EP3080318B2 - Method for manufacturing products made of aluminium-copper-lithium alloy with improved fatigue properties and distributor for this method - Google Patents
Method for manufacturing products made of aluminium-copper-lithium alloy with improved fatigue properties and distributor for this method Download PDFInfo
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- EP3080318B2 EP3080318B2 EP14828176.9A EP14828176A EP3080318B2 EP 3080318 B2 EP3080318 B2 EP 3080318B2 EP 14828176 A EP14828176 A EP 14828176A EP 3080318 B2 EP3080318 B2 EP 3080318B2
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- 238000000034 method Methods 0.000 title claims description 22
- 238000004519 manufacturing process Methods 0.000 title claims description 7
- 239000001989 lithium alloy Substances 0.000 title description 10
- 229910000733 Li alloy Inorganic materials 0.000 title description 8
- -1 aluminium-copper-lithium Chemical compound 0.000 title description 8
- 239000004744 fabric Substances 0.000 claims description 44
- 238000005266 casting Methods 0.000 claims description 39
- 229910001338 liquidmetal Inorganic materials 0.000 claims description 26
- 239000007788 liquid Substances 0.000 claims description 19
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims description 18
- 239000001301 oxygen Substances 0.000 claims description 18
- 229910052760 oxygen Inorganic materials 0.000 claims description 18
- 229910045601 alloy Inorganic materials 0.000 claims description 14
- 239000000956 alloy Substances 0.000 claims description 14
- 229910052744 lithium Inorganic materials 0.000 claims description 10
- 238000002844 melting Methods 0.000 claims description 10
- 230000008018 melting Effects 0.000 claims description 10
- 229910000838 Al alloy Inorganic materials 0.000 claims description 9
- 229910052751 metal Inorganic materials 0.000 claims description 9
- 239000002184 metal Substances 0.000 claims description 9
- 238000007711 solidification Methods 0.000 claims description 9
- 230000008023 solidification Effects 0.000 claims description 9
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims description 8
- 229910052782 aluminium Inorganic materials 0.000 claims description 8
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 8
- 229910052748 manganese Inorganic materials 0.000 claims description 8
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 7
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 claims description 7
- 238000001914 filtration Methods 0.000 claims description 7
- 239000001257 hydrogen Substances 0.000 claims description 7
- 229910052739 hydrogen Inorganic materials 0.000 claims description 7
- 150000003839 salts Chemical class 0.000 claims description 7
- 229910052719 titanium Inorganic materials 0.000 claims description 7
- 229910052726 zirconium Inorganic materials 0.000 claims description 7
- 229910052799 carbon Inorganic materials 0.000 claims description 5
- 238000009749 continuous casting Methods 0.000 claims description 5
- 238000007872 degassing Methods 0.000 claims description 5
- 239000011261 inert gas Substances 0.000 claims description 5
- 238000007789 sealing Methods 0.000 claims description 4
- 238000005242 forging Methods 0.000 claims description 3
- 238000010438 heat treatment Methods 0.000 claims description 3
- 238000003754 machining Methods 0.000 claims description 3
- 238000005096 rolling process Methods 0.000 claims description 3
- 229910002065 alloy metal Inorganic materials 0.000 claims description 2
- 229910052804 chromium Inorganic materials 0.000 claims description 2
- 238000001125 extrusion Methods 0.000 claims description 2
- 239000004033 plastic Substances 0.000 claims description 2
- 238000010791 quenching Methods 0.000 claims description 2
- 230000000171 quenching effect Effects 0.000 claims description 2
- 229910052710 silicon Inorganic materials 0.000 claims description 2
- 230000032683 aging Effects 0.000 claims 1
- 239000004411 aluminium Substances 0.000 claims 1
- 238000005482 strain hardening Methods 0.000 claims 1
- 239000000047 product Substances 0.000 description 35
- 238000012360 testing method Methods 0.000 description 18
- 238000009434 installation Methods 0.000 description 12
- 239000011572 manganese Substances 0.000 description 9
- 239000010949 copper Substances 0.000 description 7
- 239000010936 titanium Substances 0.000 description 7
- 239000011777 magnesium Substances 0.000 description 6
- 229910052709 silver Inorganic materials 0.000 description 6
- 230000003068 static effect Effects 0.000 description 6
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 5
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- 239000004332 silver Substances 0.000 description 5
- 239000011701 zinc Substances 0.000 description 5
- 239000012080 ambient air Substances 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- KWGKDLIKAYFUFQ-UHFFFAOYSA-M lithium chloride Chemical compound [Li+].[Cl-] KWGKDLIKAYFUFQ-UHFFFAOYSA-M 0.000 description 4
- 238000009941 weaving Methods 0.000 description 4
- 238000010276 construction Methods 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- 229910052802 copper Inorganic materials 0.000 description 3
- 238000009661 fatigue test Methods 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 229910052749 magnesium Inorganic materials 0.000 description 3
- 239000000523 sample Substances 0.000 description 3
- 239000003351 stiffener Substances 0.000 description 3
- 238000005496 tempering Methods 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 229910017539 Cu-Li Inorganic materials 0.000 description 2
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 2
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 2
- 238000012512 characterization method Methods 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 229910002804 graphite Inorganic materials 0.000 description 2
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- 238000002360 preparation method Methods 0.000 description 2
- 239000003381 stabilizer Substances 0.000 description 2
- 229910052725 zinc Inorganic materials 0.000 description 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- 239000004952 Polyamide Substances 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 239000004809 Teflon Substances 0.000 description 1
- 229920006362 Teflon® Polymers 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
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- JCXJVPUVTGWSNB-UHFFFAOYSA-N nitrogen dioxide Inorganic materials O=[N]=O JCXJVPUVTGWSNB-UHFFFAOYSA-N 0.000 description 1
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Images
Classifications
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/12—Alloys based on aluminium with copper as the next major constituent
- C22C21/14—Alloys based on aluminium with copper as the next major constituent with silicon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
- C22F1/057—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with copper as the next major constituent
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21B—ROLLING OF METAL
- B21B1/00—Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations
- B21B1/22—Metal-rolling methods or mills for making semi-finished products of solid or profiled cross-section; Sequence of operations in milling trains; Layout of rolling-mill plant, e.g. grouping of stands; Succession of passes or of sectional pass alternations for rolling plates, strips, bands or sheets of indefinite length
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C23/00—Extruding metal; Impact extrusion
- B21C23/21—Presses specially adapted for extruding metal
- B21C23/212—Details
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J5/00—Methods for forging, hammering, or pressing; Special equipment or accessories therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/001—Continuous casting of metals, i.e. casting in indefinite lengths of specific alloys
- B22D11/003—Aluminium alloys
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/04—Continuous casting of metals, i.e. casting in indefinite lengths into open-ended moulds
- B22D11/0408—Moulds for casting thin slabs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/04—Continuous casting of metals, i.e. casting in indefinite lengths into open-ended moulds
- B22D11/041—Continuous casting of metals, i.e. casting in indefinite lengths into open-ended moulds for vertical casting
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/04—Continuous casting of metals, i.e. casting in indefinite lengths into open-ended moulds
- B22D11/059—Mould materials or platings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/10—Supplying or treating molten metal
- B22D11/103—Distributing the molten metal, e.g. using runners, floats, distributors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/10—Supplying or treating molten metal
- B22D11/11—Treating the molten metal
- B22D11/116—Refining the metal
- B22D11/119—Refining the metal by filtering
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D21/00—Casting non-ferrous metals or metallic compounds so far as their metallurgical properties are of importance for the casting procedure; Selection of compositions therefor
- B22D21/002—Castings of light metals
- B22D21/007—Castings of light metals with low melting point, e.g. Al 659 degrees C, Mg 650 degrees C
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D21/00—Casting non-ferrous metals or metallic compounds so far as their metallurgical properties are of importance for the casting procedure; Selection of compositions therefor
- B22D21/02—Casting exceedingly oxidisable non-ferrous metals, e.g. in inert atmosphere
- B22D21/04—Casting aluminium or magnesium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
- C22C1/026—Alloys based on aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/12—Alloys based on aluminium with copper as the next major constituent
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/12—Alloys based on aluminium with copper as the next major constituent
- C22C21/16—Alloys based on aluminium with copper as the next major constituent with magnesium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
- C22C21/12—Alloys based on aluminium with copper as the next major constituent
- C22C21/18—Alloys based on aluminium with copper as the next major constituent with zinc
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/002—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working by rapid cooling or quenching; cooling agents used therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21B—ROLLING OF METAL
- B21B3/00—Rolling materials of special alloys so far as the composition of the alloy requires or permits special rolling methods or sequences ; Rolling of aluminium, copper, zinc or other non-ferrous metals
- B21B2003/001—Aluminium or its alloys
Definitions
- the invention relates to a distributor intended for the semi-continuous casting of aluminum alloy plates and a process for manufacturing wrought aluminum - copper - lithium alloy products, intended in particular for aeronautical and aerospace construction.
- Aluminum - copper - lithium alloys are particularly promising for manufacturing this type of product.
- the specifications imposed by the aeronautical industry for fatigue life are high.
- Thick Al-Cu-Li alloy products are notably described in the applications US2005/0006008 And US2009/0159159 .
- US5207974 discloses a partitioned dispenser for dispensing molten metal from a nozzle to form an ingot.
- a first object of the invention is a distributor intended for the semi-continuous casting of aluminum alloy plates according to claim 1.
- Another object of the invention is a method of manufacturing an aluminum alloy product according to claim 6.
- the static mechanical characteristics in traction are determined by a tensile test according to standard NF EN ISO 6892-1, the sampling and direction of the test being defined by standard EN 485-1.
