WO2018011443A1 - Levitation, stabilisation and propulsion system for vehicles travelling through air ducts - Google Patents
Levitation, stabilisation and propulsion system for vehicles travelling through air ducts Download PDFInfo
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- WO2018011443A1 WO2018011443A1 PCT/ES2017/000099 ES2017000099W WO2018011443A1 WO 2018011443 A1 WO2018011443 A1 WO 2018011443A1 ES 2017000099 W ES2017000099 W ES 2017000099W WO 2018011443 A1 WO2018011443 A1 WO 2018011443A1
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- air
- duct
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- wagons
- means consisting
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B61—RAILWAYS
- B61B—RAILWAY SYSTEMS; EQUIPMENT THEREFOR NOT OTHERWISE PROVIDED FOR
- B61B13/00—Other railway systems
- B61B13/08—Sliding or levitation systems
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B61—RAILWAYS
- B61B—RAILWAY SYSTEMS; EQUIPMENT THEREFOR NOT OTHERWISE PROVIDED FOR
- B61B13/00—Other railway systems
- B61B13/10—Tunnel systems
Definitions
- the front and rear feed resistance is eliminated by the suction applied to the nose and the pressure on the tail of the car.
- the propulsion is carried out with a minimum energy expenditure, whereby:
- the transport is very ecological, does not pollute or produce C02.
- the levitator, stabilizer and propeller system for vehicles that circulate through air ducts, of the invention consists of a duct of circular, oval, semicircular section, of larger segment of circle, square or rectangular parallelogram by whose interior circulates wagons of equal form but of smaller section, with a separation of 0.1 cm, and IQ cm.
- the stabilization can also be achieved by applying the separation signal received by the sensors to the peripherally distributed turbines, which vary in separation depending on their rpm or with inclined air injectors that, when separated, reduce their separating action and increase it if they are comming.
- Lateral or warping stabilization is achieved by ballasting the lower part of the cars or with gyroscopes and applying the signal to electromagnets or inclined air jets that generate a reaction that straightens the vehicle. It can also be achieved by ballasting the vehicle.
- a propellant system sucking air from the front area and throwing it backwards, and blowing air into the rear area by means of fans, fans or turbines powered by electric motors and another propulsion using the magnetic wheels operated with electric motors.
- the propulsion is achieved by large fans, fans or turbines of one or multiple stages driven by electric motors.
- the suction of the compressors is used to help the propulsion, for this the air from the frontal area of the car will be sucked.
- the fans or fans are inclined to face up to suck or direct the air back and down, producing part of the lift of the car.
- Permanent magnet magnetic wheels usually ceramic, it is not necessary to apply energy to avoid the wagons, only that used by the air jets to control the separation distance between the wagons or magnetic wheels and the ferromagnetic plate.
- Permanent magnets can have any direction, it is independent, so they have to be placed parallel to each other and in the same direction.
- the rotating magnetic wheels, on the upper face of the car, to produce or increase the avoidance, are in the form of cylindrical wheels with some peripheral convexity. In these cases they will use ducts or whips of ferromagnetic matter in the area of the duct near the car. Electromagnets can also be used, but with more energy expenditure and with a tendency to stop the vehicle.
- Levitation by means of inefficient air cushions consists in preferably applying in the lower area of the car one or more curved or flat peripheral bands that adapt to the internal face of the duct of the same curved or flat surface.
- the duct plates are very porous and when pressure is applied to their inner face, they produce multiple bubbles between the two surfaces that avoid the car. Those that are placed in the upper zone can be to stabilize or control an excessive avoidance of the car.
- the turbines or sectioning fans and air insufflators pass most of the air through the interior of the car
- the turbines or suction fans and air insufflators pass most of the air on the outside of the car
- the turbines or suction and insufflator fans are applied to the duct in the area outside the duct in open circuit sections
- the turbines or suction and insufflator fans are applied in the area outside the car, with the closed circuit conduit, which is the return and reverse or opposite direction conduit.
- the car is longitudinally and transversally levitated and stabilized, which is done automatically by keeping the carriage parallel and centered inside the duct. This can be done by applying the air jets through slots directly on the internal surface of the duct, or by the different separating chambers, so that when the car approaches the duct in some area, the air pressure increases and with this is the repulsion, which automatically keeps the separation.
- the car being surrounded by the duct, creates between both and the longitudinal and transverse joints placed on the fuselage of the car, but that do not make contact with the duct, the air separating chambers, distributed longitudinally and transversely, in which it is introduced Pressurized air through injectors and / or taking advantage of the turbine air flow.
- the cameras are levitating and stabilizing, with means to maintain the calibrated distance. Air jets and lower chambers with higher pressure produce levitation and stabilization automatically.
- the longitudinal peripheral channels act in the same way.
- the air jets have two missions: One is to produce the air avoidance chambers pressurized, another create an area, the impact of the jet, which prevents or opposes the approach of the car to the duct at that point.
- the impact zone of the air jet may be increased and delimited by a non-sealed circular or rectangular flap or joint, creating an area of greater pressure than the external chamber to said delimitation.
- Air jets or injectors can control stability in every way, the lower ones also control levitation and can be larger.
- the means for keeping the wagon at a calibrated distance from the tube or the plate may consist of: a) Damper wheels, to which air jets are applied between the lower part of these and the duct, b) Chambers or separating channels of pressure, and c) Air jets applied on all faces, in this case when the duct is approached to said jets it will be automatically rejected, all the more, the more its proximity to any of them.
- a minimum of three or four jets will be used for each section.
- the air jets can also influence tangential or inclined, both transversely and longitudinally against the duct and act in such a way that the reaction is inversely proportional to the distance.
- Gyroscopes and accelerometers can control the stabilization of wagons in straight displacement and in curves, sending warp tilt signals to electromagnets that will variably attract longitudinal ferromagnetic bands or strips or to laterally inclined injectors for compensation. You can also control the separations or deviations from the longitudinal axis.
- a minimum of two to eight chambers are used, separated from each other by means of rubber, plastic or metal separating joints, the joints leave a small separation with the surface of the conduit and can be damped by means of straps placed in the area posterior to said conduit.
- the lower separating chambers of higher pressure can be partially divided into two parts by means of a longitudinal and intermediate rubber separating joint.
- the separating chambers have several cross joints in front and rear areas of the wagons. These in conjunction with the longitudinal joints, and with their particular injectors, provide better stabilization to the wagons.
- the impact zones of the pressure air jet increased and delimited by circular joints or rectangular, they can be inside or outside the separating air chambers created between the main joints
- the longitudinal joints can be placed inside the duct.
- the joints can be toroidal or fins with aerodynamic profiles.
- Four longitudinal joints can be used, or two as in figure 2.
- Limit wheels collaborate in cases of maximum displacement of the car over the duct or when it is at rest.
- the flap or flexible fins in Sa rear area allow for better automatic control of the carriage duct separation.
- Batteries or fuel cells can be applied as electric generators. Batteries are used for emergency or 3rd power failure, both for engines and for installations.
- Fuel cells are applied because they are very ecological.
- an external propulsion system consisting of blowing air in one direction of the closed duct circuit and sucking another direction in the opposite direction can be applied by Sa. Part of this air flow is captured by fans and serves to drive Sos stabilizing injectors. The flow of insufflated or suctioned air extersormen ⁇ e, besides acting as a propeller is used to drive turbines that drive generators.
- the duct has normal and emergency exit doors, conveniently spaced, you can also use areas of weakening and easy breakage.
- side ducts In the tunnels or under eS water, side ducts must be used for emergency exit. These lateral ducts may be the return line.
- the wagons can be articulated in the form of a caterpillar and can have the center of gravity at the height of the lower third of them.
- Container wagons can be used that serve to give these cylindrical exteriors and to be able to house the turbines and facilities inside it in addition to the containers to be able to levitate, stabilize and propel them.
- rectangular parallelogram section ducts can be used
- the speed can be measured by counting with Sas sensors joints of the pipe sections in a certain period of time, with which the km / h is known. Speed is equal to the length of a section by the number of sections counted.
- conduit can be totally or partially transparent
- the engines ⁇ electrical installations will try to run through external or watertight areas, so that they rarely pollute the air to be breathed. In this case, oxygen bottles or emergency systems that communicate the car with the outside could also be available.
- the duct must not be excessively consistent, except underwater, since the applied pressures are very low.
- EN air cushion ui Sizado is very efficient and has the same and very small leaks for a car that for several cars of several cars.
- the turbines will be used in pairs in counter rotation to avoid the torque.
- the ducts can run parallel or laterally parallel to each other.
- the transfer of energy to the vehicle is done without brushes, transferring it from the two conductive bands that run the duct longitudinally or at its base, by means of radiomagnetic or radiofrequency waves and also using an alternating current in which the separation between the plates Ferromagnetic and longitudinal duct bands act as capacitors and therefore allow current to flow without contact.
- the nose and tail of the car do not need to be aerodynamic or eye-shaped, it is indifferent, it can be flat and even concave.
- Emergency braking is done by reducing the rpm of the fans, and by means of electromagnets that will attract the ferromagnetic bands or bands of the ducts.
- the batteries feed the car by driving the drive motors.
- the air is filtered and conditioned before being introduced into the wagons and breathed.
- Stabilizing means can preferably be used: Uses rimmed with air bearings, wheels with air jets between them and the conduit, jets or air tongues perpendicular or inclined towards the conduit.
- the propulsion is carried out with suction or air jets sent by the turbines or with magnetic wheels driven by electric motors.
- the wagons are printed with fuel cells or by circulating alternating current through capacitors formed by longitudinal bands of the duct and Sos wagons. If the levitation fails or with the car stopped, the car rests on wheels.
- Figure 1 shows a schematic and partially sectioned view of a car and duct of the system of the invention.
- Figures 2, 3, 6, 7, 1 0 to 1 3, 1 7b and i 8 show schematic and partially sectioned views of variants of the system of the invention.
- Figures 4, 5, 8, 9 and 14 at 1, 7, 17a, 19b and 20, 25 and 33 show schematic and partially cross-sectional views of variants of wagons and ducts of the invention.
- Figure 19 shows a wheel with multiple holes to blow air and avoid contacting the tube
- Figure 19a shows a way of applying air jets to the interior of the duct.
- Figures 26 and 27 show schematic and partially cross-sectional views of duct variants and their support columns.
- Figures 28, 29 and 29a show schematic views of two variant circuits or conduits of the system of the invention.
- Figure 30 shows a caterpillar type junction of two wagons.
- Figure 3 1 shows a schematic and perspective view of a portion of duct and wagon in a station.
- the figure ⁇ It shows a plan view of a terminal with a container storage dock.
- Figure 34 shows a block diagram of one form of operation.
- Figure 6 shows a possible embodiment of the invention, with the wagon (2) of circular section that is surrounded by the conduit (1).
- the injectors ⁇ 4ab and 4bc) apply the pressurized air to the left side, to the separating chambers generated between the duct or carcass, the car and the longitudinal joints (a, b and c). Three other circular joints not shown in the figure determine a total of eight chambers.
- the left side chambers (ab and be) are shown.
- the large fans or fans (3), front and rear are propellants and with a small angle of inclination produce part of the lift or avoidance by applying the air flow to the separating chambers.
- Stabilization can be achieved by applying the separation signal received by separation sensors to the peripherally distributed turbines (3) that vary their separation according to their rprn., Or with inclined air injectors (4 ⁇ ) which when separated reduce its separating action and vice versa if they approach.
- the lower injectors are larger or send greater pressure or flow.
- Figure 1 shows the wagon (2) of circular section that is surrounded by the conduit (1). It uses a large front fan (3) and a rear fan which force the air between the rifle's fuselage of the car and the duct (1). The forward can be placed on the tip of the nose. Carry some fins or circular joints around the fuselage of the car in the middle and rear front area (l Of, 10m and l Or). Which create two chambers longitudinally, which by adding four longitudinal joints produces eight chambers, which are used to levitate and stabilize the fuselage of the car.
- Figure 2 shows the wagon (2) of circular section that is surrounded by the conduit (1). It uses four large front fans (3) and other rear fans which force the air between the monocoque fuselage of the car and the duct (1).
- the car has a recess in its peripheral area except in its front and rear area where it carries annular projections or can carry joints.
- Figure 3 shows the wagon (2) of circular section that is surrounded by the conduit (1).
- air can be passed between the car and the duct.
- the duct is tongue and groove (1 1 ⁇ with the toroidal joint (12).
- Emergency braking is done with the electromagnets (29). It shows the levitating and stabilizing channels (15). In the upper zone fos (1 5s) which are Smaller and just stabilizers.
- Figure 4 shows the wagon (2) of circular section that is surrounded by the conduit (1) similar to that of Figure 2 adding other elements. It uses four large front fans (3), four longitudinal joints (a, b, c and d) creating between them, the fuselage and the duct the separating chambers (ab, be, cd and da) in which they discharge the air injectors (4ab , 4bc, 4cd and 4da) respectively and other rear injectors which force the air between said jaws, and that with the flow sent by the front fans generate the separation forces Fab, Fbc, Fcd and Fda respectively.
