<?xml version="1.0" encoding="UTF-8"?>
<!DOCTYPE ep-patent-document PUBLIC "-//EPO//EP PATENT DOCUMENT 1.3//EN" "ep-patent-document-v1-3.dtd">
<ep-patent-document id="EP05009433B1" file="EP05009433NWB1.xml" lang="en" country="EP" doc-number="1616639" kind="B1" date-publ="20080903" status="n" dtd-version="ep-patent-document-v1-3">
<SDOBI lang="en"><B000><eptags><B001EP>ATBECHDEDKESFRGBGRITLILUNLSEMCPTIESILT..FIRO..CY..TRBGCZEEHUPLSK....IS..........</B001EP><B005EP>J</B005EP><B007EP>DIM360 Ver 2.15 (14 Jul 2008) -  2100000/0</B007EP></eptags></B000><B100><B110>1616639</B110><B120><B121>EUROPEAN PATENT SPECIFICATION</B121></B120><B130>B1</B130><B140><date>20080903</date></B140><B190>EP</B190></B100><B200><B210>05009433.3</B210><B220><date>20050429</date></B220><B240><B241><date>20051028</date></B241><B242><date>20060424</date></B242></B240><B250>it</B250><B251EP>en</B251EP><B260>en</B260></B200><B300><B310>VR20040115</B310><B320><date>20040714</date></B320><B330><ctry>IT</ctry></B330></B300><B400><B405><date>20080903</date><bnum>200836</bnum></B405><B430><date>20060118</date><bnum>200603</bnum></B430><B450><date>20080903</date><bnum>200836</bnum></B450><B452EP><date>20080526</date></B452EP></B400><B500><B510EP><classification-ipcr sequence="1"><text>B21C  23/14        20060101AFI20051007BHEP        </text></classification-ipcr><classification-ipcr sequence="2"><text>B21C  31/00        20060101ALI20051007BHEP        </text></classification-ipcr><classification-ipcr sequence="3"><text>B21C  23/08        20060101ALI20051007BHEP        </text></classification-ipcr></B510EP><B540><B541>de</B541><B542>Verfahren zum Optimieren eines Verfahrens zum Strangpressen eines Aluminiumprofils</B542><B541>en</B541><B542>A method for optimising a process for extrusion of an aluminium section</B542><B541>fr</B541><B542>Procédé pour optimaliser un procédé de filage d'un profilé en aluminium</B542></B540><B560><B561><text>DE-A1- 19 715 308</text></B561><B561><text>US-A- 3 164 898</text></B561><B562><text>PATENT ABSTRACTS OF JAPAN vol. 1995, no. 04, 31 May 1995 (1995-05-31) &amp; JP 07 009027 A (KOBE STEEL LTD), 13 January 1995 (1995-01-13)</text></B562><B562><text>PATENT ABSTRACTS OF JAPAN vol. 1996, no. 06, 28 June 1996 (1996-06-28) &amp; JP 08 047713 A (NIPPON LIGHT METAL CO LTD), 20 February 1996 (1996-02-20)</text></B562><B562><text>PATENT ABSTRACTS OF JAPAN vol. 1997, no. 10, 31 October 1997 (1997-10-31) &amp; JP 09 150215 A (TOYAMA KEIKINZOKU KOGYO KK), 10 June 1997 (1997-06-10)</text></B562><B562><text>PATENT ABSTRACTS OF JAPAN vol. 016, no. 094 (M-1219), 9 March 1992 (1992-03-09) &amp; JP 03 275212 A (SHOWA ALUM CORP), 5 December 1991 (1991-12-05)</text></B562><B562><text>PATENT ABSTRACTS OF JAPAN vol. 015, no. 374 (M-1160), 20 September 1991 (1991-09-20) &amp; JP 03 151116 A (SHOWA ALUM CORP), 27 June 1991 (1991-06-27)</text></B562><B562><text>PATENT ABSTRACTS OF JAPAN vol. 014, no. 103 (M-0941), 26 February 1990 (1990-02-26) &amp; JP 01 309718 A (NIPPON ALUM MFG CO LTD; others: 01), 14 December 1989 (1989-12-14)</text></B562></B560></B500><B700><B720><B721><snm>Natali, Gianfranco</snm><adr><str>Via Castelletto, 8</str><city>6924 Sorengo</city><ctry>CH</ctry></adr></B721></B720><B730><B731><snm>Natali, Gianfranco</snm><iid>05078390</iid><irf>32.N1024.12EP14</irf><adr><str>Via Castelletto, 8</str><city>6924 Sorengo</city><ctry>CH</ctry></adr></B731></B730><B740><B741><snm>Ponchiroli, Simone</snm><iid>00144231</iid><adr><str>Bugnion S.p.A. 
