EP1190109A1 - Wärmebehandlung für geformte produkte aus aluminium-legierung - Google Patents

Wärmebehandlung für geformte produkte aus aluminium-legierung

Info

Publication number
EP1190109A1
EP1190109A1 EP00929167A EP00929167A EP1190109A1 EP 1190109 A1 EP1190109 A1 EP 1190109A1 EP 00929167 A EP00929167 A EP 00929167A EP 00929167 A EP00929167 A EP 00929167A EP 1190109 A1 EP1190109 A1 EP 1190109A1
Authority
EP
European Patent Office
Prior art keywords
shaped article
process according
article
temperature
range
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.)
Granted
Application number
EP00929167A
Other languages
English (en)
French (fr)
Other versions
EP1190109B1 (de
Inventor
Alok Kumar Gupta
David James Lloyd
Pierre Henri Marois
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.)
Rio Tinto Alcan International Ltd
Original Assignee
Alcan International Ltd Canada
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 Alcan International Ltd Canada filed Critical Alcan International Ltd Canada
Publication of EP1190109A1 publication Critical patent/EP1190109A1/de
Application granted granted Critical
Publication of EP1190109B1 publication Critical patent/EP1190109B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • C22F1/05Changing 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 of the Al-Si-Mg type, i.e. containing silicon and magnesium in approximately equal proportions
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • C22F1/057Changing 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

