US20070212563A1 - Workpieces Coated with an Aluminum/Magnesium Alloy - Google Patents

Workpieces Coated with an Aluminum/Magnesium Alloy Download PDF

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Publication number
US20070212563A1
US20070212563A1 US10/576,284 US57628404A US2007212563A1 US 20070212563 A1 US20070212563 A1 US 20070212563A1 US 57628404 A US57628404 A US 57628404A US 2007212563 A1 US2007212563 A1 US 2007212563A1
Authority
US
United States
Prior art keywords
layer
coated
aluminum
workpiece according
magnesium
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US10/576,284
Other languages
English (en)
Inventor
Hans de Vries
Matthias Hartel
Jorg Heller
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Aluminal Oberflachentechnik GmbH
Original Assignee
Aluminal Oberflachentechnik GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Aluminal Oberflachentechnik GmbH filed Critical Aluminal Oberflachentechnik GmbH
Assigned to ALUMINAL OBERFLACHENTECHNIK GMBH & CO. KG reassignment ALUMINAL OBERFLACHENTECHNIK GMBH & CO. KG ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: DE VRIES, HANS, HARTEL, MATTHIAS, HELLER, JORG
Publication of US20070212563A1 publication Critical patent/US20070212563A1/en
Abandoned legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C25ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25DPROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D5/00Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
    • C25D5/10Electroplating with more than one layer of the same or of different metals
    • C25D5/12Electroplating with more than one layer of the same or of different metals at least one layer being of nickel or chromium
    • CCHEMISTRY; METALLURGY
    • C25ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25DPROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D3/00Electroplating: Baths therefor
    • C25D3/02Electroplating: Baths therefor from solutions
    • C25D3/56Electroplating: Baths therefor from solutions of alloys
    • CCHEMISTRY; METALLURGY
    • C25ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25DPROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D5/00Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
    • C25D5/34Pretreatment of metallic surfaces to be electroplated
    • C25D5/36Pretreatment of metallic surfaces to be electroplated of iron or steel
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12181Composite powder [e.g., coated, etc.]

