EP0208631B1 - Alliages d'Al à hautes teneurs de Li et Si et un procédé de fabrication - Google Patents
Alliages d'Al à hautes teneurs de Li et Si et un procédé de fabrication Download PDFInfo
- Publication number
- EP0208631B1 EP0208631B1 EP86420166A EP86420166A EP0208631B1 EP 0208631 B1 EP0208631 B1 EP 0208631B1 EP 86420166 A EP86420166 A EP 86420166A EP 86420166 A EP86420166 A EP 86420166A EP 0208631 B1 EP0208631 B1 EP 0208631B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- phase
- alloy
- alloys
- hot
- solidification
- 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.)
- Expired
Links
Classifications
-
- 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
- C22C21/02—Alloys based on aluminium with silicon as the next major constituent
- C22C21/04—Modified aluminium-silicon alloys
-
- 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
- C22C1/04—Making non-ferrous alloys by powder metallurgy
- C22C1/0408—Light metal alloys
- C22C1/0416—Aluminium-based alloys
-
- 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
-
- Y—GENERAL 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/4998—Combined manufacture including applying or shaping of fluent material
- Y10T29/49988—Metal casting
Definitions
- the field of the invention relates to Al-based alloys relating to high contents of Li and Si and having a high to medium mechanical strength, a very low density and a high Young modulus; a process for obtaining it uses rapid solidification (atomization, hyper quenching on a metal substrate, etc.) densification and hot shaping.
- metallurgists have proposed additions of a few% of hardening elements such as Cu, Mg, Zn and other minor elements controlling the recrystallization or the grain size of the alloy, such as Mn, Cr, Ti, etc ...
- These alloys also contain very low Fe and Si contents (less than 0.1% by weight).
- Swiss patent CH-216 204 discloses AI-Li-Si alloys containing from 1 to 10% (by weight) of Li and Si (in undetermined amount); the example given relates to an alloy containing: 3.5% Li; 5% If; 1 ° / o Cu; 1% Ni; remains AI. However, this alloy, most probably obtained by conventional casting, probably has a low heat stability, unlike the alloys according to the invention.
- the Applicant has found that it is possible to obtain gains in specific modulus much greater than 25 ° / o on AI-Li-Si alloys containing large amounts of Si and Li, while retaining acceptable mechanical characteristics, satisfactory spontaneous corrosion resistance, and good formability.
- This objective is achieved by the choice of a specific composition, the use of rapid solidification and techniques of powder metallurgy, and finally a shaping at controlled temperature.
- the Li content is preferably kept between 4 and 7%.
- the total content of secondary elements is preferably kept below 2% .
- the properties of the products obtained are only satisfactory if the alloys are produced by rapid solidification at cooling rates from the liquid state above 1000 ° C / sec. by any known means (solidification on a wheel, atomization, etc.).
- This operation preferably takes place under an inert atmosphere, for example argon or helium.
- the alloys thus obtained are then consolidated by known techniques of powder metallurgy, for example according to the range: possible grinding, cold compaction, degassing under possible vacuum, hot compression and drawing by spinning, forging, stamping or any other technique. , with a rate of wrought (section initial cross-section / final cross-section) generally greater than 8.
- the product temperature must remain below 400 ° C, and preferably 350 ° C, to obtain acceptable mechanical characteristics.
- the products are generally used, as indicated, in the raw state of hot transformation, or after a slight additional deformation at a lower temperature, which makes it possible to improve both the flatness, the straightness or the dimensional tolerances and the mechanical resistance characteristics.
- the products thus obtained have a large volume fraction, between 15 and 60%, preferably between 20 and 50%, of particles essentially consisting of a phase of cubic structure, with a parameter close to 0 , 59 at 0.60 nm, identified as phase T - AI2 Li 3 Si 2 or AI Li Si, according to the authors.
- This phase distributed homogeneously, has a size of between 0.01 to 10 ⁇ m, more generally between 0.01 and 5 ⁇ m: it is believed that this phase contributes to cold hardening and to the average temperatures of the alloy, its fine and homogeneous precipitation being accentuated by an income between room temperature and 350 ° C, preferably between 150 and 250 ° C.
- the microstructure may optionally include a very fine globular precipitation of phase 8 '(AI 3 Li) whose diameter is less than 50 nm and also a slight precipitation of free Si or phase 8 AI Li.
