DE42872T1 - Thermische schutzbeschichtungen aus saeulenartig koernig keramischem material. - Google Patents
Thermische schutzbeschichtungen aus saeulenartig koernig keramischem material.Info
- Publication number
- DE42872T1 DE42872T1 DE198181900391T DE81900391T DE42872T1 DE 42872 T1 DE42872 T1 DE 42872T1 DE 198181900391 T DE198181900391 T DE 198181900391T DE 81900391 T DE81900391 T DE 81900391T DE 42872 T1 DE42872 T1 DE 42872T1
- Authority
- DE
- Germany
- Prior art keywords
- layer
- mcraly
- mils
- aluminum oxide
- oxide layer
- 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.)
- Pending
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/02—Pretreatment of the material to be coated
- C23C14/024—Deposition of sublayers, e.g. to promote adhesion of the coating
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
- C03C29/00—Joining metals with the aid of glass
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/14—Layered products comprising a layer of metal next to a fibrous or filamentary layer
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/02—Pretreatment of the material to be coated
- C23C14/024—Deposition of sublayers, e.g. to promote adhesion of the coating
- C23C14/025—Metallic sublayers
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/02—Pretreatment of the material to be coated
- C23C14/028—Physical treatment to alter the texture of the substrate surface, e.g. grinding, polishing
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C14/00—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
- C23C14/06—Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
- C23C14/08—Oxides
- C23C14/083—Oxides of refractory metals or yttrium
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/005—Selecting particular materials
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/922—Static electricity metal bleed-off metallic stock
- Y10S428/923—Physical dimension
- Y10S428/924—Composite
- Y10S428/926—Thickness of individual layer specified
-
- 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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
- Y10T428/12542—More than one such component
- Y10T428/12549—Adjacent to each other
-
- 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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
- Y10T428/12583—Component contains compound of adjacent metal
- Y10T428/1259—Oxide
-
- 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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
- Y10T428/12611—Oxide-containing component
- Y10T428/12618—Plural oxides
-
- 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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12861—Group VIII or IB metal-base component
- Y10T428/12931—Co-, Fe-, or Ni-base components, alternative to each other
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Organic Chemistry (AREA)
- Metallurgy (AREA)
- General Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- General Chemical & Material Sciences (AREA)
- Geochemistry & Mineralogy (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Physical Vapour Deposition (AREA)
- Coating By Spraying Or Casting (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Furnace Charging Or Discharging (AREA)
- Compositions Of Oxide Ceramics (AREA)
- Furnace Housings, Linings, Walls, And Ceilings (AREA)
Claims (21)
1. Verfahren zum Herstellen eines metallischen Gegenstands
mit einer dauerhaften thermischen Schutzbeschichtung aus keramischem Material, gekennzeichnet durch folgende Schritte:
a. Schaffen eines Superlegierungssubstrats mit einer sauberen Oberfläche
b. Aufbringen einer dünnen festhaftenden MCrAlY-Schicht
auf die saubere Oberfläche
c. Bilden einer dünnen gleichmäßigen festhaftenden Aluminiumoxidschicht
auf der MCrAlY-Schicht
d. Aufbringen einer säulenartig keramischen Beschichtung auf die Aluminiumoxidschicht durch Aufdampfen.
2. Verfahren nach Anspruch 1, dadurch gekennzeichnet, daß '.
die MCrAlY-Schicht durch Aufdampfen aufgebracht wird.
3. Verfahren nach Anspruch 1, dadurch gekennzeichnet, daß die MCrAlY-Schicht eine Dicke von etwa 25,4 - 254 μπα
(1 - 10 mils) hat.
(1 - 10 mils) hat.
4. Verfahren nach Anspruch 2, dadurch gekennzeichnet, daß das aufgedampfte MCrAlY anschließend durch Hämmern kaltgehärtet
wird.
5. Verfahren nach Anspruch 4, dadurch gekennzeichnet, daß die durch Hämmern kaltgehärtete aufgedampfte Beschichtung
anschließend wärmebehandelt wird.
