A MULTICHAMBER STRUCTURAL ELEMENT AND A MULTICHAMBER STRUCTURAL ELEMENT MANUFACTURING METHOD

Abstract

The object of the invention is a multichamber structural element manufacturing method which for forming a multichamber structural element with chamber profiles (1) extending radially from the center defined by the connection of the chamber profiles (1) comprises the following steps: at least three chamber profile preforms (2) are provided, wherein each chamber profile preform (2) comprises two walls (3) made of a sheet of metal material and arranged with respect to each other in substantially parallel planes with a gap retained between them, wherein the edges of the individual walls (3) converge, and wherein a valve element (6) is arranged on at least one wall (3); the unconnected wall (3) edges of each of the chamber profile preforms (2) are sealed with a seal (5) for forming a closed hermetic empty inner space of the chamber profile preform (2); a fluid under pressure is introduced through the valve element (6) into the inner space of the chamber profile preform (2) for forming a deformed chamber profile (1), at least three chamber profile preforms (2) or chamber profiles (1) are connected in the area of the corresponding inner edges of the chamber profile preform (2) or the chamber profile (1), proximal with respect to the connection axis (4), along at least part of the inner edges. The object of the invention is also a multichamber structural element.

Claims

1. A multichamber structural element manufacturing method wherein it comprises the following steps: a) at least three chamber profile preforms are provided, wherein each chamber profile preform comprises two walls made of a sheet of metal material and arranged with respect to each other in substantially parallel planes with a gap retained between them, wherein the edges of the individual walls converge, and wherein a valve element is arranged on at least one wall, b) the unconnected wall edges of each of the chamber profile preforms are sealed with a seal for forming a closed hermetic empty inner space of the chamber profile preform c) a fluid under pressure is introduced through the valve element into the inner space of the chamber profile preform for forming a deformed chamber profile d) at least three chamber profile preforms or chamber profiles are connected in the area of the corresponding inner edges of the chamber profile preform or the chamber profile proximal with respect to the connection axis, along at least part of the inner edges, wherein steps c) and d) may be performed in reverse sequence.

2. The multichamber structural element manufacturing method according to claim 1, wherein the chamber profile preform is made of a single sheet of metal material bent along one edge for forming two walls arranged with respect to each other in substantially parallel planes.

3. The multichamber structural element manufacturing method according to claim 1, wherein step c) is performed after the chamber profile preform is introduced between pressure plates in such a manner that the pressure plates are in contact with the walls of the chamber profile preforms .

4. The multichamber structural element manufacturing method according to claim 3, wherein during step c) a force is applied to the pressure plates in the direction of the chamber profile preform.

5. The multichamber structural element manufacturing method according to claim 1, wherein step c) is performed by connecting the valve element to a source of fluid under pressure.

6. The multichamber structural element manufacturing method according toclaim 1, wherein step c) is performed simultaneously for all of the chamber profile preforms corresponding to the chamber profiles in the multichamber structural element.

7. The multichamber structural element manufacturing method according to claim 1, wherein in step d) the chamber profiles are connected while preserving their symmetrical arrangement with respect to the connection axis.

8. The multichamber structural element manufacturing method according to claim 1, wherein step b) and/or step d) is realized by fusion welding, pressure welding, gluing or crimping.

9. The multichamber structural element manufacturing method according to claim 1, wherein the fluid is air, water, oil, fluid concrete or fluid plastic.

10. The multichamber structural element manufacturing method according to claim 1, wherein step c) is performed in a room temperature or in an elevated temperature.

11. The multichamber structural element manufacturing method according to claim 1, wherein the pressure of the fluid introduced into the chamber profile preform is 5 bars.

12. The multichamber structural element manufacturing method according to claim 1, wherein in step c) a fluid under pressure is introduced into the inner space of the chamber profile preform for 1 minute, and subsequently a constant pressure is maintained in the chamber profile preform for 30 seconds.

13. The multichamber structural element manufacturing method according to claim 1, wherein steps b) and d) are realized simultaneously.

14. The multichamber structural element manufacturing method according to claim 13, wherein the simultaneous sealing and connecting of the at least three chamber profile preforms in the area of the corresponding inner edges of the chamber profile preform, proximal with respect to the connection axis, along at least part of the inner edges, is realized by laser welding.