- the Walker equation was used to determine a maximum stress value representative of 50% non-failure at 100,000 cycles.
- IQF corresponding to the median, i.e. 50% rupture per 100,000 cycles.
- a thick wrought product is a product whose thickness is at least 6 mm.
- the thickness of the products according to the invention is at least 80 mm and preferably at least 100 mm.
- the thickness of the wrought products is at least 120 mm or preferably 140 mm.
- the thickness of the thick products according to the invention is typically at most 240 mm, generally at most 220 mm and preferably at most 180 mm.
- a sheet metal is according to the invention a rolled product of rectangular cross section whose uniform thickness is at least 6 mm and does not exceed 1/10th of the width.
- structural element or “structural element” of a mechanical construction a mechanical part for which the static and/or dynamic mechanical properties are particularly important for the performance of the structure, and for which a structural calculation is usually prescribed or carried out.
- these structural elements include in particular the elements which make up the fuselage (such as the fuselage skin), the fuselage stiffeners or stringers (stringers), the bulkheads (bulkheads), the fuselage frames.
- fuselage (circumferential frames), the wings (such as the wing skin), the stiffeners (stringers or stiffeners), the ribs (ribs) and spars (spars)) and the empennage composed in particular of horizontal and vertical stabilizers (horizontal or vertical stabilizers), as well as floor beams, seat tracks and doors.
- a casting installation may include numerous devices such as one or more furnaces necessary for melting the metal (“melting furnace”) and/or maintaining it (“maintaining furnace”) in temperature and/or for processing operations.
- preparation furnace preparation of the liquid metal and adjustment of the composition
- one or more tanks intended to carry out a treatment to eliminate impurities dissolved and/or suspended in the liquid metal
- this treatment may consist of filtering the liquid metal on a filter media in a “filtration bag” or introducing into the bath a so-called “treatment” gas which can be inert or reactive in a “degassing bag”, a degassing device.
- solidification liquid metal (or “casting craft”), by vertical semi-continuous casting by direct cooling in a casting well, which may include devices such as a mold (or “ingot mold”), a device for supplying liquid metal ( or “busette”) and a cooling system, these different furnaces, tanks and solidification devices being interconnected by transfer devices or channels called “chutes” in which the liquid metal can be transported.
- a mold or “ingot mold”
- a device for supplying liquid metal or “busette”
- a cooling system these different furnaces, tanks and solidification devices being interconnected by transfer devices or channels called “chutes” in which the liquid metal can be transported.
- the present inventors have found that, surprisingly, it is possible to obtain thick wrought products made of aluminum copper lithium alloy having improved fatigue performance by preparing these sheets using the following process.
- a bath of liquid alloy metal comprising, in % by weight Cu: 2.0 - 6.0; Li: 0.5 - 2.0; Mg: 0-1.0; Ag: 0 - 0.7; Zn 0 - 1.0; and at least one element chosen from Zr, Mn, Cr, Sc, Hf and Ti, the quantity of said element, if chosen, being 0.05 to 0.20% by weight for Zr, 0.05 to 0 .8% by weight for Mn, 0.05 to 0.3% by weight for Cr and for Sc, 0.05 to 0.5% by weight for Hf and 0.01 to 0.15% by weight for Ti , If ⁇ 0.1; Fe ⁇ 0.1; others ⁇ 0.05 each and ⁇ 0.15 in total, remains aluminum.
- An advantageous alloy for the process according to the invention comprises, in % by weight, Cu: 3.0 - 3.9; Li: 0.7 - 1.3; Mg: 0.1 - 1.0, at least one element chosen from Zr, Mn and Ti, the quantity of said element, if chosen, being 0.06 to 0.15% by weight for Zr, 0, 05 to 0.8% by weight for Mn and 0.01 to 0.15% by weight for Ti; Ag: 0 - 0.7; Zn ⁇ 0.25; If ⁇ 0.08; Fe ⁇ 0.10; others ⁇ 0.05 each and ⁇ 0.15 in total, remains aluminum.
- the copper content is at least 3.2% by weight.
- the lithium content is preferably between 0.85 and 1.15% by weight and preferably between 0.90 and 1.10% by weight.
- the magnesium content is preferably between 0.20 and 0.6% by weight.
- the simultaneous addition of manganese and zirconium is generally advantageous.
- the manganese content is between 0.20 and 0.50% by weight and the zirconium content is between 0.06 and 0.14% by weight.
- the silver content is between 0.20 and 0.7% by weight. It is advantageous if the silver content is at least 0.1% by weight. In one embodiment of the invention the silver content is at least 0.20% by weight. Preferably the silver content is at most 0.5% by weight. In one embodiment of the invention the silver content is limited to 0.3% by weight.
- the silicon content is at most 0.05% by weight and the iron content is at most 0.06% by weight.
- the titanium content is between 0.01 and 0.08% by weight.
- the zinc content is at most 0.15% by weight.
- a preferred aluminum-copper-lithium alloy is alloy AA2050.
- This liquid metal bath is prepared in a furnace of the casting installation. It is known, for example, to US 5,415,220 to use lithium-containing molten salts such as KCl/LiCl mixtures in the melting furnace to passivate the alloy as it is transferred to the casting facility.
- the present inventors have, however, obtained excellent fatigue properties for thick sheets without using molten salt containing lithium in the melting furnace, but by maintaining in this furnace an atmosphere poor in oxygen and believe that the presence of salt in the melting furnace could in certain cases have a detrimental effect on the fatigue properties of thick wrought products.
- molten salt containing lithium is not used throughout the casting installation. In an advantageous embodiment, no molten salt is used throughout the casting installation.
- an oxygen content of less than 0.5% by volume and preferably less than 0.3% by volume is maintained in the furnace(s) of the casting installation.
- an oxygen content of at least 0.05% by volume and even at least 0.1% by volume can be tolerated in the furnace(s) of the casting installation, which is advantageous in particular for the aspects economics of the process.
- the furnace(s) of the casting installation are induction furnaces. The present inventors have found that this type of oven is advantageous despite the mixing generated by induction heating.
- This liquid metal bath is then treated with a degassing bag and a filtration bag so that its hydrogen content is less than 0.4 ml/100g and preferably less than 0.35 ml/100g. .
- the hydrogen content of the liquid metal is measured using commercial equipment such as the device marketed under the brand ALSCAN TM , known to those skilled in the art, the probe being maintained under a nitrogen sweep.
- the oxygen content of the atmosphere in contact with the bath of liquid metal in the melting furnace during the degassing and filtration stages is less than 0.5% by volume and preferably less than 0.3% by volume.
- the oxygen content of the atmosphere in contact with the liquid metal bath is less than 0.5% by volume and preferably less than 0.3% by volume for the entire installation of casting.
- an oxygen content of at least 0.05% by volume and even at least 0.1% by volume can be tolerated for the entire casting installation, which is advantageous in particular for the economic aspects of the process.
- a plate is a block of aluminum with a substantially parallelepiped shape, of length L, width W and thickness T.
- the atmosphere above the liquid surface is controlled during solidification.
- An example of a device for controlling the atmosphere above the liquid surface during solidification is shown in Figure Figure 2 .
- the liquid metal coming from a chute (63) is introduced into a nozzle (4) controlled by a stopper (8) which can move up and down (81), in an ingot mold (31) placed on a false bottom (21).
- the aluminum alloy is solidified by direct cooling (5).
- the aluminum alloy (1) has at least one solid surface (11, 12, 13) and at least one liquid surface (14, 15).
- An elevator (2) makes it possible to maintain the level of the liquid surface (14, 15) substantially constant.
- a distributor (7) allows the distribution of the liquid metal.
- a cover (62) covers the liquid surface.
- the cover may include seals (61) to ensure sealing with the casting table (32).
- the liquid metal in the chute (63) can advantageously be protected by a cover (64).
- An inert gas (9) is introduced into the chamber (65) defined between the cover and the casting table.
- the inert gas is advantageously chosen from rare gases, nitrogen and carbon dioxide or mixtures of these gases.
- a preferred inert gas is argon.
- the oxygen content is measured in the chamber (65) above the liquid surface.
- the inert gas flow can be adjusted to achieve the desired oxygen content.
- the present inventors have noted that there is generally not a sufficient seal between the ingot mold (31) and the solidified metal (5), which leads to diffusion of the atmosphere from the casting well (10) towards the room (65).
- the suction of the pump (101) is such that the pressure in the enclosure (10) is lower than the pressure in the chamber (65), which can be preferably obtained by imposing a speed of the atmosphere through the open surfaces of the casting well at least 2 m/s and preferably at least 2.5 m/s.
- the pressure in the chamber (65) is close to atmospheric pressure and the pressure in the enclosure (10) is lower than atmospheric pressure, typically 0.95 times atmospheric pressure.
- an oxygen content of less than 0.5% by volume and preferably less than 0.3% by volume is maintained in the chamber (65), thanks to the devices described.
- the distributor according to the invention is made of fabric essentially comprising carbon, it comprises a lower face (76), a typically empty upper face defining the orifice through which the liquid metal is introduced (71) and a wall of substantially rectangular section typically substantially constant and of height h typically substantially constant, the wall comprising two longitudinal parts parallel to the width W of the plate (720, 721) and two transverse parts parallel to the thickness T of the plate (730, 731) said transverse parts and longitudinal being formed of at least two fabrics, a first substantially sealing and semi-rigid fabric (77) ensuring the maintenance of the shape of the distributor during casting and a second non-closing fabric (78) allowing the passage and filtration of the liquid, said first and second fabrics being linked to each other without overlap or with overlap and without gap separating them, said first fabric continuously covering at least 30% of the surface of said wall parts (720,721, 730, 731) and being positioned so that the liquid surface is in contact
- the first and second fabrics being sewn to one another without overlap or with overlap and without gap separating them, that is to say in contact, the liquid metal cannot pass through the first fabric and be deflected by the second fabric as is the case for example in a combo-bag as described in the application WO 99/44719 Figures 2 to 5 .
