EP4175775A1 - Method for manufacturing a beam with closed section - Google Patents

Abstract

The invention relates to a method for manufacturing a beam (P1, P2) with closed section, the beam being produced by combining a first profile (P10, P20) and a second profile (P11, P21), characterised in that it comprises the following steps: - producing the first profile by means of a first stamping of a first plate (5, 50) between a first punch (1, 10) having a first imprint and a second punch (2, 20) having a second imprint and incorporating a core (3, 30) modifying its second imprint; - holding the first profile (P10, P20) on the first punch and positioning the core (3, 30) above the first profile (P10, P20); - producing the second profile (P11, P21) by means of a second stamping of a second plate (6, 60) against the core (3, 30) between the first punch (2, 20) and the assembly formed by the superposition of the first punch (1, 10), the first profile (P10, P20) and the core.

Description

Description

PROCESS FOR MANUFACTURING A BEAM WITH CLOSED SECTION

Technical field of the invention The present invention relates to a method of manufacturing a beam having a closed section, formed by the association of a first section and a second section. State of the art

Conventionally, to produce beams having a closed section, a first operation of stamping a first section is carried out, then, separately, a second operation of stamping a second section, and finally the fixing of the sections. two profiles obtained, using conventional fixing means such as screw-nut, rivets, etc.

This type of process has the following drawbacks:

This requires managing two separate parts and therefore two references and two industrializations;

This requires an assembly operation; - The fixing elements generate additional weight and bulk;

Such beams are used in particular to form the structure of aircraft doors. Such a door is described in patent application WO2019 / 229074A1. Its structure comprises in particular two main beams fixed along two lateral edges of the door, and several so-called longitudinal beams arranged perpendicular to the two main beams. Each longitudinal beam has an A-shaped cross section, produced by assembling two sections, according to the principle mentioned above.

Documents EP2163324, EP1231077, and WO2018 / 122489 describe general stamping manufacturing processes.

The aim of the invention is to provide a method of manufacturing a closed section beam, formed by the association of two sections, this method being:

Easy to implement, possibly without assembly operation,

SUBSTITUTE SHEET (RULE 26) Continuous, that is to say without having to manufacture two distinct parts, separately,

And not necessarily requiring specific fixing means. Disclosure of the invention

This object is achieved by a method of manufacturing a closed section beam, said beam being produced by the association of a first section and a second section, said method comprising the following steps:

Production of the first profile by a first stamping of a first plate between a first punch having a first impression and a second punch having a second impression and incorporating a core modifying its second impression,

Maintaining of the first profile on the first punch and positioning of said core above said first profile, - Production of the second profile by a second stamping of a second plate against said core between said second punch and said assembly formed by the superposition of the first punch , the first section and said core. According to one particular feature, the method comprises a preliminary step of heating the first plate and the second plate.

According to another particularity, the method comprises a step of localized heating of at least one zone of the first profile obtained after the first stamping.

According to another feature, an intermediate punch is integrated between the second punch and the core during the first stamping.

According to another particularity, the method comprises a step of removing the intermediate punch after the first stamping and before the second stamping.

The invention relates to a system used for implementing the manufacturing method as defined above, the system comprising:

A first punch having a first impression and a second punch having a second impression,

A core adapted to fit on the first punch to modify said first impression or on said second punch to modify said second impression. According to one feature, the system comprises an intermediate punch intended to be positioned between the second punch and the core.

According to another particularity, the first punch and the second punch comprise assembly means intended to cooperate with corresponding means present on the core.

According to another feature, the first punch and / or the second punch include indexing pins arranged to ensure the positioning of each plate to be stamped.

According to another feature, the system comprises a hinge mechanism arranged between the first punch and the second punch.