Via Garibaldi, 19</str><city>37121 Verona</city><ctry>IT</ctry></adr></B741></B740></B700><B800><B840><ctry>AT</ctry><ctry>BE</ctry><ctry>BG</ctry><ctry>CH</ctry><ctry>CY</ctry><ctry>CZ</ctry><ctry>DE</ctry><ctry>DK</ctry><ctry>EE</ctry><ctry>ES</ctry><ctry>FI</ctry><ctry>FR</ctry><ctry>GB</ctry><ctry>GR</ctry><ctry>HU</ctry><ctry>IE</ctry><ctry>IS</ctry><ctry>IT</ctry><ctry>LI</ctry><ctry>LT</ctry><ctry>LU</ctry><ctry>MC</ctry><ctry>NL</ctry><ctry>PL</ctry><ctry>PT</ctry><ctry>RO</ctry><ctry>SE</ctry><ctry>SI</ctry><ctry>SK</ctry><ctry>TR</ctry></B840><B880><date>20060118</date><bnum>200603</bnum></B880></B800></SDOBI><!-- EPO <DP n="1"> -->
<description id="desc" lang="en">
<p id="p0001" num="0001">The present invention relates to a method for optimising a process for extrusion of an aluminium section as per the preamble of claim 1. An example of such a method is known from <patcit id="pcit0001" dnum="JP07009027A"><text>JP-07009027-A</text></patcit>.</p>
<p id="p0002" num="0002">The method according to the present invention was developed relative to the production of panels for industrial vehicle bodies, in particular hollow panels having one or more tubular segments.</p>
<p id="p0003" num="0003">For this reason, specific reference is often made hereinafter to sections constituting body panels. In any case the present invention is intended for application in any sector which uses aluminium sections obtained by means of extrusion.</p>
<p id="p0004" num="0004">As is known, aluminium sections are extruded by forcing the aluminium in the plastic state through a die which gives it the required shape.</p>
<p id="p0005" num="0005">As in all sectors, in the production of extruded aluminium sections, the trend over the years has been to attempt to minimise the cost per unit of length of said sections.</p>
<p id="p0006" num="0006">To summarise, it may roughly be said that the<!-- EPO <DP n="2"> --> overall cost per unit of length of a section is given by the sum of a fixed cost substantially linked to the existence of the production company with the relative extrusion plant, and a variable cost given by the quantity of material which constitutes the section (therefore, substantially the weight per unit of length).</p>
<p id="p0007" num="0007">Whilst the fixed cost per unit of length of the section produced falls as the productivity of the plant increases, the variable cost, again per unit of length produced, falls as the weight per unit of length of the section falls.</p>
<p id="p0008" num="0008">Over the years the logical consequence has been to increase the speed of extrusion and reduce the weight of the section.</p>
<p id="p0009" num="0009">But these are two factors which, under certain conditions, clash with one another.</p>
<p id="p0010" num="0010">It is known that for each section there is a maximum extrusion speed which is inseparably linked to the friction created between the aluminium extruded and the die which gives it its shape.</p>
<p id="p0011" num="0011">If this limit speed is exceeded, the surface of the product obtained at the end of the extrusion process shows signs of deterioration following the appearance of scratches and/or scoring and/or<!-- EPO <DP n="3"> --> lacerations and/or deformations and/or undulations which are more or less extensive and/or the extruding die may even be broken.</p>
<p id="p0012" num="0012">However, the limit speed which, as indicated, is determined by friction, depends, all other extrusion plant factors being equal, on the thickness of the section. As the thickness of the section is reduced, the limit speed is also reduced.</p>
<p id="p0013" num="0013">As a result, the limit speed is substantially set by the thickness of the section to be obtained. In general, in sections which do not have uniform thickness, the limit speed is determined by the thickness of the portion of the section with the minimum thickness.</p>
<p id="p0014" num="0014">Therefore, to attempt to increase the speed of extrusion of a predetermined section, its thickness would have to be increased.</p>
<p id="p0015" num="0015">However, on the other hand, to attempt to reduce the costs linked to the weight of the material, it has been increasingly necessary to reduce section thickness as far as possible.</p>
<p id="p0016" num="0016">These two opposing requirements have led to the identification, for each type of section and plant, of an optimum combination of extrusion speed and<!-- EPO <DP n="4"> --> section thickness (at least in the portion with the minimum thickness) which minimises the costs of the section to be produced.</p>
