WO2003102303A1 - Fahrweg, fahrwegmodul und verfahren zu dessen herstellung - Google Patents
Fahrweg, fahrwegmodul und verfahren zu dessen herstellung Download PDFInfo
- Publication number
- WO2003102303A1 WO2003102303A1 PCT/DE2003/001697 DE0301697W WO03102303A1 WO 2003102303 A1 WO2003102303 A1 WO 2003102303A1 DE 0301697 W DE0301697 W DE 0301697W WO 03102303 A1 WO03102303 A1 WO 03102303A1
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- WIPO (PCT)
- Prior art keywords
- modules
- module
- track according
- carrier
- track
- Prior art date
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Classifications
-
- E—FIXED CONSTRUCTIONS
- E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
- E01B—PERMANENT WAY; PERMANENT-WAY TOOLS; MACHINES FOR MAKING RAILWAYS OF ALL KINDS
- E01B25/00—Tracks for special kinds of railways
- E01B25/30—Tracks for magnetic suspension or levitation vehicles
- E01B25/305—Rails or supporting constructions
-
- E—FIXED CONSTRUCTIONS
- E01—CONSTRUCTION OF ROADS, RAILWAYS, OR BRIDGES
- E01B—PERMANENT WAY; PERMANENT-WAY TOOLS; MACHINES FOR MAKING RAILWAYS OF ALL KINDS
- E01B25/00—Tracks for special kinds of railways
- E01B25/30—Tracks for magnetic suspension or levitation vehicles
- E01B25/32—Stators, guide rails or slide rails
Definitions
- the invention relates to a guideway and a guideway module for magnetic levitation vehicles according to the preambles of claims 1 and 18 and a method for producing the guideway module.
- At least one first functional surface in the form of a side guide surface which is fastened to a first piece of equipment in the form of a side guide rail, is used for tracking.
- At least one further first functional surface in the form of a sliding surface is required when the magnetic levitation vehicles are stopped normally or in the event of an emergency stop, and is formed on a further first piece of equipment in the form of a sliding strip.
- second functional surfaces in the form of mounting surfaces which are used for the subsequent mounting of stator packs of the long-stator linear motors, are formed on second pieces of equipment in the form of stator carriers.
- the undersides of these stator packages with support and excitation magnets mounted on the magnetic levitation vehicles form a gap of approx. 10 mm in the levitation and driving condition of the vehicles.
- the routes known so far for magnetic levitation systems of this type mainly consist of one behind the other in the direction of a preselected route, z. B. 24 m to 62 m long sections.
- Each track section consists of a beam supported on two or three supports and the equipment parts attached to it.
- the first functional surfaces, ie the lateral guiding and sliding surfaces should extend over the entire length of the beam and be provided with all the necessary curvatures that result from the curves, crests, valleys, etc. of the chosen route.
- the second functional surfaces ie the mounting surfaces, generally consist of flat surface sections spaced in the direction of the route, since the stator packs attached to them are only connected to the carrier at selected locations and are arranged in such a way that their also flat undersides along one of a preselected space curve approximate polygon course (DE 199 34 912 AI).
- the functional surfaces mentioned must be manufactured and / or assembled with a high degree of precision in order to ensure that the guidance and drive system functions perfectly even at speeds of up to 500 km / h and more.
- the production of the mounting surfaces for the stator packs takes place in a first step in that the stator supports are fastened to supports made of steel by means of welding or screwing or by means of grouting mortar on supports made of concrete. Then, in a second step, the assembly surfaces are produced by providing the stator supports with notches suitable for receiving spacer sleeves, in addition to bores for fastening screws, or initially producing them with oversize and then machined to a preselected target size. In both cases, the use of computer-controlled tools and taking into account all appropriate route data ensures that the undersides of the stator packs are automatically arranged and aligned with the required tolerances after assembly (e.g. DE 34 04 061 Cl, DE 39 28 277 Cl) ,
- the length of the beam is then subjected to extensive adjustment work in order to align the lateral guide and sliding surfaces already present on the first equipment parts in line with the route and to compensate for any ripples that may exist.
- modules instead of the structural units extending over the entire beam length.