Definitions

  • This invention relates to a heat treatment process for shaped articles, particularly those suitable for use in the fabrication of automotive body panels More particularly, the invention relates to such articles made from aluminum alloy sheet material that exhibits an improvement of hardness after painting and baking operations have been carried out BACKGROUND ART
  • Aluminum alloy sheet is being used more extensively nowadays as a structural and closure sheet material for vehicle bodies as automobile manufacturers strive for improved fuel economy by reducing vehicle weight Traditionally, aluminum alloy is either direct chill cast to form ingots or continuous cast in the form of a thick strip material, and then hot rolled to a preliminary thickness In a separate operation, the strip is cold rolled to the final thickness and wound into coil The coil must then undergo solution heat treatment to allow strengthening of the formed panel during painting and baking (steps usually carried out on shaped automotive parts by vehicle manufacturers or others - also referred to as the paint bake or paint cure)
  • An object of the invention is to provide a process of producing a shaped article of enhanced hardness response without modification of a conventional procedure for produced aluminum sheet material in T4 or T4P temper
  • a process of producing a painted shaped article comprising obtaining a sheet article made of an aluminum alloy of the 2000 or 6000 series in a T4 or T4P temper, shaping the article to form a shaped article, subjecting the shaped article to a thermal spiking treatment involving heating the shaped article temporarily to a peak temperature in a range of 150 to 300°C, applying paint to the article to form a painted shaped article, and, if necessary to further enhance hardness of the painted shaped article and/or to cure the applied paint, baking the article at a temperature of at least about 177°C
  • thermal spike treatment means a step in which the article is quickly raised in temperature from ambient (or other temperature at which the sheet material may be heated on the part treatment line) to a predetermined maximum temperature and is then quickly cooled or allowed to cool with or without providing a holding period at the peak temperature
  • shaped article includes any article obtained from sheet material for use in fabricating an article or component
  • the term may include a flat article simply cut from the sheet material, but often refers to a non-planar article produced by a bending or stamping step, e g for the production of an automobile fender or door
  • the term does not include unformed or uncut sheet material of indefinite length, e g coiled sheet produced directly from ingots or cast strip
  • the present invention may be carried out with any precipitation hardening aluminum alloy of the AA2000 or AA6000 series, i e alloys containing Al-Mg-Si or Al- Mg-Si-Cu that are capable of exhibiting an age hardening response
  • the invention also relates to a painted and shaped sheet article produced by the above process
  • thermally spiked sheet material parts e g automotive panels
  • the maximum hardness response in the formed part can be obtained through a thermal spiking alone without relying on the paint cure process (or without providing a paint cure at all)
  • thermal spiking process at least in some forms of the invention, can be performed on a continuous basis in ovens typically used for paint cure processes
  • the process therefore may be integrated seamlessly into the conventional shaping and finishing processes of parts formation, thus leading to convenience, efficiency and economy
  • Figure 1 is graph illustrating a typical thermal spike treatment in accordance with the invention
  • Fig 2 is a graph as explained in the Examples below, showing the variation in yield strength (YS) of conventional AA61 1 1-T4 with (a) prestrain, and (b) prestrain plus V 2 hour at 177°C, and
  • Fig 3 is a graph as explained in the Examples below, showing the variation in yield strength (YS) of conventional AA61 1 1 , heat treated according to one form of the present invention, with (a) prestrain, and (b) prestrain plus Vi hour at 177°C BEST MODES FOR CARRYING OUT THE INVENTION
  • an article created from the sheet is subjected to a thermal spike treatment at a temperature in the range of 150-300°C after shaping (e.g. cutting/forming/stamping)
  • the treatment may either involve a thermal spike confined to the lower part of the temperature range (e.g. 150-225°C), which then relies on hardening from a subsequent paint bake step, or may involve a thermal spike into the upper part of the temperature range (e g.
  • thermal spiking to temperatures in the lower part of the range may be carried out at relatively slow heating rates (e g about 1 to 70°C/minute), especially if the article is not held at the peak temperature for any time and is merely allowed to cool (or is forcefully cooled) as soon as the peak temperature is achieved
  • relatively slow heating rate is often found to be necessary to improve the subsequent paint bake response, i e the desired improvement in hardness will often not materialize if the heating rate is any higher
  • the heating to the peak temperature in this form of the invention may take too long for the step to be incorporated into a continuous stamping and painting line A batch treatment is therefore required.
  • the heating rate may be quite rapid (e.g. 10 to 280°C/minute), even if there is essentially no holding time at the peak temperature It is found that the desired increase in hardness will occur whether the heating rate is in the lower part or the higher part of the range indicated above, but for the process to be incorporated into a continuous stamping and painting/rjaking line, the peak metal temperature (PMT) must generally be reached within about one minute If the lowest ambient temperature likely to be encountered is 15°C, the effective range for a continuous operation would likely be 210 to 285°C/minute, which is the preferred heating rate for the high temperature thermal spiking treatment
  • the period of time for which the temperature is maintained at the peak thermal spike temperature may range from zero to any time that is practical in the circumstances From the metallurgical point of view, the longer the time at which the temperature is maintained, the better it is for achieving a desirable hardness response In practice the period is usually from zero up to about 5 minutes
  • Fig 1 is a graphic representation of a preferred thermal spiking step showing the preferred PMT range, the overall heating rate range and the preferred time range at PMT
  • the invention is illustrated by the following Examples, which are not intended to be limiting
  • the invention was tested using a commercially produced AA61 1 1 material DC ingot 600 x 1600 mm double length of the AA61 1 1 alloy containing 0 72% Cu, 0 7% Mg, 0 6% Si, 0 25% Fe, 0 20% Mn and 0 06% Cr was cast on a commercial scale
  • the ingots were scalped 12 5 mm per rolling face, fully homogenized, hot rolled and cold rolled to the final 0 93mm gauge, fully solutionized, rapidly cooled, naturally aged for > 48 hours and sampled for laboratory evaluation
  • Figure 2 shows that the paint bake response of the AA61 1 1 -T4 material increased about 30 MPa due to aging for 30 minutes at 177°C (simulated paint cure)
  • YS net yield strength
  • the yield strength (YS) of the thermally spiked material decreases about 40 MPa for all levels of pre-strain, although the paint bake response is about 90 MPa, which is greater than their conventional counterparts (compare Figures 2 and 3)
  • the 10% pre-strained material shows slightly less paint bake response, which is related to the loss of strength due to recovery
  • the inventive process improves the paint bake response of the material, with and without prior pre-strain, quite considerably This means that the process can be used to heat-treat the formed part according to the invention and enhanced paint cure strength could be achieved EXAMPLE 2

Landscapes

  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)
  • Heat Treatments In General, Especially Conveying And Cooling (AREA)
  • Tunnel Furnaces (AREA)
  • Press Drives And Press Lines (AREA)
  • Forging (AREA)
EP00929167A 1999-05-14 2000-05-11 Wärmebehandlung für geformte produkte aus aluminium-legierung Expired - Lifetime EP1190109B1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13437299P 1999-05-14 1999-05-14
US134372P 1999-05-14
PCT/CA2000/000558 WO2000070115A1 (en) 1999-05-14 2000-05-11 Heat treatment of formed aluminum alloy products