<p id="p0017" num="0017">However, the present invention is a result of the discovery that, for many applications, the limit thickness determined based on the minimum cost of the section to be produced is greater than that which would be sufficient to guarantee the mechanical strength required in the end use of the section.</p>
<p id="p0018" num="0018">For example, in the case of panels for industrial vehicle bodies, in particular hollow panels with one or more tubular segments, at present sections with a minimum thickness of around 1.7 mm can be produced.</p>
<p id="p0019" num="0019">Mechanical assessments have highlighted how sufficient mechanical strength could be achieved even with thicknesses that are significantly lower (even 30% or more) if produced using the method disclosed which involves limited zones of greater thickness that promote the flow of aluminium through the die but which also act as a support - rest immediately after extrusion when the section is still hot and very weak, as well as stiffening the section during the subsequent practical end<!-- EPO <DP n="5"> --> use.</p>
<p id="p0020" num="0020">In this situation the technical need which forms the basis of the present invention is to perfect a method for optimising a process for extrusion of an aluminium section which overcomes the above-mentioned disadvantages.</p>
<p id="p0021" num="0021">In particular, the technical need of the present invention is to perfect a method for optimising a process for extrusion of an aluminium section which allows extrusion, at least at the same speed as the current plants, of sections with a weight (for the same unit of length) lower than the methods of extrusion currently known and/or which at least allows an increase in the speed of extrusion if the weight is the same per unit of length.</p>
<p id="p0022" num="0022">Another technical need of the present invention is to perfect a method for optimising a process for extrusion of an aluminium section in which the reduction in the overall weight per unit of length is achieved by reducing the thickness of the section currently considered the minimum with current extrusion methods.</p>
<p id="p0023" num="0023">A further technical need of the present invention is to perfect a method for optimising a process for extrusion of an aluminium section in which the<!-- EPO <DP n="6"> --> reduction in the overall weight per unit of length is achieved by reducing the minimum thickness of the section to be produced but substantially maintaining and/or improving the resistance to bending of the section, in particular if it is to be used for example as a panel for industrial vehicle bodies with one or more tubular segments.</p>
<p id="p0024" num="0024">The technical need specified and the aims indicated are substantially achieved by a method for optimising a process for extrusion of an aluminium section as described in claim 1.</p>
<p id="p0025" num="0025">Further characteristics and advantages of the invention are more clearly illustrated in the detailed description of several preferred embodiments of a method for optimising a process for the extrusion of an aluminium section, described with reference to the accompanying drawings, provided by way of example and without limiting the scope of application, and in which:
<ul id="ul0001" list-style="dash" compact="compact">
<li><figref idref="f0001">Figure 1</figref> is a cross-section of a section constituting a panel of an industrial vehicle body, made according to the prior art;</li>
<li><figref idref="f0001">Figure 2</figref> is a cross-section of the section illustrated in <figref idref="f0001">Figure 1</figref> obtained with an extrusion method optimised according to a first embodiment of<!-- EPO <DP n="7"> --> the present invention;</li>
<li><figref idref="f0001">Figure 3</figref> is a cross-section of the section illustrated in <figref idref="f0001">Figure 1</figref> obtained with an extrusion method optimised according to a second embodiment of the present invention;</li>
<li><figref idref="f0001">Figure 4</figref> is a cross-section of the section illustrated in <figref idref="f0001">Figure 1</figref> obtained with an extrusion method optimised according to a third embodiment of the present invention;</li>
<li><figref idref="f0002">Figure 5</figref> is a cross-section of the section illustrated in <figref idref="f0001">Figure 1</figref> obtained with an extrusion method optimised according to a fourth embodiment of the present invention; and</li>
<li><figref idref="f0002">Figure 6</figref> is a schematic cross-section of a comparison between the non-optimised section illustrated in <figref idref="f0001">Figure 1</figref> and a section optimised according to another embodiment of the present invention.</li>
</ul></p>