- the distributor is semi-rigid and does not deform significantly during casting.
- the first fabric has a height, hl, measured from the upper face on the circumference of the wall (720, 721, 730, 731) such that h1 ⁇ 0.3 h and preferably h1 ⁇ 0, 5 h, where h designates the total height of the distributor wall.
- the liquid surface being in contact with said first fabric closing the liquid metal only passes through the distributor under the liquid surface in certain directions of each part of the wall.
- the height immersed in the liquid metal of the wall (720, 721, 730, 731) of the distributor (7) covered by the first fabric is at least equal to 20%, preferably 40% and preferably 60% of the height total submerged wall.
- FIG. 4 represents the bottom and the longitudinal wall parts.
- the bottom (76) is covered by the first and second fabrics.
- the first fabric is at least located in the central part of the bottom (76) over a length L1 and/or in the central part of the longitudinal parts (720) and (721) over the entire height h and over a length L2.
- the surface portion covered by the first fabric is between 50 and 80% for the longitudinal parts (720) and (721), and between 40 and 60% for the lateral parts (730, 731) and between 50 and 80% for the bottom (76).
- length L1 of first fabric located in the bottom (76) is advantageous for the length L1 of first fabric located in the bottom (76) to be greater than the length L2 of first fabric located in the part of the longitudinal walls (720) and (721) in contact with the bottom.
- the present inventors believe that the geometry of the distributor makes it possible in particular to improve the quality of the flow of the liquid metal, to reduce turbulence and to improve the temperature distribution.
- the first fabric and the second fabric are advantageously obtained by weaving a thread essentially comprising carbon. Weaving graphite wire is particularly advantageous.
- the fabrics are typically sewn together. It is also possible, instead of a first and second fabric, to use a single diffuser fabric having at least two weaving zones, more or less dense. It is advantageous for the ease of weaving that the thread comprising carbon is coated with a layer facilitating sliding. This layer may for example comprise a fluoropolymer such as Teflon or a polyamide such as xylon.
- the first fabric is noticeably obturating. Typically this is a fabric having mesh sizes of less than 0.5 mm, preferably less than 0.2 mm.
- the second fabric is non-obstructive and allows the passage of molten metal. Typically, it is a fabric having mesh sizes of between 1 and 5 mm, preferably 2 to 4 mm. In one embodiment of the invention the first fabric locally covers the second fabric, while being in intimate contact so as not to leave a gap between the two
- the plate thus obtained is then transformed to obtain a wrought product.
- the plate thus obtained is then homogenized before or after optionally being machined to obtain a shape that can be deformed under heat.
- the plate is machined in the form of a rolling plate so as to then be hot deformed by rolling.
- the plate is machined in the form of a forging blank so as to then be hot deformed by forging.
- the plate is machined in the form of billets so as to then be deformed hot by extrusion.
- the homogenization is carried out at a temperature between 470 and 540°C for a period of between 2 and 30 hours.
- the hot deformation temperature is advantageously at least 350°C and preferably at least 400°C.
- the hot and optionally cold deformation rate that is to say the ratio between on the one hand the difference between the initial thickness, before deformation but after possible machining, and the final thickness and on the other hand the initial thickness is less than 85% and preferably less than 80%. In an embodiment in which the deformation rate during deformation is less than 75% and preferably less than 70%.
- the wrought product thus obtained is then put into solution and quenched.
- the solution temperature is advantageously between 470 and 540°C and preferably between 490 and 530°C and the duration is adapted to the thickness of the product.
- said wrought product thus put into solution is relieved by plastic deformation with a deformation of at least 1%.
- the tempering is carried out in one or more stages at a temperature advantageously between 130 and 160°C for a period of 5 to 60 hours.
- a metallurgical state T8 is obtained, such as in particular T851, T83, T84, or T85.
- the wrought products obtained by the process according to the invention have advantageous properties.
- the products obtained by the process according to the invention have advantageous static mechanical characteristics.
- wrought products whose thickness is at least 80 mm including in % by weight, Cu: 3.0 - 3.9; Li: 0.7 - 1.3; Mg: 0.1 - 1.0, at least one element chosen from Zr, Mn and Ti, the quantity of said element, if chosen, being 0.06 to 0.15% by weight for Zr, 0, 05 to 0.8% by weight for Mn and 0.01 to 0.15% by weight for Ti; Ag: 0 - 0.7; Zn ⁇ 0.25; If ⁇ 0.08; Fe ⁇ 0.10; others ⁇ 0.05 each and ⁇ 0.15 in total, remains aluminum, the yield strength measured at quarter thickness in direction L is at least 450 MPa and preferably at least 470 MPa and/or the breaking strength measured is at least 480 MPa and preferably at least 500 MPa and/or the elongation is at least 5% and preferably at least 6%.
- the wrought products obtained by the process according to the invention can advantageously be used to produce structural elements, preferably aircraft structural elements.
- Preferred aircraft structural elements are spars, ribs or frames.
- the invention is particularly advantageous for parts of complex shape obtained by integral machining, used in particular for the manufacture of aircraft wings as well as for any other use for which the properties of the products according to the invention are advantageous .
- heavy plates made of AA2050 alloy were prepared.
- AA2050 alloy plates were cast by direct-cooled vertical semi-continuous casting.
- the alloy was prepared in a melting furnace.
- a KCl/LiCl mixture was used on the surface of the liquid metal in the melting furnace.
- no salt was used in the melting furnace.
- the casting installation included a hood placed above the casting well to limit the oxygen content.
- a suction (101) was also used such that the pressure in the enclosure (10) was lower than the pressure in the chamber (65) and such that the speed of the atmosphere through the open surfaces of the casting well was at least 2 m/s.
- the oxygen content was measured using an oximeter during casting.
- the hydrogen content in the liquid aluminum was measured using an Alscan TM type probe under nitrogen sweeping. Two types of liquid metal dispensers were used.
- the casting conditions of the different tests carried out are given in table 1.
- the plates were homogenized for 12 hours at 505°C, machined to a thickness of approximately 365 mm, hot rolled to sheets with a final thickness of between 154 and 158 mm, put into solution at 504°C , quenched and relieved by controlled traction with a permanent elongation of 3.5%.
- the sheets thus obtained were tempered for 18 hours at 155°C.
- Static and toughness mechanical properties were characterized at quarter thickness. Static mechanical characteristics and toughness are given in Table 2.
- Table 2 Mechanical characteristics Essay Thickness [mm] Rm (L) MPa Rp0.2 (L) MPa A % (L) 1 158 528 495 6.5 2 155 538 507 7.0 3 155 525 493 8.3 4 158 528 four hundred ninety seven 7.0 5 158 529 495 6.0 6 158 527 496 6.8 7 154 514 486 8.3 8 158 533 502 6.3 9 158 542 512 5.8
- the fatigue properties were characterized on smooth specimens and on hole specimens for certain samples taken at mid-thickness.
Description
L'invention concerne un distributeur destiné à la coulée semi-continue des plaques en alliage d'aluminium et un procédé de fabrication de produits corroyés alliages aluminium - cuivre - lithium, destinés notamment à la construction aéronautique et aérospatiale.The invention relates to a distributor intended for the semi-continuous casting of aluminum alloy plates and a process for manufacturing wrought aluminum - copper - lithium alloy products, intended in particular for aeronautical and aerospace construction.
Des produits laminés en alliage d'aluminium sont développés pour produire des éléments structuraux destinés notamment à l'industrie aéronautique et à l'industrie aérospatiale.Rolled aluminum alloy products are developed to produce structural elements intended in particular for the aviation industry and the aerospace industry.
Les alliages aluminium - cuivre - lithium sont particulièrement prometteurs pour fabriquer ce type de produit. Les spécifications imposées par l'industrie aéronautique pour la tenue en fatigue sont élevées. Pour les produits épais elles sont particulièrement difficiles à atteindre. En effet compte tenu des épaisseurs possibles des plaques coulées, la réduction d'épaisseur par déformation à chaud est assez faible et par conséquent les sites liés à la coulée sur lesquels s'initient les fissures de fatigue ne voient pas leur taille réduite au cours de la déformation à chaud.Aluminum - copper - lithium alloys are particularly promising for manufacturing this type of product. The specifications imposed by the aeronautical industry for fatigue life are high. For thick products they are particularly difficult to reach. Indeed, taking into account the possible thicknesses of the cast plates, the reduction in thickness by hot deformation is quite low and consequently the sites linked to the casting on which the fatigue cracks initiate do not see their size reduced during hot deformation.
Le lithium étant particulièrement oxydable, la coulée des alliages aluminium-cuivre-lithium génère d'une manière générale des sites d'initiation de fissure en fatigue plus nombreux que pour les alliages de type 2XXX sans lithium ou 7XXX. Ainsi les solutions habituellement trouvées pour l'obtention de produits laminés épais en alliages de type 2XXX sans lithium ou 7XXX ne permettent pas d'obtenir des propriétés en fatigue suffisantes pour les alliages aluminium - cuivre - lithium.Lithium being particularly oxidizable, the casting of aluminum-copper-lithium alloys generally generates more fatigue crack initiation sites than for type 2XXX alloys without lithium or 7XXX. Thus the solutions usually found for obtaining thick rolled products in type 2XXX alloys without lithium or 7XXX do not make it possible to obtain sufficient fatigue properties for aluminum - copper - lithium alloys.
