US2566283A - Spinnerette - Google Patents
Spinnerette Download PDFInfo
- Publication number
- US2566283A US2566283A US81157A US8115749A US2566283A US 2566283 A US2566283 A US 2566283A US 81157 A US81157 A US 81157A US 8115749 A US8115749 A US 8115749A US 2566283 A US2566283 A US 2566283A
- Authority
- US
- United States
- Prior art keywords
- gold
- rhodium
- platinum
- alloy
- spinnerette
- 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
- BASFCYQUMIYNBI-UHFFFAOYSA-N platinum Chemical compound [Pt] BASFCYQUMIYNBI-UHFFFAOYSA-N 0.000 claims description 35
- 229910052703 rhodium Inorganic materials 0.000 claims description 23
- 239000010948 rhodium Substances 0.000 claims description 23
- MHOVAHRLVXNVSD-UHFFFAOYSA-N rhodium atom Chemical compound [Rh] MHOVAHRLVXNVSD-UHFFFAOYSA-N 0.000 claims description 23
- 229910045601 alloy Inorganic materials 0.000 claims description 21
- 239000000956 alloy Substances 0.000 claims description 21
- 229910052697 platinum Inorganic materials 0.000 claims description 18
- 229910001260 Pt alloy Inorganic materials 0.000 claims description 5
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 description 22
- 229910052737 gold Inorganic materials 0.000 description 22
- 239000010931 gold Substances 0.000 description 22
- KDLHZDBZIXYQEI-UHFFFAOYSA-N Palladium Chemical compound [Pd] KDLHZDBZIXYQEI-UHFFFAOYSA-N 0.000 description 12
- 239000000470 constituent Substances 0.000 description 7
- 229910052763 palladium Inorganic materials 0.000 description 6
- 238000010586 diagram Methods 0.000 description 5
- 238000005553 drilling Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 238000003483 aging Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 229910000923 precious metal alloy Inorganic materials 0.000 description 2
- 229920002955 Art silk Polymers 0.000 description 1
- 229920000297 Rayon Polymers 0.000 description 1
- 241000220010 Rhode Species 0.000 description 1
- KJTLSVCANCCWHF-UHFFFAOYSA-N Ruthenium Chemical compound [Ru] KJTLSVCANCCWHF-UHFFFAOYSA-N 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- JUWSSMXCCAMYGX-UHFFFAOYSA-N gold platinum Chemical compound [Pt].[Au] JUWSSMXCCAMYGX-UHFFFAOYSA-N 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000002964 rayon Substances 0.000 description 1
- 229910052707 ruthenium Inorganic materials 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 229920002994 synthetic fiber Polymers 0.000 description 1
- 229910002058 ternary alloy Inorganic materials 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 210000002268 wool Anatomy 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03B—MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
- C03B37/00—Manufacture or treatment of flakes, fibres, or filaments from softened glass, minerals, or slags
- C03B37/08—Bushings, e.g. construction, bushing reinforcement means; Spinnerettes; Nozzles; Nozzle plates
- C03B37/095—Use of materials therefor
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C5/00—Alloys based on noble metals
- C22C5/04—Alloys based on a platinum group metal
-
- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01D—MECHANICAL METHODS OR APPARATUS IN THE MANUFACTURE OF ARTIFICIAL FILAMENTS, THREADS, FIBRES, BRISTLES OR RIBBONS
- D01D4/00—Spinnerette packs; Cleaning thereof
- D01D4/02—Spinnerettes
- D01D4/022—Processes or materials for the preparation of spinnerettes
Definitions
- This invention relates to spinnerettes such as are employed in the production of synthetic fibres and filaments for production of rayon, artificial silk, artificial wool and other similar materials.
- Spinnerettes of this character essentially include a jet or nozzle through which the substance or material for extrusion is expelled under pressure. It is important that the spinner- .ette jets should be made of a metallic substance which will resist erosion and any tendency to corrode.