<p id="p0026" num="0026">With reference to the accompanying drawings, the numeral 1 denotes as a whole an optimised aluminium section obtained with an extrusion method optimised according to several non-limiting embodiments of the present invention.</p>
<p id="p0027" num="0027">In <figref idref="f0001 f0002">Figures 2 to 5</figref> the optimised section 1 consists of a panel for an industrial vehicle body, but this<!-- EPO <DP n="8"> --> is only an example of application of the optimisation method disclosed, which may, in general, be used for the production of any type of section.</p>
<p id="p0028" num="0028">The extrusion process in general involves, in the known way, the section to be produced being obtained by extrusion through a die with a predetermined shape.</p>
<p id="p0029" num="0029">As said, the present invention relates to the optimisation of an extrusion process which, each time may be used for the production of any type of optimised section 1 designed for the purpose or, as a non-limiting example, the one illustrated in <figref idref="f0001">Figure 2</figref> deriving from a non-optimised section (as a non-limiting example, the one illustrated in <figref idref="f0001">Figure 1</figref>).</p>
<p id="p0030" num="0030">As a result, for each extrusion process to be optimised, all operating parameters are known, such as the type of plant, the material used to make the die, which determines the friction between the aluminium and the die, the type of aluminium alloy to be extruded, its ideal extrusion temperature and anything else necessary for the success of the entire extrusion process.</p>
<p id="p0031" num="0031">Therefore, given a type of section (for example,<!-- EPO <DP n="9"> --> that illustrated in <figref idref="f0001">Figure 1</figref>) which can be produced with the non-optimised method, the main specifications for it are known. In particular, the (non-optimised) section will have a reference weight per unit of length PR1, at least a portion with practically uniform minimum thickness SM1, used as the basis for calculation, for the extrusion process, of an extrusion limit speed VL1 corresponding to the maximum extrusion speed which can be achieved without section surface deterioration, which generally occurs at the portion with the minimum thickness (which is the critical portion).</p>
<p id="p0032" num="0032">In one embodiment of the present invention, extrusion is performed in such a way that the optimised section 1 has, in cross-section, at least at its portion which in the case of a non-optimised section is the one with the minimum thickness SM1, alternating zones 2 with thickness less than the minimum thickness SM1, and zones 3 with thickness greater than that of said zones 2.</p>
<p id="p0033" num="0033">This alternation of zones 2, 3 may be achieved either only at the portion with minimum thickness, or at some or all of the other portions of the section 1.<!-- EPO <DP n="10"> --></p>
<p id="p0034" num="0034">At a practical level the alternation of zones 2, 3 may be easily achieved by preparing a suitable die. For all practical purposes, the zones 3 constitute, during extrusion, outlets for the aluminium which allow the zones 2 adjacent to them to be obtained without surface deterioration.</p>
<p id="p0035" num="0035">Hereinafter, a section 1 obtained according to the present invention will be indicated as an optimised section 1, or more simply as a section 1, whilst a section obtained using the non-optimised process will be indicated as a non-optimised section.</p>
<p id="p0036" num="0036">For the optimised process described above an extrusion limit speed VL2 can be identified, corresponding to the maximum extrusion speed that can be reached without surface deterioration of the section 1 obtained according to the above description.</p>
<p id="p0037" num="0037">According to choices made during definition of the configuration and dimensions of the zones 2, 3, the extrusion limit speed VL2 will be equal to the extrusion limit speed VL1 defined for the non-optimised section, if the weight per unit of length PR2 of the optimised section 1 is lower than the weight per unit of length or reference weight PR1 of the non-optimised section, whilst it will be<!-- EPO <DP n="11"> --> greater than the limit speed VL1 if the weight per unit of length PR2 of the optimised section 1 is greater than the reference weight PR1 of the non-optimised section.</p>
<p id="p0038" num="0038">In general, the optimised section 1 will have a weight per unit of length PR2 non greater than the weight for the same unit of length PR1 of the non-optimised section.</p>
