EP0201602B1 - Ring für spinnmaschinen - Google Patents
Ring für spinnmaschinen Download PDFInfo
- Publication number
- EP0201602B1 EP0201602B1 EP85904861A EP85904861A EP0201602B1 EP 0201602 B1 EP0201602 B1 EP 0201602B1 EP 85904861 A EP85904861 A EP 85904861A EP 85904861 A EP85904861 A EP 85904861A EP 0201602 B1 EP0201602 B1 EP 0201602B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- ring
- spinning
- flange
- less
- flange portion
- 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
- 238000009987 spinning Methods 0.000 title claims abstract description 28
- 239000000919 ceramic Substances 0.000 claims description 13
- 239000011247 coating layer Substances 0.000 claims description 13
- 229910000975 Carbon steel Inorganic materials 0.000 claims description 11
- 239000010962 carbon steel Substances 0.000 claims description 11
- 230000003746 surface roughness Effects 0.000 claims description 9
- 229910000851 Alloy steel Inorganic materials 0.000 claims description 7
- 239000010410 layer Substances 0.000 claims description 7
- 238000007747 plating Methods 0.000 claims description 5
- 239000011159 matrix material Substances 0.000 claims description 4
- 229910000990 Ni alloy Inorganic materials 0.000 claims description 3
- 238000009713 electroplating Methods 0.000 claims description 3
- 239000000126 substance Substances 0.000 claims description 3
- 229910018104 Ni-P Inorganic materials 0.000 claims 1
- 229910018536 Ni—P Inorganic materials 0.000 claims 1
- 239000002245 particle Substances 0.000 claims 1
- 238000005524 ceramic coating Methods 0.000 abstract description 13
- 229910010293 ceramic material Inorganic materials 0.000 abstract description 9
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 14
- 235000019589 hardness Nutrition 0.000 description 13
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 9
- MTPVUVINMAGMJL-UHFFFAOYSA-N trimethyl(1,1,2,2,2-pentafluoroethyl)silane Chemical compound C[Si](C)(C)C(F)(F)C(F)(F)F MTPVUVINMAGMJL-UHFFFAOYSA-N 0.000 description 9
- 229910010271 silicon carbide Inorganic materials 0.000 description 8
- 238000000034 method Methods 0.000 description 7
- 229910052759 nickel Inorganic materials 0.000 description 7
- 238000012360 testing method Methods 0.000 description 6
- NRTOMJZYCJJWKI-UHFFFAOYSA-N Titanium nitride Chemical compound [Ti]#N NRTOMJZYCJJWKI-UHFFFAOYSA-N 0.000 description 5
- 239000013078 crystal Substances 0.000 description 5
- 238000005299 abrasion Methods 0.000 description 4
- 238000005229 chemical vapour deposition Methods 0.000 description 4
- 238000009826 distribution Methods 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 239000002344 surface layer Substances 0.000 description 4
- 238000000576 coating method Methods 0.000 description 3
- 238000005520 cutting process Methods 0.000 description 3
- 238000000227 grinding Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- OFNHPGDEEMZPFG-UHFFFAOYSA-N phosphanylidynenickel Chemical compound [P].[Ni] OFNHPGDEEMZPFG-UHFFFAOYSA-N 0.000 description 3
- 239000011148 porous material Substances 0.000 description 3
- 238000007378 ring spinning Methods 0.000 description 3
- 238000005266 casting Methods 0.000 description 2
- 239000011248 coating agent Substances 0.000 description 2
- 239000002131 composite material Substances 0.000 description 2
- 238000002425 crystallisation Methods 0.000 description 2
- 230000008025 crystallization Effects 0.000 description 2
- 239000000835 fiber Substances 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 229910001092 metal group alloy Inorganic materials 0.000 description 2
- 150000004767 nitrides Chemical class 0.000 description 2
- 238000005240 physical vapour deposition Methods 0.000 description 2
- 238000004381 surface treatment Methods 0.000 description 2
- 229910018072 Al 2 O 3 Inorganic materials 0.000 description 1
- 229920000742 Cotton Polymers 0.000 description 1
- 229920001651 Cyanoacrylate Polymers 0.000 description 1
- 229910001209 Low-carbon steel Inorganic materials 0.000 description 1
- MWCLLHOVUTZFKS-UHFFFAOYSA-N Methyl cyanoacrylate Chemical compound COC(=O)C(=C)C#N MWCLLHOVUTZFKS-UHFFFAOYSA-N 0.000 description 1
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 1
- 229910004298 SiO 2 Inorganic materials 0.000 description 1
- DUMHRFXBHXIRTD-UHFFFAOYSA-N Tantalum carbide Chemical compound [Ta+]#[C-] DUMHRFXBHXIRTD-UHFFFAOYSA-N 0.000 description 1
- OTCHGXYCWNXDOA-UHFFFAOYSA-N [C].[Zr] Chemical compound [C].[Zr] OTCHGXYCWNXDOA-UHFFFAOYSA-N 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 238000005255 carburizing Methods 0.000 description 1
- 229910003460 diamond Inorganic materials 0.000 description 1
- 239000010432 diamond Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 230000005496 eutectics Effects 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 238000010285 flame spraying Methods 0.000 description 1
- 238000009499 grossing Methods 0.000 description 1
- 238000007733 ion plating Methods 0.000 description 1
- 150000002500 ions Chemical class 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000000873 masking effect Effects 0.000 description 1