- These modules are made entirely of steel, for example, by welding or in a composite construction by using side guide rails, slide rails and stator beams must be inserted in a steel formwork with a precise fit before concreting.
- Such modules are intended on the one hand to prevent subsequent adjustment of the relative positions of the various functional surfaces to one another.
- the invention is based on the technical problem of designing the guideway of the type described in the introduction in such a way that it has the required dimensional accuracy over its entire length, without the equipment parts having to be aligned with complex measures.
- a route module and a method for its production are to be proposed, by means of which the establishment of a route for magnetic levitation vehicles greatly simplified and can still be carried out in compliance with the tolerances explained.
- FIG. 1 shows the perspective view of an ideally illustrated guideway module with the usual lateral guide, sliding and stator package mounting surfaces in the region of a guideway section passing through a curve;
- FIG. 2 shows the perspective illustration of a guideway module produced according to the invention
- FIG. 3 shows a greatly enlarged, schematic illustration of the attachment of a stator packet to a mounting surface of the module according to FIG. 2;
- FIG. 4 shows a schematic top view of a route according to the invention, made from modules according to FIG. 2;
- FIG. 7 shows a perspective top view of a further exemplary embodiment of a module according to the invention in a non-load-bearing construction
- Fig. 8 is a bottom perspective view of the module of Fig. 7; 9 schematically shows the assembly of the module according to FIGS. 7 and 8 on a concrete support;
- FIGS. 7 to 9 shows a schematic representation of a storage scheme for the module according to FIGS. 7 to 9;
- FIG. 11 schematically shows a further exemplary embodiment for the assembly of a module according to the invention in a non-load-bearing construction
- FIG. 12 shows a cross section along the line XII-XII of FIG. 11;
- FIG. 13 schematically shows a third exemplary embodiment for the assembly of a module according to the invention in a non-load-bearing construction
- FIG. 14 to 16 schematically show a detail of a fourth exemplary embodiment for the assembly of a module according to the invention in a non-load-bearing construction in a perspective view and in a cross-section and a longitudinal section through a bearing;
- FIG. 17 schematically shows a bottom view corresponding to FIG. 8 of a module according to the invention with a load-bearing construction.
- the module 1 shows an ideally illustrated guideway module 1 made of steel, which is suitable for erecting a guideway for a magnetic levitation railway with a long-stator linear motor.
- the module 1 is curved as a whole along a predetermined route, as indicated by a spatial curve 2 shown in its central plane.
- a Cartesian coordinate system with mutually perpendicular axes x, y and z is indicated schematically.
- a curvature around the x-axis means a cross slope in the sense of an elevation of a curve
- a curvature about the y-axis means a section of a path running through a crest or a valley
- a curvature about the z-axis means a cornering.
- the module 1 has on its top two parallel, essentially horizontally arranged and serving as sliding surfaces 3 sections and on its long sides two essentially vertical side guide rails 4, which are provided on their outer sides with side guide surfaces 5.
- On the underside of the module 1 there are also two substantially horizontal stator carriers 6, which are provided on their undersides with mounting surfaces 7 indicated in the left part of FIG. 1 for stator packages 8 indicated in the right part of FIG. 1. Otherwise, the module 1 is mounted on a support, not shown.
- the module 1 that can be seen in FIG. 1 and is adapted everywhere to the course of the route would have the advantage that almost ideal driving properties would result. It would be disadvantageous, however, that each individual module 1 would have to be adapted to the curvatures present there, depending on the location at which it is installed in the guideway, which would be very expensive to manufacture.
- a route produced with such modules 1 has therefore not become known to date. Rather, it is customary to design modules 1 all identically and to provide them with sliding, lateral guide and mounting surfaces 3, 5 and 7 that are flat within the production tolerances (e.g. DE 198 08 622 C2, EP 1 048 784 A2). In the area of curves or the like, these modules 1 are laid in the manner of a polygonal curve approximating the spatial curve 2.
- a module 1 is approximately 6 m, then five such modules 1 can be arranged polygonally one behind the other on an approximately 30 m long carrier.