<p id="p0039" num="0039">This circumstance is clearer with reference to <figref idref="f0002">Figure 6</figref>, where on the right there is a non-optimised section with minimum thickness H, whilst on the left there is a section 1 optimised according to an embodiment of the present invention in which the zones 2 are stretches of optimised section 1 with uniform thickness H2, less than the minimum thickness H of the non-optimised section, and the zones 3 have a triangular cross-section with the thickness of the optimised section 1 measured at the vertex of the triangle with value H1.</p>
<p id="p0040" num="0040">In general, whilst H2 will always be less than H, H1 may have any value even if the best results are obtained with H1 greater than H.</p>
<p id="p0041" num="0041"><figref idref="f0002">Figure 6</figref> also shows, with a dashed line, a thickness H3 corresponding to the average thickness<!-- EPO <DP n="12"> --> of the optimised portion illustrated.</p>
<p id="p0042" num="0042">This thickness H3 corresponds to the theoretical average thickness that the optimised section 1 would have if it had a constant thickness, the same volume and the same weight for the same unit of length.</p>
<p id="p0043" num="0043">In general, according to the preferred embodiment of the present invention H3 will be less than or equal to H (as will the weight per unit of length). If H3 and H are equal, thanks to the optimisation method described above, the optimised section 1 could be extruded, with equal weight per unit of length (PR1=PR2), at a limit speed VL2 greater than the limit speed VL1 identified for the non-optimised section and, since the thickness H1 of the zones 3 is greater than H, it will also have a transversal resistance to bending RF2 greater than the transversal resistance RF1 verifiable on the non-optimised section.</p>
<p id="p0044" num="0044">In contrast, when H3 is less than H it will in general be possible both to maintain an extrusion speed VL2 equal to the limit speed VL1, saving only on the quantity of material, and to reach an extrusion limit speed VL2 greater than the limit speed VL1 up to the maximum speed achievable<!-- EPO <DP n="13"> --> without defects, therefore saving both on the weight and on production times per unit of length or it will be possible to reach an ideal compromise between the saving in terms of weight and production time.</p>
<p id="p0045" num="0045">By way of example, <figref idref="f0001 f0002">Figures 2 to 6</figref> illustrate some of the many possible embodiments of the present invention.</p>
<p id="p0046" num="0046">In particular:
<ul id="ul0002" list-style="dash" compact="compact">
<li>in <figref idref="f0001">Figure 2</figref> the zones 2 have a constant thickness whilst the zones 3 have, seen in cross-section, a dome shape;</li>
<li>in <figref idref="f0001">Figure 3</figref> the alternation of zones 2, 3 forms, in cross-section, a curved undulating profile;</li>
<li>in <figref idref="f0001">Figure 4</figref> the alternation of zones 2, 3 forms, in cross-section, a saw tooth profile in which the second zones 3 have the shape of an isosceles triangle;</li>
<li>in <figref idref="f0002">Figure 5</figref> the alternation of zones 2, 3 forms, in cross-section, a square wave profile; and</li>
<li>in <figref idref="f0002">Figure 6</figref>, in the part on the left relative to the optimised section 1, the zones 2 have a constant thickness, whilst the zones 3 have, seen in cross-section, a triangular shape.</li>
</ul></p>
<p id="p0047" num="0047">In the embodiments of the present invention<!-- EPO <DP n="14"> --> illustrated, in which the optimised section 1 is a panel of an industrial vehicle body, the alternation of zones 2, 3 is obtained on most of the section 1, whilst in the non-optimised embodiment, the non-optimised section has a thickness that is practically constant all over.</p>
<p id="p0048" num="0048">In general, the present invention may be applied both to solid sections (without tubular cavities), and to hollow sections, as is the case for panels for vehicle bodies, with one or more tubular segments.</p>
<p id="p0049" num="0049">In the latter case, if the optimised section 1 is tubular, advantageously, the alternation of zones 2, 3 may be achieved inside the section 1.</p>
<p id="p0050" num="0050">Obviously, the optimisation method disclosed may be applied only when the section 1 optimised or to be optimised has, at least at a portion with the limit thickness, at least one surface (visible or hidden because it is inside, as in the case of the panels illustrated in <figref idref="f0001 f0002">Figures 2 to 5</figref>) which can be produced in accordance with the present invention, without conditioning the subsequent use of the optimised section 1.</p>
