-pivot design with 2 platforms, as shown in figure 9:2 is better than the foregoing, since it provides more platform space. The lift machinery would then have to be placed on either one of these platforms. The two-pivot design, as shown in figure 9:3, is an even better solution. The optimum length L of this platform would be the length that provides the largest area, and this length is limited by:
We want the Area A = L * Wp to be as large as possible. Let´s apply some trigonometric thinking and see how big we can make A as a function of bending radius Rb and beamwidth Wb. The beam´s bending radius is properly calculated from the center of the beam, where the slit is. From the triangle in figure 9:3 we can see that:
which comes to:
Assuming a smallest bending radius of 6 meters and one of the smallest FLYWAY beamwidths of 0.80 meters, we get:
=> (Lp)2= 18.56 - 22.4*Wp - Wp2 deriving dA/dWp = 0, one gets Wp = 0.54 meters as an optimal platform width. From the equations above we get the otimum dimensions as:
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![]() Figure 9:1: One pivot point, one platform
Figure 9:2: One pivot point, two platforms
Figure 9:3: Two pivot points, one platform
Figure 9:4: Trigonometry |
| Copyright © 2004, SwedeTrack System. | Last Updated: 2007-01-17 |
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