- the lower two are levitating, stabilizing and older.
- the injectors sort greater or are flows. The upper ones are only stabilizing and add to the weight of the car.
- the separating chambers (ab, be, cd and da) are further subdivided into eight, due to the three circular joints around the fuselage. The same happens with the forces. Add the peripheral stabilizing electromagnets (12).
- Figure 5 shows the wagon (2) of circular section that is surrounded by the conduit (1) similar to that of Figure 2 adding other elements. It uses four large front fans (3) and four longitudinal joints (a, b, e and d) creating between them, the fuselage and the duct the separating chambers (ab, be on the left side and the cd, on the right). Add the limit or support wheels (6) in the lower zone for low speed and rest.
- Figure 7 shows the wagon (2) of circular section that is surrounded by the conduit (1). It uses a large front fan (3a) and another rear which suck the air inside the car. It is similar to that in Figure 3.
- the air between the car and the duct can be applied by injectors.
- Add four longitudinal joints, on the left side are shown the (a, b, c) creating between them, the fuselage and the duct the separating chambers.
- Three other circular joints not shown in the figure determine a total of eight chambers.
- the lateral chambers of (to the left (ab and be) are shown.
- the injectors (4ab and 4bc) apply the pressurized air in the left lateral area to the separating chambers generated between the duct and wagon.
- Figure 8 shows the wagon (2) of circular section that is surrounded by the conduit (1).
- a large front fan (3a) and a rear fan which propel and suck the air inside the car.
- the air is preferentially applied or only by the lower zone to produce the excitation, in a channel between the car and the duct.
- the stabilizer air injectors of the car are not shown, which will be distributed over three or four points around the car.
- Figure 9 shows the wagon (2) of circular section that is surrounded by the conduit (1). It uses as magnetic levitators the wheels (7) that are retracted by the longitudinal ferro-magnetic bands (8). Shows the wheels (6) damping or low speed, which is maintained separated by air jets applied between its lateral, front and rear areas and the duct, automatically acting as stabilizers. It shows in the lower zone Sos levitator channels and stabilizers (1 5) and in the upper zone the stabilizers (1 Ss).
- Figure 10 shows the wagon carrier (2p) of circular section that is surrounded by the conduit (I), inside it carries the containers (20). It uses four large front fans (3 ⁇ ) and another four rear which fix in the air between the [monocoque fuselage of the car and the duct (I).
- the duct is tongue and groove (1 i) with the toroidá ⁇ joint (12).
- Figure 1 S shows the container carriage (2p) of circular section that is surrounded by the duct (i). Inside it carries the containers (20). It uses a large front fan (3p) and another rear which force the air between the monocoque fuselage of the car and the duct (1).
- Figure 12 shows the wagon (2) of circular section that is surrounded by the conduit (1). Inside it carries the containers (20). It uses a large front fan (3p) and another rear which suck the air inside the container car. The air between the car and the duct is not shown in the figure.
- Figure 13 shows the wagon (2p) of circular section that is surrounded by the conduit (1), inside it carries the containers (20).
- the car is driven by turbines or impeller pumps external to said car.
- the air flow is driven as per ; show by white or contoured arrows.
- a compressor (21) provides air flow to the injector consoles of the separation or stabilization of the car with respect to the duct.
- Figure 14 shows the wagon (2p) of circular section that is surrounded by the conduit (1). Inside it carries the containers (20). The container wagon carries between its periphery and Sos containers some cameras that in this case are used to house the turbines (3p), in addition to facilities, etc.
- Figure 1 5 shows the wagon (2p) of circular section that is surrounded by the conduit (1). Inside it carries the containers (20). The container wagon carries between its periphery and Sos containers some cameras that in this case are used to house the turbines (3p), wheels (6p), in addition to facilities, etc.
- Figure 16 shows the carriage (2) of circular section that is surrounded by the conduit (1). It has two longitudinal cavities in the upper zone in which a forced air flow circulates through Sos fanes or stabilizing fans (3S), two in the front area and two in the rear. In the lower zone it has two longitudinal cavities, mainly levitating and, secondly, stabilizers in which the flow of air operated by the fans (3L), two front and two rear, circulates.
- the vectors show the stabilizing and sustaining forces applied (FS and FL).
- Figure 17 shows the wagon (2) of circular section that is surrounded by the conduit (1). It has three longitudinal cavities in the middle and upper zone in which a forced air flow circulates through the fans or stabilizing fans (38), and another three in the rear, In the lower zone it presents a longitudinal cavity mainly levitating and in the second term non stabilizer in the which circulates the air flow driven by the large fan (3L) and another in the rear area.
- the vectors show the stable lifting and sustaining forces; applied (FS and FL).
- Figure 1 7a shows the wagon (2) of circular section that is surrounded by the conduit (1). It uses levitation by air bearings, blowing pressurized air through the duct (30) the chamber (3 S) adjacent to the porous plate (32) that produces multiple air bubbles in its face in contact with the vehicle.
- the camera (33) is free in the case of the fall of an object in the internal zone.
- the wheel (6s) limits its upper travel but does not touch by having air jets between the wheel and the duct.
- Figure 17b shows the duct (I) the car (2) with a stabilization system in the nose and the car's tail in Sos that the longitudinal rudders (13) are inclined with the electromagnets (12) tilting on the kneecaps ( 14) depending on the separation signals sent by four sensors.
- Figure 1 8 shows the duct (1) and inside the car (2r) covered its surface by multiple fins tilted back (24r), which once guided by the cameras and levitator injectors, contribute, centering the car in the duct.
- Figure 19 shows the tubular rail (1), and in its inner zone Sa wheel (oj) which does not touch the duct due to air jets (62) through multiple holes in the wheel and jets ( 61) between the wheel and the upper housing (60) that surrounds and covers it,
- Figure 19a shows the ducts (70) and other verticals that apply the air jets (71 and 72) into the duct (I).
- Figure 19b shows the duct (1), inside the car (2) levitated by magnetic wheels (7) that attract the rail if it is ferromagnetic or to the band (8) and stabilized with the wheels (6a) with inetetic bearings. air. They can be used for low and medium speeds. For higher speeds, the wheels (6s) can be used with air jets between wheels and duct. The two bands (8) of the electric conduction can be used.
- Figure 20 shows an oval duct (I v) and oval wagon (2v), showing the longitudinal joints (a, b, c and d).
- Figure 2 1 shows a semicircular duct (I s) and semi-circular wagon (2s).
- Figure 22 shows a circular sector duct of about 270 ° (I g) and circular sector wagon of about 270 ° (2g).
- Figure 23 shows a rectangular duct (3 r) and rectangular wagon (2r).
- Figure 24 shows a trapezoidal section duct (I t) and trapezoidal car (2r). You can carry the joints in a similar way to figure 23.
- Figure 25 shows an open and U-shaped conduit 21 r) and wagon or container carrier (2r).
- Figure 26 shows a form of support for the ducts (1) by means of the carias stockings (26) and these are in turn ?, with the columns (27).
- Figure 27 shows a form of duct support (I) by means of the half rods (26) and you are in turn with the columns (27). Add the duct (28) ⁇ ii to carry the facilities and to move cars or maintenance personnel. All three carry the corresponding access gates to the main ducts.
- Figure 28 shows a possible closed circuit with a one-way car on (2) and another on the back (2a).
- the pumps (1 7 and 1 7a) drive the wagons by sending an air jet behind Sos themselves and sucking from their frontal zone in which the valves (1 9 and 19a) and Sos ducts (1 8 and 1 8a) intervene , which close, stopping sucking when the car approaches the area.
- Figure 29 shows a one-way circuit variant on (2b) and a return one on (2e).
- the pumps (1 7b and 17c) drive the wagons by sending an air ciorior behind them and sucking from their frontal zone in which the valves (1 9 and 19a) intervene, which close, stopping sucking when the car is Approaches the area.
- Figure 29a shows a variant of circuit or conduit (i) in e3 which is applied pressurization and external suction by sections by means of the pump or compressor (1 7d). Pressure air is applied through the rear area of the car (2d) and front suction until the car reaches the point at T or junction with the duct at which time the sections between the T and the valve are slightly compressed and open the valve (19d) forward and until it goes to the next section where this action is repeated automatically.
- Figure 30 shows the union (22) type fuel le or caterpillar, between two wagons (1).
- Figure 3 1 shows the conduit (1) with the door ⁇ 1 p) open at a station at the moment when the car door (2p) is in front of it.
- a staircase with steps (1 c) facilitates the descent and rise of passengers.
- Figure 32 shows the arrival duct (1), going up a ramp (23) for its deceleration in a load terminal and once stopped changes direction and is stored in the storage tracks (24).
- the arrows show the itinerary.
- Figure 33 shows the duct (i) and between the east and the car (2) a special duct (li) formed by longitudinal grooves or by longitudinal or transverse valves, which close the passage of air during suction and open them in emergency when pressing the car on the front air.
- the figure does not show the slots or the valves.
- Figure 34 shows a microprocessor that processes the signals of: Gyroscopes, accelerometers, four front and four rear separation sensors, gas control, brakes, front and rear area weight, or duct rupture, detected by changes in pressure along it.
- the microprocessor provides and sends multiple and repetitive signals: Four front stabilization control and four other front and rear zone levitation signals sent to injectors, fin actuators or electromagnets and fault warning signals. system, speed control, braking, propulsion and speed indication.
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Abstract
The invention relates to a levitation, stabilisation and propulsion system for vehicles travelling through air ducts, consisting of a duct through which carriages travel, said carriages having the same shape as the duct, but a smaller cross-section. The duct and the carriages are separated by between 0.1 and 10 cm by levitation means using separating air chambers or channels, air jets, distributed both longitudinally and transversely, of the air cushion type. The invention also comprises an air suction- and insufflation-based propulsion system using fans, blowers or turbines actuated with electric motors, and automatic stabilisation systems using peripheral air jets, adding to the stabilisation provided by means of suction and insufflation. A secondary propulsion, levitation and stabilisation system can be also be added, of the type using rotating permanent magnets actuated by electric motors.
Description
SISTEMA LEVITADOR, ESTABILIZADOR Y PROPULSOR PARA VEHICULOS QUE CIRCULAN POR CONDUCTOS DE AIRE LEVITATOR, STABILIZER AND PROPULSOR SYSTEM FOR VEHICLES THAT CIRCULATE BY AIR DUCTS
CAMPO DE LÁ INVENCIÓN.- En vehículos de transporte terrestre de viajeros y de mercancías de muy aíís velocidadl , evitado por colchón de aire, ruedas magnéticas, chorros de aire, coj inetes de aire y/o ruedas periféricas con chorros de aire entre dichas ruedas y conducto. FIELD OF INVENTION.- In land transport vehicles of passengers and merchandise of very high speed, avoided by air mattress, magnetic wheels, air jets, air cushions and / or peripheral wheels with air jets between said wheels and duct.
OBJETIVO DE LA INVENCIÓN Y VENTAJAS. OBJECTIVE OF THE INVENTION AND ADVANTAGES.
Obtener un vagón ultrarrápido, sencillo, que puede colocarse en todo tipo de terreno, sobre el suelo, soterrado, elevado sobre columnas en zonas arenosas, agua, etc. El morro y la cola del vagón no necesitan adoptar forma aerodinámica u ojival, es indiferente, puede ser plana e incluso cóncava. Puede ser ultraligero. Obtain an ultra-fast, simple car that can be placed on all types of terrain, on the ground, underground, raised on columns in sandy areas, water, etc. The nose and tail of the wagon do not need to take an aerodynamic or ogival shape, it is indifferent, it can be flat and even concave. It can be ultralight.
Aportar un sistema económico que no descarrila, no le afectan ios vientos, el polvo, la arena, ni la meteorología y puede competir con el avión en todo tipo de trayectos. Inicial mente se podtia usar para transportar carga. Provide an economic system that does not derail, is not affected by winds, dust, sand, or weather and can compete with the plane on all types of routes. Initially it could be used to transport cargo.
La resistencia frontal y trasera al avance se eliminan por la succión aplicada al morro y la presión en la cola del vagón. The front and rear feed resistance is eliminated by the suction applied to the nose and the pressure on the tail of the car.
Utiliza los más sencillos, simples y económicos métodos del evitación. Use the simplest, simplest and cheapest methods of avoidance.
Tiene la menor resistencia de fricción. It has the lowest friction resistance.
Aprovecha la mayor parte de la energía aplicada. (Por realizarse todo en un recinto aislado del exterior. Avalado esto por la mecánica de fluidos.) Take advantage of most of the energy applied. (Because everything is done in an enclosure isolated from the outside. Endorsed by fluid mechanics.)
La propulsión se realiza con un mínimo gasto de energía, Por lo cual : The propulsion is carried out with a minimum energy expenditure, whereby:
Tiene el mínimo eoste por kg. transportado. It has the minimum eoste per kg. transported
Tiene un m ínimo gasto de energía It has a minimum energy expenditure
El trasporte es muy ecológico, no contamina, ni produce C02. The transport is very ecological, does not pollute or produce C02.
Permite alcanzar muy altas velocidades. It allows to reach very high speeds.