Definitions

  • the present invention is directed to workpieces coated with an aluminum/magnesium alloy and to a method for the production thereof.
  • Deposition of aluminum, magnesium or aluminum/magnesium alloys on workpieces consisting of base metals is a convenient way of protecting such materials from corrosion. At the same time, they are provided with a decorative coating.
  • the protective metal layer is predominantly deposited on the workpiece by means of electroplating.
  • the deposited metal layer significantly improves the corrosion resistance of such workpieces.
  • the corrosion resistance of a workpiece depends on the adhesion of the protective layer coated on the workpiece. In the event of insufficient adhesion of the protective layer on the workpiece, the protective layer will easily be removed, e.g. when screwing a screw constituting a workpiece and provided with a surface layer of aluminum, magnesium or aluminum/magnesium alloy into a second workpiece. This results in corrosion, especially contact corrosion, in these areas. Such corrosion will inevitably lead to destruction of the workpiece. Consequently, long-term prevention of corrosion is not ensured.
  • DE 31 12 919 A1 suggests providing metal-coated iron workpieces with an adhesion-promoting intermediate layer made of cobalt, cobalt alloys or cobalt containing nickel and electroplating an aluminum layer thereon.
  • the intermediate layer serving as adhesion promoter is electroplated from an aqueous medium.
  • the electro-aluminum layer optionally can be chromatized. In this way, the corrosion resistance is further improved.
  • DE 38 04 303 suggests a method of improving the adhesion of electrodeposited aluminum layers on metal workpieces by coating an adhesion-promoting layer.
  • a non-aqueous electrolyte is used to coat the adhesion-promoting layer of iron, iron and nickel, nickel, cobalt, copper, and alloys of the above-mentioned metals, or tin-nickel alloys.
  • an electro-aluminum layer is coated on the intermediate layer.
  • Both DE 31 21 919 A1 and DE 38 04 303 A1 use coating of pure electro-aluminum layers on workpieces provided with an intermediate layer. Neither of the above printed documents describes coating of aluminum/magnesium alloys on workpieces.
  • EP 1 141 447 B1 discloses electrolytes for coating workpieces with layers of an aluminum/magnesium alloy.
  • such coating is necessary in those cases where joints with magnesium parts are to be generated, because the corrosion products of magnesium metal are alkaline, attacking the aluminum surface coatings.
  • aluminum/magnesium alloys contact corrosion is avoided and long-term resistance of the coating is provided. What is suggested is aluminum/magnesium alloy coating of steel fastening elements intended to contact magnesium component parts, especially in the automobile industry.
  • EP 1 141 447 B1 fails to disclose any intermediate metallic layers interposed between the workpiece and corrosion-reducing layer of aluminum/magnesium alloy.
  • the prior art aluminum/magnesium layers coated on a workpiece are very hard and brittle.
  • fastening means provided with an aluminum/magnesium layer e.g. screws
  • such risk is present in those cases where the component parts are made of relatively soft or brittle materials such as magnesium, for example.
  • the latter may be exposed to increased corrosion which may lead to the destruction of said component part.
  • the technical object of the present invention is to provide coated workpieces which have improved corrosion resistance, particularly in the alkaline range, and exhibit reduced corrosion in combination with other materials, especially when using the coated workpieces as fastening means to fasten component parts.
  • the technical object of the present invention is accomplished by means of a coated workpiece comprising a substrate, an intermediate metallic layer coated on the substrate, and a layer coated on said intermediate layer, which includes an aluminum/magnesium alloy.
  • the surface of the substrate is electrically conductive. In a preferred fashion, this can be achieved by coating the substrate with graphite.
  • the substrate preferably includes a metal and/or a metal alloy.
  • the substrate can be a metallized substrate, in which case the substrate can be metallized on the entire surface or part of its surface.
  • Preferred substrates include plastic materials.
  • the substrate may include constituents selected from the group of iron, steel, iron alloy, nonferrous metals, pressure-cast zinc, pressure-cast aluminum, titanium, titanium in the form of an alloy, magnesium, pressure-cast magnesium, or mixtures thereof, the above-mentioned metals preferably being present as alloy components in the substrate.
  • the intermediate metallic layer preferably includes iron, iron and nickel, tin and nickel, nickel, cobalt, copper, chromium, molybdenum, vanadium or alloys of the above-mentioned metals.
  • the intermediate metallic layer preferably has a layer thickness of from 0.1 ⁇ m to 30 ⁇ m.
  • the layer thickness of the intermediate metallic layer is from 0.5 ⁇ m to 20 ⁇ m, preferably from 1 ⁇ m to 10 ⁇ m, and more preferably from 1.5 ⁇ m to 8 ⁇ m.
  • the layer coated on the intermediate layer which includes an aluminum/magnesium alloy, preferably includes from 0.5 to 70 wt.-% magnesium.
  • the aluminum/magnesium alloy includes from 1 to 50 wt.-%, preferably from 2 to 40 wt.-% magnesium, and in another preferred embodiment from 3 to 30 wt.-%, preferably from 4 to 25 wt.-%, and more preferably from 5 to 20 wt.-% magnesium.
  • the layer including an aluminum/magnesium alloy preferably has a layer thickness of from 0.1 ⁇ m to 100 ⁇ m.
  • the layer thickness is 0.5 ⁇ m to 70 ⁇ m, preferably 1 ⁇ m to 50 ⁇ m, preferably also 2 ⁇ m to 40 ⁇ m, more preferably 3 ⁇ m to 30 ⁇ m, preferably also 4 ⁇ m to 28 ⁇ m, with 5 ⁇ m to 25 ⁇ m being most preferred.
  • the layer including the aluminum/magnesium alloy preferably is the surface layer of the coated workpiece.
  • at least one additional layer can be coated on said layer including the aluminum/magnesium alloy, which layer preferably is a passivation.
  • the coated workpieces are preferably rack goods, bulk materials, or continuous products, the coated workpiece preferably being a wire, a metal sheet, a screw, a nut, a concrete anchorage, a fastening element, or a machine component part.
  • the coated workpiece is used in the automobile industry in the transmission, engine and bodywork sectors. It can be an oil pan or a transmission oil pan.
  • Another subject matter of the present invention is to provide a method for the production of a coated workpiece, comprising the steps of:
  • the intermediate metallic layer is preferably deposited from an aqueous solution or from a non-aqueous solution.
  • the intermediate metallic layer is deposited by chemical means.
  • the intermediate metallic layer can be electrodeposited from an aqueous electrolyte in step a).