15. A multichamber structural element wherein it comprises at least three chamber profiles deformed by fluid under pressure introduced into their hermetic, empty spaces, wherein the chamber profiles are connected with each other with corresponding seals along at least a part of the seal, for forming a multichamber structural element with chamber profiles extending radially from the center defined by the connection axis.

16. The multichamber structural element according to claim 15, wherein the chamber profiles are arranged axially symmetrically with respect to the connection axis.

17. The multichamber structural element according to claim 15, wherein the chamber profile has an inner edge directed towards the connection axis of the multichamber structural element and extending in a straight line or at least partially in a curved line.

18. The multichamber structural element according to claim 15, wherein the chamber profile has an outer edge, opposite with respect to the connection axis of the multichamber structural element and extending in a straight line parallel to the connection axis, in a deviation from the connection axis, in a concave curved line with respect to the connection axis or in a convex curved line with respect to the connection axis.

19. The multichamber structural element according to claim 15, wherein the chamber profiles extend at a different radial length with respect to the connection axis.

20. The multichamber structural element according to claim 15,wherein the fluid is air, water, oil, fluid concrete or fluid plastic.

Description

[0033] The solution according to the present invention has been shown in the embodiments below and illustrated in the drawing, in which:

[0034] FIGS. 1A-B shows the steps of the multichamber structural element manufacturing method according to one embodiment of the invention,

[0035] FIGS. 2A-B shows the steps of the multichamber structural element manufacturing method according to a further embodiment of the invention,

[0036] FIGS. 3A-B shows the steps of the multichamber structural element manufacturing method according to a further embodiment of the invention,

[0037] FIGS. 4A-B shows the steps of the multichamber structural element manufacturing method according to a further embodiment of the invention,

[0038] FIGS. 5A-C shows the steps of the multichamber structural element manufacturing method according to a further embodiment of the invention,

[0039] FIGS. 6A-E shows the cross-sections of the multichamber structural element according to different embodiments of the invention,

[0040] FIGS. 7A-F shows the front views of the chamber profiles for use in the multichamber structural element according to different embodiments of the invention,

[0041] FIGS. 8A-E shows the front views of the multichamber structural element according to different embodiments of the invention,

[0042] FIGS. 9A-E shows the cross-sections of the multichamber structural element along the intersection planes indicated in FIGS. 8A-E, respectively,

[0043] FIGS. 10A-C shows the front views of the multichamber structural element according to different embodiments of the invention,

[0044] FIGS. 11A-C shows the cross-sections of the multichamber structural element along the intersection planes indicated in FIGS. 10A-C, respectively.

EMBODIMENT 1

[0045] The multichamber structural element manufacturing method according to one embodiment of the invention is partially schematically shown in FIGS. 1A-B. The presented embodiment of the multichamber structural element manufacturing method comprises the step of providing a chamber profile preform 2, which comprises two walls 3 made of metal sheet and arranged with respect to each other in substantially parallel planes with a gap retained between them, wherein the edges of the individual walls 3 converge. A valve element 6 is arranged on at least one of the walls 3. The valve element 6 is a pneumatic or hydraulic connection and allows a leakproof fastening of a supply duct 7 from an external source of pressurized fluid. In some embodiments of the invention, the valve element 6 may be a valve, particularly a non-return valve. The location of the valve element 6 is not a limitation to the scope of the present invention, and thus the valve element 6 may be arranged in any location on the metal sheet, on condition that a connection with the inner space of the chamber profile preform 2 is allowed.

[0046] In this embodiment, the chamber profile preform 2 is formed of two walls 3, each of the walls 3 being made of a separate metal sheet. In alternative embodiments, it is possible to provide a single sheet of metal material, which is bent, using the cold-bending operations known in the art, along one edge for forming two walls 3 arranged with respect to each other in substantially parallel planes. This embodiment is advantageous in that one edge of the manufactured chamber profile preform 2 is sealed (in the location where the metal sheet is bent) already at the step of providing the metal sheet, thus reducing the number of successive sealing operations.