Sube con facilidad las pendientes Easily climb the slopes
(Sin competencia en todo lo anterior). (Without competition in all of the above).
ESTADO DE LÁ TÉCNICA. Los sistemas de levitación por colchón de aire o magnéticos actuales no son prácticos, son difíciles de alimentar con energía externa al vagón, util izan vías muy caras y no adquieren muy alia velocidad. Además los de levitación magnética necesitan adquirir 1 00 km/h para que la levitación empiece a surtir efecto. Pretenden util izar tubos de vacío, los cuales reduceln a resistencia pero son sistemas más caros, peligrosos y difíciles de estabil izar. La presente invención soluciona dichos problemas ya que se aprovecha casi la total idad de la energía aplicada, los tipos de levitación apl icados son muy sencillos y económicos, y se obtienen altísimas velocidades. STATE OF TECHNICAL LAW. Current air cushion or magnetic levitation systems are not practical, they are difficult to feed with energy external to the car, use very expensive tracks and do not acquire very high speed. In addition, magnetic levitation needs to acquire 1 00 km / h for levitation to begin to take effect. They intend to use vacuum tubes, which reduce resistance but are more expensive, dangerous and difficult to stabilize systems. The present invention solves these problems since almost the totality of the energy applied is used, the types of levitation applied are very simple and economical, and very high speeds are obtained.
PROBLEMA A RESOLVER. Los aviones despilfarran mucha energía, sufren o son muy afectados por los fenómenos meteorológicos y son muy contaminantes. Los trenes tienen muchos problemas de velocidad por el gran rozam iento que sufren sus ruedas, y en el caso de los Sevkados, sus vías son excesivamente caras. Todo ello se resuelve con la presente invención.
DESCRIPCIÓN DE LÁ INVENCIÓN.- El sistema levitador, estabilizador y propulsor para vehículos que circulan por conductos de aire, de la invención, consiste en un conducto de sección circular, ovalada, semicircular, de segmento mayor de circulo, de cuadrado o paralelogramo rectángulo por cuyo interior circulan unos vagones de igual forma pero de menor sección, con una separación de 0.1 cm, y I Q cm . aproximadamente entre conducto y vagones, con unos sistemas de levitaciórs de cámaras de aire y otro de canales de aire presurizados, ambos del tipo de colchón de aire, distribuidos longitudinal y transversamente por ia periferia de ios vagones, un sistema de lev ilación con ruedas magnéticas giratorias, un sistema de levitación utilizando la corriente de aire utilizada en la propulsión de ios vagones en ia zona inferior entre vagón y conducto, un sistema de levitaciórs tipo cojinetes neumáticos, unos sistemas de levitación utilizando chorros de aire perpendiculares o inclinados hacia el conducto y levitación mediante unas ruedas periféricas con unos chorros de aire entre ia superficie de ia rueda y el conducto, que no perm iten su contacto. Con unos sistemas de estabilización utilizando las cámaras de aire y otro de canales de aire presurizados tipo colchón de aire, mediante ruedas magnéticas giratorias, con 3a corriente de aire util izada en la propulsión, con ios coj inetes de aire, con los chorros de aire perpendiculares o inclinados hacia el conducto, con las ruedas periféricas que portan chorros de aire entre estas y el conducto, con electroimanes que atraen al conducto y con múltiple aletas distribuidas incl inadas hacia atrás y el exterior, alrededor del vehículo, unas aletas que defiectan la corriente de aire, un buje o aleta en el morro y otro en la cola, que pueden desviar el aire en todas las direcciones, incl inando las turbinas periféricas, variando las rpm de algunas de los fanes periféricos, variando el flujo de los chorros de aire. La estabil ización también se puede conseguir aplicando la señal de separación recibida por los sensores a las turbinas distribuidas periféricamente, las cuales varían su separación en función de sus rpm o con unos inyectores de aire inclinados que al separarse reducen su acción separadora y la aumentan si se aproximan. La estabilización lateral o de alabeo se consigue lastrando la zona inferior de ios vagones o con giróscopos y apl icando la señal a unos electroimanes o chorros de aire incl inados que generan una reacción que endereza al vehículo. También se puede conseguir lastrando el vehículo. La mayoría son de estabilización automática cuando se aproxima excesivamente conducto y vagón. Un sistema propulsor succionando aire de la zona delantera y lanzándolo hacia atrás, e insuflando aire en ia zona posterior mediante fanes, ventiladores o turbinas accionados con motores eléctricos y otro de propulsión uti lizando las ruedas magnéticas actuadas con motores eléctricos. PROBLEM TO SOLVE. Airplanes squander a lot of energy, suffer or are very affected by weather events and are very polluting. Trains have many speed problems due to the large friction suffered by their wheels, and in the case of the Sevkados, their tracks are excessively expensive. All this is resolved with the present invention. DESCRIPTION OF THE INVENTION.- The levitator, stabilizer and propeller system for vehicles that circulate through air ducts, of the invention, consists of a duct of circular, oval, semicircular section, of larger segment of circle, square or rectangular parallelogram by whose interior circulates wagons of equal form but of smaller section, with a separation of 0.1 cm, and IQ cm. approximately between ducts and wagons, with levitation systems of air chambers and another of pressurized air channels, both of the type of air cushion, distributed longitudinally and transverse by the periphery of the wagons, a levilating system with magnetic wheels rotating, a levitation system using the air flow used in the propulsion of the wagons in the lower area between the car and duct, a system of pneumatic bearing type levitation, some levitation systems using air jets perpendicular or inclined towards the duct and levitation by peripheral wheels with air jets between the surface of the wheel and the duct, which do not allow contact. With stabilization systems using the air chambers and another of pressurized air cushions air channels, by means of rotating magnetic wheels, with the 3rd current of air used in the propulsion, with the inefficient air cushions, with the air jets perpendicular or inclined towards the conduit, with the peripheral wheels that carry air jets between them and the conduit, with electromagnets that attract the conduit and with multiple distributed fins inclined backwards and outside, around the vehicle, fins that defy the air flow, a bushing or fin on the nose and another on the tail, which can divert the air in all directions, including peripheral turbines, varying the rpm of some of the peripheral fans, varying the flow of the jets of air. The stabilization can also be achieved by applying the separation signal received by the sensors to the peripherally distributed turbines, which vary in separation depending on their rpm or with inclined air injectors that, when separated, reduce their separating action and increase it if they are comming. Lateral or warping stabilization is achieved by ballasting the lower part of the cars or with gyroscopes and applying the signal to electromagnets or inclined air jets that generate a reaction that straightens the vehicle. It can also be achieved by ballasting the vehicle. Most are automatic stabilization when the duct and wagon are approached excessively. A propellant system sucking air from the front area and throwing it backwards, and blowing air into the rear area by means of fans, fans or turbines powered by electric motors and another propulsion using the magnetic wheels operated with electric motors.
La propulsión se consigue mediante grandes ventiladores, fanes o turbinas de una o múltiples etapas accionados por motores eléctricos. Simultáneamente se aprovecha la succión de los com presores para ayudar a la propulsión, para ello se succionará el aire de la zona frontal del vagón. Si se desea, a los fanes o ventiladores se les da inc linación morro arriba para que succionen o dirijan el aire hacia atrás y hacia abajo, produciendo parte de la sustentación del vagón. Con estos sistemas de propulsión prácticamente no existe rozamiento por flotar o estar ievitado el vagón y se evitan las pérdidas que se producen en los vehículos que se mueven o apoyan en un fluido, en ios cuales se pierde como m ínimo el 50% de ia energía aplicada por las hélices.
Usando ruedas magnéticas de imanes permanentes, generalmente cerámicos, no hay que aplicar energía paral evitar ios vagones, tan solo la utilizada por los chorros de aire para controlar la distancia de separación entre ios vagones o ruedas magnéticas y la plancha ferromagnétíea. Los imanes permanentes pueden tener una dirección cualesquiera, es independiente, tan solo que hay que colocarlos paralelos entre sí y con el mismo sentido. Las ruedas magnéticas giratorias, en la cara superior del vagón, para producir o incrementar lal evitación, tienen forma de ruedas cilindricas con cierta convexidad periférica. En estos casos usarán conductos o batidas de materia l ferromagnético en la zona del conducto próxima al vagón. También se pueden uti lizar electroimanes, pero con más gasto de energía y con tendencia a frenar al vehícuta. The propulsion is achieved by large fans, fans or turbines of one or multiple stages driven by electric motors. At the same time, the suction of the compressors is used to help the propulsion, for this the air from the frontal area of the car will be sucked. If desired, the fans or fans are inclined to face up to suck or direct the air back and down, producing part of the lift of the car. With these propulsion systems, there is practically no friction due to floating or the car being avoided and the losses that occur in vehicles that move or rely on a fluid are avoided, in which at least 50% of the energy is lost applied by the propellers. Using permanent magnet magnetic wheels, usually ceramic, it is not necessary to apply energy to avoid the wagons, only that used by the air jets to control the separation distance between the wagons or magnetic wheels and the ferromagnetic plate. Permanent magnets can have any direction, it is independent, so they have to be placed parallel to each other and in the same direction. The rotating magnetic wheels, on the upper face of the car, to produce or increase the avoidance, are in the form of cylindrical wheels with some peripheral convexity. In these cases they will use ducts or whips of ferromagnetic matter in the area of the duct near the car. Electromagnets can also be used, but with more energy expenditure and with a tendency to stop the vehicle.
La levitación mediante coj inetes de aire consiste en aplicar preferentemente en ia zona inferior del vagón una o más bandas periféricas curvas o planas que se adaptan a Sa cara interna del conducto de igual superficie curva o plana. Las placas del conducto son muy porosas y al aplicarles la presión er¡ su cara interna producen múltiples burbujas entre ambas superficies quel evitan el vagón. Las que se colocan en la zona superior pueden ser para estabilizar o controlar una excesival evitación del vagón. Levitation by means of inefficient air cushions consists in preferably applying in the lower area of the car one or more curved or flat peripheral bands that adapt to the internal face of the duct of the same curved or flat surface. The duct plates are very porous and when pressure is applied to their inner face, they produce multiple bubbles between the two surfaces that avoid the car. Those that are placed in the upper zone can be to stabilize or control an excessive avoidance of the car.
Se usan varios sistemas los cuales se pueden simultanear y utilizar, complementándose entre si. Several systems are used which can be combined and used, complementing each other.
Se usan cuatro modos de operación: a) Las turbinas o venti ladores seccionadores e insufladores de aire hacen pasar la mayor parte del aire por el interior del vagón, b) Las turbinas o ventiladores succionadores e insufladores de aire hacen pasar ia mayor parte del aire por el exterior del vagón, c) Las turbinas o ventiladores succionadores e insufladores se aplican al conducto en la zona externa al conducto en tramos en circuito abierto y d) Las turbinas o ventiladores succionadores e insufladores se aplican en la zona externa al vagón, con el conducto en circuito cerrado, eS cual lo constituyen el conducto de ida y el de vuelta o de sentido contrario. Simultáneamente se levita y estabiliza longitudinal y íransversal¡r¡ente el vagón, lo cual se hace automáticamente haciendo que el vagón se mantenga paralelo y centrado en el interior del conducto. Esto se puede realizar aplicando los chorros de aire por unas ranuras directamente sobre la superficie interna del conducto, o bien por las distintas cámaras separadoras, de modo que cuando el vagón se acerca al conducto en alguna zona, la presión del aire se incrementa y con ello la repulsión, con lo cual se mantiene automáticamente ia separación. Four modes of operation are used: a) The turbines or sectioning fans and air insufflators pass most of the air through the interior of the car, b) The turbines or suction fans and air insufflators pass most of the air on the outside of the car, c) The turbines or suction and insufflator fans are applied to the duct in the area outside the duct in open circuit sections and d) The turbines or suction and insufflator fans are applied in the area outside the car, with the closed circuit conduit, which is the return and reverse or opposite direction conduit. Simultaneously, the car is longitudinally and transversally levitated and stabilized, which is done automatically by keeping the carriage parallel and centered inside the duct. This can be done by applying the air jets through slots directly on the internal surface of the duct, or by the different separating chambers, so that when the car approaches the duct in some area, the air pressure increases and with this is the repulsion, which automatically keeps the separation.
El vagón al ser circundado por el conducto, crea entre ambos y las juntas longitudinales y transversales colocadas sobre el fuselaje del vagón, pero que no hacen contacto con el conducto, las cámaras separadoras de aire, distribuidas longitudinal y transversaimente, enl as que se introduce aire a presión mediante inyectores y/o aprovechando el flujo de aire de las turbinas. Las cámaras son levitadoras y estabilizadoras, disponiendo de medios para mantener la distancia calibrada. Los chorros de aire y las cámaras inferiores con mayor presión producen la levitación y estabilización de forma automática. Los canales periféricos longitudinales actúan de igual forma. The car being surrounded by the duct, creates between both and the longitudinal and transverse joints placed on the fuselage of the car, but that do not make contact with the duct, the air separating chambers, distributed longitudinally and transversely, in which it is introduced Pressurized air through injectors and / or taking advantage of the turbine air flow. The cameras are levitating and stabilizing, with means to maintain the calibrated distance. Air jets and lower chambers with higher pressure produce levitation and stabilization automatically. The longitudinal peripheral channels act in the same way.