- spinnerette jets are made from an alloy of platinum with rhodium and gold, which alloy contains 4 to 15% of gold, 5 to of rhodium and the balance of platinum, the proportions being so selected that for gold contents less than 5% the minimum rhodium content is increased above 5% by an amount equal to five times the amount by which the gold content is below 5%.
- a gold content of 4.5% the rhodium must be not less than 7.5 and with 4% gold the rhodium must be not less than 10%.
- the total gold and rhodium content preferably should not exceed about 25%.
- jets made according to the present invention can be produced with a hardness of 400 V. P. N. or even higher.
- Example I an alloy is prepared containing:
- the alloy is produced in sheet form and is treated by raising it to a temperature of about 1050 C. to1100 C.- for 15 minutes. It is then quenched in cold water and is thereafter mechanically formed by the production of the cup and the drilling thereof. The formed jet is then heated for l to 2 hours at a temperature of 620 to 650 C. and allowed to cool. The finished jet has a hardness of 350 to 400 V. P. N or better.
- Example II an alloy is prepared contain- 1118:
- the process of producing the finished jet is substantially the same as in Example I and the hardness of the finished jet is about 450 V. P. N.
- Example 17V In this example the proportions of the constituents of an alloy are chosen to be the same as those of Example I except that 20% of the platinum is replaced by palladium, the replacement being made atom for atom. It will of course be understood that the expresison "atom for atom is used to mean that 20% of the platinum is excluded and an amount of palladium containing an equivalent number of atoms is substituted. The weight of the palladium will thus be less than that of the platinum which it replaces.
- the alloy prepared in this way is processed in the manner described in Example I and the hardness of the finished jet will be of the order of 250 to 300 V. P. N.
- Example IV It will be realised from cons deration of Example IV that it is possible to substitute under certain circumstances a certain amount of platinum by palladium.
- the alloy produced does not necessarily give as good results as those in which there is not substitution of platinum constituent but as will be appreciated it is often possible to substitute in a platinum-rich alloy a proportion of palladium without significantly altering the final desired properties of the alloy.
- the proportions of the constituents of the alloys that may be used in the fulfilment of the invention are illustrated by reference to the. accompanying diagram.
- the diagram represents the conventional diagram for a ternary alloy.
- the horizontally hatched. portion includes within it those points which define the desired ratio of proportion between the three constituents. From the diagram it can be seen that as the gold constituent is reduced from to 4% the corresponding range for rhodium increases. Thus for an increment of reduction in the gold as between 5% and 4%, the minimum rhodium content increases by an increment that is five times as great as the first mentioned increment, thereby ensuring that when the gold constituent is reduced to 4% the minimum rhodium constituent has been increased to V I claim: v n V 1.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Organic Chemistry (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Textile Engineering (AREA)
- Metallurgy (AREA)
- Life Sciences & Earth Sciences (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Geochemistry & Mineralogy (AREA)
- Manufacturing & Machinery (AREA)
- Spinning Methods And Devices For Manufacturing Artificial Fibers (AREA)
- Manufacture And Refinement Of Metals (AREA)
Description
28, 1951 A. G. DOWSON 2,566,283
SPINNERETTE Filed March 12, 1949 RHODIUM 1- PLATINUM %GOLD INVENTOR. ARTHUR ORDON DOWSON' ATTQENEY Patented Aug. 28, 1951 SPINNERETTE Arthur Gordon Dowson, London, England, as signor to Baker & Company Incorporated, N ewark, N. J., a corporation of New Jersey Application March 12, 1949, Serial No. 81,157
In Great Britain March 16, 1948 i This invention relates to spinnerettes such as are employed in the production of synthetic fibres and filaments for production of rayon, artificial silk, artificial wool and other similar materials. Spinnerettes of this character essentially include a jet or nozzle through which the substance or material for extrusion is expelled under pressure. It is important that the spinner- .ette jets should be made of a metallic substance which will resist erosion and any tendency to corrode.