Publications (2)

Publication Number Publication Date
EP1190109A1 true EP1190109A1 (de) 2002-03-27
EP1190109B1 EP1190109B1 (de) 2003-11-19

Family

ID=22463077

Family Applications (1)

Application Number Title Priority Date Filing Date
EP00929167A Expired - Lifetime EP1190109B1 (de) 1999-05-14 2000-05-11 Wärmebehandlung für geformte produkte aus aluminium-legierung

Country Status (9)

Country Link
EP (1) EP1190109B1 (de)
JP (1) JP2002544392A (de)
AT (1) ATE254673T1 (de)
BR (1) BR0010547A (de)
CA (1) CA2372736A1 (de)
DE (1) DE60006670T2 (de)
ES (1) ES2209879T3 (de)
NO (1) NO20015497L (de)
WO (1) WO2000070115A1 (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114717493A (zh) * 2022-04-21 2022-07-08 广东澳美铝业有限公司 一种挤压铝型材预时效方法及预时效铝型材挤压产线
US11874063B2 (en) 2016-10-17 2024-01-16 Novelis Inc. Metal sheet with tailored properties

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AUPR360801A0 (en) * 2001-03-08 2001-04-05 Commonwealth Scientific And Industrial Research Organisation Heat treatment of age-hardenable aluminium alloys utilising secondary precipitation
JP4631193B2 (ja) * 2001-03-29 2011-02-16 Jfeスチール株式会社 塗覆装鋼管の製造方法
WO2007076980A1 (en) * 2006-01-06 2007-07-12 Aleris Aluminum Duffel Bvba Aluminium alloy sheet for automotive applications and structural automobile body member provided with said aluminium alloy sheet
CN103710653A (zh) * 2013-12-17 2014-04-09 芜湖万润机械有限责任公司 一种高强高韧铝合金型材的制备方法
CN107580635B (zh) 2015-05-08 2020-09-04 诺维尔里斯公司 铝合金制品的冲击热处理
WO2017062398A1 (en) * 2015-10-08 2017-04-13 Novelis Inc. A process for warm forming an age hardenable aluminum alloy in t4 temper
KR102071156B1 (ko) * 2015-10-08 2020-01-29 노벨리스 인크. 경화된 알루미늄 합금의 온간 성형 방법
MX2017012112A (es) 2015-12-18 2018-02-15 Novelis Inc Aleaciones de aluminio 6xxx de alta resistencia y metodos para fabricarlas.
CA3006318C (en) 2015-12-18 2021-05-04 Novelis Inc. High strength 6xxx aluminum alloys and methods of making the same
DE102018100842B3 (de) 2018-01-16 2019-05-09 Ebner Industrieofenbau Gmbh Durchlaufofen für Aluminiumbänder

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ATE198915T1 (de) * 1994-09-06 2001-02-15 Alcan Int Ltd Wärmebehandlungsverfahren für blech aus aluminium-legierung

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO0070115A1 *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11874063B2 (en) 2016-10-17 2024-01-16 Novelis Inc. Metal sheet with tailored properties
CN114717493A (zh) * 2022-04-21 2022-07-08 广东澳美铝业有限公司 一种挤压铝型材预时效方法及预时效铝型材挤压产线
CN114717493B (zh) * 2022-04-21 2023-09-12 广东齐力澳美高新材料股份有限公司 一种挤压铝型材预时效方法及预时效铝型材挤压产线

Also Published As

Publication number Publication date
CA2372736A1 (en) 2000-11-23
NO20015497L (no) 2002-01-14
WO2000070115A1 (en) 2000-11-23
EP1190109B1 (de) 2003-11-19
ATE254673T1 (de) 2003-12-15
ES2209879T3 (es) 2004-07-01
JP2002544392A (ja) 2002-12-24
BR0010547A (pt) 2002-02-13
DE60006670T2 (de) 2004-09-30
DE60006670D1 (de) 2003-12-24
NO20015497D0 (no) 2001-11-09