Des produits épais en alliage Al-Cu-Li sont notamment décrits dans les demandes
Dans la demande
Dans la demande
Dans la demande
Il existe un besoin pour des produits épais en alliage aluminium - cuivre - lithium présentant des propriétés améliorées par rapport à celles des produits connus, en particulier en termes de propriétés en fatigue tout en ayant des propriétés de ténacité et des propriétés de résistance mécanique statique avantageuses. Par ailleurs il existe un besoin pour un procédé simple et économique d'obtention de ces produits.There is a need for thick aluminum - copper - lithium alloy products having improved properties compared to those of known products, in particular in terms of fatigue properties while having toughness properties and advantageous static mechanical resistance properties. . Furthermore, there is a need for a simple and economical process for obtaining these products.
Un premier objet de l'invention est un distributeur destiné à la coulée semi-continue de plaques en alliage d'aluminium selon la revendication 1.A first object of the invention is a distributor intended for the semi-continuous casting of aluminum alloy plates according to
Un autre objet de l'invention est un procédé de fabrication d'un produit en alliage d'aluminium selon la revendication 6.Another object of the invention is a method of manufacturing an aluminum alloy product according to claim 6.
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La
Figure 1 est le schéma des éprouvettes utilisées pour les essais en fatigue lisse (Fig 1a ) et en fatigue à trou (Fig 1b ). Les dimensions sont données en mm.ThereFigure 1 is the diagram of the specimens used for the smooth fatigue tests (Fig 1a ) and in hole fatigue (Fig 1b ). Dimensions are given in mm. -
La
Figure 2 est un schéma général du dispositif de solidification utilisé dans un mode de réalisation de l'invention.ThereFigure 2 is a general diagram of the solidification device used in one embodiment of the invention. -
La
Figure 3 est un schéma général du distributeur utilisé dans le procédé selon l'invention.ThereFigure 3 is a general diagram of the distributor used in the method according to the invention. -
La
Figure 4 présente des représentations du fond et des parties latérales et longitudinales de la paroi du distributeur selon un mode de réalisation de l'invention.ThereFigure 4 presents representations of the bottom and the lateral and longitudinal parts of the wall of the distributor according to one embodiment of the invention. -
La
Figure 5 montre la relation entre la performance en fatigue lisse et la teneur en hydrogène du bain de métal liquide lors de la solidification (Fig 5a ) ou la teneur en oxygène mesurée au-dessus de la surface liquide lors de la solidification (Fig. 5b ).ThereFigure 5 shows the relationship between smooth fatigue performance and the hydrogen content of the liquid metal bath during solidification (Fig 5a ) or the oxygen content measured above the liquid surface during the solidification (Fig. 5b ). -
La
Figure 6 montre les courbes de Wöhler obtenues avec les essais 3, 7 et 8 dans la direction L-T (Figure 6a ) et T-L (figure 6b ).ThereFigure 6 shows the Wöhler curves obtained with 3, 7 and 8 in the LT direction (tests Figure 6a ) and TL (figure 6b ).
Sauf mention contraire, toutes les indications concernant la composition chimique des alliages sont exprimées comme un pourcentage en poids basé sur le poids total de l'alliage. L'expression 1,4 Cu signifie que la teneur en cuivre exprimée en % en poids est multipliée par 1,4. La désignation des alliages se fait en conformité avec les règlements de The Aluminium Association, connus de l'homme du métier. Sauf mention contraire les définitions des états métallurgiques indiquées dans la norme européenne EN 515 s'appliquent.Unless otherwise stated, all indications regarding the chemical composition of alloys are expressed as a weight percentage based on the total weight of the alloy. The expression 1.4 Cu means that the copper content expressed in % by weight is multiplied by 1.4. The designation of alloys is done in accordance with the regulations of The Aluminum Association, known to those skilled in the art. Unless otherwise stated, the definitions of metallurgical conditions indicated in European standard EN 515 apply.
Les caractéristiques mécaniques statiques en traction, en d'autres termes la résistance à la rupture Rm, la limite d'élasticité conventionnelle à 0,2% d'allongement Rp0,2, et l'allongement à la rupture A%, sont déterminés par un essai de traction selon la norme NF EN ISO 6892-1, le prélèvement et le sens de l'essai étant définis par la norme EN 485-1. Les propriétés en fatigue sur éprouvettes lisses sont mesurées à l'air ambiant à une contrainte d'amplitude maximale de 242 MPa, une fréquence de 50 Hz, un rapport de contrainte R = 0,1, sur des éprouvettes telles que représentées sur la Figure la, prélevées à mi-largeur et à mi-épaisseur des tôles dans la direction TL. Les conditions de test obéissent à la norme ASTM E466. On détermine la moyenne logarithmique des résultats obtenus sur au moins 4 éprouvettes.The static mechanical characteristics in traction, in other words the breaking strength R m , the conventional elastic limit at 0.2% elongation R p0.2 , and the elongation at break A%, are determined by a tensile test according to standard NF EN ISO 6892-1, the sampling and direction of the test being defined by standard EN 485-1. The fatigue properties on smooth specimens are measured in ambient air at a maximum stress amplitude of 242 MPa, a frequency of 50 Hz, a stress ratio R = 0.1, on specimens as shown in Figure la, taken at half-width and half-thickness of the sheets in the TL direction. Test conditions comply with ASTM E466. The logarithmic average of the results obtained on at least 4 test pieces is determined.
Les propriétés en fatigue sur éprouvettes à trou sont mesurées à l'air ambiant pour des niveaux de contrainte variables, à une fréquence de 50 Hz, un rapport de contrainte R = 0,1, sur des éprouvettes telles que représentées sur la
Dans le cadre de l'invention, un produit corroyé épais est un produit dont l'épaisseur est au moins 6 mm. De préférence l'épaisseur des produits selon l'invention est au moins 80 mm et de manière préférée au moins 100 mm. Dans un mode de réalisation de l'invention l'épaisseur des produits corroyés est au moins 120 mm ou de préférence 140 mm. L'épaisseur des produits épais selon l'invention est typiquement au plus de 240 mm, généralement au plus de 220 mm et préférentiellement au plus de 180 mm.In the context of the invention, a thick wrought product is a product whose thickness is at least 6 mm. Preferably the thickness of the products according to the invention is at least 80 mm and preferably at least 100 mm. In one embodiment of the invention the thickness of the wrought products is at least 120 mm or preferably 140 mm. The thickness of the thick products according to the invention is typically at most 240 mm, generally at most 220 mm and preferably at most 180 mm.
Sauf mention contraire, les définitions de la norme EN 12258 s'appliquent. Notamment, une tôle est selon l'invention un produit laminé de section transversale rectangulaire dont l'épaisseur uniforme est au moins de 6 mm et n'excède pas 1/10ème de la largeur.Unless otherwise stated, the definitions in EN 12258 apply. In particular, a sheet metal is according to the invention a rolled product of rectangular cross section whose uniform thickness is at least 6 mm and does not exceed 1/10th of the width.
On appelle ici « élément de structure » ou « élément structural » d'une construction mécanique une pièce mécanique pour laquelle les propriétés mécaniques statiques et/ou dynamiques sont particulièrement importantes pour la performance de la structure, et pour laquelle un calcul de structure est habituellement prescrit ou réalisé. Il s'agit typiquement d'éléments dont la défaillance est susceptible de mettre en danger la sécurité de ladite construction, de ses utilisateurs, de ses usagers ou d'autrui. Pour un avion, ces éléments de structure comprennent notamment les éléments qui composent le fuselage (tels que la peau de fuselage (fuselage skin en anglais), les raidisseurs ou lisses de fuselage (stringers), les cloisons étanches (bulkheads), les cadres de fuselage (circumferential frames), les ailes (tels que la peau de voilure (wing skin), les raidisseurs (stringers ou stiffeners), les nervures (ribs) et longerons (spars)) et l'empennage composé notamment de stabilisateurs horizontaux et verticaux (horizontal or vertical stabilisers), ainsi que les profilés de plancher (floor beams), les rails de sièges (seat tracks) et les portes.Here we call "structural element" or "structural element" of a mechanical construction a mechanical part for which the static and/or dynamic mechanical properties are particularly important for the performance of the structure, and for which a structural calculation is usually prescribed or carried out. These are typically elements whose failure is likely to endanger the safety of said construction, its users, its users or others. For an aircraft, these structural elements include in particular the elements which make up the fuselage (such as the fuselage skin), the fuselage stiffeners or stringers (stringers), the bulkheads (bulkheads), the fuselage frames. fuselage (circumferential frames), the wings (such as the wing skin), the stiffeners (stringers or stiffeners), the ribs (ribs) and spars (spars)) and the empennage composed in particular of horizontal and vertical stabilizers (horizontal or vertical stabilizers), as well as floor beams, seat tracks and doors.