[0047] In the next step of the multichamber structural element manufacturing method, the chamber profile preform 2 is sealed for creating a sealed hermetic inner space. The sealing is performed on the edges of the metal sheet forming the walls 3 of the chamber profile preform 2 after they have been matched with each other. In this embodiment, the sealing is thus performed on all the circumferential edges of the matched walls 3 of the chamber profile preform 2, wherein FIG. 1A shows only the longitudinal seals 5. In this embodiment, the sealing was performed by means of welding the corresponding edges together, forming inter alia longitudinal welds. The sealing is moreover performed on the edges of the matched walls 3, located on the front and on the back of the chamber profile preform 2. By sealing all of the above-listed edges, a leakproof hermetic inner space is formed in the chamber profile preform 2, as schematically shown in the cross-section of FIG. 1A. The type of seal 5 is in this case not a limitation to the scope of the invention, and it is possible in alternative embodiments to use any type of seal 5, on condition that a leakproof inner space is formed in the chamber profile preform 2, by means for example of pressure welding, soldering, gluing, bending or pressing.

[0048] In the next step, an external source of fluid under pressure is connected to the valve element 6 through the supply duct 7. In this embodiment, the fluid is air, the source of fluid under pressure is a compressor, and the supply duct 7 together with the valve element 6 form a pneumatic connection. The type of the external source of fluid under pressure and of the connection equipment is not a limitation to the scope of this invention and in alternative embodiments it is possible to use fluid in the form of water, fluid cement, machine oil, fluid plastic such as a one-, two- or three-component foam (e.g. a flex 140 type), etc. together with the connection equipment and the source of fluid under pressure appropriate for those fluids. The less compressible the fluid is, the more controlled the deformation conditions of the chamber profile preform 2 are.

[0049] In the next step of the multichamber structural element manufacturing method according to the invention, fluid under a defined pressure is delivered to the sealed inner space of the chamber profile preform 2. The technology of introducing fluid under pressure into closed sealed chamber elements made of sheet metal for their deformation and providing them with the final form is known inter alia from patent application No. EP2110189A1. As a result of delivering fluid under pressure into the inner space of the chamber profile preform 2, the walls 3 of the chamber profile preform 2 are deformed, with the greatest deformation level being located in the center of the chamber profile 1, as best illustrated in FIG. 1B, which shows the cross-section of the chamber profile 1 manufactured from the chamber profile preform 2. As can be observed, the walls 3 of the chamber profile preform 2 are significantly deformed. The next two chamber profiles 1 are manufactured by the same method in order to obtain three chamber profiles 1.

[0050] Note should be taken that although the introduction of fluid under pressure into the inner space of the chamber profile preform 2 is performed in cold technology (i.e. in room temperature), it is not a limitation to the scope of this invention, and in alternative embodiments the process may be performed in elevated or high temperatures.

[0051] In one embodiment of the invention, the step of introducing fluid under pressure was performed with the following process parameters: [0052] process temperature: 20° C., [0053] working pressure: 5 bars, [0054] deformation time: 1 minute until pressure is equalized in the chamber profile preform, [0055] pressure hold time: 30 seconds, [0056] total deformation time: 1.5 minute.

[0057] In an alternative implementation of the multichamber structural element manufacturing method, the step of introducing fluid under pressure into the inner space of the chamber profile preform 2 may be preceded by placing the chamber profile preform 2 between the pressure plates 8 so that the pressure plates 8 are in contact with the walls 3 of the chamber profile preform 2, as illustrated in FIG. 5B. The pressure plates 8 may be the working elements of a mechanical press. In this case, a controlled force may be applied to the pressure plates 8, particularly in the direction towards the chamber profile preform 2. In the step of delivering fluid under pressure into the sealed inner space of the chamber profile preform 2, the chamber profile preform 2 is kept between the pressure plates 8. As a result, the chamber profiles 1 formed following this method have flattened surfaces in the central area of the walls 3, as best illustrated in the cross-section of the multichamber structural element shown in FIG. 5C.