Similar Documents

Publication Publication Date Title
US4946517A (en) Unrecrystallized aluminum plate product by ramp annealing
EP0368005B1 (de) Verfahren zur Herstellung eines nichtkristallisierten, flachgewalzten, dünnen, wärmebehandelten Produktes auf Aluminiumbasis
JP2006118047A (ja) 自動車車体用に適するアルミニウム合金およびアルミニウム合金圧延シートの製造方法
EP1190109B1 (de) Wärmebehandlung für geformte produkte aus aluminium-legierung
JP2000503069A (ja) アルミニウム薄板材料の塗料焼付け反応及び時効安定性を向上させる方法と装置及びその製品
WO2009130175A1 (en) Method of manufacturing a structural aluminium alloy part
JPH07197219A (ja) 成形用アルミニウム合金板材の製造方法
US5194102A (en) Method for increasing the strength of aluminum alloy products through warm working
JPS623225B2 (de)
US6406571B1 (en) Heat treatment of formed aluminum alloy products
US20020174920A1 (en) Heat treatment of formed aluminum alloy products
CN110621797A (zh) 具有优异成型性的Al-Si-Mg合金轧制片材产品的制造方法
WO2020182506A1 (en) Method of manufacturing a 5xxx-series sheet product
JP2004527658A (ja) 曲げ特性を改善したアルミニウム合金シートを製造する方法及びその製造方法により製造されたアルミニウム合金シート
JP2001504551A (ja) 修正溶体化熱処理を施されたaa7000系アルミニウム鍛造製品を製造する方法
EP0990058B1 (de) Verfahren zur herstellung eines bleches aus wärmebehandlungsfähiger aluminium-legierung
EP0931170A1 (de) Aluminiumlegierung zum walzen
CA2336687C (en) Process for producing heat-treatable sheet articles
US4295901A (en) Method of imparting a fine grain structure to aluminum alloys having precipitating constituents
US20020157742A1 (en) Aluminum alloys and methods of making the same
JPH06340940A (ja) プレス成形性、焼付硬化性に優れたアルミニウム合金板及びその製造方法
US4358324A (en) Method of imparting a fine grain structure to aluminum alloys having precipitating constituents
JPH08176764A (ja) 成形加工用アルミニウム合金板の製造方法
JP3278119B2 (ja) 成形性及び焼付硬化性に優れたAl−Mg−Si系合金板の製造方法
JPH0672295B2 (ja) 微細結晶粒を有するアルミニウム合金材料の製造方法

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20011206

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE

AX Request for extension of the european patent

Free format text: AL;LT;LV;MK;RO;SI

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE CH CY DE DK ES FI FR GB GR IE IT LI LU MC NL PT SE

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20031119

Ref country code: FI

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20031119

Ref country code: CY

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20031119

Ref country code: BE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20031119

Ref country code: AT

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20031119

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REG Reference to a national code

Ref country code: CH

Ref legal event code: EP

REF Corresponds to:

Ref document number: 60006670

Country of ref document: DE

Date of ref document: 20031224

Kind code of ref document: P

REG Reference to a national code

Ref country code: IE

Ref legal event code: FG4D

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20040219

Ref country code: GR

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20040219

Ref country code: DK

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20040219

REG Reference to a national code

Ref country code: CH

Ref legal event code: NV

Representative=s name: E. BLUM & CO. PATENTANWAELTE

LTIE Lt: invalidation of european patent or patent extension

Effective date: 20031119

NLV1 Nl: lapsed or annulled due to failure to fulfill the requirements of art. 29p and 29m of the patents act
PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LU

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20040511

Ref country code: IE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20040511

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: MC

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20040531

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2209879

Country of ref document: ES

Kind code of ref document: T3

ET Fr: translation filed
PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20040820

REG Reference to a national code

Ref country code: IE

Ref legal event code: MM4A

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20050504

Year of fee payment: 6

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20050517

Year of fee payment: 6

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: CH

Payment date: 20050520

Year of fee payment: 6

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: ES

Payment date: 20050609

Year of fee payment: 6

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20050630

Year of fee payment: 6

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20060511

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20060512

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: LI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20060531

Ref country code: CH

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20060531

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20060531

Year of fee payment: 7

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20061201

REG Reference to a national code

Ref country code: CH

Ref legal event code: PL

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20060511

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20070131

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20060512

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20040419

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20060531

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20070511