Finally, the invention relates to an A-section beam, produced by the association of a first section and a second section, the first section comprising over its entire length: - Two support bars,

A top wall located opposite the support bars,

Two side wings extending obliquely towards each other to each join a separate support bar to the top bar,

The second section comprising: - A flat wall and two lateral fixing wings each intended to rest on the internal face of a lateral wing distinct from the first section,

Said beam being produced by the method as defined above. Brief description of the figures

Other characteristics and advantages will appear in the detailed description which follows, given in conjunction with the appended figures listed below:

FIGS. 1A and 1B represent, respectively perspective and side view, an A-section beam, obtainable by the method of the invention;

FIG. 2 represents, in perspective, the various elements of the system used to manufacture, according to the method of the invention, an A-section beam such as that of FIGS. 1 A and 1 B;

FIG. 3 represents a side view of the various elements of the system used to manufacture, according to the method of the invention, an A-section beam such as that of FIGS. 1A and 1B; FIGS. 4A to 4G illustrate, in side view, the various steps of the method of the invention, for manufacturing a beam with an A-section such as that of FIGS. 1A and 1B;

FIG. 5 shows, in side view, a beam with circular closed section;

FIG. 6 represents, in side view, the various elements of the system used to manufacture, according to the method of the invention, a beam with circular closed section such as that of FIG. 5;

FIGS. 7A to 7G illustrate, in side view, the various steps of the method of the invention, pourfabriquer a beam with circular closed section.

Detailed description of at least one embodiment

In the remainder of the description and in the appended figures, the terms "upper", "lower", "above" and "below" are to be considered taking into account an axis (Y) drawn vertically in the plan of the sheet.

The invention relates to a method of manufacturing a beam P1, P2, said beam extending along a so-called longitudinal axis (X). The beam is generated by the association of at least two sections, the two sections defining between them a closed cross section. By way of example, it may be a beam with a cross-section in the form of an A, with a cross-section in the shape of a double omega head-to-tail ... Other shapes could of course be envisaged.

A beam P1 having an A-shaped cross section can in particular be used in the structure of an aircraft door, in particular an aircraft door. Since the cabin of an aircraft is pressurized, its doors must be designed to guarantee a reliable and perfectly hermetic closure. The door therefore has a reinforced structure on which is fixed the panel forming part of the outer casing of the aircraft. This structure may include two main beams, arranged vertically along two parallel edges of the panel and so-called longitudinal beams each extending between the two main beams, at the rear of the panel. These longitudinal beams can be implemented according to the manufacturing method of the invention.

In a nonlimiting manner, for an application of the door type for an aircraft or the like, the beam can be made of a material of the composite type, for example formed from 4 to 5 layers of carbon mat embedded in a thermoplastic resin. In general, the method of the invention consists in directly obtaining a beam at the end of two successive stamping operations, ensuring the shaping of the two sections and their assembly.

The method of the invention is based on the use of a system which comprises: - A first punch, called the lower punch 1, 10;

A second punch called upper punch 2, 20;

A single nucleus 3, 30;

A possible third punch, called intermediate punch 4, 40; Two separate plates 5, 50, 6, 60 are applied to the system in order to form the two sections of the beam.

The principle consists in particular in fixing the single core 3, 30 to one of the two lower or upper punches during the stamping of the first plate 5, 50 and to the other of the two punches, respectively upper or lower, when of the stamping of the second plate 6, 60.

As shown in FIGS. 1A and 1B, in the case of a beam P1 having an A-shaped cross section, this is produced by the association of a first section P10 and a second section P11. The first P10 profile comprises over its entire length:

- Two support bars 100, 101,

A top wall 102 located opposite the support bars,

Two side wings 103, 104 extending obliquely towards each other to each join a separate support bar to the top bar,

The second profile P11 comprises over its entire length:

A flat wall 105 and two lateral fixing wings 106, 107 each intended to be supported on the internal face of a separate lateral wing from the first section.

With reference to FIG. 2 and to FIG. 3, for the manufacture of such an A-section beam, the system employed is more particularly the following:

The lower punch 1 has a cross section defining a relief pattern 108 in the shape of a trapezoid. - The core 3 has a solid cross section in the shape of a trapezoid, intended to complete the relief pattern drawn by the lower punch. The upper punch 2 has a cross section defining a recessed pattern 109, of complementary shape to that of the lower punch accompanied by that of the core.

If employed, the intermediate punch 4 is in the form of a profile having a hollow trapezoidal cross section open at its base.

Assembly means can be provided to assemble the core on the lower punch as well as on the upper punch.