- phase 8 represents less than 10% (by volume).
- the products thus obtained are characterized by an extremely fine grain whose size is less than 20 ⁇ m, and generally less than 10 ⁇ m.
- phase 8 AI Li which is spontaneously corrodible and also of phase phase 'AI 3 Li weakening is favored.
- the Applicant has on the other hand, found that for an equal composition, the hardness of the products is all the higher the smaller the size of the T phase particles (AI, Li, Si); in particular the very rapid solidification of the thin ribbons (20 to 30 ⁇ m thick) on a metallic substrate ("melt spinning") leads, on the substrate side, to T-phase particle sizes of 0.01 to 0.5 ⁇ m.
- microhardness is then approximately 40% greater than that obtained on the external face of the thicker ribbons or on powders obtained by atomization, for which the size of particles of phase T is of the order of 0.5 to 5 ⁇ m.
- Alloys the composition of which is given in Table 1, were obtained in the form of powder, by centrifugal spraying with helium, the latter being sieved to 200 ⁇ m maximum.
- These powders were made from cast ingots, made with a pure base having an Fe content ⁇ 0.05%.
- the bars obtained were air-cooled, and characterized by density measurement, Young's modulus, tensile tests (long sense) and micrographic examinations.
- Table I brings together the targeted chemical compositions determined by atomic absorption and the results obtained (average of 5 tests).
- the oxygen content is around 0.5%.
- phase T present was coarse (average size 2 ⁇ m, maximum size 5 ⁇ m), but homogeneously dispersed except for a few large particles of phase T (100 to 200 ⁇ m) whose presence explains the low elongations observed (primers premature rupture).
- Alloys AI, Li, Si including the compositions given in Example 1 were cast in strips of 10 mm x 40 ⁇ m approximately, of cross section, on a copper wheel 0 480 mm rotating at 1000 rpm, since 730 to 830 ° C; they were characterized by Vickers microhardness under 10 g micrographic examination by optical microscopy, electron and X-ray diffraction in the raw casting state, and after heat treatment of tempering from 1 to 10 h between 200 and 350 ° C, to evaluate hot stability and structural evolution.
- the external part of the ribbons B, C, D and the entire thickness of the ribbons (E, F) had a coarse structure of the order of 1 ⁇ m on average (maximum size of 4 ⁇ m) in the raw state of casting and after income.
- the volume fraction of the precipitates did not vary significantly during the incomes.
- the hardness increases with the contents of Li and Si, and the volume fraction of phase T, at least as long as the latter remains in the form of fine particles.
- the fine structures give the alloys according to the invention a very high level of hardness after tempering at 200 ° C, and this remains high even after tempering at 350 ° C, unlike the alloys outside the invention.
- phase T very coarse particles of phase T (AI, Li, Si, of very heterogeneous sizes, rather coarse, of several ⁇ m to several hundreds of ⁇ m, and clearly higher than 10 ⁇ m on average, associated with a small amount of phase 8 AI Li.
- This example shows the need to use a method involving rapid solidification for the alloys according to the invention.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacture Of Metal Powder And Suspensions Thereof (AREA)
- Silicon Compounds (AREA)
- Conductive Materials (AREA)
- Powder Metallurgy (AREA)
- Ceramic Products (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
- Crystals, And After-Treatments Of Crystals (AREA)
- Superconductors And Manufacturing Methods Therefor (AREA)
- Materials For Medical Uses (AREA)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AT86420166T ATE45189T1 (de) | 1985-06-28 | 1986-06-25 | Aluminiumlegierungen mit hohem lithium- und siliziumgehalt und verfahren zu ihrer herstellung. |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR8510375A FR2584095A1 (fr) | 1985-06-28 | 1985-06-28 | Alliages d'al a hautes teneurs en li et si et un procede de fabrication |