- a polygonal laying of the modules 1 for magnetic levitation vehicles operated at speeds of 500 km / h and more is, however, only justifiable in the case of straight sections of the route or those with very large radii of curvature.
- Such an overall plate-shaped guideway module 10 essentially consists of a comparatively thin, plane-parallel one made of sheet steel
- Cover plate 11 on the underside of which serve the stiffening, vertically projecting webs 12 are preferably attached by welding.
- Conventional side guide rails 14 extending in the x direction are mounted on the lateral longitudinal edges of the cover plate 11.
- cover plate 11 On the upper side of the cover plate 11, two slide strips 15, also extending in the x direction, are attached.
- all guideway modules 10 are preferably manufactured identically, the side guide rails 14 and slide strips 15, which are generally referred to as first equipment parts, and the stator carriers 16, which are referred to as second equipment parts, all of which are designed to be straight and z. B. consist of substantially plane-parallel profiles.
- the equipment parts 14, 15 and 16 have on their outer, upper and lower sides the first functional surfaces explained with reference to FIG. 1 in the form of lateral guide surfaces 17 and sliding surfaces 18 and / or second functional surfaces in the form of mounting surfaces 19.
- These functional surfaces 17, 18 and 19 are produced according to the invention in that the equipment parts 14, 15 and 16 are all manufactured with a sufficient oversize and are then machined to a predetermined nominal size by machining. This is indicated in Fig. 2 by the hatched areas of the equipment parts, which represent an addition of material.
- the side guide rails 14 are machined to a final dimension d, the slide strips 15 to a final dimension h1 and the stator carriers 16 to a final dimension h2.
- the oversize or the original thickness of the side guide rails 14 is selected such that the outer surfaces of the side guide rails 14 are at a greater distance from one another after the manufacture of the module 10 than corresponds to the required track width.
- the oversizes or the heights of the slide bars 15 and stator carriers 16 are chosen so large that the upper sides of the slide bars 15 and the undersides of the stator carriers 16 have a greater distance from one another after the manufacture of the module 10 than corresponds to the required pincer dimension.
- the final completion of the module 10 takes place in a work step following the welding work by machining the surfaces produced with oversize. This machining is preferably done by milling, but could also be replaced by planing or any other suitable machining. The procedure is as follows, for example:
- a fictitious center or symmetry axis running parallel to the x-axis is first defined taking into account the individual oversize.
- This fictitious central axis can deviate from the actually existing (geometric) component axis in extreme cases by a few millimeters on both sides, e.g. B. because the side guide rails 14 or the slide rails 15 were not attached exactly.
- the side guide rails 14 are now machined on their outer sides in the y direction and the slide strips 15 on their upper sides in the z direction in order to thereby obtain the side guide surfaces 17 and the slide surfaces 18 according to FIG. 2. It is noteworthy that the side contact surfaces 17 in the z direction and the sliding surfaces 18 in the y direction do not require exact alignment and their position is therefore not critical in this respect.
- An advantage of the procedure described is that the side guide and sliding surfaces 17, 18 with the same workpiece clamping z. B. in a portal milling machine can be edited by z. B. an end mill is first used in a vertical position for the production of the side guide surfaces 17 and then in a horizontal position pivoted by 90 ° for the production of the sliding surfaces 18 and is moved once to the left and right of the fictitious central axis.
- the processing of the side guide rails 14 and slide strips 15 carried out in an individual case depends on whether it is a module 10 intended for straight travel or a module 10 intended for cornering, ascending or descending or the like.
- the finished lateral guide and sliding surfaces 14, 15 are each produced as planes running parallel to the xz or xy plane. If, on the other hand, there are modules 10 which are intended for a curved guideway section analogous to FIG. 1, then the side guide rails 14 and sliding surfaces 15 are machined in such a way that the side guide surfaces 17 and the sliding surfaces 18 assume a curvature that corresponds to that corresponding section of the space curve (eg 2 in Fig. 1) corresponds exactly.
- the milling process is carried out using a computer-controlled tool using all the necessary route data.
