This application is the United States national phase of International Application No. PCT/EP2018/062221 filed May 11, 2018, and claims priority to United Kingdom Patent Application No. 1707571.4 filed May 11, 2017, the disclosures of which are hereby incorporated by reference in their entirety.
The present invention relates to a running gear for a rail vehicle, in particular of a locomotive. It also relates to a vehicle provided with one or more such running gears.
Rail vehicles often comprise two suspension stages, namely a primary suspension stage between axle and running gear frame and a secondary suspension stage between the running gear frame and the vehicle body. The primary suspension stage ensures the stability of the vehicle and minimises the burden on the infrastructure, particularly in curves. To fulfil these functions, the primary suspension should have a low stiffness in a longitudinal direction of the vehicle, so that the wheel axle can turn around a vertical axis, and a high stiffness in the transverse direction to ensure a sufficient driving stability.
The primary suspension stage of many rail vehicles, locomotives in particular, includes primary springs such as helical springs, which have the same stiffness in the longitudinal and transverse directions. Thus, the above-mentioned requirement for simultaneous high transverse stiffness and low longitudinal stiffness cannot be met. For safety reasons, the driving stability is granted priority and, therefore, the primary springs are designed so that they have a high horizontal stiffness. This results in a high longitudinal stiffness and increased loads on the tracks.
A primary suspension comprising helical springs having a low horizontal stiffness was proposed in EP1569835. To increase the lateral stiffness of the primary suspension an additional rubber-metal spring is mounted parallel to the helical springs. The rubber-metal spring has a higher stiffness in the transverse direction than in the longitudinal and vertical. In this way, the transverse stiffness is increased while the longitudinal stiffness remains virtually unchanged. However, additional space is necessary for the parallel connection of the rubber-metal springs and helical springs.
Another cumbersome design with multiple parallel springs for generating different longitudinal and transverse stiffness is known from U.S. Pat. No. 4,674,413.
A series connection of two springs is known from EP2000383. Here, a helical spring and a serially connected second rubber-metal spring provide together a two-stage spring characteristic. However, no differentiation of the stiffness in the longitudinal and transverse directions is obtained.
The invention aims to provide a running gear with a two-stage suspension that has an improved primary stage characteristic, to provide a low longitudinal stiffness and a higher transverse stiffness in a compact layout.
According to a first aspect of the invention, there is provided, a running gear for a rail vehicle, comprising one or more wheel sets, each having a revolution axis, each of the wheel sets being guided by a pair of transversally spaced axle boxes, a running gear frame, a primary suspension assembly between each of the axle boxes and the running gear frame, and a secondary suspension stage for supporting a vehicle superstructure of the rail vehicle on the running gear frame, wherein each primary suspension assembly comprises at least a main spring assembly having a vertical stiffness and a horizontal stiffness that is identical in a transverse direction of the running gear frame and in a longitudinal direction of the running gear frame perpendicular to the transverse direction, characterised in that the primary suspension assembly further comprises an anisotropic interface assembly in series with the main spring assembly between the running gear frame and the axle box, wherein the anisotropic interface assembly is such that the primary suspension assembly has a transverse stiffness and a longitudinal stiffness, wherein the transverse stiffness is substantially different from the longitudinal stiffness.
The series connection of two spring assemblies with different characteristics enables to define the resulting longitudinal stiffness and transverse stiffness independently from one another.
According to a preferred embodiment, the anisotropic interface assembly comprises an intermediate spring seat for receiving an end of the main spring assembly, which can be an upper end if the anisotropic interface assembly is located between the main spring assembly and the running gear frame, or a lower end if the anisotropic interface assembly is located between the main spring assembly and the axle box.
According to a preferred embodiment, the anisotropic interface assembly comprises a guiding structure and guiding means for limiting or suppressing at least two degrees of freedom of motion of the intermediate spring seat relative to the guiding structure, comprising at least one degree of freedom of translation in a longitudinal or transversal direction and at least one degree of freedom of rotation about a longitudinal or transversal axis. Preferably, the guiding means are such as to limit or suppress at least one degree of freedom of translation in the transversal direction and at least one degree of freedom of rotation about an axis parallel to the longitudinal axis. Advantageously, the anisotropic interface comprises at least one resilient element between the guiding structure and the intermediate spring seat.
According to one embodiment, the guiding means are such that the intermediate spring seat has only one degree of freedom of rotation relative to the guiding structure, about a transverse axis of rotation.
According to one embodiment, the guiding means are such that the intermediate spring seat has only one degree of freedom of translation relative to the guiding structure, parallel to a longitudinal direction or the running gear.
The installation space, in particular the height, is a constraint for accommodating the first and second spring assemblies. According to a preferred embodiment, the main spring assembly consists of one or more helical springs. Preferably, the anisotropic interface assembly is at least partially received in an inner volume axially and radially confined within the one or more helical springs of the main spring assembly.
According to one embodiment the anisotropic interface assembly has a torsional stiffness about a pitch axis parallel to the transverse direction. Preferably, the torsional stiffness is substantially constant or increases when the angular deflection increases relative to a nominal position increases.
