US3268368A - Process for the production of wrought nickel strip and sheet of low hardness - Google Patents
Process for the production of wrought nickel strip and sheet of low hardness Download PDFInfo
- Publication number
- US3268368A US3268368A US317780A US31778063A US3268368A US 3268368 A US3268368 A US 3268368A US 317780 A US317780 A US 317780A US 31778063 A US31778063 A US 31778063A US 3268368 A US3268368 A US 3268368A
- Authority
- US
- United States
- Prior art keywords
- strip
- sheet
- hardness
- density
- nickel
- 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 - Lifetime
Links
Classifications
-
- 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
- C22C1/0433—Nickel- or cobalt-based alloys
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/18—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces by using pressure rollers
-
- 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
-
- 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
- Y10S75/00—Specialized metallurgical processes, compositions for use therein, consolidated metal powder compositions, and loose metal particulate mixtures
- Y10S75/95—Consolidated metal powder compositions of >95% theoretical density, e.g. wrought
Definitions
- This invention relates to a process for the production of high purity wrought nickel shapes, particularly nickel strip or sheet, of high density, low hardness and high ductility.
- the particles are fed into the roll gap of a conventional, r-oll compacting unit to produce a green strip or sheet of a density of from about 50% to 95% of the theoretical density, i.e., about 8.902 grams per cubic centimetre :at 20 C.
- the green strip or sheet is of sufiicient mechanical strength to be selfsupporting and to withstand a limited amount of handling.
- the green strip or sheet is sintered in a heated furnace, usually a reducing atmosphere, and then treated by a sequence of hot and/or cold working steps, with or without intermediate annealing stages, to increase the density to approximately 100% of the theoretical density :and to reduce it to a predetermined thickness.
- Nickel strip or sheet produced by these conventional processes is strong, relatively ductile and generally has a hardness of the order of from about 35 to 45 measured by the Rockwell 30T hardness scale, regardless of whether it is produced from ingots or bil-lets or from nickel metal particles.
- Such nickel strip or sheet has many uses, particularly in the electronics industry.
- nickel coinage is produced from blanks stamped from nickel strip or sheet of required thickness.
- the blanks are then die stamped, obverse and reverse, with the denomination of the particular coin and designs which are characteristic of the country which issues them. It is difficult to obtain sharply defined impressions from the die when the blanks have a hardness such as that produced by conventional rolling processes, that is, from about 35 to 45, measured by the Rockwell 30T hardness scale. Also, the hardness of the blanks causes rapid wear, and even breakage, of the dies.
- Nickel metal particles are fed into the roll gap of a conventional roll 3,268,368 Patented August 23, 1966 "ice compacting unit at a predetermined rate to produce a green strip or sheet of desired thickness and adensity within the range of from about 50% to 95% of the theoretical density.
- Green strip or sheet produced in the roll compacting unit is sintered in a controlled atmosphere at a temperature within the range of from about 1500 F. to about 2100 F. to lower the sulphur and carbon contents of the strip or sheet to safely below specific maximum levels.
- the sintered strip or sheet is then hot rolled at a temperature about or slightly above the recrystallization temperature of the nickel particles to increase the density to about 100% of its theoretical density.
- the strip or sheet of substantially 100% density is cold rolled and/ or otherwise cold worked at about ambient temperature to reduce its thickness and/or to produce semi-finished or finished products.
- the cold worked material is heated to a temperature within the range of from about 1200 F. to about 1800 F. and then cooled to atmospheric temperature in a protective atmosphere which prevents re-oxidation.
- Wrought nickel produced by this process is of high purity, of substantially 100% density, of which ductility, and of low hardness, within the range of from about 20 to 35, Rockwell 30T hardness scale.
- the process is independent of the source of the nickel powder used as a starting material. That is, the powder can be produced by conventional pyrometallurgical, or hydrometallurgical processes.
- the powder may contain minor amounts, in the order of 0.2% or less, of metallic impurities generally found in association with nickel, such as cobalt, iron and copper, for example.
- Other impurities such as carbon and sulphur may also be present in the starting material but must be reduced below certain specific minimum levels as described hereinafter. It is, of course, preferable to select a nickel powder which is of high purity and which readily compacts to form a strong green strip when rolled in a conventional metal powder rolling mill.
- Nickel powder produced by precipitation from a solution in which it is present as a dissolved salt by reacting the solution with a reducing gas at elevated temperature and pressure is particularly suitable.
- Nickel powder produced in this manner is of high purity, generally over 99.8% pure nickel, and is readily available in grades which are particularly suitable for roll compacting.