- the side guide and sliding surfaces 17, 18 according to FIG. 2 despite the modules 10 and equipment parts 14, 15 and 16 originally formed straight after machining, have exactly the same curvatures as in FIG. 1 for the side guide surfaces shown there 5 and sliding surfaces 3 have been described as ideal because they follow the route exactly.
- the invention thus has the advantage that the lateral guide and sliding surfaces 17, 18 are not only formed exactly parallel to one another with the aid of a comparatively simple milling operation, but are also optimally adapted to the route of the route over the entire beam length because of the selected oversize can.
- the resulting tolerance deviations are much smaller than those that would result from polygonal laying of identically designed straight modules.
- the effort to be made in the manufacture of the modules 10 is considerably less than if the side guide rails 14 and slide strips 15 were to be adapted to the associated space curve sections as before, or the modules as a whole had to be individually curved analogously to FIG. 1.
- the stator packs 8 can be attached to the stator supports 16 in various ways known per se (for example DE 34 04 061 C2, DE 39 28 278 C2).
- the fastening means shown in FIG. 3 are provided in analogy to DE 39 28 278 C2.
- the mounting surfaces 19 on the undersides of the stator carriers 16 are designed as first stop surfaces 20 (FIG. 3). These stop surfaces 20 not only have to be manufactured precisely and arranged as parallel as possible to the sliding surfaces 18 (FIG. 2), since they determine the exact position of the stator packs 8 on the modules 10.
- a preselected distance from the sliding surfaces 18 in the z direction which is used to define a preselected pliers dimension serves, which corresponds to the distance of the sliding surfaces 18 from the undersides 21 of the stator packs 8 in the installed state and determines, among other things, the extent to which the vehicles have to be lifted from a standstill to the floating state when starting.
- the undersides 21 interact in a known manner with the support and excitation magnets of the vehicles to form a gap.
- the stator packs 8 are fixedly connected on their upper sides to traverses 22 which extend transversely to their longitudinal directions or in the y direction and which have projections 22a with dovetail or T-shaped cross sections which project above the stator packs 8 and also run in the y direction.
- the upper sides of these projections 22a are designed as second stop surfaces 23 (FIG. 3), which run exactly parallel and at constant distances from the lower sides 21.
- the lugs 22a are used to produce a redundant, detachable connection to the modules 10 in grooves 24 (FIG. 3), which are formed on the undersides of the stator carrier 16, dovetail or T-shaped cross sections substantially corresponding to the cross sections of the lugs 22a have and are arranged substantially parallel to the y direction of the modules 10.
- the bottoms of these grooves 24 form the stop surfaces 20, which interact with the stop surfaces 23 and determine the position and orientation of the stator packs 8 and the undersides 21.
- the guideway modules 10 are clamped in a drilling and / or slot milling machine in order to produce the grooves 24, the stop surfaces 20 in a manner known per se and to form the bores for the fastening screws in the stator carrier 16.
- the extent of the stop surfaces 20 in the y direction is not critical, and in the x direction there are as many first stop surfaces 20 in each case as preselected distances as cross members 22 are attached to the stator packs 8.
- the stator supports 16 can have lengths corresponding to the stator packs 8 or the modules 10 or can consist of individual components spaced apart according to the grooves 24.
- all of the stop surfaces 20 assigned to a specific stator package 8 each lie in one plane. As long as straight track sections are involved, the stop surfaces 20 of all associated stator packs 8 lie in the same (xy) plane. If, on the other hand, there are curved travel path sections, then the abutment surfaces 20 each lie in planes that differ from one another in such a way that after assembly of the stator packs 8, the polygonal arrangement explained above automatically results.
- stator packs 8 are fastened to the stator supports 16 after the lugs 22a have been inserted into the grooves 24 with the aid of only schematically illustrated fastening screws which pass through the crossbeams 22, the cross-sections of the lugs 22a and the grooves 24 described ensuring that, in the case of a possible later fatigue fracture of any of these fastening screws does not drop the stator package 8 in question.
- the projections 22a can also be arranged with a slight play in the grooves 24.
- stop surfaces 20, 23 are then only in the assembled state of the stator packs 8 produced by the fastening screws, while in the absence of fastening screws between the stop surfaces 20, 23 there is a small gap which is detected by sensors carried on the vehicles and for detection a broken screw can be used.