[0058] In the subsequent step, the three chamber profiles 1 are connected with each other by connecting the corresponding inner edges of the chamber profile 1, proximal with respect to the connection axis 4, along at least part of the inner edges. In this embodiment, it is realized by connecting the corresponding seals 5. The connection area of the chamber profiles 1 includes three edges (seals 5) of the chamber profiles 1 which, together with the connecting weld, form the connection axis 4. In this embodiment, the chamber profiles 1 are connected with each other by welding, but it is not a limitation to the scope of the invention and it is possible in alternative embodiments to use other connecting techniques, such as: pressure welding, soldering, gluing, bending or pressing.

[0059] The connection of the chamber profiles 1 is realized in an axially symmetrical arrangement of the chamber profiles 1 with respect to the connection axis 4, i.e. in the cross-sectional view, as shown in FIG. 6A, each of the chamber profiles 1 extends in a radial direction outwards from the connection axis 4, wherein the chamber profiles 1 are arranged around the connection axis 4 by an equal angle, in this embodiment by an angle of 120°.

EMBODIMENT 2

[0060] The multichamber structural element manufacturing method according to the second embodiment of the invention is schematically shown in FIGS. 2A-B. The presented embodiment of the multichamber structural element manufacturing method is substantially similar to the multichamber structural element manufacturing method shown in embodiment 1, and therefore the similar steps will not be discussed in detail for the clarity of this disclosure.

[0061] In the second embodiment of the multichamber structural element manufacturing method, in the first step two metal sheets are provided which are two walls 3 of the chamber profile preform 2. The walls 3 of the chamber profile preform 2, which are matched with each other, are subsequently sealed on the free edges for forming a sealed hermetic inner space. Following this method, three chamber profile preforms 2 are manufactured.

[0062] Unlike in the structural element manufacturing method shown in embodiment 1, the structural element manufacturing method according to the second embodiment comprises the connecting with each other of the thus formed chamber profile preforms 2 by connecting the corresponding seals 5, along the at least part of the seal 5 (as shown in FIG. 2A). The connection area of the chamber profile preforms 2 includes three edges (seals 5) of the chamber profile preforms 2, which form, together with the connecting weld, the connection axis 4 in the final multichamber structural element. In this embodiment, the chamber profile preforms 2 are connected with each other by welding, and the connected chamber profile preforms 2 are shown in FIG. 2A.

[0063] In the subsequent step of the multichamber structural element manufacturing method according to the second embodiment of the invention, fluid under a defined pressure is delivered to the sealed inner space of the chamber profile preform 2, wherein this delivery is realized by connecting an external source of fluid under pressure to the valve element 6 through a supply duct 7 (see FIG. 2B). The introduction of fluid under pressure into the inner space of the chamber profile preform 2 may be realized separately for each chamber profile preform 2 as an operation in series (i.e. one after another) or simultaneously for all chamber profile preforms 2, as shown in FIG. 2B. The simultaneous introduction of fluid under pressure into the inner space of the chamber profile preform 2 requires, however, the use of a greater number of supply ducts 7 and an appropriate source of fluid under pressure ensuring the possibility to simultaneously connect the same number of supply ducts 7.

[0064] As a result, there is obtained a multichamber structural element, with a cross-section shown in FIG. 6A, having three chamber profiles 1 extending radially and symmetrically arranged with respect to the connection axis 4, deformed by fluid under pressure introduced into their hermetic, sealed inner space.

EMBODIMENT 3

[0065] The multichamber structural element manufacturing method according to the next embodiment of the invention is schematically shown in FIGS. 3A-B. The presented embodiment of the multichamber structural element manufacturing method is substantially similar to the multichamber structural element manufacturing method shown in embodiment 2, and therefore the similar steps will not be discussed in detail for the clarity of this disclosure.

[0066] In the third embodiment of the multichamber structural element manufacturing method, in the first step there are provided three metal sheets which are V-shaped profiles and which each form one wall 3 of the adjacent chamber profile preforms 2. The V-shaped profiles are matched with each other in such a manner that the arms of the V-shaped profiles extend in planes parallel to the arms of the adjacent V-shaped profiles and form three chamber profile preforms 2, respectively. Subsequently, the sealing step is performed on the free edges (outer edges) of the so-formed chamber profile preforms 2 for forming a sealed hermetic inner space. In the next step (or simultaneously), seals 5 are made within the central area of the connected chamber profile preforms 2. The step of sealing the inner edges of the chamber profile preforms 2 is realized using a sealing technique through the gap maintained between the corresponding walls 3 of the chamber profile preform 2, forming the seal 5 hermetically closing the inner space of the chamber profile preform 2. In this case, the sealing technique preferably comprises laser welding, which allows the walls 3 of the chamber profile preform 2 to be connected with each other by forming a welding seam (weld) through the gap and sealing the space formed between the walls 3 of the chamber profile preform 2. Following this method, three chamber profile preforms 2 are manufactured simultaneously, as shown in FIG. 3A.