- the powder particle size should be below about 300 microns and preferably at least about 40% should be in the size range of about 10 microns to about 44 microns.
- the finely divided nickel powder is formed into a green strip by compacting it in a conventional metal powder rolling mill.
- a conventional metal powder rolling mill comprises, for example, a feeding device arranged to feed the metal powder into the roll gap of a pair of horizontally disposed rolls spaced apart a predetermined distance to compact the particles into a green strip or sheet of desired thickness.
- a feeding device arranged to feed the metal powder into the roll gap of a pair of horizontally disposed rolls spaced apart a predetermined distance to compact the particles into a green strip or sheet of desired thickness.
- the green strip or sheet leaving the rolls has a density of from about to about of the theoretical density of the particulate matter of which it is formed. It is self-supporting and possesses sufficient mechanical strength that it can be passed directly to the sintering step.
- the green strip is passed into afurnace which is maintained at the desired temperature and in which the atmosphere is controlled to obtain efficient removal of excess sulphur and/ or carbon.
- a single green strip may be treated or one or more green strips may be superimposed one on top of the other to form a thick, laminated strip.
- Sulphur content is reduced to below the minimum critical level by flowing a continuous stream of hydrogen through the sintering furnace.
- the velocity of the hydrogen gas through the sintering furnace is an important factor in the efficient desulphurization of the metal strip. This velocity should be above about 300 centimetres per minute, the optimum and maximum velocity being determined by operating economics in each particular case. If the hydrogen gas velocity is below the lower level mentioned, the desulphurization proceeds at an uneconomically slow rate, if it proceeds at all.
- any excess must be removed.
- Dry hydrogen is relatively ineffective in removing carbon contamination from the strip; thus, it is necessary to provide, in addition to the hydrogen required for sulphur removal, a reagent that will react with the carbon content of the nickel and effectively remove it.
- the preferred procedure s to provide water in the hydrogen.
- the exact moisture content of the hydrogen is not critical, but the time required for carbon removal increases as the dryness of the gas is increased. For most purposes we have found that hydrogen having a dew point of 50 to 80 F. is suitable; however, this may be lower when low-carbon nickel powder is used or higher if high carbon nickel powder is used.
- An alternative procedure is to provide a small amount of carbon dioxide in the sintering atmosphere. Satisfactory results are obtained when the hydrogen fed into the furnace contains about double the stoichiometric carbon dioxide concentration required for decarbonization.
- the sintering furnace temperature is maintained in the range of from about 1500 F. to about 2100 F.
- the strip or sheet is treated under these conditions for a time sufficient to reduce the sulphur content to below about 0.003% by weight and the carbon content of the metal to below about 0.005% by weight.
- a time period of from about minutes to about 45 minutes is sufficient to reduce the sulphur and carbon contents to the desired levels, the exact time depending on operating conditions and the amount of sulphur and/or carbon contamination in the starting material.
- the type of furnace used is not critical except that it must be designed to provide a constant and uniform temperature throughout, and it must allow for the free flow of hydrogen gas around or over the strip at a velocity preferably greater than about 300 centimetres per minute.
- a coil furnace is quite suitable where a single strip of compacted metal is being treated.
- a long horizontal furnace is most suitable. In using such a furnace, the stacked green strips are cut into lengths equal to the effective heat-treating length of the furnace, and each length is sintered for the required period of time on a batch basis.
- the hot rolled strip which, at this stage, is relatively hard having, for example, a hardness in the range of from about 45 to 50 Rockwell 30T hardness scale may be passed to a first annealing step.
- the strip is heat-treated at a temperature within the range of from about 800 F. to about 2200 F. under a deoxidizing atmosphere, preferably hydrogen gas.
- the anneal is con tinued at least until the surface oxidation formed during the Sintering and hot rolling steps is removed.
- the time required usually is from about 5 to about 60 minutes.
- this first anneal step is not required if surface oxidation of the hot rolled strip is prevented by other means such as by maintaining the strip in a reducing atmosphere while it is being fed into the hot rolling mill, immediately when it emerges from the hot rolling mill, and while it is being cooled to cold working temperature.
- the cooled de-oxidized strip is then passed to a cold working step where it is cold rolled to reduce it to the desired thickness and further Worked to produce the rough form of the end product.
- the strip is cold rolled to the thickness required for the blanks; then the blanks are punched out of the strip using conventional equipment.