- a straight track section 25 with a plurality of straight modules 10a intended for straight travel is followed by a transition section 26 with two modules 10b, 10c, which form a transition from the straight track section 25 to a curve section 27 which is curved with a comparatively small radius of curvature and includes a plurality of modules 10d, 10e and 10f, etc.
- the route modules 10a are manufactured in a completely straight design and are provided with flat lateral guide and sliding surfaces 17a, 18a.
- the modules 10d, 10e and 10f etc. are also produced in a completely straight design in the manner explained with reference to FIGS. 2 and 3, but with this then provided with side guide and sliding surfaces 17b, 18b, which are curved in all three directions (Fig. 1).
- the travel path modules 10b, 10c in the transition section 26 could in principle be designed analogously to those in the curve section 27. According to the invention, however, a modified manufacturing technique compared to FIG. 2 is used for these modules 10b, 10c. It is assumed that in the transition section 26 the curvatures still run along such large radii that a polygon-like laying of completely straight modules 10b, 10c corresponding to the modules 10a would in principle suffice. However, since a comparatively large tilting of the modules 10d, 10c, 10f, etc. is required in the curve section 27 (maximum approx.
- the modules 10b, 10c can be twisted, for example, before they are attached to the relevant support by means of grout or the like. With the aid of a mounting frame carried on a laying train or simply by screwing them in the area of their end faces with the aid of screw connections adjustable in the z direction concerned carrier are attached. To enable such a twist, the modules 10b, 10c are either designed to be sufficiently flexible by, for example, B. ver stiffening bulkheads and other cross connections can be omitted or by making them from a comparatively soft material. As the twisting is only required by a few millimeters, it also poses no problems for modules with a length of up to approx. 6 m. Apart from this, it is clear that the curvatures in FIG. 4 are exaggerated and that the invisible parts of the modules are essentially straight and identical.
- FIG. 7 and 8 show details of a module 10g according to the invention from above and below analogous to FIG. 2, but in the still unprocessed state of the various pieces of equipment. It can be seen in particular from FIG. 8 that the webs 12 can be connected by bulkheads 29 in order to obtain a rigid overall construction with the cover plates 11.
- the cover plates 11, webs 12 and bulkheads 29 are expediently connected by welding.
- the module 10g according to FIGS. 7 and 8 is designed as a so-called "non-supporting" component and, according to the invention, is provided with an integral bearing. This means that the forces exerted on the module 10g are introduced directly into the carrier located underneath, but adjacent modules 10g are connected to one another in the x-direction but not in a shear-resistant manner.
- Rod-shaped or band-shaped bearing elements which are flexible at least in a predetermined direction, are preferably used as integral bearings.
- Fig. 8 shows, z. B. in the region of the front and rear end faces band-shaped bearing elements 30 are provided, which are flexible in the x direction (FIG. 1), but are essentially rigid in the y direction.
- band-shaped bearing elements 31 are attached, which are only flexible in the y direction but not in the x direction.
- the bearing elements 30, 31 thus fulfill the function of a flexible bearing that is flexible in one direction.
- a fixed bearing can expediently be provided in a central region of the module 10g, by assembling a bearing element 32 with a cross-shaped cross section from each of the bearing elements 30, 31 (see also FIG. 10).
- Suitable materials for the bearing elements 30, 31 and 32 are bearing plates with a correspondingly reduced bending stiffness or with particular advantage spring plates, ie sheet metal strips made from spring steel.
- the module 10g can be mounted on a primary carrier 33 made of concrete according to FIG.
- FIGS. 11 and 12 An alternative embodiment of the invention for the bearing elements is shown in FIGS. 11 and 12.
- rod-shaped bearing elements 36 in the form of rods with a square cross section are provided here.
- the bearing elements 36 are attached to the undersides of modules 10a in a cross-shaped pattern, indicated in FIG. 12, and are fastened to a carrier 37 in a manner not shown in more detail (eg analogously to FIG. 9).