Up to the present it has been proposed to make spinnerette jets from precious metal alloys, such for example as gold alloyed with up to 40% platinum; and also platinum alloyed with up to 15% of rhodium. In British Patent No. 563,648 there is disclosed an alloy for a spinnerette in which platinum and rhodium are combined with ruthenium. These platinum-rich alloys have been found particularly advantageous as compared with the known gold-rich gold platinum alloys in that they possess the highest possible resistance to corrosion and can be produced with a very fine grain, which enables the holes to be accurately drilled and the walls to be given a very high polish.
It is an object of the present invention to devise a superior precious metal alloy for constructing spinnerette jets which will retain all the advantages of the platinum-rich alloys referred to above but which will have in addition a very high hardness. This is achieved by employing alloys of platinum with rhodium and gold which are age-hardening, and it is therefore possible to make a sheet of the alloy in a reasonably soft condition to allow mechanical forming of the spinnerette cups and drilling of the holes. The formed spinnerettes can then be hardened by heat treatment.
In accordance with the present invention, spinnerette jets are made from an alloy of platinum with rhodium and gold, which alloy contains 4 to 15% of gold, 5 to of rhodium and the balance of platinum, the proportions being so selected that for gold contents less than 5% the minimum rhodium content is increased above 5% by an amount equal to five times the amount by which the gold content is below 5%. Thus with a gold content of 4.5% the rhodium must be not less than 7.5 and with 4% gold the rhodium must be not less than 10%. When both rhodium and gold are present in quantities approaching the stated maxima the hardness oi the allow in the softest condition is increased so that the forming and drilling operations become difficult.
seams. (01. 18 -8),
For practical purposes the total gold and rhodium content preferably should not exceed about 25%. Whereas with the previously known platinumrich alloys it was not feasible to produce jets having a finished hardness greater than about 200 .V. P. N., jets made according to the present invention can be produced with a hardness of 400 V. P. N. or even higher.
The above alloys are shown in the drawing which represents a graph or diagram thereof.
To show how the invention may be carried into effect several examples will now be given.
Example I In this example, an alloy is prepared containing:
% platinum '7 rhodium 7 Vs gold The alloy is produced in sheet form and is treated by raising it to a temperature of about 1050 C. to1100 C.- for 15 minutes. It is then quenched in cold water and is thereafter mechanically formed by the production of the cup and the drilling thereof. The formed jet is then heated for l to 2 hours at a temperature of 620 to 650 C. and allowed to cool. The finished jet has a hardness of 350 to 400 V. P. N or better.
Example II In this example, an alloy is prepared contain- 1118:
85% platinum 5% gold 10% rhodium The process of producing the finished jet is substantially the same as in Example I and the hardness of the finished jet is about 450 V. P. N.
Example 17V In this example the proportions of the constituents of an alloy are chosen to be the same as those of Example I except that 20% of the platinum is replaced by palladium, the replacement being made atom for atom. It will of course be understood that the expresison "atom for atom is used to mean that 20% of the platinum is excluded and an amount of palladium containing an equivalent number of atoms is substituted. The weight of the palladium will thus be less than that of the platinum which it replaces. The alloy prepared in this way is processed in the manner described in Example I and the hardness of the finished jet will be of the order of 250 to 300 V. P. N.
It will be realised from cons deration of Example IV that it is possible to substitute under certain circumstances a certain amount of platinum by palladium. The alloy produced does not necessarily give as good results as those in which there is not substitution of platinum constituent but as will be appreciated it is often possible to substitute in a platinum-rich alloy a proportion of palladium without significantly altering the final desired properties of the alloy.
The proportions of the constituents of the alloys that may be used in the fulfilment of the invention are illustrated by reference to the. accompanying diagram. The diagram represents the conventional diagram for a ternary alloy. The horizontally hatched. portion includes within it those points which define the desired ratio of proportion between the three constituents. From the diagram it can be seen that as the gold constituent is reduced from to 4% the corresponding range for rhodium increases. Thus for an increment of reduction in the gold as between 5% and 4%, the minimum rhodium content increases by an increment that is five times as great as the first mentioned increment, thereby ensuring that when the gold constituent is reduced to 4% the minimum rhodium constituent has been increased to V I claim: v n V 1. A spinnerette of an alloy of platinum with rhodium and gold, which alloy contains 4 to of gold, 5 to 15% of rhodium and the balance of platinum, the proportions being so selected that for gold contents less than 5% the minimum rhodium content is increased above 5% by an 4 amount equal to five times the amount by which the gold content is below 5%.
