The invention at hand relates to a tank container (1) having a tank (2) and a framework which receives the tank (2) via end frames (3). Here, the end frames (3) are connected to one another in the lower region via a longitudinal frame structure (5) that has two lateral longitudinal carriers, with the latter being additionally connected to the end frame at their ends in each case via a lateral diagonal member and a base diagonal member. Here, the lateral diagonal members each run in lateral vertical planes at a slant between the longitudinal carrier and a corner support and the base diagonal member—also at a slant—in a horizontal plane close to the bottom between the longitudinal carrier and a lower transverse spar. Here, the corner support and lower transverse spar are elements of the end frame.
Tank containers in which the tank is coupled to an end frame at each of its ends have been known from DE 202 11 594 U1, DE 297 05 851 U1 and from EP 0 425 190 A1, for example.
DE 297 05 851 U1 and DE 202 11 594 U1 show a coupling between tank and end frame via so-called end ring saddling mechanisms.
EP 0 425 190 A1 shows specific saddle elements that connect the tank to the end frame in particular in the area of the corner fittings. This way, transport and handling forces are to be transmitted to the corner fittings as directly as possible and in particular in the area of the lower corner fittings. However, such saddle structures have the disadvantage that they are costly to manufacture and complicate the insulation of the tank since, on the one hand, insulation layers and coverings must be interrupted in this area and, on the other hand, the specific saddle structures represent thermal bridges that cause a great thermal transfer between the tank and its surroundings.
In the meantime, in order to solve this problem, the majority of tank containers that are being manufactured are those in which the tank is connected to the end frame only via the end rings or, respectively, end ring segments. For reinforcement and stabilization, the end frames are provided with additional longitudinal frame structures at least in the area of the lower corner fittings.
During switching operations during rail transportation, acceleration forces may occur in the direction of the longitudinal axis 64 that are caused by acceleration forces that amount to four to six times those of gravity (g). Therefore, the longitudinal carrier 62 is made very strong in conventional tank containers. Only in this way can it absorb the reaction forces introduced locally by the base and lateral diagonal members 68, 66 without any plastic deformation. In particular the structural elements of the frame make this known design relatively heavy.
Starting from this set of problems, the objective of the invention at hand is to provide an end-saddled tank container with a lighter frame structure. An additional objective may be the optimization of the transfer of forces between tank and frame structure in such a way that the frame structure and in particular the introduction of forces between corner supports, lateral diagonal members and longitudinal carriers or, respectively, between transverse spars, base diagonal members and longitudinal carriers is carried out in such a way that in particular these structural components can be made lighter while having the same stability.
The tank container in accordance with Claim 1 meets this objective, being characterized by the fact that the base and/or lateral diagonal members have an open cross-sectional profile. Such an open cross-sectional profile permits a design of the respective structural elements (base and/or lateral diagonal members) so that the tensions occurring during periods of stress are distributed more evenly and local tension peaks at the connection locations of the structural elements in question (longitudinal carrier, lateral diagonal members, corner support; longitudinal carrier, base diagonal member, transverse spar) are reduced. The open cross-sectional profile permits a “soft” connection that permits a high degree of own elasticity of the overall structure without reducing the necessary stability too much. Therefore, considerably lighter structural elements can be used as longitudinal carriers and as corner supports without reducing the stability of the overall structure too much.
In the further development of the invention in accordance with Claim 2, an open trapeze cross section is provided for the lateral diagonal member, with two lateral portions protruding from a base flange at an angle of between 145 and 165° each. This design permits an extended connection segment of the lateral diagonal member to the longitudinal carriers and to the corner supports. The specially selected slant assures in the marginal areas (i.e. in the areas of the lateral portions) a relatively soft and long coupling with the upper side of the longitudinal carriers that becomes gradually stiffer towards the base flange. Undesired point loads are avoided and buckling stresses on the longitudinal carrier are reduced. The symmetric structure in accordance with Claim 3 permits a cutting scrap-poor manufacture of the lateral diagonal members by trimming correspondingly profiled materials sold by the meter.
The further embodiment of the invention in accordance with Claim 4 permits a further improved load transmission between longitudinal carrier and corner support. The longitudinal design of the lateral diagonal member in accordance with Claim 5 optimizes the free buckling lengths on the longitudinal carrier and leads, together with the measure in accordance with Claim 6, to a further optimized construction in terms of material and weight.
The version in accordance with Claim 7 improves the flow of forces between lateral diagonal member and longitudinal carrier. In this version—with a corresponding design of the longitudinal carrier as a hollow profile—the relatively stable base flange area engages with a relatively soft connecting segment of the longitudinal carrier. This results in an elastic coupling of components with improved stress distribution as well.
The further embodiments of the invention indicated in Claims 8 through 13 relate to the design of the base diagonal member which in accordance with Claim 8 has a cap profile cross section that is open downward. Such a cap profile has structural advantages similar to the open trapeze cross section of the lateral diagonal member described above. But here, the free edges of the lateral shanks are stiffened by means of additional brim shanks (Claim 9). This makes it possible to design the overall profile even flatter while still having sufficient buckling or, respectively, bulging stability. This flat construction allows more ground clearance for connections or, respectively, for insulations of the tank in particular in the connecting area of the base diagonal member to the end-side transverse spars.
This effect is additionally reinforced through the inclination in accordance with Claim 10; at the same time, this design prevents wetness and dirt from collecting on the main flange of the base diagonal member, thereby creating corrosion problems. The arrangement of the angle relative to the longitudinal carrier in accordance with Claim 11 permits a structurally particularly favorable connection here as well and an improved load transfer between transverse spar and longitudinal bearing.