The longitudinal stiffness has a shear stiffness component and a bending stiffness component about a transverse axis. According to one embodiment, the pitch axis is located above an upper end of the main spring assembly or below a lower end of the main spring assembly. Preferably the longitudinal stiffness of the primary suspension assembly is such that the one or more wheel sets is able to pivot about a vertical axis of the running gear.
According to another aspect of the invention, there is provided a rail vehicle, in particular a locomotive, provided with at least one running gear as described hereinbefore.
Other advantages and features of the invention will become more clearly apparent from the following description of a specific embodiment of the invention given as non-restrictive examples only and represented in the accompanying drawings in which:
Corresponding reference numerals refer to the same or corresponding parts in each of the figures.
Each wheels set 16 comprises a pair of left and right wheels 24 attached to an axle 26 guided by a pair of laterally opposite axle boxes 28 so as to revolve about a revolution axis RR. In a standard rest position of the rail vehicle on a straight horizontal track, the revolution axes RR of the wheel sets 16 are horizontal and parallel to one another and to the transverse reference axis TT of the running gear frame 18.
The primary suspension stage 20 comprises a primary suspension assembly 30 between each axle box 28 and the running gear frame 18. Each primary suspension assembly 30 comprises a main spring assembly 32 and an anisotropic interface assembly 34 in series with the main spring assembly 36, which can be located between the main spring assembly 36 and the axle box 28 or between the main spring assembly 36 and the running gear frame 18.
According to a first embodiment of the primary suspension assembly illustrated in
The anisotropic interface assembly 34 consists of the intermediate spring seat 40, of a guiding structure 42 that is rigidly attached to or integral with the running gear frame 18 and of an intermediate elastomeric structure 44 which extends between the intermediate spring seat 40 and the guiding structure 42. The guiding structure 42 comprises an upper rigid convex cylindrical surface 46 which faces a lower rigid concave cylindrical surface 48 formed on the intermediate spring seat 40. The intermediate elastomeric structure 44 forms a cylindrical layer between the concave and convex cylindrical surfaces 46, 48.
The cylinder axis CC is located above the main spring assembly 32. Remarkably, the intermediate spring seat 40 is cup-shaped and has a central part 50 that extends within the inner cylindrical space CS surrounded by the helical spring. As a result, the anisotropic interface assembly 34 partly overlaps with the main spring assembly 32 in the vertical direction and the overall height of the primary suspension assembly 30 is not substantially increased by the presence of the anisotropic interface assembly 34.
This arrangement allows the intermediate spring seat 40 to pivot with respect to the guiding structure 42 about the cylinder axis CC with a low stiffness. This movement is referred to as tilting and results in a limited freedom of movement of each axle box 28 in the longitudinal direction LL. On the other hand, due to the cylindrical shape of the elastomeric layer 44, the turning stiffness about an axis perpendicular to the cylinder axis CC, is substantially higher than in the longitudinal direction LL.
The anisotropic interface assembly 34 substantially reduces the longitudinal stiffness of each primary suspension assembly 30, and does not substantially impact the stiffness in the vertical and transverse directions.
The freedom of movement of each axle box 28 with respect to the running gear frame 18 in the longitudinal direction LL of the running gear frame allows each wheel axle 26 to pivot about an imaginary vertical axis so as to minimise the load on the track.
Due to the compact layout of the anisotropic interface assembly 34 within the main spring assembly 32, this embodiment is particularly suitable for retrofitting pre-existing vehicles.
The behaviour of the anisotropic interface assembly 34 and of the whole primary suspension assembly is essentially the same as for the embodiment of
The embodiment of
As a variant, the protrusion can be formed on the intermediate spring seat 40 and the recess in the guiding structure 42.
The embodiment of
The embodiment of
The embodiment of
As a result, the anisotropic interface assembly 34 provides one degree of freedom of rotation to the upper end of the main helical springs 32 about the pitch axis CC. When subjected to load in the longitudinal direction LL, the upper end of the helical spring 32 does not remain parallel to its lower end and the helical spring 32 is allowed to bend slightly. In the transverse direction TT on the other hand, the anisotropic interface assembly 34 does not provide any degree of freedom, and the two ends of the helical spring 32 remain parallel to one another. As a result, the stiffness in the longitudinal direction LL is substantially lower than in the lateral direction TT.
The running gear of
Number | Date | Country | Kind |
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1707571 | May 2017 | GB | national |
Filing Document | Filing Date | Country | Kind |
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PCT/EP2018/062221 | 5/11/2018 | WO |
Publishing Document | Publishing Date | Country | Kind |
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WO2018/206771 | 11/15/2018 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
1758350 | Bush | May 1930 | A |
4674413 | Eggert, Jr. | Jun 1987 | A |
5005489 | Terlecky | Apr 1991 | A |
7448329 | Muller et al. | Nov 2008 | B2 |
8047514 | Wolf | Nov 2011 | B2 |
20190344811 | Wolf | Nov 2019 | A1 |
Number | Date | Country |
---|---|---|
19546007 | Jun 1997 | DE |
0050727 | May 1982 | EP |
1569835 | Sep 2005 | EP |
2000383 | Dec 2008 | EP |
H0370569 | Mar 1991 | JP |
2007045275 | Feb 2007 | JP |
2007045275 | Feb 2007 | JP |
Number | Date | Country | |
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20200070854 A1 | Mar 2020 | US |