On appelle ici « ensemble de l'installation de coulée » l'ensemble des dispositifs permettant de transformer un métal sous forme quelconque en demi-produit de forme brute en passant par la phase liquide. Une installation de coulée peut comprendre de nombreux dispositifs tels que un ou plusieurs fours nécessaires à la fusion du métal (« four de fusion ») et/ou à son maintien (« four de maintien ») en température et/ou à des opérations de préparation du métal liquide et d'ajustement de la composition (« four d'élaboration »), une ou plusieurs cuves (ou « poches ») destinées à effectuer un traitement d'élimination des impuretés dissoutes et/ou en suspension dans le métal liquide, ce traitement pouvant consister à filtrer le métal liquide sur un média filtrant dans une « poche de filtration » ou à introduire dans le bain un gaz dit « de traitement » pouvant être inerte ou réactif dans une « poche de dégazage », un dispositif de solidification du métal liquide (ou « métier de coulée »), par coulée semi-continue verticale par refroidissement direct dans un puits de coulée, pouvant comprendre des dispositifs tels que un moule (ou « lingotière ») un dispositif d'approvisionnement du métal liquide (ou «busette ») et un système de refroidissement, ces différents fours, cuves et dispositifs de solidification étant reliés entre eux par des dispositifs de transfert ou chenaux appelés « goulottes » dans lesquels le métal liquide peut être transporté.Here we call “assembly of the casting installation” all of the devices making it possible to transform a metal in any form into a semi-finished product in raw form by passing through the liquid phase. A casting installation may include numerous devices such as one or more furnaces necessary for melting the metal (“melting furnace”) and/or maintaining it (“maintaining furnace”) in temperature and/or for processing operations. preparation of the liquid metal and adjustment of the composition (“preparation furnace”), one or more tanks (or “pockets”) intended to carry out a treatment to eliminate impurities dissolved and/or suspended in the liquid metal , this treatment may consist of filtering the liquid metal on a filter media in a “filtration bag” or introducing into the bath a so-called “treatment” gas which can be inert or reactive in a “degassing bag”, a degassing device. solidification liquid metal (or “casting craft”), by vertical semi-continuous casting by direct cooling in a casting well, which may include devices such as a mold (or “ingot mold”), a device for supplying liquid metal ( or “busette”) and a cooling system, these different furnaces, tanks and solidification devices being interconnected by transfer devices or channels called “chutes” in which the liquid metal can be transported.
Les présents inventeurs ont constaté que de manière surprenante on peut obtenir des produits corroyés épais en alliage aluminium cuivre lithium présentant une performance en fatigue améliorée en préparant ces tôles à l'aide du procédé suivant.The present inventors have found that, surprisingly, it is possible to obtain thick wrought products made of aluminum copper lithium alloy having improved fatigue performance by preparing these sheets using the following process.
Dans une première étape on élabore un bain de métal liquide en alliage comprenant, en % en poids Cu: 2,0 - 6,0; Li : 0,5 - 2,0 ; Mg : 0- 1,0 ; Ag: 0 - 0,7 ; Zn 0 - 1,0 ; et au moins un élément choisi parmi Zr, Mn, Cr, Sc, Hf et Ti, la quantité dudit élément, s'il est choisi, étant de 0,05 à 0,20 % en poids pour Zr, 0,05 à 0,8 % en poids pour Mn, 0,05 à 0,3 % en poids pour Cr et pour Sc, 0,05 à 0,5 % en poids pour Hf et de 0,01 à 0,15 % en poids pour Ti, Si ≤ 0,1 ; Fe ≤ 0,1; autres ≤ 0,05 chacun et ≤ 0,15 au total, reste aluminium.In a first step, a bath of liquid alloy metal is produced comprising, in % by weight Cu: 2.0 - 6.0; Li: 0.5 - 2.0; Mg: 0-1.0; Ag: 0 - 0.7; Zn 0 - 1.0; and at least one element chosen from Zr, Mn, Cr, Sc, Hf and Ti, the quantity of said element, if chosen, being 0.05 to 0.20% by weight for Zr, 0.05 to 0 .8% by weight for Mn, 0.05 to 0.3% by weight for Cr and for Sc, 0.05 to 0.5% by weight for Hf and 0.01 to 0.15% by weight for Ti , If ≤ 0.1; Fe ≤ 0.1; others ≤ 0.05 each and ≤ 0.15 in total, remains aluminum.
Un alliage avantageux pour le procédé selon l'invention comprend, en % en poids, Cu : 3,0 - 3,9 ; Li : 0,7 - 1,3 ; Mg : 0,1 - 1,0, au moins un élément choisi parmi Zr, Mn et Ti, la quantité dudit élément, s'il est choisi, étant de 0,06 à 0,15 % en poids pour Zr, 0,05 à 0,8 % en poids pour Mn et de 0,01 à 0,15 % en poids pour Ti; Ag: 0 - 0,7 ; Zn ≤ 0,25 ; Si ≤ 0,08 ; Fe ≤ 0,10 ; autres ≤ 0,05 chacun et ≤ 0,15 au total, reste aluminium.An advantageous alloy for the process according to the invention comprises, in % by weight, Cu: 3.0 - 3.9; Li: 0.7 - 1.3; Mg: 0.1 - 1.0, at least one element chosen from Zr, Mn and Ti, the quantity of said element, if chosen, being 0.06 to 0.15% by weight for Zr, 0, 05 to 0.8% by weight for Mn and 0.01 to 0.15% by weight for Ti; Ag: 0 - 0.7; Zn ≤ 0.25; If ≤ 0.08; Fe ≤ 0.10; others ≤ 0.05 each and ≤ 0.15 in total, remains aluminum.
Avantageusement la teneur en cuivre est au moins de 3,2 % en poids. La teneur en lithium est de préférence comprise entre 0,85 et 1,15 % en poids et de préférence entre 0,90 et 1,10 % en poids. La teneur en magnésium est de préférence comprise entre 0,20 et 0,6 % en poids. L'addition simultanée de manganèse et de zirconium est généralement avantageuse. De façon préférée la teneur en manganèse est comprise entre 0,20 et 0,50 % en poids et la teneur en zirconium est comprise entre 0,06 et 0,14 % en poids. Avantageusement la teneur en argent est comprise entre 0,20 et 0,7 % en poids. Il est avantageux que la teneur en argent soit au moins 0,1 % en poids. Dans un mode de réalisation de l'invention la teneur en argent est au moins 0,20 % en poids. Préférentiellement la teneur en argent est au plus 0,5 % en poids. Dans un mode de réalisation de l'invention la teneur en argent est limitée à 0,3 % en poids. Préférentiellement la teneur en silicium est au plus de 0,05 % en poids et la teneur en fer est au plus de 0,06 % en poids. Avantageusement la teneur en titane est comprise entre 0,01 et 0,08 % en poids. Dans un mode de réalisation de l'invention la teneur en zinc est au plus de 0,15 % en poids.Advantageously the copper content is at least 3.2% by weight. The lithium content is preferably between 0.85 and 1.15% by weight and preferably between 0.90 and 1.10% by weight. The magnesium content is preferably between 0.20 and 0.6% by weight. The simultaneous addition of manganese and zirconium is generally advantageous. Preferably the manganese content is between 0.20 and 0.50% by weight and the zirconium content is between 0.06 and 0.14% by weight. Advantageously, the silver content is between 0.20 and 0.7% by weight. It is advantageous if the silver content is at least 0.1% by weight. In one embodiment of the invention the silver content is at least 0.20% by weight. Preferably the silver content is at most 0.5% by weight. In one embodiment of the invention the silver content is limited to 0.3% by weight. Preferably the silicon content is at most 0.05% by weight and the iron content is at most 0.06% by weight. Advantageously, the titanium content is between 0.01 and 0.08% by weight. In one embodiment of the invention the zinc content is at most 0.15% by weight.
Un alliage aluminium-cuivre-lithium préféré est l'alliage AA2050.A preferred aluminum-copper-lithium alloy is alloy AA2050.
Ce bain de métal liquide est préparé dans un four de l'installation de coulée. Il est connu, par exemple de
Ce bain de métal liquide est ensuite traité avec dans une poche de dégazage et dans une poche de filtration de façon notamment à ce que sa teneur en hydrogène soit inférieure à 0,4 ml/100g et de préférence inférieure à 0,35 ml/100g. La teneur en hydrogène du métal liquide est mesurée à l'aide d'un appareillage commercial tel que l'appareil commercialisé sous la marque ALSCAN™, connu de l'homme du métier, la sonde étant maintenue sous un balayage d'azote. Avantageusement la teneur en oxygène de l'atmosphère en contact avec le bain de métal liquide dans le four de fusion lors des étapes de dégazage, filtration est inférieure à 0,5 % en volume et de préférence inférieure à 0,3 % en volume. De préférence, la teneur en oxygène de l'atmosphère en contact avec le bain de métal liquide est inférieure est inférieure à 0,5 % en volume et de préférence inférieure à 0,3 % en volume pour l'ensemble de l'installation de coulée. Cependant on peut tolérer une teneur en oxygène d'au moins 0,05 % en volume et même d'au moins 0,1 % en volume pour l'ensemble de l'installation de coulée ce qui est avantageux notamment pour les aspects économiques du procédé.This liquid metal bath is then treated with a degassing bag and a filtration bag so that its hydrogen content is less than 0.4 ml/100g and preferably less than 0.35 ml/100g. . The hydrogen content of the liquid metal is measured using commercial equipment such as the device marketed under the brand ALSCAN ™ , known to those skilled in the art, the probe being maintained under a nitrogen sweep. Advantageously the oxygen content of the atmosphere in contact with the bath of liquid metal in the melting furnace during the degassing and filtration stages is less than 0.5% by volume and preferably less than 0.3% by volume. Preferably, the oxygen content of the atmosphere in contact with the liquid metal bath is less than 0.5% by volume and preferably less than 0.3% by volume for the entire installation of casting. However, an oxygen content of at least 0.05% by volume and even at least 0.1% by volume can be tolerated for the entire casting installation, which is advantageous in particular for the economic aspects of the process.