| FR8510375 | 1985-06-28 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP0208631A1 EP0208631A1 (fr) | 1987-01-14 |
| EP0208631B1 true EP0208631B1 (fr) | 1989-08-02 |
Family
ID=9321039
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP86420166A Expired EP0208631B1 (fr) | 1985-06-28 | 1986-06-25 | Alliages d'Al à hautes teneurs de Li et Si et un procédé de fabrication |
Country Status (10)
Families Citing this family (34)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4758273A (en) * | 1984-10-23 | 1988-07-19 | Inco Alloys International, Inc. | Dispersion strengthened aluminum alloys |
| GB2196647A (en) * | 1986-10-21 | 1988-05-05 | Secr Defence | Rapid solidification route aluminium alloys |
| FR2626009B2 (fr) * | 1987-02-18 | 1992-05-29 | Cegedur | Produit en alliage d'al contenant du li resistant a la corrosion sous tension |
| FR2637914B1 (fr) * | 1988-10-17 | 1992-12-18 | Pechiney Rhenalu | Procede permettant de diminuer le taux de recristallisation de l'aluminium et de ses alliages |
| US5091019A (en) * | 1990-02-12 | 1992-02-25 | Allied-Signal, Inc. | Rapidly solidified aluminum lithium alloys having zirconium |
| US5045125A (en) * | 1990-04-02 | 1991-09-03 | Allied-Signal Inc. | Case toughening of aluminum-lithium forgings |
| JP2965774B2 (ja) * | 1992-02-13 | 1999-10-18 | ワイケイケイ株式会社 | 高強度耐摩耗性アルミニウム合金 |
| JP2954775B2 (ja) * | 1992-02-14 | 1999-09-27 | ワイケイケイ株式会社 | 微細結晶組織からなる高強度急冷凝固合金 |
| JP2911673B2 (ja) * | 1992-03-18 | 1999-06-23 | 健 増本 | 高強度アルミニウム合金 |
| JP2002144018A (ja) * | 2000-11-02 | 2002-05-21 | Yorozu Corp | 軽量高強度部材の製造方法 |
| JP2004204836A (ja) * | 2002-12-13 | 2004-07-22 | Sanyo Electric Co Ltd | 電弧溶接により組み立てられるアルミニウム部材及び圧縮機 |
| US8002912B2 (en) | 2008-04-18 | 2011-08-23 | United Technologies Corporation | High strength L12 aluminum alloys |
| US8017072B2 (en) | 2008-04-18 | 2011-09-13 | United Technologies Corporation | Dispersion strengthened L12 aluminum alloys |
| US7875131B2 (en) | 2008-04-18 | 2011-01-25 | United Technologies Corporation | L12 strengthened amorphous aluminum alloys |
| US7879162B2 (en) | 2008-04-18 | 2011-02-01 | United Technologies Corporation | High strength aluminum alloys with L12 precipitates |
| US20090260724A1 (en) * | 2008-04-18 | 2009-10-22 | United Technologies Corporation | Heat treatable L12 aluminum alloys |
| US7875133B2 (en) | 2008-04-18 | 2011-01-25 | United Technologies Corporation | Heat treatable L12 aluminum alloys |
| US7811395B2 (en) | 2008-04-18 | 2010-10-12 | United Technologies Corporation | High strength L12 aluminum alloys |
| US7871477B2 (en) | 2008-04-18 | 2011-01-18 | United Technologies Corporation | High strength L12 aluminum alloys |
| US8409373B2 (en) | 2008-04-18 | 2013-04-02 | United Technologies Corporation | L12 aluminum alloys with bimodal and trimodal distribution |
| US8778099B2 (en) | 2008-12-09 | 2014-07-15 | United Technologies Corporation | Conversion process for heat treatable L12 aluminum alloys |
| US9611522B2 (en) | 2009-05-06 | 2017-04-04 | United Technologies Corporation | Spray deposition of L12 aluminum alloys |
| US9127334B2 (en) | 2009-05-07 | 2015-09-08 | United Technologies Corporation | Direct forging and rolling of L12 aluminum alloys for armor applications |
| US8728389B2 (en) | 2009-09-01 | 2014-05-20 | United Technologies Corporation | Fabrication of L12 aluminum alloy tanks and other vessels by roll forming, spin forming, and friction stir welding |
| US8409496B2 (en) | 2009-09-14 | 2013-04-02 | United Technologies Corporation | Superplastic forming high strength L12 aluminum alloys |
| US9194027B2 (en) | 2009-10-14 | 2015-11-24 | United Technologies Corporation | Method of forming high strength aluminum alloy parts containing L12 intermetallic dispersoids by ring rolling |