6. Verfahren nach Anspruch 1, dadurch gekennzeichnet, daß die gleichmäßige festhaftende Oxidschicht durch thermische
Oxidation gebildet wird.
7. Verfahren nach Anspruch 1, dadurch gekennzeichnet, daß die Dicke der Aluminiumoxidschicht etwa 0,254 μπι (.01 mils)
bis etwa 2,54 μΐη (.1 mils) beträgt.
8. Verfahren nach Anspruch 1, dadurch gekennzeichnet, daß der Gegenstand während des Aufbringens der Keramikschicht
manipuliert wird, so daß die Bildung eines Säulengefüges
gefördert wird.
9. Verfahren nach Anspruch 1, dadurch gekennzeichnet, daß nach dem Aufbringen der säulenartig keramischen Schicht
der beschichtete Gegenstand in einer Sauerstoff enthaltenden Atmosphäre wärmebehandelt wird, so daß eine stöchio-
der beschichtete Gegenstand in einer Sauerstoff enthaltenden Atmosphäre wärmebehandelt wird, so daß eine stöchio-
metrische Keramikzusammensetzung erzielt wird.
10. Verfahren zum Herstellen eines metallischen Gegen-
stands mit einer dauerhaften thermischen Schutzbeschichtung aus keramischem Material, gekennzeichnet durch folgende
Schritte:
a. Schaffen eines Superlegierungssubstrats mit einer sauberen Oberfläche
b. Aufbringen einer dünnen festhaftenden MCrAlY-Schicht
auf die saubere Oberfläche
c. Aufbringen einer säulenartig keramischem Beschichtung auf die MCrAlY-Schicht durch Aufdampfen
d. Wärmebehandeln des mit der säulenartig keramischen Beschichtung
versehenen Gegenstands in einer Sauerstoff enthaltenden Atmosphäre, um eine Aluminiumoxidschicht
zwischen dem MCrAlY und der säulenartig keramischen Beschichtung zu bilden.
11- Verfahren nach Anspruch 10, dadurch gekennzeichnet,
daß die FCrAlY-Schicht durch Aufdampfen aufgebracht wird.
12. Verfahren nach Anspruch 10, dadurch gekennzeichnet, daß die MCrAlY-Schicht eine Dicke von etwa 25,4 - 254 μπι
(1 - 10 mils) hat.
13. Verfahren nach Anspruch 11, dadurch gekennzeichnet, daß das aufgedampfte MCrAlY anschließend durch Hämmern
kaltgehärtet wird.
14. Verfahren nach Anspruch 13, dadurch gekennzeichnet, daß die durch Hämmern kaltgehärtete aufgedampfte Beschichtung
anschließend wärmebehandelt wird.
15. Verfahren nach Anspruch 10, dadurch gekennzeichnet, daß die gleichmäßige festhaftende Schicht durch thermische
Oxidation gebildet wird.
16. Verfahren nach Anspruch 10, dadurch gekennzeichnet,
daß die Dicke der Aluminiumoxidschicht etwa 0,254 μΐη (.01
mils) bis etwa 2,54 μΐη (.1 mils) beträgt.
17. Verfahren nach Anspruch 10, dadurch gekennzeichnet,
daß der Gegenstand während des Aufbringens der Keramikschicht manipuliert wird, so daß die Bildung eines Säulengefüges
gefördert wird.
18. Superlegierungsgegenstand mit einer festhaftenden dauerhaften
thermischen Schutzbeschichtung aus keramischem Material, gekennzeichnet durch:
a. ein Superlegierungssubstrat
b. eine festhaftende dichte MCrAlY-Beschichtung auf dem Substrat,
c. eine Aluminiumoxidschicht auf der MCrAlY-Oberflache,
d. eine festhaftende säulenartig keramische Schicht auf der Aluminiumoxidschicht.
19. Beschichteter Gegenstand nach Anspruch 18, dadurch
gekennzeichnet, daß die Dicke des MCrAlY etwa 25,4 μΐη
(1 mil) bis etwa 254 μΐη (10 mils) beträgt.
20. Beschichteter Gegenstand nach Anspruch 18, dadurch
gekennzeichnet, daß die Aluminiumoxidschicht eine Dicke von etwa 0,254 μΐη (.01 mils) bis etwa 2,54 μΐη (.1 mils)
hat.