Le bain de métal liquide est ensuite solidifié sous forme de plaque. Une plaque est un bloc d'aluminium de forme substantiellement parallélépipédique, de longueur L, de largeur W et d'épaisseur T. On contrôle l'atmosphère au-dessus de la surface liquide lors de la solidification. Un exemple de dispositif permettant de contrôler l'atmosphère au-dessus de la surface liquide lors de la solidification est présenté sur la
Dans cet exemple de dispositif approprié, le métal liquide provenant d'une goulotte (63) est introduit dans une busette (4) contrôlée par une quenouille (8) pouvant se déplacer vers le haut et vers le bas (81), dans une lingotière (31) placée sur un faux fond (21). L'alliage d'aluminium est solidifié par refroidissement direct (5). L'alliage d'aluminium (1) a au moins une surface solide (11, 12, 13) et au moins une surface liquide (14, 15). Un ascenseur (2) permet de maintenir le niveau de la surface liquide (14, 15) sensiblement constant. Un distributeur (7) permet la répartition du métal liquide. Un couvercle (62) recouvre la surface liquide. Le couvercle peut comprendre des joints (61) pour assurer une étanchéité avec la table de coulée (32). Le métal liquide dans la goulotte (63) peut être avantageusement protégé par un couvercle (64). Un gaz inerte (9) est introduit dans la chambre (65) définie entre le couvercle et la table de coulée. Le gaz inerte est avantageusement choisi parmi les gaz rares, l'azote et le dioxyde de carbone ou des mélanges de ces gaz. Un gaz inerte préféré est l'argon. La teneur en oxygène est mesurée dans la chambre (65) au-dessus de la surface liquide. Le débit de gaz inerte peut être ajusté pour atteindre la teneur en oxygène désirée. Cependant il est avantageux de maintenir une aspiration suffisante dans le puits de coulée (10) grâce à une pompe (101). En effet les présents inventeurs ont constaté qu'il n'existe pas en général une étanchéité suffisante entre la lingotière (31) et le métal solidifié (5) ce qui conduit à une diffusion de l'atmosphère du puits de coulée (10) vers la chambre (65). Avantageusement l'aspiration de la pompe (101) est telle que la pression dans l'enceinte (10) soit inférieure à la pression dans la chambre (65), ce qui est peut être obtenu de préférence en imposant une vitesse de l'atmosphère au travers des surfaces ouvertes du puits de coulée d'au moins de 2 m/s et de préférence d'au moins de 2,5 m/s. Typiquement la pression dans la chambre (65) est proche de la pression atmosphérique et la pression dans l'enceinte (10) est inférieure à la pression atmosphérique, typiquement 0,95 fois la pression atmosphérique. Dans le cadre du procédé selon l'invention, on maintient dans la chambre (65), grâce aux dispositifs décrits, une teneur en oxygène inférieure à 0,5 % en volume et de préférence inférieure à 0,3 % en volume.In this example of a suitable device, the liquid metal coming from a chute (63) is introduced into a nozzle (4) controlled by a stopper (8) which can move up and down (81), in an ingot mold (31) placed on a false bottom (21). The aluminum alloy is solidified by direct cooling (5). The aluminum alloy (1) has at least one solid surface (11, 12, 13) and at least one liquid surface (14, 15). An elevator (2) makes it possible to maintain the level of the liquid surface (14, 15) substantially constant. A distributor (7) allows the distribution of the liquid metal. A cover (62) covers the liquid surface. The cover may include seals (61) to ensure sealing with the casting table (32). The liquid metal in the chute (63) can advantageously be protected by a cover (64). An inert gas (9) is introduced into the chamber (65) defined between the cover and the casting table. The inert gas is advantageously chosen from rare gases, nitrogen and carbon dioxide or mixtures of these gases. A preferred inert gas is argon. The oxygen content is measured in the chamber (65) above the liquid surface. The inert gas flow can be adjusted to achieve the desired oxygen content. However, it is advantageous to maintain sufficient suction in the casting well (10) using a pump (101). In fact, the present inventors have noted that there is generally not a sufficient seal between the ingot mold (31) and the solidified metal (5), which leads to diffusion of the atmosphere from the casting well (10) towards the room (65). Advantageously the suction of the pump (101) is such that the pressure in the enclosure (10) is lower than the pressure in the chamber (65), which can be preferably obtained by imposing a speed of the atmosphere through the open surfaces of the casting well at least 2 m/s and preferably at least 2.5 m/s. Typically the pressure in the chamber (65) is close to atmospheric pressure and the pressure in the enclosure (10) is lower than atmospheric pressure, typically 0.95 times atmospheric pressure. As part of the process according to the invention, an oxygen content of less than 0.5% by volume and preferably less than 0.3% by volume is maintained in the chamber (65), thanks to the devices described.
Un exemple de distributeur (7) du procédé selon l'invention est présenté sur les
La surface liquide étant en contact avec ledit premier tissu obturant le métal liquide ne traverse le distributeur que sous la surface liquide dans certaines directions de chaque partie de la paroi. De préférence la hauteur immergée dans le métal liquide de paroi (720, 721, 730, 731) du distributeur (7) couverte par le premier tissu est au moins égale à 20 %, préférentiellement 40 % et de manière préférée 60 % de la hauteur totale de paroi immergée.The liquid surface being in contact with said first fabric closing the liquid metal only passes through the distributor under the liquid surface in certain directions of each part of the wall. Preferably the height immersed in the liquid metal of the wall (720, 721, 730, 731) of the distributor (7) covered by the first fabric is at least equal to 20%, preferably 40% and preferably 60% of the height total submerged wall.
La
La portion de surface couverte par le premier tissu est comprise entre 50 et 80 % pour les parties longitudinales (720) et (721), et entre 40 et 60 % pour les parties latérales (730, 731) et entre 50 et 80 % pour le fond (76).The surface portion covered by the first fabric is between 50 and 80% for the longitudinal parts (720) and (721), and between 40 and 60% for the lateral parts (730, 731) and between 50 and 80% for the bottom (76).
Il est avantageux que la longueur L1 de premier tissu situé dans le fond (76) soit supérieure à la longueur L2 de premier tissu situé dans la partie des parois longitudinales (720) et (721) en contact avec le fond.It is advantageous for the length L1 of first fabric located in the bottom (76) to be greater than the length L2 of first fabric located in the part of the longitudinal walls (720) and (721) in contact with the bottom.
Les présents inventeurs pensent que la géométrie du distributeur permet notamment d'améliorer la qualité du flux du métal liquide, de réduire les turbulences et d'améliorer la distribution de température.The present inventors believe that the geometry of the distributor makes it possible in particular to improve the quality of the flow of the liquid metal, to reduce turbulence and to improve the temperature distribution.
Le premier tissu et le deuxième tissu sont avantageusement obtenus par tissage d'un fil comprenant essentiellement du carbone. Le tissage de fil graphite est particulièrement avantageux. Les tissus sont typiquement cousus l'un à l'autre. Il est possible également en lieu et place d'un premier et deuxième tissus d'utiliser un tissu diffuseur unique présentant au moins deux zones de tissage, plus ou moins denses. Il est avantageux pour la facilité du tissage que le fil comprenant du carbone soit revêtu d'une couche facilitant le glissement. Cette couche peut par exemple comprendre un polymère fluoré tel que le Teflon ou une polyamide telle que le xylon. Le premier tissu est sensiblement obturant. Typiquement il s'agit d'un tissu présentant des mailles de dimension inférieure à 0,5 mm, de préférence inférieure à 0,2 mm. Le second tissu est non obturant et permet le passage du métal en fusion. Typiquement, il s'agit d'un tissu présentant des mailles de dimension comprise entre 1 et 5 mm, de préférence de 2 à 4 mm. Dans un mode de réalisation de l'invention le premier tissu recouvre localement le second tissu, tout en étant en contact intime de façon à ne pas laisser d'interstice entre les deux tissus.The first fabric and the second fabric are advantageously obtained by weaving a thread essentially comprising carbon. Weaving graphite wire is particularly advantageous. The fabrics are typically sewn together. It is also possible, instead of a first and second fabric, to use a single diffuser fabric having at least two weaving zones, more or less dense. It is advantageous for the ease of weaving that the thread comprising carbon is coated with a layer facilitating sliding. This layer may for example comprise a fluoropolymer such as Teflon or a polyamide such as xylon. The first fabric is noticeably obturating. Typically this is a fabric having mesh sizes of less than 0.5 mm, preferably less than 0.2 mm. The second fabric is non-obstructive and allows the passage of molten metal. Typically, it is a fabric having mesh sizes of between 1 and 5 mm, preferably 2 to 4 mm. In one embodiment of the invention the first fabric locally covers the second fabric, while being in intimate contact so as not to leave a gap between the two fabrics.
Avantageusement la plaque ainsi obtenue est ensuite transformée pour obtenir un produit corroyé. La plaque ainsi obtenue est ensuite homogénéisée avant ou après avoir optionnellement été usinée pour obtenir une forme pouvant être déformée à chaud. Dans un mode de réalisation, la plaque est usinée sous forme de plaque de laminage de façon à ensuite être déformée à chaud par laminage. Dans un autre mode de réalisation, la plaque est usinée sous forme de d'ébauche de forge de façon à ensuite être déformée à chaud par forgeage. Dans encore une autre mode de réalisation la plaque est usinée sous forme de billettes de façon à ensuite être déformée à chaud par extrusion. De préférence l'homogénéisation est réalisée à une température comprise entre 470 et 540°C pendant une durée comprise entre 2 et 30 heures.Advantageously, the plate thus obtained is then transformed to obtain a wrought product. The plate thus obtained is then homogenized before or after optionally being machined to obtain a shape that can be deformed under heat. In one embodiment, the plate is machined in the form of a rolling plate so as to then be hot deformed by rolling. In another embodiment, the plate is machined in the form of a forging blank so as to then be hot deformed by forging. In yet another embodiment the plate is machined in the form of billets so as to then be deformed hot by extrusion. Preferably the homogenization is carried out at a temperature between 470 and 540°C for a period of between 2 and 30 hours.