[0067] In the subsequent step of the multichamber structural element manufacturing method according to the third embodiment of the invention, fluid under a defined pressure is delivered to the sealed inner space of the chamber profile preform 2, wherein this delivery is realized by connecting an external source of fluid under pressure to the valve element 6 through a supply duct 7 (see FIG. 3B). The introduction of fluid under pressure into the inner space of the chamber profile preform 2 is realized simultaneously for all chamber profile preforms 2, as shown in FIG. 3B.

[0068] As a result, there is obtained a multichamber structural element, with a cross-section shown in FIG. 6A, having three chamber profiles 1 extending radially and symmetrically arranged with respect to the connection axis 4, deformed by fluid under pressure introduced into their hermetic, sealed inner space.

EMBODIMENT 4

[0069] The multichamber structural element manufacturing method according to the next embodiment of the invention is schematically shown in FIGS. 4A-B. The presented embodiment of the multichamber structural element manufacturing method is substantially similar to the multichamber structural element manufacturing method shown in embodiment 2, and therefore the similar steps will not be discussed in detail for the clarity of this disclosure.

[0070] In the fourth embodiment of the multichamber structural element manufacturing method, in the first step there are six metal sheets provided and matched correspondingly for forming the chamber profile preforms 2. Each of the chamber profile preforms 2 is sealed on its outer edges, analogically to the previous embodiments. Unlike in the previous embodiments, the inner edges of the chamber profile preforms 2 remain unsealed and in the subsequent step they are positioned with respect to each other by matching the corresponding chamber profile preforms 2 with the inner edges towards each other. The matched inner edges of the chamber profile preforms 2 are subsequently sealed and connected with each other in one operation for forming the connection axis 4 and the sealed, hermetic closure of the inner spaces of all chamber profile preforms 2, as shown in FIG. 4A.

[0071] In the subsequent step of the multichamber structural element manufacturing method according to the fourth embodiment of the invention, fluid under a defined pressure is delivered to the sealed inner space of the chamber profile preform 2, wherein this delivery is realized by connecting an external source of fluid under pressure to the valve element 6 through a supply duct 7 (see FIG. 4B).

[0072] The introduction of fluid under pressure into the inner space of the chamber profile preform 2 is realized simultaneously for all chamber profile preforms 2, as shown in FIG. 4 B.

[0073] As a result, there is obtained a multichamber structural element, with a cross-section shown in FIG. 6A, having three chamber profiles 1 extending radially and symmetrically arranged with respect to the connection axis 4, deformed by fluid under pressure introduced into their hermetic, sealed inner space.

EMBODIMENT 5

[0074] Further non-limiting embodiments of the multichamber structural element are shown in the cross-section in FIGS. 4A-E.

[0075] Unlike in the multichamber structural element described in embodiments 1-4, which was a structural element formed from three chamber profiles 1, as shown in FIG. 6A, other embodiments of the multichamber structural element may comprise a greater number of the component chamber profiles 1. The multichamber structural element may comprise four chamber profiles 1 (FIG. 6B), six chamber profiles 1 (FIG. 6C), and/or eight chamber profiles 1 (FIG. 6D). Importantly, the multichamber structural element is not limited to a multichamber structural element formed from geometrically identical chamber profiles 1, and it is possible to have chamber profiles 1 of different geometries within the same multichamber structural element. Such an embodiment is shown in FIG. 6E, in which four chamber profiles 1 extending radially from and symmetrically with respect to the connection axis 4 have a first length, and the remaining four chamber profiles 1 arranged between the first four chamber profiles 1 have a second length greater than the first length. This embodiment illustrates the freedom range in designing the multichamber structural element which allows the technical parameters of the multichamber structural element to be adjusted to the particular arrow of force characteristic of a particular solution.