Aunque se aplica aire, a presión a cada una de las cámaras separadoras y a los canales, parte del aire presisrízado circula entre las distintas cámaras o canales. Although air is applied, under pressure to each of the separating chambers and to the channels, part of the pressurized air circulates between the different chambers or channels.
Los chorros de aire tienen dos m isiones: Una es producir las cámarals evitadoras de aire
presurizado, otra crear una zona, la de impacto del chorro, que evita o se opone a la aproximación del vagón al conducto en dicho punto. La zona de impacto del chorro de aire puede estar incrementada y delimitada por una aleta o junta circular o rectangular no estanca, creando una zona de mayor presión que 3a cámara externa a dicha delimitación. Los chorros de aire o ios inyectores pueden controlar la estabilidad en todos los sentidos, los inferiores además controlan la levitación y pueden ser mayores. The air jets have two missions: One is to produce the air avoidance chambers pressurized, another create an area, the impact of the jet, which prevents or opposes the approach of the car to the duct at that point. The impact zone of the air jet may be increased and delimited by a non-sealed circular or rectangular flap or joint, creating an area of greater pressure than the external chamber to said delimitation. Air jets or injectors can control stability in every way, the lower ones also control levitation and can be larger.
Los medios para mantener al vagón a una distancia calibrada del tubo o la plancha pueden consistir ers: a) Ruedas amortiguadoras, a las que se les apl ican chorros de aire entre ia zona inferior de estas y el conducto, b) Cámaras o canales separadores de presión, y c) Chorros de aire aplicados sobre todas las caras, en este caso al acercarse el conducto a dichos chorros será rechazado automáticamente, tanto más, cuanto más sea su proximidad a alguno de ellos. Se usarán un mínimo de tres o cuatro chorros por cada tramo. Los chorros de aire también pueden incidir tangenciales o inclinados, tanto transversal como longitudinalmente contra el conducto y actúan de tal modo que la reacción es inversamente proporcional a la distancia. The means for keeping the wagon at a calibrated distance from the tube or the plate may consist of: a) Damper wheels, to which air jets are applied between the lower part of these and the duct, b) Chambers or separating channels of pressure, and c) Air jets applied on all faces, in this case when the duct is approached to said jets it will be automatically rejected, all the more, the more its proximity to any of them. A minimum of three or four jets will be used for each section. The air jets can also influence tangential or inclined, both transversely and longitudinally against the duct and act in such a way that the reaction is inversely proportional to the distance.
Debido a la gran precisión y pequeña separación entre el conducto y las cubiertas de las cámaras de aire, las fugas de aire y ia baja presión utilizada son pequeñas, y la energía necesaria para mantener el vagón suspendido es mínima. Due to the high precision and small separation between the duct and the covers of the air chambers, the air leaks and the low pressure used are small, and the energy required to keep the wagon suspended is minimal.
Teniendo el centro de gravedad por debajo del conducto, el vagón se mantiene estabilizado y actúa pendular y automáticamente en las curvas y durante su desplazam iento lineal. Unos giróscopos y acelerómetros pueden controlar ia estabil ización de los vagones en desplazamiento recto y en las curvas, enviando señales de inclinación de alabeo a unos electroimanes que atraerán de forma variable las bandas o franjas ferromagnétícas longitudinales o a unos inyectores inclinados lateralmente para su compensación. También se pueden controlar las separaciones o desvíos respecto al eje longitudinal. With the center of gravity below the duct, the car remains stabilized and acts pendulously and automatically in the curves and during its linear displacement. Gyroscopes and accelerometers can control the stabilization of wagons in straight displacement and in curves, sending warp tilt signals to electromagnets that will variably attract longitudinal ferromagnetic bands or strips or to laterally inclined injectors for compensation. You can also control the separations or deviations from the longitudinal axis.
Se utilizan un mínimo de dos a ocho cámaras, separadas entre si mediante juntas separadoras de goma, plástico o metal, las juntas dejan una pequeña separación con ia superficie del conducto y pueden estar amortiguadas mediante unos flejes colocados en la zona posterior a dicho conducto. Las cámaras separadoras inferiores de mayor presión pueden estar parcialmente divididas en dos partes mediante una junta separadora de goma longitudinal e intermedia, Las cámaras separadoras presentan varias juntas transversales ers zonas delanteras y traseras de los vagones. Estas en conjunción con las juntas longitudinales, y con sus inyectores particulares, proporcionan una mejor estabilización a los vagones. Una variante, en lugar de juntas, utiliza unos salientes o resaltes del mismo material en la superficie del vagón o unos rebajes en la zona periférica central, figura 2. Las zonas de impacto del chorro de aire de presión incrementadas y delimitadas por juntas circulares o rectangulares, pueden estar dentro o fuera de las cámaras de aire separadoras creadas entre las juntas principales Las juntas longitudinales pueden colocarse en el interior del conducto. Las juntas pueden ser toroidales o aletas con perfiles aerodinámicos. Pueden utilizarse cuatro juntas longitudinales, o dos como en figura 2. A minimum of two to eight chambers are used, separated from each other by means of rubber, plastic or metal separating joints, the joints leave a small separation with the surface of the conduit and can be damped by means of straps placed in the area posterior to said conduit. The lower separating chambers of higher pressure can be partially divided into two parts by means of a longitudinal and intermediate rubber separating joint. The separating chambers have several cross joints in front and rear areas of the wagons. These in conjunction with the longitudinal joints, and with their particular injectors, provide better stabilization to the wagons. A variant, instead of joints, uses projections or projections of the same material on the surface of the car or recesses in the central peripheral area, figure 2. The impact zones of the pressure air jet increased and delimited by circular joints or rectangular, they can be inside or outside the separating air chambers created between the main joints The longitudinal joints can be placed inside the duct. The joints can be toroidal or fins with aerodynamic profiles. Four longitudinal joints can be used, or two as in figure 2.
Unas ruedas de límite colaboran en los casos de desplazamiento máximo del vagón sobre el conducto o cuando se haya en reposo.
La aleta o aletas flexibles en Sa zona posterior perm iten un mejor control automático de la separación conducto vagón. Limit wheels collaborate in cases of maximum displacement of the car over the duct or when it is at rest. The flap or flexible fins in Sa rear area allow for better automatic control of the carriage duct separation.
Pueden aplicarse pilas o células de combustible como generadores eléctricos. Se usan baterías para emergencia o fallo de 3a alimentación eléctrica, tanto para motores como para las instalaciones. Batteries or fuel cells can be applied as electric generators. Batteries are used for emergency or 3rd power failure, both for engines and for installations.
Se aplican células de combustible por ser muy ecológicas. Fuel cells are applied because they are very ecological.
Además de la propulsión incorporada en el vagón, se puede aplicar un sistema de propulsión externo consistente en insuflar aire en una dirección del circuito cerrado del conducto y succionar por Sa otra dirección en sentido contrario. Parte de este flujo de aire se capta mediante fanes y sirve para accionar Sos inyectores estabilizadores. El flujo de aire insuflado o succionado extersormeníe, además de actuar como propuEsor se aprovecha para accionar turbinas que accionan generadores. In addition to the propulsion incorporated in the car, an external propulsion system consisting of blowing air in one direction of the closed duct circuit and sucking another direction in the opposite direction can be applied by Sa. Part of this air flow is captured by fans and serves to drive Sos stabilizing injectors. The flow of insufflated or suctioned air extersormeníe, besides acting as a propeller is used to drive turbines that drive generators.
El conducto dispone de puertas de salida normales y de emergencia, espaciadas convenientemente, también puede utilizar zonas de debilitam iento y de fácil rotura. The duct has normal and emergency exit doors, conveniently spaced, you can also use areas of weakening and easy breakage.
En los túneles o bajo eS agua deben utilizarse conductos laterales para salida en caso de emergencia. Esos conductos laterales pueden ser ios de Sa linea de retorno. In the tunnels or under eS water, side ducts must be used for emergency exit. These lateral ducts may be the return line.
Los vagones pueden estar articulados en forma de oruga y pueden tener el centro de gravedad a la altura del tercio inferior de ios mismos. The wagons can be articulated in the form of a caterpillar and can have the center of gravity at the height of the lower third of them.
Se pueden utilizar vagones portacontenedores que sirven para dar exteriormerste a estos la forma cilindrica y poder alojar en su interior además de los contenedores las turbinas e instalaciones para poder leviíarlos, estabilizarlos y propulsarlos. Como alternativa se pueden utilizar conductos de sección de paralelogramo rectángulo Container wagons can be used that serve to give these cylindrical exteriors and to be able to house the turbines and facilities inside it in addition to the containers to be able to levitate, stabilize and propel them. Alternatively, rectangular parallelogram section ducts can be used
La velocidad se puede medir contando con sensores Sas uniones de los tramos de tubos en un determinado periodo de tiempo, con lo cual se sabe los km/h. Velocidad es igual a longitud de un tramo por el número de tramos contados. The speed can be measured by counting with Sas sensors joints of the pipe sections in a certain period of time, with which the km / h is known. Speed is equal to the length of a section by the number of sections counted.
Para los viajeros se pueden utilizar vistas exteriores por televisión, o el conducto puede ser total o parcialmente transparente For exterior travelers, television views can be used, or the conduit can be totally or partially transparent
Los motores ε instalaciones eléctricas se procurará discurran por zonas externas o estancas, con el fin de que rao contaminen el aire que hay que respirar. En este caso también se podría disponer de botetlas de oxígeno o sistema de emergencia que comunicasen el vagón con el exterior. The engines ε electrical installations will try to run through external or watertight areas, so that they rarely pollute the air to be breathed. In this case, oxygen bottles or emergency systems that communicate the car with the outside could also be available.
ES conducto no debe ser excesivamente consistente, excepto bajo el agua, ya que las presiones aplicadas son muy bajas. The duct must not be excessively consistent, except underwater, since the applied pressures are very low.
ES colchón de aire uíi Sizado es muy eficiente y tiene las m ismas y muy pequeñas fugas para un vagón que para urs convoy de varios vagones. EN air cushion ui Sizado is very efficient and has the same and very small leaks for a car that for several cars of several cars.
Se usarán las turbinas por parejas en contrarrotación para evitar el par de giro. The turbines will be used in pairs in counter rotation to avoid the torque.
Los conductos pueden discurrir paralelos lateral o verticalmente entre si. The ducts can run parallel or laterally parallel to each other.
La trasferencia de energía al vehículo se hace sin escobilias, transfiriéndola desde las dos bandas conductoras que recorren el conducto longitudinalmente o por su base, mediante ondas radiomagnéticas o de radiofrecuencia y también utilizando una corriente alterna en ia que la separación entre las placas
ferromagnéticas y ias bandas longitudinales del conducto actúan de condensadores y por lo tamo permiten la circulación de la corriente sin hacer contacto. The transfer of energy to the vehicle is done without brushes, transferring it from the two conductive bands that run the duct longitudinally or at its base, by means of radiomagnetic or radiofrequency waves and also using an alternating current in which the separation between the plates Ferromagnetic and longitudinal duct bands act as capacitors and therefore allow current to flow without contact.
El morro y la cola del vagón no necesitan adoptar forma aerodinámica u oj ival, es indiferente, puede ser plana e incluso cóncava. The nose and tail of the car do not need to be aerodynamic or eye-shaped, it is indifferent, it can be flat and even concave.
El frenado en emergencia se realiza reduciendo las rpm de los fanes, y mediante unos electroimanes que atraerán las bandas o franjas ferromagnéticas del os conductos. Emergency braking is done by reducing the rpm of the fans, and by means of electromagnets that will attract the ferromagnetic bands or bands of the ducts.
En caso de fal lo eléctrico o en emergencia, las haterías alimentan al vagón accionando los motores propulsores. In the event of an electrical or emergency failure, the batteries feed the car by driving the drive motors.
El aire se filtra y acondiciona antes de ser introducido er¡ los vagones y respirado. The air is filtered and conditioned before being introduced into the wagons and breathed.
Funcionam iento: Al apl icar la potencia se produce lal evitación mediante alguno de los sistemas principales: Ruedas magnéticas, cámaras de aire presurizadas, conductos circulación aire fanes o turbinas, canales presurizados, chorros de aire, aletas alrededor de los vagones y coj inetes de aire. Como medios estabilizadores se pueden usar preferentemente: Usas ryedas con cojinetes de aire, unas ruedas con chorros de aire entre ias mismas y el conducto, unos chorros o lenguas de aire perpendiculares o inclinados hacia el conducto. La propulsión se realiza con ia succión o los chorros de aire enviados por las turbinas o con Sas ruedas magnéticas accionadas por lo motores eléctricos. Los vagones se al imentan con células de combustible o haciendo circular corriente alterna a través de unos condensadores formados por unas bandas longitudinales del conducto y de Sos vagones. Si falla la levitación o con el vagón parado, el vagón se apoya sobre unas ruedas. Functioning: When applying power, avoidance occurs through one of the main systems: Magnetic wheels, pressurized air chambers, air circulation ducts, turbines, pressurized channels, air jets, fins around wagons and inefficient bearings. air. Stabilizing means can preferably be used: Uses rimmed with air bearings, wheels with air jets between them and the conduit, jets or air tongues perpendicular or inclined towards the conduit. The propulsion is carried out with suction or air jets sent by the turbines or with magnetic wheels driven by electric motors. The wagons are printed with fuel cells or by circulating alternating current through capacitors formed by longitudinal bands of the duct and Sos wagons. If the levitation fails or with the car stopped, the car rests on wheels.