On déforme à chaud et optionnellement à froid ladite forme ainsi homogénéisée pour obtenir un produit corroyé. La température de déformation à chaud est avantageusement au moins 350°C et de préférence au moins 400 °C. Le taux de déformation à chaud et optionnellement à froid, c'est-à-dire le rapport entre d'une part la différence entre l'épaisseur initiale, avant déformation mais après l'éventuel usinage, et l'épaisseur finale et d'autre part l'épaisseur initiale est inférieur à 85% et de préférence inférieur à 80 %. Dans un mode de réalisation lequel le taux de déformation lors de la déformation est inférieur à 75% et de préférence inférieur à 70 %.Said form thus homogenized is deformed hot and optionally cold to obtain a wrought product. The hot deformation temperature is advantageously at least 350°C and preferably at least 400°C. The hot and optionally cold deformation rate, that is to say the ratio between on the one hand the difference between the initial thickness, before deformation but after possible machining, and the final thickness and on the other hand the initial thickness is less than 85% and preferably less than 80%. In an embodiment in which the deformation rate during deformation is less than 75% and preferably less than 70%.
Le produit corroyé ainsi obtenu est ensuite mis en solution et trempé. La température de mise en solution est avantageusement comprise entre 470 et 540°C et de préférence entre 490 et 530 °C et la durée est adaptée à l'épaisseur du produit.The wrought product thus obtained is then put into solution and quenched. The solution temperature is advantageously between 470 and 540°C and preferably between 490 and 530°C and the duration is adapted to the thickness of the product.
Optionnellement on détensionne ledit produit corroyé ainsi mis en solution par déformation plastique avec une déformation d'au moins 1%. Dans le cas des produits laminés il est avantageux de détensionner par traction contrôlée ledit produit corroyé ainsi mis en solution avec un allongement permanent d'au moins 1% et de préférence compris entre 2 et 5%.Optionally, said wrought product thus put into solution is relieved by plastic deformation with a deformation of at least 1%. In the case of rolled products it is advantageous to relieve tension by controlled traction of said wrought product thus put into solution with a permanent elongation of at least 1% and preferably between 2 and 5%.
Enfin on fait subir un revenu au produit ainsi mis en solution et optionnellement détensionné. Le revenu est effectué en un ou plusieurs paliers à une température avantageusement comprise entre 130 et 160 °C pendant une durée de 5 à 60 heures. De préférence on obtient à l'issue du revenu un état métallurgique T8, tel que notamment T851, T83, T84, ou T85.Finally, the product thus placed in solution and optionally released is subjected to an income. The tempering is carried out in one or more stages at a temperature advantageously between 130 and 160°C for a period of 5 to 60 hours. Preferably, at the end of the tempering, a metallurgical state T8 is obtained, such as in particular T851, T83, T84, or T85.
Les produits corroyés obtenus par le procédé selon l'invention présentent des propriétés avantageuses.The wrought products obtained by the process according to the invention have advantageous properties.
La moyenne logarithmique de fatigue des produits corroyés dont l'épaisseur est au moins 80 mm, obtenus par le procédé selon l'invention, mesurée à mi-épaisseur dans la directionThe logarithmic average fatigue of wrought products whose thickness is at least 80 mm, obtained by the process according to the invention, measured at mid-thickness in the direction
TL sur éprouvettes lisses selon la Figure la à une contrainte d'amplitude maximale de 242 MPa, une fréquence de 50 Hz, un rapport de contrainte R = 0,1 est au moins 250 000 cycles, avantageusement la propriété en fatigue est obtenue pour les produits corroyés obtenus par le procédé selon l'invention dont l'épaisseur est au moins 100 mm ou de préférence au moins 120 mm ou même au moins 140 mm.TL on smooth specimens according to Figure la at a maximum amplitude stress of 242 MPa, a frequency of 50 Hz, a stress ratio R = 0.1 is at least 250,000 cycles, advantageously the fatigue property is obtained for the wrought products obtained by the process according to the invention whose thickness is at least 100 mm or preferably at least 120 mm or even at least 140 mm.
Les produits corroyés selon l'invention d'épaisseur au moins 80 mm présentent également des propriétés en fatigue avantageuse pour des éprouvettes à trou, ainsi l'indice de qualité fatigue IQF obtenu sur des éprouvettes à trou Kt = 2,3 selon la
De plus les produits obtenus par le procédé selon l'invention ont des caractéristiques mécaniques statiques avantageuses. Ainsi pour les produits corroyés dont l'épaisseur est au moins 80 mm comprenant en % en poids, Cu : 3,0 - 3,9 ; Li : 0,7 - 1,3 ; Mg : 0,1 - 1,0, au moins un élément choisi parmi Zr, Mn et Ti, la quantité dudit élément, s'il est choisi, étant de 0,06 à 0,15 % en poids pour Zr, 0,05 à 0,8 % en poids pour Mn et de 0,01 à 0,15 % en poids pour Ti,; Ag : 0 - 0,7 ; Zn ≤ 0,25 ; Si ≤ 0,08 ; Fe ≤ 0,10 ; autres ≤ 0,05 chacun et ≤ 0,15 au total, reste aluminium, la limite d'élasticité mesurée à quart épaisseur dans le sens L est au moins 450 MPa et de préférence au moins 470 MPa et/ou la résistance à la rupture mesurée est au moins 480 MPa et de préférence au moins 500 MPa et/ou l'allongement est au moins 5% et de préférence au moins 6%.In addition, the products obtained by the process according to the invention have advantageous static mechanical characteristics. Thus for wrought products whose thickness is at least 80 mm including in % by weight, Cu: 3.0 - 3.9; Li: 0.7 - 1.3; Mg: 0.1 - 1.0, at least one element chosen from Zr, Mn and Ti, the quantity of said element, if chosen, being 0.06 to 0.15% by weight for Zr, 0, 05 to 0.8% by weight for Mn and 0.01 to 0.15% by weight for Ti; Ag: 0 - 0.7; Zn ≤ 0.25; If ≤ 0.08; Fe ≤ 0.10; others ≤ 0.05 each and ≤ 0.15 in total, remains aluminum, the yield strength measured at quarter thickness in direction L is at least 450 MPa and preferably at least 470 MPa and/or the breaking strength measured is at least 480 MPa and preferably at least 500 MPa and/or the elongation is at least 5% and preferably at least 6%.
Les produits corroyés obtenus par le procédé selon l'invention peuvent de manière avantageuse être utilisées pour réaliser des éléments de structure, de préférence des éléments de structure d'avion. Des éléments de structure d'avion préférés sont les longerons, nervures ou un cadres. L'invention est particulièrement avantageuse pour des pièces de forme complexe obtenues par usinage intégral, utilisées en particulier pour la fabrication d'ailes d'avion ainsi que pour n'importe quel autre usage pour lequel les propriétés des produits selon l'invention sont avantageuses.The wrought products obtained by the process according to the invention can advantageously be used to produce structural elements, preferably aircraft structural elements. Preferred aircraft structural elements are spars, ribs or frames. The invention is particularly advantageous for parts of complex shape obtained by integral machining, used in particular for the manufacture of aircraft wings as well as for any other use for which the properties of the products according to the invention are advantageous .
Dans cet exemple, on a préparé des tôles fortes en alliage AA2050. Des plaques en alliage AA2050 ont été coulées par coulée semi-continue verticale à refroidissement direct. L'alliage a été préparé dans un four de fusion. Pour les exemples 1 à 7 on a utilisé un mélange KCl/LiCl en surface du métal liquide dans le four de fusion. Pour les exemples 8 à 9 on n'a pas utilisé de sel dans le four de fusion. Pour les exemples 8 à 9 l'atmosphère en contact avec le métal liquide avec une teneur en oxygène inférieure à 0,3 % en volume pour l'ensemble de l'installation de coulée. L'installation de coulée comprenait un capot disposé au-dessus du puits de coulée permettant de limiter la teneur en oxygène. Pour les essais 8 et 9 on avait en plus utilisé une aspiration (101) telle que la pression dans l'enceinte (10) était inférieure à la pression dans la chambre (65) et telle que la vitesse de l'atmosphère au travers des surfaces ouvertes du puits de coulée était au moins de 2 m/s. La teneur en oxygène a été mesurée à l'aide d'un oxymètre lors de la coulée. Par ailleurs, la teneur en hydrogène dans l'aluminium liquide a été mesurée à l'aide d'une sonde de type Alscan™ ·sous balayage d'azote. Deux types de distributeurs de métal liquide ont été utilisés. Un premier distributeur de type « Combo Bag » tel que décrit par exemple dans les
Les conditions de coulée des différents essais réalisés sont données dans le tableau 1.
The casting conditions of the different tests carried out are given in table 1.
Les plaques ont été homogénéisées 12 heures à 505°C, usinées jusqu'à une épaisseur d'environ 365 mm, laminées à chaud jusqu'à des tôles d'épaisseur finale comprise entre 154 et 158 mm, mises en solution à 504 °C, trempées et détensionnée par traction contrôlée avec un allongement permanent de 3,5%. Les tôles ainsi obtenues ont subi un revenu de 18 heures à 155 °C.The plates were homogenized for 12 hours at 505°C, machined to a thickness of approximately 365 mm, hot rolled to sheets with a final thickness of between 154 and 158 mm, put into solution at 504°C , quenched and relieved by controlled traction with a permanent elongation of 3.5%. The sheets thus obtained were tempered for 18 hours at 155°C.