  • Possible electrolytes are solutions of metal salts of iron, cobalt, nickel, copper or tin. They can be present in the form of halides, sulfates, sulfonates or fluoborates. The electrolytes may contain further additives such as complexing substances.
  • the intermediate metallic layer can also be electrodeposited from a non-aqueous electrolyte in step a).
  • Possible electrolytes contain compounds of molybdenum or vanadium or any other of the metals mentioned above which can be included in the intermediate layer.
  • the metals are preferably in the form of halides which can be complexed or reacted with ether, especially diethyl ether, and/or acetylacetonate (acac) to form the corresponding metal acetylacetonates.
  • the layer including an aluminum/magnesium alloy is preferably deposited from an anhydrous electrolyte.
  • the layer including an aluminum/magnesium alloy is preferably electrodeposited from an anhydrous electrolyte in step b). Any electrolyte known to those skilled in the art can be used as electrolyte.
  • the electrolyte includes organoaluminum compounds of general formulas (I) and (II): M[(R 1 ) 3 Al—(H—Al(R 2 ) 2 ) n —R 3] (I) Al(R 4 ) 3 (II) wherein n is equal to 0 or 1, M is sodium or potassium, and R 1 , R 2 , R 3 , R 4 can be the same or different, R 1 , R 2 , R 3 , R 4 being a C 1 -C 4 alkyl group, and a halogen-free, aprotic solvent being used as solvent for the electrolyte.
  • a mixture of K[AlEt 4 ], Na[AlEt 4 ] complexes and AlEt 3 can be employed as electrolyte.
  • the molar ratio of complexes to AlEt 3 is preferably from 1:0.5 to 1:3, more preferably 1:2.
  • Electrolytic deposition on the workpiece of the layer including an aluminum/magnesium alloy is performed using a soluble aluminum anode and a likewise soluble magnesium anode, or using an anode made of an aluminum/magnesium alloy.
  • Electrolytic coating is preferably performed at a temperature of from 80 to 105° C. Preferred is an electroplating bath temperature of from 91 to 100° C.
  • an electrically conductive layer is coated on the substrate prior to coating the intermediate metallic layer in step a).
  • the electroconductive layer can be coated on the substrate using any method known to those skilled in the art.
  • the electrically conductive layer is coated on the substrate by means of metallization.
  • the coated workpiece of the present invention there is no impairment of the coated workpiece when using the coated workpiece of the present invention as fastening means.
  • the surface layer of an aluminum/magnesium alloy is very hard, brittle and sparingly ductile, the coating still adheres very tightly to the coated workpiece during and after use as fastening means.
  • the coating being used consisting of the intermediate layer and the surface layer, is flexible to such an extent that it is not adversely changed following use as fastening means.
  • the coated workpiece e.g. in the form of a screw
  • the surface treatment of the workpiece unexpectedly backs away, resulting in a further reduction of strain on the coated workpiece. Because no damage is done to the intermediate metallic layer and the surface layer including an aluminum/magnesium alloy, the coated workpiece is reliably protected from corrosion, especially contact corrosion, even after and during use thereof.
  • Prior art workpieces provided with an aluminum/magnesium coating fail to offer the advantages mentioned above.
  • the surface layer which consists of an aluminum/magnesium layer, either is destroyed, so that the workpiece will undergo corrosion, or the very hard and brittle layer of aluminum/magnesium alloy of prior art workpieces destroys the surface of the component parts to be fastened, so that the latter are subsequently exposed to increased corrosion.
  • a sheet of St37 steel 100 ⁇ 25 ⁇ 1 mm in size is provided with a nickel intermediate layer having a thickness of about 1 ⁇ m.
  • the nickel layer is electrodeposited from an aqueous nickel sulfamate electrolyte.
  • a layer of an aluminum/magnesium alloy with a magnesium content of 20 wt.-% and a layer thickness of 12 ⁇ m is deposited on the nickel layer from a non-aqueous electrolyte by means of electroplating.
  • the coated metal sheet is bent lengthways by an angle of 180°, and the coated metal layers remain intact in the area of the bending edge.
  • a sheet of St37 steel 100 ⁇ 25 ⁇ 1 mm in size is provided with a layer of an aluminum/magnesium alloy with a magnesium content of 20 wt.-% and a layer thickness of 12 ⁇ m by means of electrodeposition from a non-aqueous electrolyte.
  • the metal sheet thus coated is bent lengthways by an angle of 180°, during which process the coating is partially disrupted along the bending edge, partially undergoing flaking in the form of ultrafine needles.
  • Five M6 ⁇ 55 size screws are provided with an aluminum/magnesium alloy with a magnesium content of 15 wt.-% and a layer thickness of 16 ⁇ m by means of electro-deposition from a non-aqueous electrolyte.
  • Nickel layer having a layer thickness of about 1 ⁇ m.
  • the nickel layer is electrodeposited from an aqueous nickel sulfamate electrolyte. Thereafter, a layer of an aluminum/magnesium alloy with a magnesium content of 15 wt.-% and a layer thickness of 16 ⁇ m is deposited on the nickel layer from a non-aqueous electrolyte by means of electroplating.
  • M5 ⁇ 5 size screws are electroplated with an aluminum/magnesium alloy with a magnesium content of 10 wt.-% and an average layer thickness of 14 ⁇ m from a non-aqueous electrolyte in a drum.
  • Additional screws are provided with a nickel intermediate layer having a layer thickness of about 1-2 ⁇ m of nickel.
  • the nickel layer is electrodeposited from an aqueous nickel sulfamate electrolyte. Thereafter, a layer of an aluminum/magnesium alloy with a magnesium content of 10 wt.-% and an average layer thickness of 15 ⁇ m is electrodeposited on the nickel layer from a non-aqueous electrolyte in a drum.
  • the examples specified above indicate that the intermediate metallic layer causes a significant improvement of the corrosion resistance.
  • Coated workpieces comprising a substrate, an intermediate metallic layer coated on the substrate, and a layer coated on said intermediate layer, which includes an aluminum/magnesium alloy, show a superior pattern of properties which is not seen in prior art workpieces.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Electrochemistry (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Electroplating Methods And Accessories (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Laminated Bodies (AREA)
  • Electroplating And Plating Baths Therefor (AREA)
US10/576,284 2003-10-18 2004-09-09 Workpieces Coated with an Aluminum/Magnesium Alloy Abandoned US20070212563A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP03023454A EP1524336A1 (de) 2003-10-18 2003-10-18 Mit einer Aluminium-/Magnesium-Legierung beschichtete Werkstücke
EP03023454.6 2003-10-18
PCT/EP2004/052097 WO2005035835A2 (de) 2003-10-18 2004-09-09 Mit einer aluminium/magnesium-legierung beschichtete werkstücke