[0076] Various embodiments of multichamber structural elements according to the present invention comprise multichamber structural elements formed from chamber profiles 1 of different geometries. The geometry of the chamber profiles 1 is strictly related to the geometry of the chamber profile preform 2, which is subjected to deformation due to the introduction of fluid under pressure into the hermetic, sealed inner space of the chamber profile preform 2. The large surfaces of the walls 3 of the chamber profile preform 2 are subjected to the most extensive deformation, with a limited or no deformation level in the area of the seals 5. This means that the geometry of the chamber profiles 1 within the seals 5 is substantially identical to the geometry of the chamber profile preforms 2 which allows the free shaping of the final shape of the chamber profile 1, and thus also of the multichamber structural element. FIGS. 7A-F is a side view of various geometries of the chamber profile preform 2 which is used in the manufacturing of the chamber profiles 1 being in further steps the components of the multichamber structural element.

[0077] In FIG. 7A, the chamber profile preform 2, and thus the chamber profile 1, has an inner edge which is directed towards the connection axis 4 of the multichamber structural element and which extends in a straight line and parallel to the connection axis 4, and an outer edge, opposite with respect to the connection axis 4 of the multichamber structural element, which extends in a straight line parallel to the connection axis 4. The multichamber structural element manufactured from the chamber profiles 1 presented in FIG. 7A is shown in a side view in FIG. 8A and in a cross-sectional view in FIG. 9A.

[0078] In FIG. 7B, the chamber profile preform 2, and thus the chamber profile 1, has an inner edge which is directed towards the connection axis 4 of the multichamber structural element and which extends in a straight line and parallel to the connection axis 4, and an outer edge, opposite with respect to the connection axis 4 of the multichamber structural element, which extends in a straight line sloping with respect to the connection axis 4, wherein the width of the chamber profile 1 increases towards the bottom. The multichamber structural element manufactured from the chamber profiles 1 presented in FIG. 7B is shown in a side view in FIG. 8D and in a cross-sectional view in FIG. 9D.

[0079] In FIG. 7C, the chamber profile preform 2, and thus the chamber profile 1, has an inner edge which is directed towards the connection axis 4 of the multichamber structural element and which extends in a straight line and parallel to the connection axis 4, and an outer edge, opposite with respect to the connection axis 4 of the multichamber structural element, which extends in a straight line sloping with respect to the connection axis 4, wherein the width of the chamber profile 1 decreases towards the bottom.

[0080] In FIG. 7D, the chamber profile preform 2, and thus the chamber profile 1, has an inner edge which is directed towards the connection axis 4 of the multichamber structural element and which extends in a curved line, with an upper region and a lower region extending in a straight line parallel to the connection axis 4, and an outer edge, opposite with respect to the connection axis 4 of the multichamber structural element, which extends in a straight line parallel to the connection axis 4. The multichamber structural element formed from the chamber profiles 1 presented in FIG. 7D is shown in a side view in FIG. 8E and in a cross-sectional view in FIG. 9E.

[0081] In FIG. 7E, the chamber profile preform 2, and thus the chamber profile 1, has an inner edge which is directed towards the connection axis 4 of the multichamber structural element and which extends in a straight line and parallel to the connection axis 4, and an outer edge, opposite with respect to the connection axis 4 of the multichamber structural element, which extends in a concave curved line. The multichamber structural element formed from the chamber profiles 1 presented in FIG. 7E is shown in a side view in FIG. 8C and in a cross-sectional view in FIG. 9C.

[0082] In FIG. 7F, the chamber profile preform 2, and thus the chamber profile 1, has an inner edge which is directed towards the connection axis 4 of the multichamber structural element and which extends in a straight line and parallel to the connection axis 4, and an outer edge, opposite with respect to the connection axis 4 of the multichamber structural element, which extends in a convex curved line. The multichamber structural element formed from the chamber profiles 1 presented in FIG. 7F is shown in a side view in FIG. 8B and in a cross-sectional view in FIG. 9B.