- the material passed from the cold working steps is hard and has low ductility as a result of accumulated work hardening, and the final annealing step is required to produce a product with the desired hardness and ductility.
- This final step which is referred to herein as the final anneal, is carried out under a protective atmosphere and at a temperature within the range of from about 1200 F. to about 1800 F. The exact temperature will depend on the hardness desired for the final product. We have found that hardness of the annealed product can be largely controlled by controlling the temperature of the final anneal. Generally, the hardness of the annealed product decreases with increasing temperature. The time required for the final anneal depends on the size and shape of the wrought products being treated.
- the products from the final anneal step are semifinished forms of wrought nickel of exceptionally low hardness which can be readily cold worked to produce finished products.
- Example 1 Nickel metal particles having properties set out in Table l were compacted in a conventional roll compacting unit:
- the density of the green strip produced by the roll compacting unit was 84% of the theoretical density, and the'strip had sufficient green strength to be self-supporting for handling in the sintering operation.
- the green strip was sintered at 1800 F. for 35 minutes in a stream of hydrogen flowing through the furnace at 7200 centimetres per minute.
- the sintered strip contained 0.003% sulphur and 0.004% carbon.
- the surface of the strip was discoloured from surface oxidation.
- the sintered strip was passed, in a protective atmosphere, to a hot rolling mill comprised of two horizontally mounted, oppositely positioned rolls.
- the strip emerging from these rolls had a density substantially 100% of the theoretical density.
- the hot rolled strip was heated at 2000 F. for minutes under a hydrogen atmosphere.
- the annealed strip had a bright surface, indicating that surface oxidation had been removed, and a hardness of 40 (Rockwell 30T).
- the de-oxidized strip was cold rolled to a thickness of 0.058 inch and coinage blanks were punched from the strip with conventional punching equipment. It was found that the work hardening resulting from these cold working operations had increased the hardness of the nickel strip to 75 (Rockwell 30T).
- the coinage blanks were annealed, under a hydrogen atmosphere, for 30 minutes at 1200 F.
- the resulting product had a hardness of (Rockwell T).
- Example 2 reduction of nickel from an ammoniacal nickel ammonium sulphate solution. The analyses of these powders is shown below.
- wrought nickel strip produced in accordance with the method of claim 3 containing at least 99.8% nickel and containing less than 0.003% of sulphur, less than 0.005 of carbon and having a hardness below about Rockwell 30T hardness scale.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacturing & Machinery (AREA)
- Powder Metallurgy (AREA)
- Heat Treatment Of Nonferrous Metals Or Alloys (AREA)
- Manufacture Of Metal Powder And Suspensions Thereof (AREA)
Priority Applications (8)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1053594D GB1053594A (fr) | 1963-10-21 | ||
US317780A US3268368A (en) | 1963-10-21 | 1963-10-21 | Process for the production of wrought nickel strip and sheet of low hardness |
NL6410279A NL6410279A (fr) | 1963-10-21 | 1964-09-03 | |
DE1458482A DE1458482C3 (de) | 1963-10-21 | 1964-09-23 | Verfahren zur pulvermetallurgischen Herstellung eines Nickelbandes |
CH1352964A CH465783A (de) | 1963-10-21 | 1964-10-19 | Verfahren zur Herstellung von Nickelblech und -band |
JP39059359A JPS4825860B1 (fr) | 1963-10-21 | 1964-10-20 | |
FR992195A FR1412233A (fr) | 1963-10-21 | 1964-10-21 | Procédé de production de bandes et tôles de nickel ouvré à faible dureté |