Para medianas velocidades se pueden util izar los sistemas anteriores en negrita, los cuales por ser automáticos sin mecanismos, resultan muy sencillos. For medium speeds, the previous systems can be used in bold, which because they are automatic without mechanisms, are very simple.
BREVE DESCRIPCION DE LOS DI BUJOS BRIEF DESCRIPTION OF THE DI BUJOS
La figura 1 muestra una vista esquematizada y parcialmente seccionada de un vagón y conducto del sistema de la invención. Figure 1 shows a schematic and partially sectioned view of a car and duct of the system of the invention.
Las figura 2, 3, 6, 7, 1 0 a la 1 3, 1 7b y i 8 muestran vistas esquematizadas y parcialmente seccionadas de variantes del sistema de la invención. Figures 2, 3, 6, 7, 1 0 to 1 3, 1 7b and i 8 show schematic and partially sectioned views of variants of the system of the invention.
Las figuras 4, 5, 8, 9 y 14 a la 1 7, 17a, 19b y 20 la 25 y 33 muestran vistas esquematizadas y parcialmente seccionadas transversalmente de variantes de vagones y conductos de la invención. Figures 4, 5, 8, 9 and 14 at 1, 7, 17a, 19b and 20, 25 and 33 show schematic and partially cross-sectional views of variants of wagons and ducts of the invention.
La figura 19 muestra una rueda con múltiples orificios para insuflar aire y evitar contacte con el tubo, Figure 19 shows a wheel with multiple holes to blow air and avoid contacting the tube,
La figura 19a muestra una forma de aplicar chorros de aire al interior del conducto. Figure 19a shows a way of applying air jets to the interior of the duct.
Las figuras 26 y 27 muestran vistas esquematizadas y parcialmente seccionadas transversalmente de variantes de conductos y sus columnas de soporte. Figures 26 and 27 show schematic and partially cross-sectional views of duct variants and their support columns.
Las figuras 28, 29 y 29a muestran vistas esquematizadas de dos circuitos o conductos variantes del sistema de la invención. Figures 28, 29 and 29a show schematic views of two variant circuits or conduits of the system of the invention.
La figura 30 muestra una unión tipo oruga de dos vagones. Figure 30 shows a caterpillar type junction of two wagons.
La figura 3 1 muestra una vista esquematizada y en perspectiva de una porción de conducto y
vagón en una estación. Figure 3 1 shows a schematic and perspective view of a portion of duct and wagon in a station.
La figura Ώ. muestra una vista er¡ planta de una terminal con un muelle de almacenamiento de portacontenedores. The figure Ώ. It shows a plan view of a terminal with a container storage dock.
La figura 34 muestra un diagrama de b loques de una forma de funcionamiento. Figure 34 shows a block diagram of one form of operation.
DESCRIPCION MÁS DETALLADA DE UNA FORMA DE REALIZACIÓN DE LA INVENCIÓN MORE DETAILED DESCRIPTION OF A FORM OF EMBODIMENT OF THE INVENTION
La figura 6 muestra una posible forma de realización de la invención, con el vagón (2) de sección circular que está rodeado por el conducto ( 1 ). Los inyectores {4ab y 4bc) aplican en zona lateral izquierda el aire a presión, a las cámaras separadoras generadas entre el conducto o carcasa, el vagón y las juntas longitudinales (a, b y c). Otras tres juntas circulares no mostradas en la ftgura determinan en total ocho cámaras. Se muestran las cámaras laterales de la izquierda (ab y be). Los grandes ventiladores o fanes (3), delanteros y traseros son propulsores y con un pequeño ángulo de inclinación producen parte de la sustentación ol evitación aplicando el flujo de aire a las cámaras separadoras. La estabilización se puede conseguir apl icando la señal de separación recibida por unos sensores de separación a las turbinas (3) distribuidas periféricamente que varían su separación en función de sus rprn ., o con los inyectores de aire inclinados (4í) que al separarse reducen su acción separadora y viceversa si se aproximan. Los inyectores inferiores son mayores o envían mayor presión o flujo. Figure 6 shows a possible embodiment of the invention, with the wagon (2) of circular section that is surrounded by the conduit (1). The injectors {4ab and 4bc) apply the pressurized air to the left side, to the separating chambers generated between the duct or carcass, the car and the longitudinal joints (a, b and c). Three other circular joints not shown in the figure determine a total of eight chambers. The left side chambers (ab and be) are shown. The large fans or fans (3), front and rear are propellants and with a small angle of inclination produce part of the lift or avoidance by applying the air flow to the separating chambers. Stabilization can be achieved by applying the separation signal received by separation sensors to the peripherally distributed turbines (3) that vary their separation according to their rprn., Or with inclined air injectors (4í) which when separated reduce its separating action and vice versa if they approach. The lower injectors are larger or send greater pressure or flow.
Utilizando turbinas propulsoras de aire externas al vagón no son necesarias estas turbinas, tan solo se utilizarían los compresores e inyectores de aire y los motores para actuación en emergencia. La corriente eléctrica se generaría med iante una turbina accionada por el chorro de aire. Ai aproximase excesivamente alguna de las cámaras al conducto se incrementa su presión y automáticamente se separa. Using air propeller turbines outside the car, these turbines are not necessary, only compressors and air injectors and engines for emergency operation would be used. The electric current would be generated by a turbine driven by the air jet. If any of the chambers are approached excessively to the duct, its pressure is increased and automatically separated.
La figura 1 muestra el vagón (2) de sección circular que está rodeado por el conducto ( 1 ). Utiliza un gran ventilador delantero (3) y otro trasero los cuales fuerzan al aire entre el fuselaje rnonoeaseo del vagón y el conducto ( 1 ). El delantero puede colocarse en la punta del morro. Porta unas aletas o juntas circulares alrededor del fuselaje del vagón en la zona delantera media y trasera ( l Of, 10m y l Or). Las cuales crean dos cámaras longitudinalmente, que al añadir cuatro juntas longitudinales se producen ocho cámaras, que se usan para levitar y estabi lizar el fuselaje del vagón. Figure 1 shows the wagon (2) of circular section that is surrounded by the conduit (1). It uses a large front fan (3) and a rear fan which force the air between the rifle's fuselage of the car and the duct (1). The forward can be placed on the tip of the nose. Carry some fins or circular joints around the fuselage of the car in the middle and rear front area (l Of, 10m and l Or). Which create two chambers longitudinally, which by adding four longitudinal joints produces eight chambers, which are used to levitate and stabilize the fuselage of the car.
La figura 2 muestra el vagón (2) de sección circular que está rodeado por el conducto ( 1 ). Uti l iza cuatro grandes ventiladores delanteros (3) y otros traseros los cuales fuerzan al aire entre el fuselaje monocasco del vagón y el conducto ( 1 ). Ei vagón tiene un rebaje en su zona periférica excepto en su zona delantera y posterior donde porta unos resaltes anulares o puede portar unas juntas. Mediante las juntas laterales (d) y la (b) del lado opuesto se crean dos cámaras presurizadas la superior de baja presión y la inferior de alta presión para producir la levitación, puede ser necesario añadir las juntas ( l Of y l Or) de la figura 1 , Añadiendo las juntas circulares ( S Of, 1 0m y l Or) de la figura 1 se obtienen cuatro cámaras presurizadas, las cuales además de levitar sirven para estabilizar ios vagones variando la presión de las m ismas. Figure 2 shows the wagon (2) of circular section that is surrounded by the conduit (1). It uses four large front fans (3) and other rear fans which force the air between the monocoque fuselage of the car and the duct (1). The car has a recess in its peripheral area except in its front and rear area where it carries annular projections or can carry joints. By means of the side joints (d) and the (b) of the opposite side, two pressurized chambers are created, the upper one of low pressure and the lower one of high pressure to produce levitation, it may be necessary to add the seals (l Of and l Or) of the Figure 1, Adding the circular joints (S Of, 1 0m and l Or) of Figure 1, four pressurized chambers are obtained, which in addition to levitate serve to stabilize the wagons by varying the pressure of the same.
La figura 3 muestra el vagón (2) de sección circular que está rodeado por el conducto ( 1 ). Util iza
urs gran ventilador delantero (3a) y otro trasero los cuales impulsan y succionan el aire entre εl vagón y el conducto. Preferentemente por la zona inferior para producir lal evitación, el aire se puede hacer pasar entre el vagón y el conducto. El conducto se machihembra ( 1 1 } con la junta toroidal ( 12). El frenado en emergencia se realiza con los electroimanes (29), Muestra los canales levitadores y estabilizadores ( 15). Enl a zona superior fos ( 1 5s) que son más pequeños y solo estabilizadores. Figure 3 shows the wagon (2) of circular section that is surrounded by the conduit (1). Use urs large front fan (3a) and another rear which propel and suck the air between the car and the duct. Preferably through the lower area to produce the avoidance, air can be passed between the car and the duct. The duct is tongue and groove (1 1} with the toroidal joint (12). Emergency braking is done with the electromagnets (29). It shows the levitating and stabilizing channels (15). In the upper zone fos (1 5s) which are Smaller and just stabilizers.
La figura 4 muestra el vagón (2) de sección circular que está rodeado por el conducto ( 1 ) similar al de la figura 2 añadiendo otros elementos. Utiliza cuatro grandes ventiladores delanteros (3 ), cuatro juntas longitudinales (a, b, c y d) creando entre estas, el fuselaje y el conducto las cámaras separadoras (ab, be, cd y da) en las cuales descargan ios inyectores de aire (4ab, 4bc, 4cd y 4da) respectivamente y otros inyectores traseros los cuales fuerzan al aire entre dichas cántaras, y que jante con el flujo enviado por los ventiladores delanteros generan las fuerzas de separación Fab, Fbc, Fcd y Fda respectivamente. Las dos inferiores son levitadoras, estabilizadoras y mayores. También los inyectores sort mayores o sos flujos. Las superiores son solo estabilizadoras y se suman al peso del vagón. Las cámaras separadoras (ab, be, cd y da) se subdividen a su vez en ocho, debido a las tres juntas circulares alrededor del fuselaje. Lo m ismo ocurre con las fuerzas. Añade los electroimanes estabilizadores periféricos ( 12). Figure 4 shows the wagon (2) of circular section that is surrounded by the conduit (1) similar to that of Figure 2 adding other elements. It uses four large front fans (3), four longitudinal joints (a, b, c and d) creating between them, the fuselage and the duct the separating chambers (ab, be, cd and da) in which they discharge the air injectors (4ab , 4bc, 4cd and 4da) respectively and other rear injectors which force the air between said jaws, and that with the flow sent by the front fans generate the separation forces Fab, Fbc, Fcd and Fda respectively. The lower two are levitating, stabilizing and older. Also the injectors sort greater or are flows. The upper ones are only stabilizing and add to the weight of the car. The separating chambers (ab, be, cd and da) are further subdivided into eight, due to the three circular joints around the fuselage. The same happens with the forces. Add the peripheral stabilizing electromagnets (12).
La figura 5 muestra el vagón (2) de sección circular que está rodeado por el conducto ( 1 ) similar al de ia figura 2 añadiendo otros elementos. Utiliza cuatro grandes ventiladores delanteros (3) y cuatro juntas longitudinales (a, b, e y d) creando entre estas, el fuselaje y el conducto las cámaras separadoras (ab, be en el lado izqu ierdo y las cd, da en el derecho). Ánade las ruedas de lím ite o apoyo (6) en la zona inferior para baja velocidad y reposo. Figure 5 shows the wagon (2) of circular section that is surrounded by the conduit (1) similar to that of Figure 2 adding other elements. It uses four large front fans (3) and four longitudinal joints (a, b, e and d) creating between them, the fuselage and the duct the separating chambers (ab, be on the left side and the cd, on the right). Add the limit or support wheels (6) in the lower zone for low speed and rest.
La figura 7 muestra el vagón (2) de sección circular que está rodeado por el conducto ( 1 ). Utiliza un gran ventilador delantero (3a) y otro trasero los cuales succionan el aire por el interior del vagón. Es similar al de la figura 3. Ei aire entre el vagón y el conducto se puede aplicar mediante inyectores. Añade cuatro juntas longitudinales, en el lateral izquierdo se muestran las (a, b, c) creando entre estas, el fuselaje y el conducto las cámaras separadoras. Otras tres juntas circulares no mostradas en la figura determinan en total ocho cámaras. Se muestran las cámaras laterales de (a izquierda (ab y be). Los inyectores (4ab y 4bc) aplican en zona lateral izquierda el aire a presión, a las cámaras separadoras generadas entre el conducto y vagón. Figure 7 shows the wagon (2) of circular section that is surrounded by the conduit (1). It uses a large front fan (3a) and another rear which suck the air inside the car. It is similar to that in Figure 3. The air between the car and the duct can be applied by injectors. Add four longitudinal joints, on the left side are shown the (a, b, c) creating between them, the fuselage and the duct the separating chambers. Three other circular joints not shown in the figure determine a total of eight chambers. The lateral chambers of (to the left (ab and be) are shown. The injectors (4ab and 4bc) apply the pressurized air in the left lateral area to the separating chambers generated between the duct and wagon.