Publications (1)

Publication Number Publication Date
US20070212563A1 true US20070212563A1 (en) 2007-09-13

Family

ID=34354482

Family Applications (1)

Application Number Title Priority Date Filing Date
US10/576,284 Abandoned US20070212563A1 (en) 2003-10-18 2004-09-09 Workpieces Coated with an Aluminum/Magnesium Alloy

Country Status (7)

Country Link
US (1) US20070212563A1 (ja)
EP (2) EP1524336A1 (ja)
JP (1) JP2007509233A (ja)
KR (1) KR20060097016A (ja)
CN (1) CN1871375A (ja)
RU (1) RU2353714C2 (ja)
WO (1) WO2005035835A2 (ja)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100068554A1 (en) * 2007-03-29 2010-03-18 Lutz Mueller System having at least one metal part which is in contact with at least one plastic component
US20120055691A1 (en) * 2010-09-03 2012-03-08 Hon Hai Precision Industry Co., Ltd. Housing and method for manufacturing housing

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008051883A1 (de) 2008-10-16 2010-04-22 Nano-X Gmbh Beschichtung zum kathodischen Korrosionsschutz von Metall, Verfahren zum Herstellen der Beschichtung und Verwendung der Beschichtung.
RU2519694C1 (ru) * 2013-05-23 2014-06-20 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Московский государственный технологический университет "СТАНКИН" (ФГБОУ ВПО МГТУ "СТАНКИН") Способ нанесения антикоррозийных покрытий на подложку из высокотвердых сплавов
KR102471961B1 (ko) * 2017-07-12 2022-11-28 르노코리아자동차 주식회사 자동차용 이중 금속판재구조 및 이의 제조방법
DE102017126590A1 (de) * 2017-11-13 2019-05-16 Doduco Solutions Gmbh Verfahren zum Herstellen einer Bodenplatte für ein Elektronikmodul
RU2713771C1 (ru) * 2019-10-23 2020-02-07 Федеральное государственное бюджетное образовательное учреждение высшего образования "Елецкий государственный университет им. И.А. Бунина" Электролит для осаждения сплава Cr-V