- 238000010002 mechanical finishing Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 229910052698 phosphorus Inorganic materials 0.000 description 1
- 239000011574 phosphorus Substances 0.000 description 1
- 238000007750 plasma spraying Methods 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 239000002861 polymer material Substances 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 239000002356 single layer Substances 0.000 description 1
- 238000005476 soldering Methods 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
- 238000005019 vapor deposition process Methods 0.000 description 1
Images
Classifications
-
- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01H—SPINNING OR TWISTING
- D01H1/00—Spinning or twisting machines in which the product is wound-up continuously
- D01H1/02—Spinning or twisting machines in which the product is wound-up continuously ring type
-
- D—TEXTILES; PAPER
- D01—NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
- D01H—SPINNING OR TWISTING
- D01H7/00—Spinning or twisting arrangements
- D01H7/02—Spinning or twisting arrangements for imparting permanent twist
- D01H7/52—Ring-and-traveller arrangements
- D01H7/60—Rings or travellers; Manufacture thereof not otherwise provided for ; Cleaning means for rings
- D01H7/602—Rings
Definitions
- the invention relates to a ring for spinning and twisting machines with a flange area, a neck area and a shaft area.
- Such rings are exposed to increased temperatures and increased abrasion during the spinning process due to the frictional contact between the ring flange, rotor and thread. This reduces the service life and the running properties of the ring.
- the hardened surface also results in a higher thread tension, which is particularly the case in high-speed operation with spindle speeds of more than 20,000 revolutions / min. leads to frequent thread breakage.
- the object of the invention is therefore to develop a ring for spinning and twisting machines, the service life and running properties of which are considerably improved, so that it can also be used without problems in high-performance spinning machines with a high spindle revolution.
- At least the flange area of the ring is formed from a fine ceramic material and that after the grain growth the fine ceramic material has a grain size of less than 10 pm and a surface roughness of less than 5 ⁇ m.
- the ring is made of a metal alloy, e.g. made of carbon steel, then, according to the teaching of the invention, at least the surface of the flange area should have a coating layer made of fine ceramic material, which has the aforementioned grain size and surface consistency.
- rings made of a metal alloy according to the teaching of the invention can also have a non-electrolytic plating layer which is produced as a matrix with a fine ceramic grain smaller than 3 ⁇ m grain size as a eutectoid substance and a nickel alloy which contains nickel phosphorus.
- Fig. 1 shows a cross section through a preferred embodiment of a ring for a spinning machine according to the invention.
- the ring 5 comprises a flange part 1, a neck region 2 and a shaft region 4 with a ring rail fitting region 3.
- At least the part that is in contact with a rotor, that is, the flange portion 1 of the ring, is made by casting in the desired shape, using ceramic grain material selected from oxide, carbide, nitride, boride or other groups, e.g. SiC, Si 3 N 4 , Al 2 0 3 , Zr0 2 , TiC, TiN etc.
- the ceramic flange thus obtained is subjected to fire treatment at a high temperature to have a hardness of 1000 to 3500 Hv and a grain diameter after the growth of the crystal grain to get less than 10 pm.
- the neck region 2 and the shaft region 4, which carries the ring rail fitting region 3, consist of carbon steel, alloy steel, light metal or a high polymer material in the desired shape and are produced by mechanical processing or by casting molds.
- a smooth surface finish is transferred to the surface of the ceramic flange described above by physical or mechanical finishing methods such as cylinder grinding, lapping or polishing etc. so that the surface roughness is less than 5 pm and preferably less than 1 pm.
- ceramic materials is not limited to the flange area of the ring, but it can be made entirely of the ceramic material.
- 3A and 3B show a ring for a spinning machine, the flange area of which bears a ceramic coating layer.
- This ring 5 is made of carbon steel, a steel alloy, light metal, plastic, composite materials or the like.
- a ceramic coating layer 6 was formed on the surface of the ring where it is in contact with the rotor by a coating method such as CVD (chemical vapor deposition Process) including a plasma spraying process and an optical CVD, PVD (physical vapor deposition process) including vacuum plating and spraying, IVD (ion vapor deposition process), flame spraying, firing, etc.
- a ceramic coating layer 8 was formed by composite plating, or by uniformly dispersing the ceramic grain, using the ceramic grain 7 as a eutectic substance and a nickel alloy containing nickel and phosphorus as a matrix.