<p id="p0051" num="0051">In general, depending on the type of section 1 to be obtained, a technician in the field will be able<!-- EPO <DP n="15"> --> to define, with simple tests, the most suitable configuration and alternation of the zones 2, 3, for the best optimisation of the extrusion process. A technician in the field can also immediately check whether or not, once a section has been produced according to the optimisation method described above, the latter really constitutes an optimisation, even when he does not know the limit speed VL1 and the limit thickness SM1 of the non-optimised products.</p>
<p id="p0052" num="0052">It is sufficient to substitute the die considered optimised with an equivalent die in which the portions which in the optimised die have alternating zones 2, 3 have a uniform thickness equal to the thickness of the zones 2 of the optimised section, and to perform the entire extrusion process under the same operating conditions used for the previous optimised die.</p>
<p id="p0053" num="0053">In this way, if the previous process was effectively optimised, with the new die one would obtain a non-optimised section with a deteriorated surface, following the appearance of scratches and/or scoring and/or lacerations and/or deformations and/or undulations which are more or less extensive and/or breakage of the extrusion die<!-- EPO <DP n="16"> --> and for example in the non-limiting case of a section for panels for vehicle bodies with one or more tubular segments, with the optimisation process disclosed applied in the tubular cavities as indicated in the non-limiting example in <figref idref="f0001 f0002">Figures 2 - 5</figref>, lower resistance to bending following forces applied perpendicular to the 2 largest walls. In contrast, if the process was not optimised, one would obtain a non-optimised section with a surface that had not deteriorated and again in the non-limiting case of a section for panels for vehicle bodies with one or more tubular segments, an equal resistance to transversal bending following forces applied perpendicularly to the 2 largest walls.</p>
<p id="p0054" num="0054">The present invention brings important advantages.</p>
<p id="p0055" num="0055">Thanks to the present invention, a method for optimising a process for extrusion of an aluminium section 1 has been perfected, which allows extrusion, at the same speed as current plants, of sections with a lower weight for the same unit of length compared with the extrusion methods currently known, with a consequent economic saving in terms of the cost of the material.</p>
<p id="p0056" num="0056">Alternatively, thanks to the present invention the extrusion speed can be increased with the same<!-- EPO <DP n="17"> --> weight per unit of length or an ideal compromise can be reached between weight and extrusion speed.</p>
<p id="p0057" num="0057">Another advantage of the present invention is seen when the section 1 has, at the zones 3, a thickness H1 equal to or greater than the thickness H of an equivalent non-optimised section. In this case, the zones 3 form a kind of ribbing for the section 1, guaranteeing the optimised section 1 a mechanical strength substantially equal to (if the thickness of H1 is equal to H) or greater than (when the thickness of H1 is greater than H) the non-optimised sections. The advantage just described is particularly appreciable in the production of hollow sections, with one or more tubular segments, for example such as those of panels for vehicles bodies with the optimisation disclosed applied in the cavities in the section 1, therefore, in a zone that is not visible during use of the finished product.</p>
<p id="p0058" num="0058">In addition, the present invention for the production of sections with low thickness allows a reduction in the pressure which acts on the die by improving the flow of aluminium through the die thanks to the presence of the zones 3, significantly reducing the risk of the die breaking<!-- EPO <DP n="18"> --> compared with the current extrusion methods.</p>
<p id="p0059" num="0059">It should also be noticed that the present invention is relatively easy to produce and even the cost linked to implementation of the invention is not very high.</p>
<p id="p0060" num="0060">The invention described may be subject to modifications and variations without thereby departing from the scope of the claims.</p>
<p id="p0061" num="0061">All details of the invention may be substituted by other technically equivalent elements and in practice all of the materials used, as well as the shapes and dimensions of the various components, may be any according to requirements.</p>
</description><!-- EPO <DP n="19"> -->