The tapering in accordance with Claim 12 permits a weight-optimized design of the base diagonal member together with a tension-optimized load transfer between transverse spar and longitudinal carrier. The profile depth of the cap profile (height H) in accordance with Claim 13 permits the connection of a relatively flat (low) transverse spar to a relatively high longitudinal spar (seen in vertical direction)—here with a “soft” connection between base diagonal member and longitudinal carrier or, respectively, transverse spar as well.
The overlapping connection areas in accordance with Claim 14 permit a particularly buckle-optimized load introduction of the base and lateral diagonal members into the lateral longitudinal carriers.
The form of the longitudinal carrier in accordance with Claim 15 permits the further optimizable load introductions into the longitudinal carriers in vertical direction (lateral diagonal members) and horizontal direction base diagonal members).
The further embodiment of the invention in accordance with Claims 16 through 18, in conjunction with the special lateral and base diagonal members, permits a considerably lighter version as compared with conventional end ring designs. In this regard, the coupling socket segment in accordance with Claim 17 is particularly easy to install in the alignment of the end frame with the tank, and the further embodiment in accordance with Claim 18 permits a particularly economical manufacture of the saddle ring elements.
An example of an embodiment of the invention at hand is explained by way of the drawings in exemplary fashion; shown are:
The basic structure of a tank container 1 in accordance with the invention will now be explained in detail by way of
The tank 2 is represented in
The left half of
The longitudinal frame structure 5 here comprises lower longitudinal carriers 12 whose ends are in each case connected with the end frame 3. In addition, lateral diagonal members 14 are provided that lead to the end frames 3, starting from the lower longitudinal carriers and running upward at an angle. The base diagonal members 16 are provided in the bottom area that also extend at an angle to the end frames 3 in a vertical plane close to the ground, starting from the lower longitudinal carriers 12 (see also
The end frames 3 are each composed of corner supports 18, lower corner fittings 20, upper corner fittings 22, an upper transverse spar 24, a lower transverse spar 26 or, respectively, 26′, upper end diagonals 28 and lower end diagonals 30.
The lateral diagonal members 14 each connect a segment L (see
The cross section of the lateral diagonal member 14 represented in
The lateral diagonal members 14, together with the lower longitudinal carrier, form an angle α (see
The structure and the arrangement of the lateral diagonal member 14 described above permit a particularly favorable transfer of the tension load between the connection area M to the corner supports 18 and the connection area L on the lower longitudinal carrier 12. The open trapeze profile assures in this context favorable tension transitions with high structural strength and low weight.
Structure and arrangement of the base diagonal member 16 will be explained below in detail by way of
In addition, the main flange shows an inclination of approximately 5° relative to the horizontal. In other embodiments this inclination is at least 2°. This measure prevents water or dirt from accumulating on the upper side of the base diagonal member 16.
The cap profile cross section of the base diagonal member 16 represented in
The construction and arrangement of the base diagonal member 16 described above permits a tension-optimized load transfer between the lower transverse spars 26 and 26′ and the longitudinal carriers 12, and at the same time a flat design. To this effect, the brim shanks 36 and 37 assure a soft attachment to the longitudinal carriers 12 or, respectively, the lower transverse spars 26 and 26′ and at the same time provide relatively high buckling stability against pressure forces along the main axis with a flat design.
In the example of an embodiment shown the longitudinal carriers 12 are formed from a square tube with a square cross section. Here, the connection areas L and N of the lateral diagonal member 16 have an overlapping (shaded area in
The wide end of the conical saddle ring segment 39 is connected via its end surface to the corner supports 18, the upper end diagonal member 28 as well as to the lower end diagonal member 30. End ring segments 38 and conical saddle ring segments 39 may either form a closed ring (see frontal view in
In the example of an embodiment shown, the lateral diagonal member 14 has an open trapeze profile and the base diagonal member 16, a cap profile. In other embodiments, the base diagonal member 16 may have a trapeze profile as well or, respectively, the lateral diagonal member may have a cap profile.
The base flange 31 of the trapeze profile and the main flange 33 of the cap profile are shown level in
Additional embodiments and variations will be obvious to the expert within the framework of the patent claims set forth below.
Number | Date | Country | Kind |
---|---|---|---|
20 2006 008 574 U | May 2006 | DE | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/EP2006/012406 | 12/21/2006 | WO | 00 | 6/29/2009 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2007/137619 | 12/6/2007 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
1761969 | Chalmers | Jun 1930 | A |
3115982 | Morrison | Dec 1963 | A |
3402845 | Eriksson | Sep 1968 | A |
3661293 | Gerhard et al. | May 1972 | A |
3726431 | Botkin | Apr 1973 | A |
4065022 | Cainaud | Dec 1977 | A |
4098426 | Gerhard | Jul 1978 | A |
4441678 | Dorpmund | Apr 1984 | A |
4593832 | Gerhard | Jun 1986 | A |
4603788 | Gerhard | Aug 1986 | A |
5190179 | Richter et al. | Mar 1993 | A |
5779077 | Fossey | Jul 1998 | A |
Number | Date | Country |
---|---|---|
2423245 | Mar 2001 | CN |
2 325 058 | May 1973 | DE |
27 07 891 | Sep 1977 | DE |
32 12 696 | Apr 1982 | DE |
83 35 251 | Feb 1984 | DE |
297 05 851 | Aug 1998 | DE |
297 20 675 | Apr 1999 | DE |
201 11 808 | Oct 2001 | DE |
202 11 594 | Dec 2003 | DE |
0 425 190 | Feb 1991 | EP |
Number | Date | Country | |
---|---|---|---|
20110049165 A1 | Mar 2011 | US |