[0083] In other embodiments, the multichamber structural element may be formed of chamber profiles 1 having different geometries, forming an axially asymmetrical multichamber structural element. Non-limiting embodiment of the axially asymmetrical multichamber structural element are shown in a side view in FIG. 10A and in a cross-sectional view in FIG. 11A, in which the multichamber structural element is manufactured using the chamber profiles 1 presented in FIG. 7A and in FIG. 7B. Another embodiment of the axially asymmetrical multichamber structural element is shown in a side view in FIG. 10B and in a cross-sectional view in FIG. 11B, in which the multichamber structural element is manufactured using the chamber profiles 1 presented in FIG. 7A and in FIG. 7F, and the chamber profile 1 whose outer edge is in the shape of a curve extending from the upper part of the multichamber structural element and gently passing into a straight-line fragment in the lower portion of the multichamber structural element. Yet another embodiment of the axially asymmetrical multichamber structural element is shown in a side view in FIG. 10C and in a cross-sectional view in FIG. 11C, in which the multichamber structural element is manufactured using the chamber profiles 1 presented in FIG. 5A and in FIG. 5E, and the chamber profile 1 whose outer edge is in the shape of a curve extending from the lower part of the multichamber structural element and gently passing into a straight-line fragment in the upper portion of the multichamber structural element.

[0084] Importantly, the number of the chamber profiles 1 being part of the multichamber structural element, as well as the geometry of the chamber profile 1 being part of the multichamber structural element are not limited to the scope presented in these embodiments, which are only examples of the possible implementations of the invention. In alternative embodiments, the multichamber structural element may comprise more than three chamber profiles 1, and the chamber profiles 1 may have a shape different than the shapes presented, including a shape being a combination of the shapes here disclosed.

EMBODIMENT 6

[0085] The multichamber structural element manufactured with the method according to the invention were subjected to comparative tests (based on numerical calculations) with a standard structural element commonly used in the art. The results of the comparative tests are presented in Table 1. The tested multichamber structural element manufactured with the method of the invention was designated in Table 1 as FIDU200. The compared structural element, designated as HEB120 is a standardized wide-flange I-profile with the flange width of 120 mm and the profile height of 120 mm, and with the web thickness of 6.5 mm. The material used in the simulations for the HEB120 profile was steel S235JR. The multichamber structural element of the present invention was formed of four chamber profiles 1 illustrated in FIG. 7A and is shown in the cross-sectional view in FIG. 6B. Each component chamber profile 1 had a width, i.e. a radial dimension with respect to the connection axis 4, of 200 mm and was formed of sheet steel S235JR 2 mm in thickness by using process parameters shown in embodiment 1.

TABLE-US-00001 Technical Parameters of the Structural Elements FIDU200 HEB120 Moment of inertia, I [mm.sup.4] 23835309 3180000 Cross-sectional area [mm.sup.2] 3371.5 3400 Radius of gyration, i [mm] 84.1 30.6 Length of the element, l [mm] 2000 2000 Mass of 1 meter, m [kg] 25.2 26.7 Buckling force, Fe [N] 3084462 411515 Stress at buckling, σ.sub.e [N/mm.sup.2] 915 121 Material yield force, F [N] 792302.5 799000

[0086] As can be observed in Table 1, the cross-sectional area of the FIDU200 element is smaller by approximately 0.8% than the cross-sectional area of the HEB120 profile. Furthermore, the FIDU200 element is lighter than the HEB120 by approximately 5.9%, with the minimum geometric moment of inertia of the FIDU200 cross-section is approximately 7.5-fold greater than the HEB120. As a result, the FIDU200 element is characterized by an approximately 7.5-fold greater buckling force and by approximately 0.8% smaller material yield force than the HEB120.

[0087] The comparison of these parameters demonstrates that the cross-section of the multichamber structural element according to this invention (FIDU200) is used better than in the standard profile, commonly applied in the art (HEB120). Furthermore, with lower mass and smaller cross-sectional area, the multichamber structural element according to this invention reaches 7.5-fold greater moment of inertia and 7.5-fold greater buckling strength.

LIST OF REFERENCE NUMERALS

[0088] 1 - chamber profile [0089] 2 - chamber profile preform [0090] 3 - wall of the chamber profile preform [0091] 4 - connection axis [0092] 5 - seal [0093] 6 - valve element [0094] 7 - supply duct [0095] 8 - pressure plate