<claims id="claims01" lang="en">
<claim id="c-en-01-0001" num="0001">
<claim-text>A method for optimising a process for extrusion of an aluminium section, in which process a non-optimised section is obtained using a die with a predetermined shape, the section having at least a portion with a practically uniform minimum thickness (H) and a reference weight per unit of length (PR1), for said process an extrusion limit speed (VL1) corresponding to the maximum extrusion speed that can be reached without deterioration of the surface of said portion of the section is determined,<br/>
the optimisation method being <b>characterised in that</b>:
<claim-text>said extrusion is performed in such a way that instead of said portion with uniform minimum thickness an optimised section having a portion with alternating first zones (2) having a first thickness (H2) less than the minimum thickness (H), and second zones (3) having a second thickness (H1)<!-- EPO <DP n="20"> --> greater than the first thickness (H2) is provided; for said optimised portion a theoretical average thickness (H3) which is the thickness that the portion would have if it had the same volume and weight for unit of length but a constant thickness is defined; said portion of the section being extruded in such a way that said theoretical average thickness (H3) is not greater than said minimum thickness (H), so that the weight for the same unit of length (PR2) of the optimised section (1) is equal or less than the reference weight (PR1)</claim-text>
<claim-text>and <b>in that</b> said extrusion step is performed with an extrusion speed equal to or greater than the limit speed (VL1).</claim-text><!-- EPO <DP n="21"> --></claim-text></claim>
<claim id="c-en-01-0002" num="0002">
<claim-text>The optimisation method according to claim 1, <b>characterised in that</b> the second zones (3) have a triangular shape in cross-section.</claim-text></claim>
<claim id="c-en-01-0003" num="0003">
<claim-text>The optimisation method according to claim 1, <b>characterised in that</b> the second zones (3) have a rectangular shape in cross-section.</claim-text></claim>
<claim id="c-en-01-0004" num="0004">
<claim-text>The optimisation method according to claim 1, <b>characterised in that</b> the second zones (3) have a dome shape in cross-section.</claim-text></claim>
<claim id="c-en-01-0005" num="0005">
<claim-text>The optimisation method according to claim 1, <b>characterised in that</b> the alternation of zones (2), (3) forms an undulating profile in cross-section.</claim-text></claim>
</claims><!-- EPO <DP n="22"> -->
<claims id="claims02" lang="de">
<claim id="c-de-01-0001" num="0001">
<claim-text>Verfahren zum Optimieren eines Prozesses zum Strangpressen eines Aluminiumprofils, bei welchem Prozess ein nicht optimiertes Profil erhalten wird, und zwar unter Verwendung einer Matrize von einer vorgegebenen Form, wobei das Profil wenigstens einen Abschnitt von einer praktisch gleichmässigen minimalen Stärke (H) hat, sowie ein Bezugsgewicht pro Längeneinheit (PR1), wobei für den genannten Prozess eine Extrusions-Grenzgeschwindigkeit (VL1) entsprechend der maximalen Extrusionsgeschwindigkeit festgelegt ist, die ohne Qualitätsminderung der Oberfläche des genannten Abschnittes des Profils erreicht werden kann, wobei das Optimierverfahren <b>dadurch gekennzeichnet ist, dass</b>:
<claim-text>die genannte Extrusion auf solche Weise durchgeführt wird, dass anstelle des genannten Abschnittes von einer gleichmässigen minimalen Stärke ein optimiertes Profil vorgesehen ist, das einen Abschnitt mit abwechselnden ersten Bereichen (2) von einer ersten Stärke (H2), geringer als die minimale Stärke (H), und zweiten Bereichen (3) von einer zweiten Stärke (H1), grösser als die erste Stärke (H2), aufweist; für den genannten optimierten Abschnitt eine theoretische Durchschnittsstärke (H3) festgelegt wird, welche die Stärke ist, die der Abschnitt haben würde, wenn er das gleiche Volumen und Gewicht pro Längeneinheit, aber eine gleichbleibende Stärke hätte; wobei der genannte Abschnitt des Profils auf solche Weise extrudiert wird, dass die genannte theoretische Durchschnittsstärke (H3) nicht grösser ist als die genannte minimale Stärke (H), so dass das Gewicht für die gleiche Längeneinheit (PR2) des optimierten Profils (1) gleich oder geringer ist als das Bezugsgewicht (PR1);</claim-text>
<claim-text>und <b>dadurch,</b> dass die Extrusionsphase mit einer Extrusionsgeschwindigkeit gleich oder höher als die Grenzgeschwindigkeit<!-- EPO <DP n="23"> --> (VL1) durchgeführt wird.</claim-text></claim-text></claim>
<claim id="c-de-01-0002" num="0002">