Les propriétés mécaniques statiques et de ténacité ont été caractérisées à quart-épaisseur. Les caractéristiques mécaniques statiques et la ténacité sont données dans le Tableau 2.
Les propriétés en fatigue ont été caractérisées sur des éprouvettes lisses et sur des éprouvettes à trou pour certains échantillons prélevées à mi-épaisseur.The fatigue properties were characterized on smooth specimens and on hole specimens for certain samples taken at mid-thickness.
Pour les caractérisations de fatigue lisse, quatre éprouvettes, dont le schéma est donné enFor smooth fatigue characterizations, four specimens, the diagram of which is given in
Figure la, ont été testées à mi-épaisseur et mi-largeur dans le sens TL, les conditions de test étant σ = 242 MPa, R = 0,1. Certains tests ont été arrêtés après 200 000 cycles et d'autres tests ont été arrêtés après 300 000 cycles.Figure la, were tested at half-thickness and half-width in the TL direction, the test conditions being σ = 242 MPa, R = 0.1. Some tests were stopped after 200,000 cycles and other tests were stopped after 300,000 cycles.
Pour les caractérisations de fatigue à trou, on a utilisé l'éprouvette reproduite sur la
La combinaison d'une teneur en hydrogène inférieure à 0,4 ml/100g d'une teneur en oxygène mesurée au-dessus de la surface liquide inférieure à 0,3 % en volume et du distributeur B permet d'atteindre un excellent niveau de performance en fatigue. Ces résultats sont présentés sur la
La combinaison d'une teneur en hydrogène inférieure à 0,4 ml/100g d'une teneur en oxygène mesurée au-dessus de la surface liquide inférieure à 0,3 % en volume et du distributeur B permet d'atteindre un excellent niveau de performance en fatigue. Ces résultats sont présentés sur la
Claims (12)
- Dispenser used for semi-continuous casting of aluminium alloy slabs made of fabric comprising essentially carbon, having a lower face (76), an upper face defining the opening through which the molten metal is introduced (71) and a wall of substantially rectangular section, the wall comprising two longitudinal portions parallel with width W (720, 721) and two transverse portions parallel with thickness T (730, 731), said transverse and longitudinal portions being formed from at least two fabrics, a first fabric having mesh sizes of less than 0.5 mm and semi-rigid (77) ensuring that the dispenser keeps its shape during casting, and a second non-sealing fabric (78) allowing the passage and filtration of liquid, said first and second fabrics being bonded to each other without overlap or with overlap and no gap separating them, said first fabric continuously covering at least 30% of the surface of said wall portions (720, 721, 730, 731) and being positioned so that the liquid surface is in contact therewith over the entire section, and characterized in that the surface area covered by the first fabric is between 50 and 80% for the longitudinal portions (720) and (721), and between 40 and 60% for the lateral portions (730, 731) and between 50 and 80% for the base (76).
- Dispenser according to claim 1 characterized in that the first fabric has a height h1 as measured from the upper face on the circumference of the wall (720, 721, 730, 731) such that h1 ≥ 0.3 h and preferably h1 ≥ 0.5 h, where h is the total height of the wall of the dispenser.
- Dispenser according to claim 1 or claim 2 characterized in that the section of the wall changes linearly as a function of height h, typically so that the surface of the lower face (76) of the dispenser is higher or lower by at most 10% than the surface of the upper face (71) of the dispenser .
- Dispenser according to any of claims 1 to 3 characterized in that length L1 of the first fabric located in the base (76) is greater than length L2 of the first fabric in the portion of the longitudinal walls (720) and (721) in contact with the base.
- Dispenser according to any of claims 1 to 4 characterized in that the first fabric has a mesh size of less than 0.2 mm and/or the second fabric is non-sealing and allows molten metal to pass through, typically having a mesh size of between 1 and 5 mm, preferably 2 to 4 mm.
- Method of manufacturing an aluminium alloy wrought product comprising steps in which(a) a bath of molten alloy metal is prepared comprising, as a percentage by weight, Cu: 2.0 - 6.0; Li: 0.5 - 2.0, Mg: 0 - 1.0; Ag: 0 - 0.7; Zn 0 - 1.0; and at least one element selected from Zr, Mn, Cr, Sc, Hf and Ti, the amount of said element, if selected, being 0.05 to 0.20 by weight for Zr, 0.05 to 0.8% by weight for Mn, 0.05 to 0.3 by weight for Cr and for Sc, 0.05 to 0.5 by weight Hf and 0.01 to 0.15% by weight for Ti, Si ≤ 0.1; Fe ≤ 0.1; others ≤ 0.05 each and ≤ 0.15 in total, the rest aluminium,(b) said alloy is cast by semi-continuous vertical casting to obtain a slab of thickness T and width W so that upon solidification,- the hydrogen content of said molten metal bath (1) is less than 0.4 ml/100g,- the oxygen content measured above the liquid surface (14,15) is less than 0.5% by volume,- the dispenser used (7) for casting is a dispenser according to any one of claims 1 to 5.(c) said slab is homogenized before or after optionally machining it to get a shape that can be hot-worked(d) said shape, homogenized in this way, is hot worked and optionally cold worked to obtain a wrought product,(e) said wrought product undergoes solution heat treatment and quenching,(f) optionally said wrought product that has undergone solution heat treatment is stress-relieved by plastic deformation with a deformation of at least 1 %.(g) said solution heat-treated and optionally stress-relieved product is subjected to ageing.
- Method according to claim 6 wherein the oxygen content of the atmosphere in contact with the liquid metal bath in the melting furnace during the degassing step, filtration is less than 0.5% by volume and preferably wherein the oxygen content of the atmosphere in contact with the liquid metal bath is less than 0.5% by volume for the entire casting facility.
- Method according to either of claims 6 or 7 wherein a lid (62) covers the liquid surface during solidification (14,15), said lid preferably comprising seals (61) to ensure pressure tightness with the casting table (32) and wherein an inert gas (9) is introduced into the chamber (65) defined between the lid and the casting table and wherein suction is maintained in the casting pit (10) by means of a pump (101), preferably so that the pressure within the containment (10) is less than the pressure in the chamber (65).
- Method according to any of claims 6 to 8 in which a molten salt containing lithium is not used throughout the entire casting facility.
- Method according to any of claims 6 to 9 in which said hot and/or cold working is performed by extrusion, rolling and/or forging.
- Method according to any of claims 6 to 10 in which the deformation ratio during step (d) is lower than 85% and preferably lower than 80%.
- Method according to any of claims 6 to 7 in which the alloy comprises, as a percentage by weight, Cu: 3.0 - 3.9; Li: 0.7 - 1.3, Mg: 0.1 to 1.0, at least one element selected from Zr, Mn and Ti, the amount of said element, if selected, is from 0.06 to 0.15 by weight for Zr, 0.05 to 0.8 by weight for Mn and 0.01 to 0.15% by weight for Ti; Ag: 0 - 0.7; Zn ≤ 0.25; Si ≤ 0.08; Fe ≤ 0.10; others ≤ 0.05 each and ≤ 0.15 in total.
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DE14828176.9T DE14828176T1 (en) | 2013-12-13 | 2014-12-11 | A process for making aluminum-copper-lithium alloy products having improved fatigue properties and manifolds for this process |
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FR1302932A FR3014905B1 (en) | 2013-12-13 | 2013-12-13 | ALUMINUM-COPPER-LITHIUM ALLOY PRODUCTS WITH IMPROVED FATIGUE PROPERTIES |
PCT/FR2014/000273 WO2015086922A2 (en) | 2013-12-13 | 2014-12-11 | Method for manufacturing products made of aluminium-copper-lithium alloy with improved fatigue properties |
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EP3080318A2 EP3080318A2 (en) | 2016-10-19 |
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US (2) | US10689739B2 (en) |
EP (2) | EP3080317B1 (en) |
JP (2) | JP6683611B2 (en) |
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DE (2) | DE14828176T1 (en) |
FR (1) | FR3014905B1 (en) |
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WO2015086921A2 (en) | 2015-06-18 |
CN106170573A (en) | 2016-11-30 |
EP3080318A2 (en) | 2016-10-19 |
JP2017505378A (en) | 2017-02-16 |
JP2017507240A (en) | 2017-03-16 |
CA2932989C (en) | 2021-10-26 |
US20160237532A1 (en) | 2016-08-18 |
JP6683611B2 (en) | 2020-04-22 |
US20160355916A1 (en) | 2016-12-08 |
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BR112016012288A8 (en) | 2020-05-05 |
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CA2932991C (en) | 2021-10-26 |
WO2015086922A2 (en) | 2015-06-18 |
EP3080317A2 (en) | 2016-10-19 |
US10689739B2 (en) | 2020-06-23 |
JP6604949B2 (en) | 2019-11-13 |
DE14828176T1 (en) | 2017-01-05 |
RU2674789C1 (en) | 2018-12-13 |
FR3014905B1 (en) | 2015-12-11 |
RU2674790C1 (en) | 2018-12-13 |
DE14825363T1 (en) | 2017-01-12 |
CN105814222B (en) | 2019-07-23 |
BR112016012288B1 (en) | 2021-05-04 |
CN105814222A (en) | 2016-07-27 |
CN106170573B (en) | 2018-12-21 |
FR3014905A1 (en) | 2015-06-19 |
WO2015086921A3 (en) | 2015-08-20 |
EP3080317B1 (en) | 2018-09-19 |
WO2015086922A3 (en) | 2015-08-27 |
EP3080318B1 (en) | 2018-10-24 |
CA2932989A1 (en) | 2015-06-18 |
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