BE654645A BE654645A (fr) | 1963-10-21 | 1964-10-21 |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US317780A US3268368A (en) | 1963-10-21 | 1963-10-21 | Process for the production of wrought nickel strip and sheet of low hardness |
BE654645A BE654645A (fr) | 1963-10-21 | 1964-10-21 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3268368A true US3268368A (en) | 1966-08-23 |
Family
ID=25656045
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US317780A Expired - Lifetime US3268368A (en) | 1963-10-21 | 1963-10-21 | Process for the production of wrought nickel strip and sheet of low hardness |
Country Status (7)
Country | Link |
---|---|
US (1) | US3268368A (fr) |
JP (1) | JPS4825860B1 (fr) |
BE (1) | BE654645A (fr) |
CH (1) | CH465783A (fr) |
DE (1) | DE1458482C3 (fr) |
GB (1) | GB1053594A (fr) |
NL (1) | NL6410279A (fr) |
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3390985A (en) * | 1966-08-10 | 1968-07-02 | Us Interior | Consolidation and forming by high-energy-rate extrusion of powder material |
US3403058A (en) * | 1964-12-02 | 1968-09-24 | Fansteel Metallurgical Corp | Process for preventing blistering of nickel metal containing dispersed refractory oxide particles |
US3418112A (en) * | 1966-10-07 | 1968-12-24 | United Aircraft Corp | Method for forming seamless pressure vessels |
US3436802A (en) * | 1967-11-14 | 1969-04-08 | Magnetics Inc | Powder metallurgy |
US3724050A (en) * | 1968-09-19 | 1973-04-03 | Beryllium Corp | Method of making beryllium shapes from powder metal |
US3839026A (en) * | 1966-11-18 | 1974-10-01 | British Steel Corp | PROCESS FOR THE PRODUCTION OF METAL STRIP FROM Fe POWDER |
US3975193A (en) * | 1973-04-18 | 1976-08-17 | Airco, Inc. | Powder metallurgy process for producing stainless steel stock |
US3976547A (en) * | 1972-01-24 | 1976-08-24 | Merck & Co., Inc. | Cell and vaccine production |
US20070051007A1 (en) * | 2005-09-08 | 2007-03-08 | Bridgewater, Inc. | Heat exchanger assembly with air mover |
US20070181526A1 (en) * | 2006-01-14 | 2007-08-09 | Abe Frishman | Easy-pull bottle cap |
US20100200534A1 (en) * | 2007-01-25 | 2010-08-12 | Abe Frishman | Easy pull bottle cap |
CN102350439A (zh) * | 2011-09-23 | 2012-02-15 | 宁波江丰电子材料有限公司 | 半导体用镍靶坯热轧方法 |
US9321562B2 (en) | 2006-01-14 | 2016-04-26 | World Bottling Cap Llc | Bottle crown with opener assembly |
US9533800B2 (en) | 2014-03-28 | 2017-01-03 | World Bottling Cap, LLC | Bottle crown with opener assembly |
US9649254B2 (en) | 2006-01-14 | 2017-05-16 | World Bottling Cap, LLC | Medical vial cap |
US11548683B2 (en) | 2014-03-28 | 2023-01-10 | World Bottling Cap, LLC | Bottle crown with opener assembly |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3019449C2 (de) * | 1979-05-25 | 1985-06-13 | Nippon Gakki Seizo K.K., Hamamatsu, Shizuoka | Verfahren zur Herstellung von Magnetkopf-Kernen |
US20090142221A1 (en) * | 2007-11-30 | 2009-06-04 | Honeywell International, Inc. | Engine components and methods of forming engine components |
JP6201192B2 (ja) * | 2014-06-17 | 2017-09-27 | 住友金属鉱山株式会社 | ニッケルの軟化処理方法及びニッケルの切断方法 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2159231A (en) * | 1934-10-25 | 1939-05-23 | Ig Farbenindustrie Ag | Producing nickel alloy articles |
US2159604A (en) * | 1928-03-26 | 1939-05-23 | Ig Farbenindustrie Ag | Metallic article |
US2826805A (en) * | 1954-01-13 | 1958-03-18 | Federal Mogul Corp | Sintered stainless steel metal alloy |
US2889224A (en) * | 1955-07-20 | 1959-06-02 | Int Nickel Co | Manufacture of metal strip from metal powder |
US2900254A (en) * | 1954-10-13 | 1959-08-18 | Sylvania Electric Prod | Process of producing sintered metal sheets |
-
0
- GB GB1053594D patent/GB1053594A/en active Active
-
1963
- 1963-10-21 US US317780A patent/US3268368A/en not_active Expired - Lifetime
-
1964
- 1964-09-03 NL NL6410279A patent/NL6410279A/xx unknown
- 1964-09-23 DE DE1458482A patent/DE1458482C3/de not_active Expired
- 1964-10-19 CH CH1352964A patent/CH465783A/de unknown