- the bearing elements 36 are z. B. from bending rods that are flexible at least in the x and y directions and when using circular cross sections in practically all directions transverse to their longitudinal axes. They therefore essentially fulfill the task of free bearings that can absorb forces in several directions, such as z. B. occur with temperature fluctuations. Such free camps can, for. B. can be provided in Fig. 10 at the points marked with circles.
- the number of bearing elements 36 that are used per bearing location depends in particular on the materials selected and the desired spacing of the modules 10h from the supports 37.
- FIG. 13 shows a further exemplary embodiment according to the invention for fastening modules 10i to a carrier 38.
- FIGS. de bearing elements 39 firmly attached to the tops of the carrier 38 and provided at their upper ends with connecting flanges 40.
- connection flanges 41 arranged at the respective fastening points.
- B. attached by welding. It is then only necessary to place the modules 10 with their flanges 41 on the flanges 40 and then to connect the two by means of fastening screws 42 projecting through the flanges 40, 41.
- This has the advantage that the modules 10 are releasably connected to the supports 38 and can be easily dismantled and replaced if necessary.
- this variant offers the advantage over FIGS. 9 and 11 that, by introducing shims between the flanges 40, 41, it is easily possible to align the individual modules 10 i in line with the route and in the region of the joints without an offset on the support 38.
- the bearing elements 39 can be designed analogously to FIGS. 7 to 12.
- FIGS. 14 to 16 A further exemplary embodiment, which was previously considered to be the best for a component that does not support, is shown in FIGS. 14 to 16.
- the bearing elements 30 according to FIGS. 7 and 8 are replaced here by pairs 43 each consisting of two band-shaped bearing elements 43a, 43b arranged parallel to one another in the manner of leaf springs. Similar to the exemplary embodiments according to FIGS. 11 and 13, the bearing elements 43a, 43b are separate components that are flexible in the x-direction (see also FIG. 1). As shown in particular in FIGS. 14 to 16, the underside of the Module lOj on front and rear
- plate-shaped spacers or spacer plates are preferably arranged between the mounting strips 44 and the bearing elements 43a, 43b.
- these serve the purpose of allowing resilient movements of the bearing elements 43a, 43b without abutment on the mounting strips 44 or without bending around their lower ends.
- comparatively short spacers can enlarge the lever arms of the bearing elements 43a, 43b, which improves the spring properties.
- two pairs 43 of bearing elements 43a, 43b are provided in the front and rear area of the module 10j, which are flexible in the x direction but not in the y direction are and how the bearing elements 30 perform the function of floating bearings.
- Two or more further bearing elements 49 provided in a central region of the module lOj preferably also represent separate components which can be connected to the module lOj by screws, but are designed as fixed bearings which, for. B. fulfill the function of the fixed bearing 32 in Fig. 8 to 10.
- a major advantage of the embodiment according to FIGS. 14 to 16 is that the modules 10j and the bearing elements 49 are made of a sufficiently rigid material for static purposes, while the spring elements 43a, 43b are made of a material such as. B. spring steel can be made, the temperature expansions or compressions.
- Another resulting advantage over the exemplary embodiment according to FIGS. 7 to 10 is that shorter bearing elements in the z-direction and thus lower mounting heights of the modules 10j above the supports 33 can be realized.
- Floating bearings effective in the y direction are not provided in the exemplary embodiment according to FIGS. 14 to 16. They can be omitted if the expected temperature expansions or compressions z. B. due to small module widths of z. B. 1 m are comparatively small. It is also clear that instead of using the bearing elements or leaf springs 43a, 43b in pairs, the use of only one bearing element or of more than two bearing elements per bearing point could also be provided.
- FIG. 17 shows an exemplary embodiment of the invention for a module 10k in the form of a "load-bearing" component, i. H. of a component that is connected to both the associated carrier and to corresponding modules 10k of the same carrier that are in front of or behind it in the x direction.
- the bearing elements 30, 31, 32, 36, 39 and 43 are replaced here by comparatively rigid strips or webs 50 and 51 which protrude downwards from the underside of the modules 10k and run in the transverse and longitudinal directions, in which holes 52, 53 are trained.