2. A spinnerette as claimed in claim 1 wherein said alloy has a maximum aggregate amount of gold and rhodium equal to 25%.
3. A spinnerette as claimed in claim 2 wherein the alloy is age-hardened, said age-hardening being carried out after the spinnerette has been formed.
4. A spinnerette as claimed in claim 3 wherein the spinnerette is formed from a sheet of the alloy after the latter has been heat treated for approximately 15 minutes at 1050 to 1100 C. and quenched, the formed spinnerette being then heated for 1 to 2 hours at 620 to 650 C. and allowed to cool.
5. A spinnerette as set forth in claim 1 wherein the platinum content is replaced to anextent of not more than 20% by an atom for atom quantity of palladium.
. ARTHUR GORDON DOWSON.
REFERENCES CITED" The following references are of record in the file of this patent:
UNITED STATES PATENTS OTHER REFERENCES Rhodes, treatise in Metal Industry, May ll, 1945, pages 290, 291.
Claims (1)
1. A SPINNERETTE OF AN ALLOY OF PLATINUM WITH RHODIUM AND GOLD, WHICH ALLOY CONTAINS 4 TO 15% OF GOLD, 5 TO 15% OF RHODIUM AND THE BALANCE OF PLATINUM, THE PROPORTIONS BEING SO SELECTED THAT FOR GOLD CONTENTS LESS THAN 50% THE MINIUM RHODIUM CONTENT IS INCREASED ABOVE 5% BY AN AMOUNT EQUAL TO FIVE TIMES THE AMOUNT BY WHICH THE GOLD CONTENT IS BELOW 5%.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB280429X | 1948-03-16 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2566283A true US2566283A (en) | 1951-08-28 |
Family
ID=586724
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US81157A Expired - Lifetime US2566283A (en) | 1948-03-16 | 1949-03-12 | Spinnerette |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US2566283A (en) |
| CH (1) | CH280429A (en) |
| DE (1) | DE812842C (en) |
| FR (1) | FR983234A (en) |
| NL (1) | NL72535C (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2923969A (en) * | 1960-02-09 | Certificate of correction | ||
| US2938788A (en) * | 1958-02-20 | 1960-05-31 | Ruthardt Konrad | Spinning nozzles |
| US2967792A (en) * | 1953-12-01 | 1961-01-10 | Heraeus Gmbh W C | Spinnerette |
| US3904740A (en) * | 1972-03-30 | 1975-09-09 | Engelhard Min & Chem | Catalyst and process for ammonia oxidation |
| US4155730A (en) * | 1977-01-29 | 1979-05-22 | W. C. Heraeus Gmbh | Alloys for jets, nozzles, and perforated base plates for producing glass fibers |
| US5472333A (en) * | 1992-11-09 | 1995-12-05 | Elephant Edelmetaal B.V. | Spinnerette from gold-platinum-palladium-rhodium alloy |
| US20090218647A1 (en) * | 2008-01-23 | 2009-09-03 | Ev Products, Inc. | Semiconductor Radiation Detector With Thin Film Platinum Alloyed Electrode |
Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1323834A (en) * | 1919-12-02 | Adolph cohjst | ||
| US1378996A (en) * | 1920-07-17 | 1921-05-24 | Baker & Co Inc | Alloy |
| US1515464A (en) * | 1920-12-14 | 1924-11-11 | Dentists Supply Co | Alloy |
| DE585545C (en) * | 1930-10-21 | 1933-10-05 | Heraeus Gmbh W C | Palladium alloys containing rhodium |
| US2071216A (en) * | 1935-05-13 | 1937-02-16 | Johnson Matthey Co Ltd | Precious metal alloys |
| FR825702A (en) * | 1937-08-17 | 1938-03-11 | Siebert G M B H G | Spinning nozzle |