- 1964-10-20 JP JP39059359A patent/JPS4825860B1/ja active Pending
- 1964-10-21 BE BE654645A patent/BE654645A/xx unknown
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2159604A (en) * | 1928-03-26 | 1939-05-23 | Ig Farbenindustrie Ag | Metallic article |
US2159231A (en) * | 1934-10-25 | 1939-05-23 | Ig Farbenindustrie Ag | Producing nickel alloy articles |
US2826805A (en) * | 1954-01-13 | 1958-03-18 | Federal Mogul Corp | Sintered stainless steel metal alloy |
US2900254A (en) * | 1954-10-13 | 1959-08-18 | Sylvania Electric Prod | Process of producing sintered metal sheets |
US2889224A (en) * | 1955-07-20 | 1959-06-02 | Int Nickel Co | Manufacture of metal strip from metal powder |
Cited By (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3403058A (en) * | 1964-12-02 | 1968-09-24 | Fansteel Metallurgical Corp | Process for preventing blistering of nickel metal containing dispersed refractory oxide particles |
US3390985A (en) * | 1966-08-10 | 1968-07-02 | Us Interior | Consolidation and forming by high-energy-rate extrusion of powder material |
US3418112A (en) * | 1966-10-07 | 1968-12-24 | United Aircraft Corp | Method for forming seamless pressure vessels |
US3839026A (en) * | 1966-11-18 | 1974-10-01 | British Steel Corp | PROCESS FOR THE PRODUCTION OF METAL STRIP FROM Fe POWDER |
US3436802A (en) * | 1967-11-14 | 1969-04-08 | Magnetics Inc | Powder metallurgy |
US3724050A (en) * | 1968-09-19 | 1973-04-03 | Beryllium Corp | Method of making beryllium shapes from powder metal |
US3976547A (en) * | 1972-01-24 | 1976-08-24 | Merck & Co., Inc. | Cell and vaccine production |
US3975193A (en) * | 1973-04-18 | 1976-08-17 | Airco, Inc. | Powder metallurgy process for producing stainless steel stock |
US20070051007A1 (en) * | 2005-09-08 | 2007-03-08 | Bridgewater, Inc. | Heat exchanger assembly with air mover |
US8789291B2 (en) | 2005-09-08 | 2014-07-29 | Bridgewater LLC | Heat exchanger assembly with air mover |
US8061544B2 (en) * | 2006-01-14 | 2011-11-22 | World Bottling Cap, LLC | Easy-pull crown bottle cap |
US20070181526A1 (en) * | 2006-01-14 | 2007-08-09 | Abe Frishman | Easy-pull bottle cap |
US11104492B2 (en) * | 2006-01-14 | 2021-08-31 | World Bottling Cap, LLC | Bottle crown with opener assembly |
US10618700B2 (en) | 2006-01-14 | 2020-04-14 | World Bottling Cap, LLC | Medical vial cap |
US8276773B2 (en) * | 2006-01-14 | 2012-10-02 | World Bottling Cap, LLC | Bottle crown with removable frangible portion |
US9649254B2 (en) | 2006-01-14 | 2017-05-16 | World Bottling Cap, LLC | Medical vial cap |
US9592936B2 (en) | 2006-01-14 | 2017-03-14 | World Bottling Cap, LLC | Bottle crown with opener assembly |
US20110024381A1 (en) * | 2006-01-14 | 2011-02-03 | Abe Frishman | Easy-pull bottle cap |
US9321562B2 (en) | 2006-01-14 | 2016-04-26 | World Bottling Cap Llc | Bottle crown with opener assembly |
US8365940B2 (en) * | 2007-01-25 | 2013-02-05 | World Bottling Cap, LLC | Bottle crown with opener assembly |
US20100200534A1 (en) * | 2007-01-25 | 2010-08-12 | Abe Frishman | Easy pull bottle cap |
CN102350439B (zh) * | 2011-09-23 | 2014-04-23 | 宁波江丰电子材料有限公司 | 半导体用镍靶坯热轧方法 |
CN102350439A (zh) * | 2011-09-23 | 2012-02-15 | 宁波江丰电子材料有限公司 | 半导体用镍靶坯热轧方法 |
US9533800B2 (en) | 2014-03-28 | 2017-01-03 | World Bottling Cap, LLC | Bottle crown with opener assembly |
US11046479B2 (en) | 2014-03-28 | 2021-06-29 | World Bottling Cap Llc | Non-metal and hybrid bottle crowns with opener assembly |
US11548683B2 (en) | 2014-03-28 | 2023-01-10 | World Bottling Cap, LLC | Bottle crown with opener assembly |
Also Published As
Publication number | Publication date |
---|---|
DE1458482B2 (de) | 1973-10-04 |
NL6410279A (fr) | 1965-04-22 |
DE1458482A1 (de) | 1969-01-23 |
CH465783A (de) | 1968-11-30 |
BE654645A (fr) | 1965-02-15 |
DE1458482C3 (de) | 1974-05-02 |
GB1053594A (fr) | |
JPS4825860B1 (fr) | 1973-08-01 |
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