- these holes 52, 53 can be used to hold screws or dowels in order to fasten abutting modules 10k to one another or to the relevant support, or they can serve as openings for concrete or reinforcement bars and protrude into corresponding recesses in a concrete support.
- the modules 10k are also preferably provided with through holes 54 which are formed in the cover plates 11 and which can be used as concreting openings and allow secondary mortar to flow into the recess bars of the beams.
- other thrust composite means in the form of head anchors or the like can also be provided.
- the exemplary embodiments described all make it possible to prefabricate the modules 10 by welding or in some other way, and only then to provide the individual functional surfaces 17, 18 and 19 with precise machining by machining, in particular milling. This prevents the functional surfaces 17, 18 from being distorted due to welding or straightening work to be carried out subsequently and 19 occurs, which would then require reprocessing or fine adjustment.
- the modules 10 can be produced in series production and identically, since the final shaping of the side guide, sliding and mounting surfaces 17, 18 and 19 takes place only afterwards. It is clear that the respective oversize of the associated functional components 14, 15 and 16 is expediently chosen to be larger than the greatest material thickness to be removed by machining in a projected travel path. So far, values of approx.
- the slide strips 15 are made according to a particularly preferred embodiment of the invention made of stainless steel or weatherproof steel. This results in the advantage that in the event of any emergency stops of the vehicles, when the skids of the vehicles are deposited on the slide rails 15 for other reasons or, for. B. when clearing snow with a snow removal vehicle, which has a clearing blade resting on the sliding strips 15, there is no danger that an insulation layer provided on the sliding strips 15 is damaged or completely scraped off. Such an insulation layer is generally applied in particular for corrosion protection on all three functional surfaces 17, 18 and 19 and also the stop surfaces 20 and has a thickness of e.g. 0.5 mm usually comparatively thin. When using slide strips 15 made of stainless steel or weatherproof steel, their insulation layer can be omitted.
- the invention is not limited to the exemplary embodiments described, which could be modified in many ways. This applies in particular to the number and the Arrangement of the side guide rails 14 and slide strips 15 used in individual cases. Depending on the type of magnetic levitation vehicle, it can be e.g. B. be sufficient to provide only a single slide bar 15 and side guide rail 14 in a central region of the modules 10, which side guide rail 14 could be provided on both sides of an imaginary central axis with side guide surfaces. Accordingly, only a single linear motor could be used for the drive, in which case it would be sufficient to provide the modules with only one row of stator supports 16 running in the longitudinal direction and grooves 24 or stop faces 20 formed on them.
- the length of the modules 10 can be varied and, for example, only be approximately 2 m instead of approximately 6 m.
- the various bearing elements described with reference to FIGS. 7 to 16 serve only as examples, which can be replaced by other bearing elements as needed and appropriate.
- the shape and design of the modules 10 as a whole were only given as examples. So it would be z. B. possible to connect the equipment parts 14, 15 and 16 by welding to form a rigid frame and then pour it in a manner known per se with concrete. Following this, the machining of the various pieces of equipment could then take place as described.
- the various supports (FIGS. 7 to 17) can also be advantageously used independently of the special modules according to FIGS. 1 to 6.