La figura 8 muestra el vagón (2) de sección circular que está rodeado por el conducto ( 1 ). Utiliza uíi gran venti lador delantero (3a) y otro trasero los cuales impulsan y succionan el aire por el interior del vagón. Ei aire se aplica preferente o únicamente por la zona inferior para producir la ievitación, en un canal entre el vagón y el conducto. No se muestran los inyectores de aire estabilizadores del vagón, que se distribuirán por tres o cuatro puntos alrededor del vagón. Usa los chorros de aire como estabilizadores que las cámaras estabilizadoras. Muestra las ruedas (ó) amortiguadoras o de baja velocidad. Figure 8 shows the wagon (2) of circular section that is surrounded by the conduit (1). Use a large front fan (3a) and a rear fan which propel and suck the air inside the car. The air is preferentially applied or only by the lower zone to produce the excitation, in a channel between the car and the duct. The stabilizer air injectors of the car are not shown, which will be distributed over three or four points around the car. Use air jets as stabilizers than stabilizer chambers. Shows the wheels (or) dampers or low speed.
La figura 9 muestra el vagón (2) de sección circular que está rodeado por el conducto ( 1 ). Utiliza como levitadoras las ruedas magnéticas (7) que son retraídas por las bandas longitudinales ferroroagnéticas (8). Muestra las ruedas (6) amortiguadoras o de baja velocidad, las cuales se mantiene
separadas mediante chorros de aire aplicados entre sus zonas laterales, frontales y posteriores y el conducto, actuando automáticamente como esfabilizadoras. Muestra en la zona inferior Sos canales levítadores y estabilizadores ( 1 5) y en la zona superior los estabilizadores ( 1 Ss). Figure 9 shows the wagon (2) of circular section that is surrounded by the conduit (1). It uses as magnetic levitators the wheels (7) that are retracted by the longitudinal ferro-magnetic bands (8). Shows the wheels (6) damping or low speed, which is maintained separated by air jets applied between its lateral, front and rear areas and the duct, automatically acting as stabilizers. It shows in the lower zone Sos levitator channels and stabilizers (1 5) and in the upper zone the stabilizers (1 Ss).
La figura 10 muestra el vagón portaeonfenedores (2p) de sección circular que está rodeado por el conducto ( I ), en su interior porta los contenedores (20). Utiliza cuatro grandes ventiladores delanteros (3ρ) y otros cuatro traseros los cuales fijerzan al aire entre el [fuselaje monocaseo del vagón y el conducto ( I ). El conducto se machihembra ( 1 i) con la junta toroidáí ( 12). Figure 10 shows the wagon carrier (2p) of circular section that is surrounded by the conduit (I), inside it carries the containers (20). It uses four large front fans (3ρ) and another four rear which fix in the air between the [monocoque fuselage of the car and the duct (I). The duct is tongue and groove (1 i) with the toroidáí joint (12).
La figura 1 S muestra el vagón portaeontenedores (2p) de sección circular que está rodeado por el conducto ( i ). En su interior porta los contenedores (20). Utiliza un gran ventilador delantero (3p) y otro trasero los cuales fuerzan al aire entre el fuselaje monocaseo del vagón y el conducto ( 1 ). Figure 1 S shows the container carriage (2p) of circular section that is surrounded by the duct (i). Inside it carries the containers (20). It uses a large front fan (3p) and another rear which force the air between the monocoque fuselage of the car and the duct (1).
La figura 12 muestra el vagón (2) de sección circular que está rodeado por el conducto ( 1 ). En su interior porta los contenedores (20). Utiliza un gran ventilador delantero (3p) y otro trasero los cuales succionan el aire por el interior deS vagón contenedor. El aire entre el vagón y el conducto no se muestra en la figura. Figure 12 shows the wagon (2) of circular section that is surrounded by the conduit (1). Inside it carries the containers (20). It uses a large front fan (3p) and another rear which suck the air inside the container car. The air between the car and the duct is not shown in the figure.
La figura 13 muestra ei vagón (2p) de sección circular que está rodeado por el conducto ( 1 ), En su interior porta los contenedores (20). El vagón es impulsado por unas turbinas o bombas impulsoras externas a dicho vagón. El flujo de aire es impulsado según se ; muestran por las flechas blancas o contorneadas. Un compresor (21 ) proporciona el flujo de aire a los inyectores consoladores de la separación o estabilización del vagón respecto al conducto. Figure 13 shows the wagon (2p) of circular section that is surrounded by the conduit (1), inside it carries the containers (20). The car is driven by turbines or impeller pumps external to said car. The air flow is driven as per ; show by white or contoured arrows. A compressor (21) provides air flow to the injector consoles of the separation or stabilization of the car with respect to the duct.
La figura 14 muestra el vagón (2p) de sección circular que está rodeado por el conducto ( 1 ). En su interior porta los contenedores (20). Eí vagón portaeontenedor lleva entre su periferia y Sos contenedores unas cámaras que en este caso se utilizan para alojar las turbinas propulsoras (3p), además de instalaciones, etc. Figure 14 shows the wagon (2p) of circular section that is surrounded by the conduit (1). Inside it carries the containers (20). The container wagon carries between its periphery and Sos containers some cameras that in this case are used to house the turbines (3p), in addition to facilities, etc.
La figura 1 5 muestra el vagón (2p) de sección circular que está rodeado por el conducto ( 1 ). En su interior porta los contenedores (20). El vagón portacontenedor lleva entre su periferia y Sos contenedores unas cámaras que en este caso se utilizan para alojar las turbinas propulsoras (3p), ruedas (6p), además de instalaciones, etc. Figure 1 5 shows the wagon (2p) of circular section that is surrounded by the conduit (1). Inside it carries the containers (20). The container wagon carries between its periphery and Sos containers some cameras that in this case are used to house the turbines (3p), wheels (6p), in addition to facilities, etc.
La figura 16 muestra el vagón (2) de sección circular que está rodeado por el conducto ( 1 ). Presenta dos cavidades longitudinales en la zona superior en las cuales circula un flujo de aire forzado por Sos fanes o ventiladores estabilizadores (3S), dos en la zona delantera y dos en la trasera. En la zona inferior presenta dos cavidades longitudinales principalmente levitadoras y en segundo término esíabilizadoras en las cuales circula el flujo de aire accionado por los fanes (3L), dos delanteros y dos traseros. Los vectores muestran las fuerzas estabilizadores y sustentadoras aplicadas (FS y FL). Figure 16 shows the carriage (2) of circular section that is surrounded by the conduit (1). It has two longitudinal cavities in the upper zone in which a forced air flow circulates through Sos fanes or stabilizing fans (3S), two in the front area and two in the rear. In the lower zone it has two longitudinal cavities, mainly levitating and, secondly, stabilizers in which the flow of air operated by the fans (3L), two front and two rear, circulates. The vectors show the stabilizing and sustaining forces applied (FS and FL).
La figura 17 muestra el vagón (2) de sección circular que está rodeado por el conducto ( 1 ). Presenta tres cavidades longitudinales en la zona media y superior en las cuales circula un flujo de aire forzado por los fanes o ventiladores estabilizadores (38), y otros tres en la trasera, En la zona inferior presenta una cavidad longitudinal principalmente levitadora y en segundo térm ino estabilizadora en la
cual circula el flujo de aire accionado por el gran fan (3L) y otro en la zona trasera. Los vectores muestran las fuerzas estábil szadoras y sustentadoras; apl icadas (FS y FL). Figure 17 shows the wagon (2) of circular section that is surrounded by the conduit (1). It has three longitudinal cavities in the middle and upper zone in which a forced air flow circulates through the fans or stabilizing fans (38), and another three in the rear, In the lower zone it presents a longitudinal cavity mainly levitating and in the second term non stabilizer in the which circulates the air flow driven by the large fan (3L) and another in the rear area. The vectors show the stable lifting and sustaining forces; applied (FS and FL).
La figura 1 7a muestra el vagón (2) de sección circular que está rodeado por el conducto ( 1 ). Utiliza levitación por cojinetes de aire, insuflando aire a presión por el conducto (30) la cámara (3 S ) contigua a la placa porosa (32) que produce múltiple burbujas de aire en su cara en contacto con el vehículo. La cámara (33) está libre para el caso de la caída de algún objeto en la zona interna. La rueda (6s) limita su recorrido superior pero no toca por tener chorros de aire entre la rueda y el conducto. Figure 1 7a shows the wagon (2) of circular section that is surrounded by the conduit (1). It uses levitation by air bearings, blowing pressurized air through the duct (30) the chamber (3 S) adjacent to the porous plate (32) that produces multiple air bubbles in its face in contact with the vehicle. The camera (33) is free in the case of the fall of an object in the internal zone. The wheel (6s) limits its upper travel but does not touch by having air jets between the wheel and the duct.
La figura 17b muestra el conducto ( I ) el vagón (2) con un sistema de estabi lización en el morro y la cola del vagón en Sos que ios timones longitudinales ( 13) son inclinados con los electroimanes ( 12) basculando sobre las rótulas ( 14) en función de las señales de separación enviadas por cuatro sensores. Figure 17b shows the duct (I) the car (2) with a stabilization system in the nose and the car's tail in Sos that the longitudinal rudders (13) are inclined with the electromagnets (12) tilting on the kneecaps ( 14) depending on the separation signals sent by four sensors.
La figura 1 8 m uestra el conducto ( 1 ) y en su interior el vagón (2r) cubierta su superficie por múltiples aletas inclinadas hacia atrás (24r), las cuales una vez íeviíado por las cámaras e inyectores levitadores, contribuyen, centrando el vagón en el conducto. Figure 1 8 shows the duct (1) and inside the car (2r) covered its surface by multiple fins tilted back (24r), which once guided by the cameras and levitator injectors, contribute, centering the car in the duct.
La figura 19 muestra el rail tubular ( 1 ), y en su zona interna Sa rueda (ój) la cual no llega a tocar al conducto debido a los chorros de aire (62) a través de múltiples orificios de la rueda y los chorros (61 ) entre la rueda y la carcasa superior (60) que la rodea y cubre, Figure 19 shows the tubular rail (1), and in its inner zone Sa wheel (oj) which does not touch the duct due to air jets (62) through multiple holes in the wheel and jets ( 61) between the wheel and the upper housing (60) that surrounds and covers it,
La figura 19a muestra los conductos (70) y otros verticales que aplican los chorros de aire (71 y 72) hacia el interior del conducto ( I ). Figure 19a shows the ducts (70) and other verticals that apply the air jets (71 and 72) into the duct (I).
La figura 19b muestra el conducto ( 1 ), en su interior el vagón (2) levitado mediante ruedas magnéticas (7) que atraen al rail si es ferromagnélico o a la banda (8) y estabilizado con las ruedas (6a) con coj inetes de aire. Pueden usarse para bajas y medianas velocidades. Para velocidades mayores se pueden usar las ruedas (6s) con chorros de aire incidiendo entre ruedas y conducto. Pueden usarse las dos bandas (8) de la conducción eléctrica. Figure 19b shows the duct (1), inside the car (2) levitated by magnetic wheels (7) that attract the rail if it is ferromagnetic or to the band (8) and stabilized with the wheels (6a) with inetetic bearings. air. They can be used for low and medium speeds. For higher speeds, the wheels (6s) can be used with air jets between wheels and duct. The two bands (8) of the electric conduction can be used.
La figura 20 muestra un conducto ovalado ( I v) y vagón ovalado (2v), mostrando las juntas longitudinales (a, b, c y d). Figure 20 shows an oval duct (I v) and oval wagon (2v), showing the longitudinal joints (a, b, c and d).
La figura 2 1 muestra un conducto semicircular ( I s) y vagón semicircular (2s). Figure 2 1 shows a semicircular duct (I s) and semi-circular wagon (2s).
La figura 22 muestra un conducto de sector circular de unos 270° ( I g) y vagón de sector circular de unos 270° (2g). Figure 22 shows a circular sector duct of about 270 ° (I g) and circular sector wagon of about 270 ° (2g).
La figura 23 muestra un conducto rectangular ( 3 r) y vagón rectangular (2r). Figure 23 shows a rectangular duct (3 r) and rectangular wagon (2r).
La figura 24 muestra un conducto de sección trapecial ( I t) y vagón trapecial (2r). Puede portar las juntas de forma similar a la figura 23. Figure 24 shows a trapezoidal section duct (I t) and trapezoidal car (2r). You can carry the joints in a similar way to figure 23.