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4778575A (en) * 1988-01-21 1988-10-18 The United States Of America As Represented By The United States Department Of Energy Electrodeposition of magnesium and magnesium/aluminum alloys
US5225291A (en) * 1990-11-07 1993-07-06 Alupower, Inc. Deferred actuated battery assembly
US6203936B1 (en) * 1999-03-03 2001-03-20 Lynntech Inc. Lightweight metal bipolar plates and methods for making the same
US20060137990A1 (en) * 2002-09-25 2006-06-29 Aluminal Oberflachentechnik Gmbh & Co., Kg Method for electrolytic coating of materials with aluminum, magnesium or aluminum and magnesium alloys
US20070108061A1 (en) * 2003-09-27 2007-05-17 Richard Lisowsky Electrolyte for the galvanic deposition of aluminum-magnesium alloys
US20070261965A1 (en) * 2003-11-07 2007-11-15 Jorg Heller Coating of Substrates

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3112919A1 (de) * 1981-03-31 1982-10-07 Siemens AG, 1000 Berlin und 8000 München "metallbeschichtete eisenwerkstoffe"
DE3804303A1 (de) * 1988-02-12 1989-08-24 Studiengesellschaft Kohle Mbh Verfahren zur haftvermittlung zwischen metallwerkstoffen und glavanischen aluminiumschichten und hierbei eingesetzte nichtwaessrige elektrolyte
DE19855666A1 (de) * 1998-12-01 2000-06-08 Studiengesellschaft Kohle Mbh Aluminiumorganische Elektrolyte und Verfahren zur elektrolytischen Beschichtung mit Aluminium oder Aluminium-Magnesium Legierungen
WO2002088434A1 (en) * 2001-04-30 2002-11-07 Alumiplate Incorporated Aluminium electroplating formulations
EP1279751A1 (de) * 2001-07-28 2003-01-29 Aluminal Oberflächtentechnik GmbH & Co. KG Vorrichtung zum galvanischen Abscheiden von Aluminium oder Aluminiumlegierungen aus metallorganischen Aluminiumalkylhaltigen Elektrolyten

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4778575A (en) * 1988-01-21 1988-10-18 The United States Of America As Represented By The United States Department Of Energy Electrodeposition of magnesium and magnesium/aluminum alloys
US5225291A (en) * 1990-11-07 1993-07-06 Alupower, Inc. Deferred actuated battery assembly
US6203936B1 (en) * 1999-03-03 2001-03-20 Lynntech Inc. Lightweight metal bipolar plates and methods for making the same
US20060137990A1 (en) * 2002-09-25 2006-06-29 Aluminal Oberflachentechnik Gmbh & Co., Kg Method for electrolytic coating of materials with aluminum, magnesium or aluminum and magnesium alloys
US7468123B2 (en) * 2002-09-25 2008-12-23 Aluminal Oberflachentechnik Gmbh & Co. Kg Method for electrolytic coating of materials with aluminum, magnesium or aluminum and magnesium alloys
US20070108061A1 (en) * 2003-09-27 2007-05-17 Richard Lisowsky Electrolyte for the galvanic deposition of aluminum-magnesium alloys
US20070261965A1 (en) * 2003-11-07 2007-11-15 Jorg Heller Coating of Substrates

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100068554A1 (en) * 2007-03-29 2010-03-18 Lutz Mueller System having at least one metal part which is in contact with at least one plastic component
US20120055691A1 (en) * 2010-09-03 2012-03-08 Hon Hai Precision Industry Co., Ltd. Housing and method for manufacturing housing

Also Published As

Publication number Publication date
EP1524336A1 (de) 2005-04-20
JP2007509233A (ja) 2007-04-12
RU2353714C2 (ru) 2009-04-27
CN1871375A (zh) 2006-11-29
RU2006117025A (ru) 2007-11-27
WO2005035835A2 (de) 2005-04-21
EP1675974A2 (de) 2006-07-05
WO2005035835A3 (de) 2005-06-23
KR20060097016A (ko) 2006-09-13

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Owner name: ALUMINAL OBERFLACHENTECHNIK GMBH & CO. KG, GERMANY

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:DE VRIES, HANS;HARTEL, MATTHIAS;HELLER, JORG;REEL/FRAME:019199/0394;SIGNING DATES FROM 20070315 TO 20070320

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