- the various features can also be used in combinations other than those described and illustrated.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Railway Tracks (AREA)
- Buildings Adapted To Withstand Abnormal External Influences (AREA)
- Working Measures On Existing Buildindgs (AREA)
- Connection Of Plates (AREA)
- Bridges Or Land Bridges (AREA)
Abstract
Description
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Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU2003273369A AU2003273369A1 (en) | 2002-05-28 | 2003-05-23 | Driveway, driveway module, and method for the production thereof |
US10/517,354 US20060032395A1 (en) | 2002-05-28 | 2003-05-23 | Driveway, driveway module, and method for the production thereof |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
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DE10224148.1 | 2002-05-28 | ||
DE2002124148 DE10224148A1 (de) | 2002-05-28 | 2002-05-28 | Fahrweg, Fahrwegmodul und Verfahren zu dessen Herstellung |
DE20210808.2 | 2002-07-15 | ||
DE20210808U DE20210808U1 (de) | 2002-07-15 | 2002-07-15 | Fahrweg und Fahrwegmodul für Magnetschwebefahrzeuge |
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WO2003102303A1 true WO2003102303A1 (de) | 2003-12-11 |
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PCT/DE2003/001697 WO2003102303A1 (de) | 2002-05-28 | 2003-05-23 | Fahrweg, fahrwegmodul und verfahren zu dessen herstellung |
PCT/DE2003/001698 WO2003102304A1 (de) | 2002-05-28 | 2003-05-23 | Fahrweg für magnetschwebefahrzeuge |
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PCT/DE2003/001698 WO2003102304A1 (de) | 2002-05-28 | 2003-05-23 | Fahrweg für magnetschwebefahrzeuge |
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US (2) | US20050232698A1 (de) |
CN (2) | CN100489194C (de) |
AU (2) | AU2003249841A1 (de) |
WO (2) | WO2003102303A1 (de) |
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DE10353949A1 (de) | 2003-11-18 | 2005-06-16 | Max Bögl Bauunternehmung GmbH & Co. KG | Verfahren zum lagegenauen Aufstellen eines Trägers für einen Fahrweg und Fahrweg |
DE102006003680A1 (de) * | 2006-01-24 | 2007-07-26 | Thyssenkrupp Transrapid Gmbh | Biegeträger aus Stahl und eine damit hergestellte Weichenanordnung für Magnetschwebebahnen |
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DE102006025014A1 (de) * | 2006-05-26 | 2007-11-29 | Max Bögl Bauunternehmung GmbH & Co. KG | Fahrweg |
CN101619921B (zh) * | 2008-07-02 | 2010-08-25 | 江苏华宇印涂设备集团有限公司 | 一种输送链条导轨浮动支承烘房 |
WO2012101624A1 (en) | 2011-01-26 | 2012-08-02 | Rainis Dov | A support apparatus and method for a sliding frame |
CA2840255C (en) * | 2011-06-30 | 2018-03-20 | Hm Attractions Inc. | Motion control system and method for an amusement ride |
CN103769801B (zh) * | 2012-10-23 | 2017-02-01 | 南京梅山冶金发展有限公司 | 底侧卸式矿车卸载站空间曲轨制作方法 |
WO2017083499A1 (en) * | 2015-11-10 | 2017-05-18 | Skytran Inc. | Segmented track for a maglev vehicle |
US10584448B1 (en) * | 2017-03-17 | 2020-03-10 | David Ralph Ward | Continuous serpentine concrete beamway forming system and a method for creating a hollow continuous serpentine concrete beamway |
CN110195385A (zh) * | 2019-06-28 | 2019-09-03 | 上海交通大学 | 一种用于磁悬浮线路的迭合式轨道梁 |
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- 2003-05-23 CN CNB038119455A patent/CN100489194C/zh not_active Expired - Fee Related
- 2003-05-23 AU AU2003249841A patent/AU2003249841A1/en not_active Abandoned
- 2003-05-23 WO PCT/DE2003/001697 patent/WO2003102303A1/de not_active Application Discontinuation
- 2003-05-23 CN CNB038119463A patent/CN100547163C/zh not_active Expired - Fee Related
- 2003-05-23 AU AU2003273369A patent/AU2003273369A1/en not_active Abandoned
- 2003-05-23 US US10/517,353 patent/US20050232698A1/en not_active Abandoned
- 2003-05-23 US US10/517,354 patent/US20060032395A1/en not_active Abandoned
- 2003-05-23 WO PCT/DE2003/001698 patent/WO2003102304A1/de not_active Application Discontinuation
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Also Published As
Publication number | Publication date |
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US20050232698A1 (en) | 2005-10-20 |
CN100547163C (zh) | 2009-10-07 |
CN1656284A (zh) | 2005-08-17 |
AU2003249841A1 (en) | 2003-12-19 |
WO2003102304A1 (de) | 2003-12-11 |
US20060032395A1 (en) | 2006-02-16 |
AU2003273369A1 (en) | 2003-12-19 |
CN1656285A (zh) | 2005-08-17 |
CN100489194C (zh) | 2009-05-20 |
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