The core 3 can thus include one or more through openings 111 made along its plane of symmetry. The lower punch may include one or more corresponding studs 110 rising above its upper plane. The upper punch as well as the intermediate punch can also include openings 112, 113 made in the same axis as those of the core and as the studs of the lower punch in order to allow superimposed assembly of the various elements.

In Figure 2, each plate is positioned on a handling frame 114, 115, allowing it to be handled and to be held in position during stamping.

With reference to FIGS. 4A to 4G, for the manufacture of the beam P1 with an A-shaped cross section, the steps are described below. In this embodiment, the intermediate punch 4 is used but it would be possible to do without it.

Figure 4A:

A first plate 5 to be stamped is disposed on the upper plane of the lower punch 1. The first plate 5 has a rectangular surface.

The intermediate punch 4 is housed in the hollow pattern of the upper punch 2 as well as the core 3, the intermediate punch 4 being arranged between the upper punch 2 and the core 3.

Figure 4B:

The assembly formed by the upper punch 2, the intermediate punch 4 and the core 3 is closed on the lower punch 1 to stamp the first plate 5 taken between the lower punch and this assembly. The first plate 5 is stamped, thus forming a first section P10 comprising a flat central core and two symmetrical oblique wings, arranged on either side of its upper core. Figure 4C:

The upper punch 2 and the intermediate punch 4 are raised, the core 3 being held on the upper plane of the central web of the first section P10.

Figure 4D:

The intermediate punch 4 is withdrawn.

Optionally, heating C of the two oblique wings of the first section can be undertaken in order to soften the material. This step is optional, because before stamping, each plate is likely to come out of the oven and can thus already be at temperature.

Figure 4E:

While maintaining the configuration of Figure 4D, a second plate 6 is positioned between the upper punch 2 and the assembly formed by the superposition of the lower punch 1, the first profile P10 and the core 3.

Figure 4F:

The upper punch is closed on the assembly defined above in FIG. 4E, with a view to stamping the second plate 6, taken between the upper punch and this assembly. The second plate 6 has a rectangular surface area greater than that of the first plate.

Figure 4G:

The second plate 6 is stamped, thus forming a second section P11 comprising a flat central core and two symmetrical oblique wings, arranged on either side of its upper core and two flat support bars each extending a separate wing. Its two oblique wings each come to bear against the external face of an oblique wing of the first section P10, bringing them to temperature making it possible to ensure their cohesion and assembly, thus forming the beam P1 with A-section shown in FIGS. 1A and 1 B.

The same principle can be applied for the manufacture of a beam P2 made from two profiles P20, P21 in the shape of an omega, assembled head to tail, so as to form a closed section of circular shape. This beam is shown in side view in Figure 5. With reference to FIG. 6, for the manufacture of such a beam P2, the system employed is then the following:

The lower punch 10 has a cross section defining a recessed pattern 200 in the shape of a semicircle. On either side of its hollow pattern, the lower punch has two bearing planes.

The upper punch 20 has a cross section defining a recessed pattern 201, in the shape of a semicircle of diameter identical to that of the lower punch. On either side of its hollow pattern, the upper punch has two bearing planes. - The core 30 has a solid cross section in the form of a disc, so as to be able to be housed in the hollow space defined by the two recessed patterns of the upper and lower punches.

If employed, the intermediate punch 40 is in the form of a profile having a hollow cross section in the shape of a semicircle. It is intended to be positioned between the upper punch and the core.

Fastening means (not shown) can be provided to assemble the core on the lower punch as well as on the upper punch. Figures 7A to 7G illustrate this principle.

Figure 7A:

A first plate 50 is positioned on the bearing planes of the lower punch 10. The first plate 50 has a rectangular surface.

The intermediate punch 40 is housed in the hollow pattern of the upper punch as well as the core 30, the intermediate punch 40 being disposed between the upper punch 20 and the core 30.

Figure 7B:

The assembly formed of the upper punch 20, the intermediate punch 40 and the core 30 is closed on the lower punch 10 to stamp the first plate 50 taken between the lower punch 10 and this assembly. The first plate 50 is stamped, thus forming a first section P20 comprising a central core with a semi-circular section and two flat side wings, symmetrical, on either side of its central core.