21. Beschichteter Gegenstand nach Anspruch 18, dadurch gekennzeichnet, daß die säulenartig keramische Beschichtung
eine Dicke von etwa 25,4 μΐη (1 mil) bis etwa 1270
μΐη (50 mils) hat.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/109,956 US4321311A (en) | 1980-01-07 | 1980-01-07 | Columnar grain ceramic thermal barrier coatings |
PCT/US1981/000021 WO1981001982A1 (en) | 1980-01-07 | 1981-01-07 | Columnar grain ceramic thermal barrier coatings |
Publications (1)
Publication Number | Publication Date |
---|---|
DE42872T1 true DE42872T1 (de) | 1983-01-20 |
Family
ID=22330490
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE8181900391T Expired DE3163778D1 (en) | 1980-01-07 | 1981-01-07 | Columnar grain ceramic thermal barrier coatings |
DE198181900391T Pending DE42872T1 (de) | 1980-01-07 | 1981-01-07 | Thermische schutzbeschichtungen aus saeulenartig koernig keramischem material. |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE8181900391T Expired DE3163778D1 (en) | 1980-01-07 | 1981-01-07 | Columnar grain ceramic thermal barrier coatings |
Country Status (13)
Country | Link |
---|---|
US (1) | US4321311A (de) |
EP (1) | EP0042872B1 (de) |
JP (1) | JPH0118993B2 (de) |
KR (1) | KR840001683B1 (de) |
AU (1) | AU543223B2 (de) |
BE (1) | BE886975A (de) |
BR (1) | BR8105750A (de) |
CA (1) | CA1167329A (de) |
DE (2) | DE3163778D1 (de) |
IL (1) | IL61878A (de) |
IT (1) | IT1134957B (de) |
NO (1) | NO156748C (de) |
WO (1) | WO1981001982A1 (de) |
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IL75304A (en) * | 1984-06-08 | 1989-03-31 | United Technologies Corp | Coated superalloy articles and method of strengthening same |
DE3426201A1 (de) * | 1984-07-17 | 1986-01-23 | BBC Aktiengesellschaft Brown, Boveri & Cie., Baden, Aargau | Verfahren zum aufbringen von schutzschichten |
JPS61174385A (ja) * | 1984-09-10 | 1986-08-06 | Hitachi Ltd | セラミツク被覆耐熱部材及びその製造方法 |
US4576874A (en) * | 1984-10-03 | 1986-03-18 | Westinghouse Electric Corp. | Spalling and corrosion resistant ceramic coating for land and marine combustion turbines |
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GB2236750B (en) * | 1989-09-08 | 1993-11-17 | United Technologies Corp | Ceramic material and insulating coating made thereof |
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- 1981-01-07 DE DE8181900391T patent/DE3163778D1/de not_active Expired
- 1981-01-07 JP JP56500559A patent/JPH0118993B2/ja not_active Expired
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BE886975A (fr) | 1981-05-04 |
NO156748B (no) | 1987-08-10 |
EP0042872B1 (de) | 1984-05-30 |
US4321311A (en) | 1982-03-23 |
JPH0118993B2 (de) | 1989-04-10 |
DE3163778D1 (en) | 1984-07-05 |
EP0042872A4 (de) | 1982-06-10 |
JPS57500291A (de) | 1982-02-18 |
AU543223B2 (en) | 1985-04-04 |
IT8119030A0 (it) | 1981-01-07 |
KR840001683B1 (ko) | 1984-10-15 |
IT1134957B (it) | 1986-08-20 |
WO1981001982A1 (en) | 1981-07-23 |
IL61878A (en) | 1984-09-30 |
NO156748C (no) | 1987-11-18 |
CA1167329A (en) | 1984-05-15 |
EP0042872A1 (de) | 1982-01-06 |
BR8105750A (pt) | 1981-11-24 |
NO813000L (no) | 1981-09-04 |
AU6774381A (en) | 1981-08-07 |
KR830005068A (ko) | 1983-07-23 |
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