| US8409497B2 (en) | 2009-10-16 | 2013-04-02 | United Technologies Corporation | Hot and cold rolling high strength L12 aluminum alloys |
| CN109423564A (zh) * | 2017-08-28 | 2019-03-05 | 昭和电工株式会社 | 磁记录介质用铝合金基板、磁记录介质用基板、磁记录介质和硬盘驱动器 |
| CN107675038B (zh) * | 2017-09-26 | 2019-04-23 | 沈阳航空航天大学 | 一种轻质铸造Al-Si-Li-Cu合金材料及其制备方法 |
| CN107699747B (zh) * | 2017-09-26 | 2019-05-21 | 沈阳航空航天大学 | 一种高Cu含量Al-Si-Li-Cu铸造合金及其制备方法 |
| CN107587012B (zh) * | 2017-09-26 | 2019-04-23 | 沈阳航空航天大学 | 一种轻质铸造Al-Si-Li合金材料及其制备方法 |
| WO2019161137A1 (en) * | 2018-02-14 | 2019-08-22 | Arconic Inc. | Aluminum alloy products and methods for producing the same |
| CN114058912B (zh) * | 2022-01-17 | 2022-04-08 | 北京理工大学 | 一种高比强度、比刚度铝锂合金厚壁环形件及其制备方法 |
| US11739395B1 (en) * | 2022-05-05 | 2023-08-29 | The United States Of America As Represented By The Secretary Of The Navy | Embrittled aluminum alloys for powder manufacturing |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CH216204A (de) * | 1937-10-29 | 1941-08-15 | Kommanditgesellschaft Mahle | Aluminium-Legierung, insbesondere für Kolben von Brennkraftmaschinen. |
| FR1148719A (fr) * | 1955-04-05 | 1957-12-13 | Stone & Company Charlton Ltd J | Perfectionnements aux alliages à base d'aluminium |
| FR2555610B1 (fr) * | 1983-11-29 | 1987-10-16 | Cegedur | Alliages a base d'aluminium presentant une grande stabilite a chaud |
| US4661172A (en) * | 1984-02-29 | 1987-04-28 | Allied Corporation | Low density aluminum alloys and method |
-
1985
- 1985-06-28 FR FR8510375A patent/FR2584095A1/fr not_active Withdrawn
-
1986
- 1986-06-23 IL IL79198A patent/IL79198A0/xx unknown
- 1986-06-23 CA CA000512207A patent/CA1274107A/fr not_active Expired - Fee Related
- 1986-06-24 JP JP61148019A patent/JPS627828A/ja active Granted
- 1986-06-25 EP EP86420166A patent/EP0208631B1/fr not_active Expired
- 1986-06-25 DE DE8686420166T patent/DE3664789D1/de not_active Expired
- 1986-06-25 AT AT86420166T patent/ATE45189T1/de active
- 1986-06-27 US US06/879,347 patent/US4804423A/en not_active Expired - Fee Related
- 1986-06-27 BR BR8602980A patent/BR8602980A/pt unknown
- 1986-06-27 ES ES8600019A patent/ES2000175A6/es not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| FR2584095A1 (fr) | 1987-01-02 |
| EP0208631A1 (fr) | 1987-01-14 |
| JPS627828A (ja) | 1987-01-14 |
| IL79198A0 (en) | 1986-09-30 |
| ES2000175A6 (es) | 1988-01-01 |
| US4804423A (en) | 1989-02-14 |
| DE3664789D1 (en) | 1989-09-07 |
| JPH0328500B2 (enrdf_load_stackoverflow) | 1991-04-19 |
| ATE45189T1 (de) | 1989-08-15 |
| BR8602980A (pt) | 1987-02-17 |
| CA1274107A (fr) | 1990-09-18 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP0208631B1 (fr) | Alliages d'Al à hautes teneurs de Li et Si et un procédé de fabrication | |
| US5316598A (en) | Superplastically formed product from rolled magnesium base metal alloy sheet | |
| EP0419375B1 (fr) | Alliages de magnésium à haute résistance mécanique et procédé d'obtention par solidification rapide | |
| EP0088578B1 (en) | Production of mechanically alloyed powder | |
| JP2001049371A (ja) | 振動吸収性能に優れたAl−Zn合金およびその製造方法 | |
| JPS6283446A (ja) | 急速固化した高力、耐食性マグネシウムベ−スメタル合金、その製法およびこれから圧縮された金属物品 | |
| JPH0754114A (ja) | 改良された低コストTi−6Al−4Vバリスティック合金 | |
| FR2841263A1 (fr) | PROCEDE DE PRODUCTION D'UN PRODUIT EN ALLAIGE Al-Mg-Si EQUILIBRE A HAUTE RESISTANCE, ET PRODUIT SOUDABLE ET MATERIAU DE REVETEMENT POUR AVION, OBTENUS PAR UN TEL PROCEDE | |
| US5433799A (en) | Method of making Cr-bearing gamma titanium aluminides | |
| EP0391815B1 (fr) | Alliage à base d'A1 à haut module et à resistance mécanique élevée et procédé d'obtention | |
| FR2650297A1 (fr) | Alliages gamma de titane et d'aluminium modifies au carbone, au chrome et au niobium | |
| US12319984B2 (en) | Metal matrix composites and methods of making and use thereof | |
| JP3173452B2 (ja) | 耐摩耗性被覆部材及びその製造方法 | |
| EP0558977B1 (en) | High-strength, rapidly solidified alloy | |