| GB489375A (en) * | 1937-01-26 | 1938-07-26 | Mond Nickel Co Ltd | Improvements in spinnerets |
| US2135611A (en) * | 1933-12-20 | 1938-11-08 | Du Pont | Spinneret |
| GB511513A (en) * | 1938-02-18 | 1939-08-21 | Alan Richard Powell | Improvements in or relating to precious metal alloys for use at high temperatures |
| US2273806A (en) * | 1941-04-24 | 1942-02-17 | Int Nickel Co | Platinum alloy |
| US2384502A (en) * | 1942-11-21 | 1945-09-11 | American Platinum Works | Method of preventing corrosion by phosphorus |
-
0
- NL NL72535D patent/NL72535C/xx active
-
1949
- 1949-03-04 DE DEP35683D patent/DE812842C/en not_active Expired
- 1949-03-12 US US81157A patent/US2566283A/en not_active Expired - Lifetime
- 1949-03-15 CH CH280429D patent/CH280429A/en unknown
- 1949-03-16 FR FR983234D patent/FR983234A/en not_active Expired
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1323834A (en) * | 1919-12-02 | Adolph cohjst | ||
| US1378996A (en) * | 1920-07-17 | 1921-05-24 | Baker & Co Inc | Alloy |
| US1515464A (en) * | 1920-12-14 | 1924-11-11 | Dentists Supply Co | Alloy |
| DE585545C (en) * | 1930-10-21 | 1933-10-05 | Heraeus Gmbh W C | Palladium alloys containing rhodium |
| US2135611A (en) * | 1933-12-20 | 1938-11-08 | Du Pont | Spinneret |
| US2071216A (en) * | 1935-05-13 | 1937-02-16 | Johnson Matthey Co Ltd | Precious metal alloys |
| GB489375A (en) * | 1937-01-26 | 1938-07-26 | Mond Nickel Co Ltd | Improvements in spinnerets |
| FR825702A (en) * | 1937-08-17 | 1938-03-11 | Siebert G M B H G | Spinning nozzle |
| GB511513A (en) * | 1938-02-18 | 1939-08-21 | Alan Richard Powell | Improvements in or relating to precious metal alloys for use at high temperatures |
| US2273806A (en) * | 1941-04-24 | 1942-02-17 | Int Nickel Co | Platinum alloy |
| US2384502A (en) * | 1942-11-21 | 1945-09-11 | American Platinum Works | Method of preventing corrosion by phosphorus |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2923969A (en) * | 1960-02-09 | Certificate of correction | ||
| US2967792A (en) * | 1953-12-01 | 1961-01-10 | Heraeus Gmbh W C | Spinnerette |
| US2938788A (en) * | 1958-02-20 | 1960-05-31 | Ruthardt Konrad | Spinning nozzles |
| US3904740A (en) * | 1972-03-30 | 1975-09-09 | Engelhard Min & Chem | Catalyst and process for ammonia oxidation |
| US4155730A (en) * | 1977-01-29 | 1979-05-22 | W. C. Heraeus Gmbh | Alloys for jets, nozzles, and perforated base plates for producing glass fibers |
| US5472333A (en) * | 1992-11-09 | 1995-12-05 | Elephant Edelmetaal B.V. | Spinnerette from gold-platinum-palladium-rhodium alloy |
| US20090218647A1 (en) * | 2008-01-23 | 2009-09-03 | Ev Products, Inc. | Semiconductor Radiation Detector With Thin Film Platinum Alloyed Electrode |
| US8896075B2 (en) | 2008-01-23 | 2014-11-25 | Ev Products, Inc. | Semiconductor radiation detector with thin film platinum alloyed electrode |
Also Published As
| Publication number | Publication date |
|---|---|
| NL72535C (en) | |
| CH280429A (en) | 1952-01-31 |
| FR983234A (en) | 1951-06-20 |
| DE812842C (en) | 1951-09-06 |
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