Figure 7C: The upper punch 20 and the intermediate punch 40 are raised, the core 30 being held on the upper plane of the central web of the first section P20.

Figure 7D: The intermediate punch is removed.

Optionally, heating C of the two side wings of the first section can be undertaken in order to soften the material. This step is optional, because before stamping, each plate is likely to come out of the oven and can thus already be at temperature.

Figure 7E:

While maintaining the configuration of FIG. 7D, a second plate 60 is positioned between the upper punch 20 and the assembly formed by the superposition of the lower punch 10, the first profile P20 and the core 30. The second plate 60 has a surface. rectangular with dimensions identical to those of the first plate.

Figure 7F:

The upper punch 20 is closed on the assembly defined above in FIG. 7E, with a view to stamping the second plate 60, taken between the upper punch 20 and this assembly.

Figure 7G:

The second plate 60 is stamped, thus forming a second section P21 comprising a semicircular central core and two symmetrical side wings, arranged on either side of its upper core. Its two lateral wings each come to bear against the upper face of a lateral wing of the first section, bringing them to temperature making it possible to ensure their cohesion and assembly, thus forming the beam with a circular closed section.

It should be noted that indexing pins can be provided on the bearing plane of the lower punch 1, 10, in order to facilitate the positioning of the first plate 5, 50.

Alternatively, the system can incorporate a hinge mechanism between the upper punch 2, 20 and the lower punch 1, 10, in order to perfectly adjust the upper punch relative to the lower punch, that is to say without risk of slipping, during stamping operations. By stamping the second plate 6, 60 directly on the first profile already formed, the process is simpler, faster and makes it possible to:

Avoid certain operations, in particular fixing, when fixing is permitted by thermal cohesion between the two profiles;

Have only one reference to manage; - Reduce the amount of material needed for stamping operations

(in particular a single common core for the two operations);

Obtain a lighter beam, thanks to the elimination of fixing means such as screw-nut, rivets, etc.

Claims

1. A method of manufacturing a beam (P1, P2) with closed section, said beam being produced by the association of a first section (P10, P20) and a second section (P11, P21), characterized in which comprises the following steps: - Production of the first profile by a first stamping of a first plate (5, 50) between a first punch (1, 10) having a first impression and a second punch (2, 20) having a second cavity and integrating a core (3, 30) modifying its second cavity, Holding of the first profile (P10, P20) on the first punch and positioning of said core (3, 30) above said first profile (P10, P20), Production of the second profile (P11, P21) by a second stamping of a second plate (6, 60) against said core (3, 30) between said second punch (2, 20) and said assembly formed by the superposition of the first punch (1, 10), of the first section (P10, P20) and of said core. 2. Method according to claim 1, characterized in that it comprises a preliminary step of heating the first plate (5, 50) and the second plate (6, 60). 3. Method according to claim 1 or 2, characterized in that it comprises a step of localized heating of at least one zone of the first profile (P10, P20) obtained after the first stamping. 4. Method according to one of claims 1 to 3, characterized in that an intermediate punch (4, 40) is integrated between the second punch (2, 20) and the core (3, 30) during the first stamping. 5. Method according to claim 4, characterized in that it comprises a step of removing the intermediate punch (4, 40) after the first stamping and before the second stamping. 6. System used for the implementation of the manufacturing method as defined in one of claims 1 to 5, characterized in that it comprises: - A first punch (1, 10) having a first cavity and a second punch (2, 20) having a second impression, A core (3, 30) adapted to fit on the first punch to modify said first impression or on said second punch to modify said second impression; an intermediate punch (4, 40) intended to be positioned between the second punch (2, 20) and the core (3, 30). 7. System according to claim 6, characterized in that the first punch (1, 10) and the second punch (2, 20) comprise assembly means intended to cooperate with corresponding means present on the core. 8. System according to one of claims 6 or 7, characterized in that the first punch (1, 10) and / or the second punch (2, 20) comprise indexing pins arranged to ensure the positioning of each plate to stamp. 9. System according to one of claims 6 to 8, characterized in that it comprises a hinge mechanism arranged between the first punch and the second punch.