| FR2632323A1 (fr) | Alliage usinable d'acier inoxydable contenant du bore, article produit a partir de cet alliage et procede pour sa production | |
| JPH07238336A (ja) | 高強度アルミニウム基合金 | |
| Harada et al. | Mechanical properties of cold-rolled and annealed Al–12% Mg alloy sheet with high Mg solid solubility fabricated from vertical-type high-speed twin-roll cast strip | |
| JP2001049375A (ja) | 優れた振動吸収性能を有するAl合金およびその製造方法 | |
| Beddoes et al. | The technology of titanium aluminides for aerospace applications | |
| US5071474A (en) | Method for forging rapidly solidified magnesium base metal alloy billet | |
| JPH06501056A (ja) | 急速凝固マグネシウムベース合金シート | |
| US5129960A (en) | Method for superplastic forming of rapidly solidified magnesium base alloy sheet | |
| JPS648066B2 (enrdf_load_stackoverflow) | ||
| US4857109A (en) | Rapidly solidified high strength, corrosion resistant magnesium base metal alloys | |
| US6245164B1 (en) | Dual-phase Cr-Ta alloys for structural applications |
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 |
|
| AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AT BE CH DE FR GB IT LI NL SE |
|
| 17P | Request for examination filed |
Effective date: 19870130 |
|
| 17Q | First examination report despatched |
Effective date: 19880414 |
|
| 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 DE FR GB IT LI NL SE |
|
| REF | Corresponds to: |
Ref document number: 45189 Country of ref document: AT Date of ref document: 19890815 Kind code of ref document: T |
|
| ITF | It: translation for a ep patent filed | ||
| GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) | ||
| REF | Corresponds to: |
Ref document number: 3664789 Country of ref document: DE Date of ref document: 19890907 |
|
| 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 | ||
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 19910514 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: 19910521 Year of fee payment: 6 Ref country code: CH Payment date: 19910521 Year of fee payment: 6 Ref country code: AT Payment date: 19910521 Year of fee payment: 6 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: SE Payment date: 19910523 Year of fee payment: 6 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: BE Payment date: 19910613 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: 19910617 Year of fee payment: 6 |
|
| PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: NL Payment date: 19910630 Year of fee payment: 6 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Effective date: 19920625 Ref country code: AT Effective date: 19920625 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SE Effective date: 19920626 |
|
| ITTA | It: last paid annual fee | ||
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LI Effective date: 19920630 Ref country code: CH Effective date: 19920630 Ref country code: BE Effective date: 19920630 |
|
| BERE | Be: lapsed |
Owner name: CEGEDUR SOC. DE TRANSFORMATION DE L'ALUMINIUM PEC Effective date: 19920630 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Effective date: 19930101 |
|
| NLV4 | Nl: lapsed or anulled due to non-payment of the annual fee | ||
| GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 19920625 |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Effective date: 19930226 |
|
| REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
| PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DE Effective date: 19930302 |
|
| REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST |
|
| EUG | Se: european patent has lapsed |
Ref document number: 86420166.0 Effective date: 19930109 |
|
| 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;WARNING: LAPSES OF ITALIAN PATENTS WITH EFFECTIVE DATE BEFORE 2007 MAY HAVE OCCURRED AT ANY TIME BEFORE 2007. THE CORRECT EFFECTIVE DATE MAY BE DIFFERENT FROM THE ONE RECORDED. Effective date: 20050625 |