La figura 25 muestra un conducto abierto y en forma de U 21 r) y vagón o portacontenedor (2r). Figure 25 shows an open and U-shaped conduit 21 r) and wagon or container carrier (2r).
En las figuras 2 1 a la 25 se util izan, pero no se mencionan, las juntas longitudinales. En los sistemas de las figuras 20 a la 25 la estabilización lateral es más sencilla. In Figures 2 1 to 25, longitudinal joints are used, but not mentioned. In the systems of Figures 20 through 25, lateral stabilization is easier.
La figura 26 muestra una forma de soporte de los conductos ( 1 ) mediante las medias carias (26) y estas a su ve?, con las columnas (27). Figure 26 shows a form of support for the ducts (1) by means of the carias stockings (26) and these are in turn ?, with the columns (27).
La figura 27 muestra una forma de soporte de los conductos ( I ) med iante las medias cañas (26)
y estas a su vez con las colum nas (27). Añade el conducto (28) úíii para portar las instalaciones y para desplazamiento de vagones o personal de mantenimiento. Los tres portan las correspondientes compuertas de acceso a los conductos principales. Figure 27 shows a form of duct support (I) by means of the half rods (26) and you are in turn with the columns (27). Add the duct (28) úíii to carry the facilities and to move cars or maintenance personnel. All three carry the corresponding access gates to the main ducts.
La figura 28 muestra un posible circuito cerrado con un vagón de ida el (2) y otro de regreso el (2a). Las bombas ( 1 7 y 1 7a) impulsan los vagones enviando un chorro de aire por detrás de Sos mismos y succionando de su zona frontal en lo que intervienen las válvulas ( 1 9 y 19a) y Sos conductos ( 1 8 y 1 8a), las cuales se cierran dejando de succionar cuando el vagón se aproxima a la zona. Figure 28 shows a possible closed circuit with a one-way car on (2) and another on the back (2a). The pumps (1 7 and 1 7a) drive the wagons by sending an air jet behind Sos themselves and sucking from their frontal zone in which the valves (1 9 and 19a) and Sos ducts (1 8 and 1 8a) intervene , which close, stopping sucking when the car approaches the area.
La figura 29 muestra una variante de circuito de ida el (2b) y otro de regreso el (2e). Las bombas ( 1 7b y 17c) impulsan los vagones enviando un cSiorro de aire por detrás de ios mismos y succionando de su zona frontal en lo que intervienen las válvulas ( 1 9 y 19a), que se cierran dejando de succionar cuando el vagón se aproxima a la zona. Este en lugar de usar un circuito cerrado, en Sos extremos utiliza un cambio de dirección y de vía. Figure 29 shows a one-way circuit variant on (2b) and a return one on (2e). The pumps (1 7b and 17c) drive the wagons by sending an air ciorior behind them and sucking from their frontal zone in which the valves (1 9 and 19a) intervene, which close, stopping sucking when the car is Approaches the area. This instead of using a closed circuit, in extreme Sos uses a change of direction and track.
La figura 29a muestra una variante de circuito o conducto ( i ) en e3 cual se aplica presurizaeión y succión externa por tramos mediante ía bomba o compresor ( 1 7d). Se apl ica aire a presión por la zona posterior del vagón (2d) y succión delantera hasta que el vagón alcanza el punto en T o de unión con el conducto en cuyo momento el tramos entre la T y la válvula se comprime ligeramente y abre la válvula ( 19d) delantera y hasta que pasa al tramo siguiente donde se repite esta actuación automáticamente. Figure 29a shows a variant of circuit or conduit (i) in e3 which is applied pressurization and external suction by sections by means of the pump or compressor (1 7d). Pressure air is applied through the rear area of the car (2d) and front suction until the car reaches the point at T or junction with the duct at which time the sections between the T and the valve are slightly compressed and open the valve (19d) forward and until it goes to the next section where this action is repeated automatically.
La figura 30 muestra la unión (22) tipo fuel le u oruga, entre dos vagones ( 1 ). Figure 30 shows the union (22) type fuel le or caterpillar, between two wagons (1).
La figura 3 1 muestra el conducto ( 1 ) con la puerta { 1 p) abierta en una estación en el momento en que la puerta del vagón (2p) está enfrente de la misma. Una escalera con peldaños ( 1 c) facilita la bajada y subida de los pasajeros. Figure 3 1 shows the conduit (1) with the door {1 p) open at a station at the moment when the car door (2p) is in front of it. A staircase with steps (1 c) facilitates the descent and rise of passengers.
La figura 32 muestra el conducto de llegada ( 1 ), subiendo por una rampa (23) para su desaceleración en una term inal de carga y una vez parado cambia de sentido y se almacenan en las vias de almacenaje (24). Las flechas muestran el itinerario. Figure 32 shows the arrival duct (1), going up a ramp (23) for its deceleration in a load terminal and once stopped changes direction and is stored in the storage tracks (24). The arrows show the itinerary.
La figura 33 muestra el conducto ( i ) y entre el este y el vagón (2) un conducto especial ( l i) formado por ranuras longitudinales o por unas válvulas longitudinales o transversales, que cierran el paso del aire durante la succión y las abren en emergencia al presionar el vagón sobre el aire frontal. La figura no muestra las ranuras ni las válvulas. Figure 33 shows the duct (i) and between the east and the car (2) a special duct (li) formed by longitudinal grooves or by longitudinal or transverse valves, which close the passage of air during suction and open them in emergency when pressing the car on the front air. The figure does not show the slots or the valves.
La figura 34 muestra un m icroprocesador que procesa las señales de: Giróscopos, acelerómetros, cuatro sensores de separación delanteros y cuatro traseros, mando de gases, frenos, peso de la zona delantera y trasera, o rotura del conducto, detectado por los cambios de presión a lo largo del mismo. El microprocesador una vez procesados proporciona y envía múltiples y repetitivas señales: Cuatro de control de estabilización delantera y otras cuatro señales de levitaeión zona delantera y de la zona trasera enviadas a los inyectores, actuadores de las aletas o a Sos electroimanes y señales de aviso de fallos del sistema, control de veSocidad, frenado, propulsión e indicación de velocidad.
Figure 34 shows a microprocessor that processes the signals of: Gyroscopes, accelerometers, four front and four rear separation sensors, gas control, brakes, front and rear area weight, or duct rupture, detected by changes in pressure along it. Once processed, the microprocessor provides and sends multiple and repetitive signals: Four front stabilization control and four other front and rear zone levitation signals sent to injectors, fin actuators or electromagnets and fault warning signals. system, speed control, braking, propulsion and speed indication.
Claims
REIVINDICACIONES
1 . Sistema Eevitador, estabil izador y propulsor para vehículos con vagones que circulan por conductos de aire caracterizado por que la separación entre vagones y conducto está en e3 rango de 0. 1 cm a 10 era y por que comprende: one . Eevitator, hoist and propeller system for vehicles with wagons that circulate through air ducts characterized in that the separation between wagons and conduit is in the range of 0. 1 cm to 10 era and because it comprises:
a) medios Ieviíadores consistentes en cámaras de aire presurizadas formadas por juntas entre los vagones y el conducto, siendo las cámaras inferiores de mayores dimensiones o de mayor presión: entre los vagones, eS conducto y unas juntas, ías cámaras inferiores son de mayores dimensiones o de mayor presión; a) Ieviators means consisting of pressurized air chambers formed by joints between the wagons and the duct, the lower chambers being of greater dimensions or of greater pressure: between the wagons, the duct and some joints, the lower chambers are of greater dimensions or of higher pressure;
b) medios estabilizadores consistentes en chorros de aire, perpendiculares o incl inados en relación al conducto; b) stabilizing means consisting of air jets, perpendicular or inclined in relation to the duct;
c) medios propulsores consistentes en ventiladores accionados con motores eléctricos; c) propellant means consisting of fans driven by electric motors;
d) y medios de al imentación eléctrica consistentes en baterías. d) and means of electrical installation consisting of batteries.
2. Sistema según reivindicación 1 , caracterizado por que adicionaimente comprende medios Ieviíadores consistentes en canales de aire aírededor de ios vagones, ambos del tipo de colchón de aire, distribuidos longitudinal y transversalmente por la periferia de Sos vagones, los inferiores son de mayores dimensiones o de mayor presión 2. System according to claim 1, characterized in that it additionally comprises means consisting of air channels of the wagons, both of the type of air cushion, distributed longitudinally and transversely along the periphery of Sos wagons, the lower ones are of larger dimensions or higher pressure
3. Sistema según reivindicación 1 , caracterizado por que adicionaimente comprende medios Ieviíadores consistentes en ruedas magnéticas giratorias. 3. System according to claim 1, characterized in that it additionally comprises means consisting of rotating magnetic wheels.
4. Sistema según reivindicación 1 , caracterizado por que adicionaimente comprende como medios Ieviíadores la corriente de aire utilizada en la propulsión de ios vagones en la zona inferior entre vagón y conducto. 4. System according to claim 1, characterized in that it additionally comprises as air means the air flow used in the propulsion of the wagons in the lower area between car and duct.
5. Sistema según reivindicación 1 , caracterizado por que adicionaimente comprende medios Ievitadores consistentes en coj inetes de aire. 5. System according to claim 1, characterized in that it additionally comprises preventive means consisting of inefficient air cushions.
6. Sistema según reivindicación 1 , caracterizado por que adicionaimente comprende medios Ieviíadores consistentes en aletas que defíeeían la corriente de aire hacia abajo. 6. System according to claim 1, characterized in that it additionally comprises means consisting of fins that deflect the air flow downwards.
7. Sistema según reivindicación 1 , caracterizado por que adicionaimente comprende medios Ievitadores consistentes en chorros de aire perpendiculares o inclinados en relación al conducto. 7. System according to claim 1, characterized in that it additionally comprises means that are avoidants consisting of perpendicular or inclined air jets in relation to the duct.
8. Sistema según reivindicación 1 , caracterizado por que adicionaimente comprende medios ievitadores consistentes en ruedas periféricas con unos chorros de aire entre la superficie de la rueda y el conducto. System according to claim 1, characterized in that it additionally comprises means ievitators consisting of peripheral wheels with air jets between the surface of the wheel and the conduit.
9. Sistema según reivindicación 1 , caracterizado por que adicionaimente comprende medios de estabi lización consistemes en cámaras de aire presurizadas del tipo colchón de aire, colocadas alrededor de los vagones, 9. System according to claim 1, characterized in that it additionally comprises stabilization means consisting of pressurized air chambers of the air mattress type, placed around the wagons,
10 Sistema según reivindicación i , caracterizado por que adicionaimente comprende medios de estabilización consistentes en canales de aire presurÍ2ados, del tipo colchón de aire, colocados alrededor de los vagones. System according to claim i, characterized in that it additionally comprises stabilization means consisting of pressurized air channels, of the air mattress type, placed around the wagons.
1 1. Sistema según reivindicación 1 , caracterizado por que adicionaimente comprende, medios de
estabilización consistentes en ruedas magnéticas giratorias. 1 1. System according to claim 1, characterized in that it additionally comprises stabilization consisting of rotating magnetic wheels.
12. Sistema según reivindicación 1, caracterizado por que adicionalmente comprende medios de estabilización consistentes en la corriente de aire utilizada en la propulsión. 12. System according to claim 1, characterized in that it additionally comprises stabilization means consisting of the air flow used in the propulsion.
13. Sistema según reivindicación 1, caracterizado por que adicionalmente comprende medios de estabilización consistentes en cojinetes de aire. 13. System according to claim 1, characterized in that it additionally comprises stabilization means consisting of air bearings.
14. Sistema según reivindicación 1, caracterizado por que adicionalmente comprende medios de estabilización consistentes en ruedas periféricas que portan chorros de aire entre estas y el conducto. 14. System according to claim 1, characterized in that it additionally comprises stabilization means consisting of peripheral wheels carrying air jets between them and the conduit.
15. Sistema según reivindicación 1, caracterizado por que adicionalmente comprende medios de estabilización consistentes en electroimanes que atraen al conducto. 15. System according to claim 1, characterized in that it additionally comprises stabilization means consisting of electromagnets that attract the conduit.
16. Sistema según reivindicación 1, caracterizado por que adicionalmente comprende medios de estabilización consistentes en múltiples aletas distribuidas inclinadas hacia atrás y hacia el exterior, alrededor del vehículo. 16. System according to claim 1, characterized in that it additionally comprises stabilization means consisting of multiple distributed fins inclined backward and outward, around the vehicle.
17. Sistema según reivindicación 1, caracterizado por que adicionalmente comprende medios de estabilización consistentes en un buje o aleta en el morro y otro en la cola. 17. System according to claim 1, characterized in that it additionally comprises stabilization means consisting of a bushing or fin in the nose and another in the tail.
18. Sistema según reivindicación 1 , caracterizado por que adicionalmente comprende medios de estabilización consistentes en la inclinación de las turbinas periféricas. 18. System according to claim 1, characterized in that it additionally comprises stabilization means consisting of the inclination of the peripheral turbines.