<claim-text>Optimierverfahren nach Patentanspruch 1, <b>dadurch gekennzeichnet, dass</b> die zweiten Bereiche (3) im Querschnitt eine dreieckige Form aufweisen.</claim-text></claim>
<claim id="c-de-01-0003" num="0003">
<claim-text>Optimierverfahren nach Patentanspruch 1, <b>dadurch gekennzeichnet, dass</b> die zweiten Bereiche (3) im Querschnitt eine rechteckige Form aufweisen.</claim-text></claim>
<claim id="c-de-01-0004" num="0004">
<claim-text>Optimierverfahren nach Patentanspruch 1, <b>dadurch gekennzeichnet, dass</b> die zweiten Bereiche (3) im Querschnitt eine Kuppelform aufweisen.</claim-text></claim>
<claim id="c-de-01-0005" num="0005">
<claim-text>Optimierverfahren nach Patentanspruch 1, <b>dadurch gekennzeichnet, dass</b> der Wechsel der Bereiche (2), (3) im Querschnitt ein gewelltes Profil bildet.</claim-text></claim>
</claims><!-- EPO <DP n="24"> -->
<claims id="claims03" lang="fr">
<claim id="c-fr-01-0001" num="0001">
<claim-text>Une méthode pour optimaliser un procédé de filage d'un profilé en aluminium, un profilé non-optimalisé étant obtenu dans ce procédé en utilisant une matrice ayant une forme prédéfinie, le profilé présentant au moins une portion ayant une épaisseur minimum (H) pratiquement uniforme et un poids de référence par unité de longueur (PR1), pour ledit procédé une vitesse limite de filage (VL1) correspondant à la vitesse de filage maximum pouvant être atteinte sans détérioration de la surface de ladite portion du profilé étant définie,<br/>
la méthode d'optimalisation étant <b>caractérisée en ce que :</b>
<claim-text>ledit filage est effectué de manière à obtenir, au lieu de ladite portion ayant une épaisseur minimum uniforme, un profilé optimalisé ayant une portion présentant de façon alternée des premières zones (2) ayant une première épaisseur (H2) inférieure à l'épaisseur minimum (H) et des deuxièmes zones (3) ayant une deuxième épaisseur (H1) supérieure à la première épaisseur (H2) ; pour ladite portion optimalisée une épaisseur moyenne théorique (H3), qui correspond à l'épaisseur que la portion aurait si elle avait les mêmes volume et poids par unité de longueur mais une épaisseur constante, est définie ; ladite portion du profilé étant filée de manière à ce que ladite épaisseur moyenne théorique (H3) ne soit pas supérieure à ladite épaisseur minimum (H), afin que le poids par même unité de longueur (PR2) du profilé optimalisé (1) soit égal ou inférieur au poids de référence (PR1)</claim-text>
<claim-text>et <b>en ce que</b> ladite phase de filage est effectuée avec une vitesse de filage égale ou supérieure à la vitesse limite (VL1).</claim-text><!-- EPO <DP n="25"> --></claim-text></claim>
<claim id="c-fr-01-0002" num="0002">
<claim-text>La méthode d'optimalisation selon la revendication 1, <b>caractérisée en ce que</b> les deuxièmes zones (3) ont, en coupe, une forme triangulaire.</claim-text></claim>
<claim id="c-fr-01-0003" num="0003">
<claim-text>La méthode d'optimalisation selon la revendication 1, <b>caractérisée en ce que</b> les deuxièmes zones (3) ont, en coupe, une forme rectangulaire.</claim-text></claim>
<claim id="c-fr-01-0004" num="0004">
<claim-text>La méthode d'optimalisation selon la revendication 1, <b>caractérisée en ce que</b> les deuxièmes zones (3) ont, en coupe, la forme d'un dôme.</claim-text></claim>
<claim id="c-fr-01-0005" num="0005">
<claim-text>La méthode d'optimalisation selon la revendication 1, <b>caractérisée en ce que</b> l'alternance des zones (2), (3) forme, en coupe, un profil onduleux.</claim-text></claim>
</claims><!-- EPO <DP n="26"> -->
<drawings id="draw" lang="en">
<figure id="f0001" num="1,2,3,4"><img id="if0001" file="imgf0001.tif" wi="165" he="229" img-content="drawing" img-format="tif"/></figure><!-- EPO <DP n="27"> -->
<figure id="f0002" num="5,6"><img id="if0002" file="imgf0002.tif" wi="144" he="233" img-content="drawing" img-format="tif"/></figure>
</drawings>
<ep-reference-list id="ref-list">
<heading id="ref-h0001"><b>REFERENCES CITED IN THE DESCRIPTION</b></heading>
<p id="ref-p0001" num=""><i>This list of references cited by the applicant is for the reader's convenience only. It does not form part of the European patent document. Even though great care has been taken in compiling the references, errors or omissions cannot be excluded and the EPO disclaims all liability in this regard.</i></p>
<heading id="ref-h0002"><b>Patent documents cited in the description</b></heading>
<p id="ref-p0002" num="">
<ul id="ref-ul0001" list-style="bullet">
<li><patcit id="ref-pcit0001" dnum="JP07009027A"><document-id><country>JP</country><doc-number>07009027</doc-number><kind>A</kind></document-id></patcit><crossref idref="pcit0001">[0001]</crossref></li>
</ul></p>
</ep-reference-list>
</ep-patent-document>