19. Sistema según reivindicación 1, caracterizado por que adicionalmente comprende medios de estabilización consistentes en la variación de las rpm de al menos uno de los fanes periféricos. 19. System according to claim 1, characterized in that it additionally comprises stabilization means consisting of the variation of the rpm of at least one of the peripheral slanes.
20. Sistema según reivindicación 1, caracterizado por que adicionalmente comprende medios de estabilización consistentes en la señal de separación recibida por los sensores y la aplica a las turbinas distribuidas periféricamente. 20. System according to claim 1, characterized in that it additionally comprises stabilization means consisting of the separation signal received by the sensors and applied to peripherally distributed turbines.
21. Sistema según reivindicación 1, caracterizado por que adicionalmente comprende medios de estabilización consistentes en unos inyectores inclinados, los cuales al separarse reducen su acción separadora y viceversa cuando se aproximan. 21. System according to claim 1, characterized in that it additionally comprises stabilization means consisting of inclined injectors, which when separated reduce their separating action and vice versa when they approach.
22. Sistema según reivindicación 1, caracterizado por que adicionalmente comprende medios de estabilización lateral o de alabeo que consistente en el lastrado de ios vagones y aplicación de la señal a unos electroimanes o chorros de aire inclinados que generan una reacción que endereza al vehículo. 22. System according to claim 1, characterized in that it additionally comprises lateral stabilization or warping means consisting of the ballasting of the wagons and application of the signal to electromagnets or inclined air jets that generate a reaction that straightens the vehicle.
23. Sistema según reivindicación 1, adicionalmente comprende medios de propulsión consistentes en ruedas magnéticas actuadas con motores eléctricos. 23. System according to claim 1, further comprising propulsion means consisting of magnetic wheels actuated with electric motors.
24. Sistema según reivindicación 1, caracterizado por que adicionalmente comprende medios de alimentación eléctrica consistentes en células de combustible. 24. System according to claim 1, characterized in that it additionally comprises power supply means consisting of fuel cells.
25. Sistema según reivindicación 1, caracterizado por que adicionalmente comprende medios de alimentación eléctrica consistentes en bandas eléctricas a lo largo del conducto y la corriente es transferida al interior por ondas electromagnéticas o de radiofrecuencia. 25. System according to claim 1, characterized in that it additionally comprises power supply means consisting of electrical bands along the conduit and the current is transferred to the interior by electromagnetic or radiofrequency waves.
26. Sistema según reivindicación 1, caracterizado por que adicionalmente comprende medios de alimentación eléctrica consistentes en bandas eléctricas a lo largo del conducto y la corriente es transferida al interior como corriente alterna utilizando bandas en conducto y vehículo que actúan de
condensadores. 26. System according to claim 1, characterized in that it additionally comprises power supply means consisting of electrical bands along the conduit and the current is transferred to the interior as an alternating current using conduit and vehicle bands acting as capacitors
27. Sistema según reivindicación i , caracterizado por que adieionalmeníe comprende medios de control de la elvitación, estabil ización, propulsión y avisos, consistentes en un microprocesador el cual procesa las señales de: giróscopos, acelerómetros, cuatro sensores de separación delanteros y otros cuatro traseros distribuidos alrededor del vagón, mando de gases, frenos, detección fagas del conducto, peso de la zona delantera y de a tral sera, el m icroprocesador una vez procesados proporciona y envía múltiples y repetitivas señales: Cuatro de control de estabi lización delantera y otras cuatro traseras, señal o señales de Sevitación zona delantera y de la zona trasera enviadas a los inyectores, acíuadores de las aletas o a los electroimanes y señales de aviso de fallos del sistema, control de velocidad, frenado, propulsión e indicación de velocidad. 27. System according to claim i, characterized in that it additionally comprises means for controlling elvitation, stabilization, propulsion and warnings, consisting of a microprocessor which processes the signals of: gyroscopes, accelerometers, four front separation sensors and four other rear distributed around the wagon, gas control, brakes, phage detection of the duct, weight of the front and rear zone, the microprocessor once processed provides and sends multiple and repetitive signals: Four of front stabilization control and others four rear, signal or signals of Sevitation front and rear zone sent to injectors, fin actuators or electromagnets and warning signals of system failures, speed control, braking, propulsion and speed indication.
28. Sistema según reivindicación 1 , caracterizado porque utiliza unos filtros para fi ltrado del aire que se introduce en los vagones, 28. System according to claim 1, characterized in that it uses filters for filtering the air that is introduced into the cars,
29. Sistema según reivindicación 3, caracterizado por que las ruedas magnéticas giratorias tienen forma cilindrica y convexidad periférica. 29. System according to claim 3, characterized in that the rotating magnetic wheels have cylindrical shape and peripheral convexity.
30. Sistema según reivindicación 2, caracterizado por que las cámaras de aire utilizan juntas separadoras de goma, plástico o metal, y dejasi una pequeña separación con la superficie del conducto, se crean entre dos o cuatro juntas longitudinales y dos o tres 30. System according to claim 2, characterized in that the air chambers use rubber, plastic or metal separating joints, and leaving a small separation with the duct surface, are created between two or four longitudinal joints and two or three
3 3 . Sistema según reivindicación 1 , caracterizado per que las zonas de impacto del chorro de aire a presión están delimitadas por juntas de sección circular o rectangular, que se colocan dentro y fuera de las cámaras de aire. 3 3. System according to claim 1, characterized in that the impact areas of the pressurized air jet are delimited by circular or rectangular section joints, which are placed inside and outside the air chambers.
32. Sistema según reivindicación 1 , caracterizado por que la zona trasera y delantera de los vagones, donde finalizan las cámaras de aire, están rematadas por aletas flexibles. 32. System according to claim 1, characterized in that the rear and front area of the wagons, where the air chambers end, are topped by flexible fins.
33. Sistema según reivindicación i , caracterizado por que los vagones presentan el centro de gravedad en el tercio inferior de los m ismos, colocando la mayor parte de la carga e instalaciones en dicha zona. 33. System according to claim i, characterized in that the cars have the center of gravity in the lower third of the same, placing most of the cargo and facilities in said area.
34. Sistema según reivindicación l , caracterizado por que el conducto d ispone de puertas de salida normal y de emergencia por todo el circuito, convenientemente espaciadas, y el conducto tiene zonas de debilitamiento y de fácil rotura. 34. System according to claim 1, characterized in that the duct has normal and emergency exit doors throughout the circuit, conveniently spaced, and the duct has areas of weakening and easy breakage.
35. Sistema según reivindicación i , caracterizado por uti lizar unos vagones portacontenedores de forma cilindrica que alojan en su interior además de los contenedores las turbinas e instalaciones. 35. System according to claim i, characterized in that it uses cylindrical container wagons that house turbines and installations inside it, in addition to the containers.
36. Sistema según reivindicación 1 , caracterizado por que Sos vagones son de sección circular y presentan dos cavidades longitudinales en la zona superior en las cuales circula un flujo de aire forzado por tos fanes o ventiladores estabilizadores (3S) y en la zona inferior presenta dos cavidades longitudinales principalmente Sevitadoras y en segundo término estabiiizadoras en las cuales circula el flujo de aire impulsado por los fanes (3L), estos fanes se aplican en 2ona anterior y posterior de los vagones. 36. System according to claim 1, characterized in that Sos wagons are of circular section and have two longitudinal cavities in the upper zone in which a forced air flow circulates through coughs or stabilizing fans (3S) and in the lower zone it has two Longitudinal cavities, mainly Sevitator and, secondly, stabilizers in which the air flow driven by the fans (3L) circulates, these fanes are applied in the anterior and posterior part of the wagons.
37. Sistema según reivindicación 1 , caracterizado por que los vagones son de sección circular y
presentan tres cavidades longitudinales en a zonal media y superior en las cuales circula un flujo de aire forzado por unos fanes o ventiladores estabilizadores (3 S) y oíros tres en la zona posterior, en la zona in ferior presenta una cavidad longitudinal, principalmente leviíadora y en segundo término estábil izadora y por la cual circula el flujo de aire mediante un fian (3L) en zona delantera y otro eí¡ la zona posterior. 37. System according to claim 1, characterized in that the wagons are of circular section and they have three longitudinal cavities in a middle and upper zone in which a forced air flow circulates through fans or stabilizing fans (3 S) and three others in the rear zone, in the lower zone it presents a longitudinal cavity, mainly leviíadora and secondly, it is a stable hoist and through which the air flow circulates through a fian (3L) in the front area and another one in the rear area.
38. Sistema según reivindicación 1 , caracterizado por que utiliza parejas de turbinas, fanes o ventiladores que giran en eorstrarroíaeión. 38. System according to claim 1, characterized in that it uses pairs of turbines, fans or fans that rotate in eorstrarroíaeión.
39. Sistema según reivindicación S , caracterizado por que el conducto es de sección circular. 39. System according to claim S, characterized in that the duct is circular in section.
40. Sistema según reivindicación I , caracterizado por que el conducto es de sección ovalada. 43. Sistema según reivindicación 1 , caracterizado por que el conducto es de sección semicircular. 40. System according to claim I, characterized in that the duct is oval in section. 43. System according to claim 1, characterized in that the duct is of semicircular section.
42. Sistema según reivindicación 1 , caracterizado por que el conducto es de sección de segmento mayor de circulo. 42. System according to claim 1, characterized in that the duct is of a larger segment segment.
43. Sistema según reivind icación 1 , caracterizado por que el conducto es de sección cuadrada. 43. System according to claim 1, characterized in that the duct is square in section.
44. Sistema según reivindicación S , caracterizado por que conducto es de sección de paralelogramo rectángulo. 44. System according to claim S, characterized in that the duct is of rectangular parallelogram section.
45. Sistema según reivindicación 1 , caracterizado por que los vagones tienen la misma forma externa que los conductos, pero de menor sección. 45. System according to claim 1, characterized in that the wagons have the same external shape as the ducts, but of smaller section.
46. Sistema según reivindicación 1 , caracterizado por que el frenado en emergencia se realiza mediante unos electroimanes que atraerán las bandas o franjas ferromagnéticas de los conducios y reduciendo las rpm de ios ventiladores. 46. System according to claim 1, characterized in that the emergency braking is carried out by means of electromagnets that will attract the ferromagnetic bands or bands of the conduits and reducing the rpm of the fans.
47. Sistema según reivindicación 1 , caracterizado por que los vagones portan cuatro o más tanques con líquidos colocados en las esquinas o periferia del vagón para equilibrarlo o mantener los pesos estables en cada punto en caso de desplazamiento de la carga, pasaje o por el consumo de combustible. 47. System according to claim 1, characterized in that the wagons carry four or more tanks with liquids placed in the corners or periphery of the wagon to balance or maintain stable weights at each point in case of displacement of the load, passage or consumption made out of fuel.
48. Sistema según reivind icación 1 , caracterizado por que entre el conducto ( 1 ) y el vagón (2) se coloca un conducto especial ( 3 i) con múltiples ranuras longitudi nales. 48. System according to claim 1, characterized in that a special duct (3 i) with multiple longitudinal grooves is placed between the conduit (1) and the car (2).
49. Sistema según reivind icación 1 , caracterizado por que entre el conducto ( 1 ) y el vagón (2) se coloca un conducto especial formado por unas válvulas longitudinales o transversales, que cierran el paso del aire durante la succión y las abren en emergencia al presionar el vagón sobre el aire frontal,
49. System according to claim 1, characterized in that a special conduit formed by longitudinal or transverse valves is placed between the duct (1) and the car (2), which close the passage of air during suction and open them in emergency by pressing the car on the front air,
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
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ESP201600640 | 2016-07-14 | ||
ES201600640A ES2654912B1 (en) | 2016-07-14 | 2016-07-14 | Levitator, stabilizer and propeller system for vehicles that circulate through air ducts |
ESP201700040 | 2016-12-29 | ||
ES201700040A ES2677156B1 (en) | 2016-12-29 | 2016-12-29 | Levitator, stabilizer and propulsion system for vehicles circulating in air ducts |
Publications (1)
Publication Number | Publication Date |
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WO2018011443A1 true WO2018011443A1 (en) | 2018-01-18 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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PCT/ES2017/000099 WO2018011443A1 (en) | 2016-07-14 | 2017-07-13 | Levitation, stabilisation and propulsion system for vehicles travelling through air ducts |
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FR3085021A1 (en) * | 2018-08-17 | 2020-02-21 | Emile Weisman | HIGH SPEED TRAINS IN ATMOSPHERIC PRESSURE TUBES |
ES2842242A1 (en) * | 2020-01-13 | 2021-07-13 | Zeleros Global S L | GAS FLOW CHANNELING SYSTEM FOR VEHICLES DRIVEN BY COMPRESSED GAS JET IN CONFINED LOW PRESSURE ENVIRONMENTS (Machine-translation by Google Translate, not legally binding) |
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WO2021144482A1 (en) * | 2020-01-13 | 2021-07-22 | Zeleros Global, S.L. | Gas flow channelling system for compressed gas jet-propelled vehicles in low-pressure confined environments |
GB2601729A (en) * | 2020-11-13 | 2022-06-15 | Trevor Willden Ian | Tube or tunnel traversing ducted fan driven vehicle |
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