- the ceramic coating layer described above can be applied to the entire surface of a ring, but it is also sufficient to apply it only to the surface area which is in contact with a rotor, which surface area is subjected to a masking treatment before the coating.
- Ceramic materials that can be used according to the invention alone or in combination with others are Al 2 O 3 , ZrO 2 , SiO 2 , Ti0 2 , In 2 0 31 ZaO, Cr 2 0 3 , SiO, TiO, MgO, BeO , Th0 2 , etc. as oxide groups, SiC, TiC, TaC, ZrC, WC, HfC, B 4 C, NbC, C (diamond) etc. as carbide group, Si 3 N 4 , TiN, TiC, N. TaN, ZrN , AIN, GaN, BN, InN etc. as a nitride group and TiB 2 , ZrB 2 , HfB 2 , etc. as a boride group.
- the neck region 2 and the shaft region 4 with the ring rail fitting region 3 were produced mechanically, using carbon steel as the material.
- the flange portion 1 and the other portions have been joined together by soldering, or by means of an adhesive such as an epoxy resin, cyanoacrylate, etc., to manufacture the ring for a spinning machine according to the invention.
- the ring thus obtained was examined for wear by a wear testing machine under the following conditions.
- the ring A shows according to the invention a much smaller increase in the amount of wear over time than the conventional ring B.
- the flange portion made of silicon carbide (SiC) has high strength, high heat resistance, and high abrasion resistance.
- the silicon carbide flange portion has almost the same thermal conductivity as the metallic rotor, the heat generated by the sliding of the rotor can easily radiate, which contributes to a reduction in burning and wear of the rotor, and accordingly the lifespan of the runner is extended.
- the ring was carbored, it was subjected to an ion plating treatment by glow discharge at 1-5 ⁇ 10 -2 torr in a reigning gas atmosphere with C 2 H 2 as a main component to form a ceramic coating layer 6 of a thickness of 1 to 20 ⁇ m with titanium carbide (TiC ) on the surface that is in contact with the runner.
- a ceramic coating layer 6 of a thickness of 1 to 20 ⁇ m with titanium carbide (TiC ) on the surface that is in contact with the runner.
- TiC titanium carbide
- the ring C thus obtained has a hardness of 2500 to 3400 Hv, which is much higher than that of the conventional ring B which has been carburized and hardened, as shown in Fig. 4, which shows the curves of the cross-sectional hardness distribution.
- the ring C according to the invention shows only about 1/5 of the amount of wear, while the life is more than 5 times.
- the conventional ring B experiences an increase in thread tension due to the increase in friction between the ring and the rotor, causing yarn breakage, "flying" of the rotor and other troubles while it becomes difficult to run continuously.
- the ring according to the invention shows a reduction in the coefficient of friction, while no running-in is required and high-speed running can be carried out immediately after starting.
- FIG. 6 shows a cross section through the ring according to embodiment 3 of the invention.
- the flange 12 ring 12 shown in Fig. 6 was manufactured by a low carbon steel cutting process.
- the above ring was subjected to carburizing treatment and surface grinding, it was subjected to a chemical vapor deposition process at a temperature of 850 to 1050 ° C in a gas atmosphere with TiCl 4 , H 2 , CH 4 , N 2 as a main component to form a ceramic coating layer 13A of 2 to 20 ⁇ m in thickness, containing titanium carbide (TiC) and a ceramic coating layer 13B, 1 ⁇ m in thickness, containing titanium nitride (TiN) on the surface which comes into contact with the rotor.
- TiC titanium carbide
- TiN titanium nitride
- Fig. 9 shows a cross section of a ring according to embodiment 4 according to the invention.
- This ring was made of carbon steel, for example S15CK material, and formed into a simple flange 16 by means of a cutting process. It was subjected to carburization, quenching and surface treatment. A plated nickel layer 17 about 1 ⁇ m thick was applied to the surface of the ring by an electron nickel process, as shown in FIG. 10.
- FIG. 12 is a modification of the ring according to FIG. 1, a concave region 9 (FIG. 12A) being formed on the underside of the flange region 1, the flange region and the neck region being connected to one another to form the ring.
- a concave region 9 FIG. 12A
- connection and the adhesion of the two parts to each other is stronger.
- the sintered rings described above have a significantly improved abrasion resistance because they carry a single layer of several layers of the ceramic coating on the pore surface of the surface layer area.
- the spinning belt is drawn off from a drafting system, passes through a thread guide and is fed to the ring spinning machine, a twist being transferred to the belt by the rotor which is held on the ring according to the invention, the thread being placed around the bobbin.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Textile Engineering (AREA)
- Spinning Or Twisting Of Yarns (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP146976/84U | 1984-09-27 | ||
JP1984146976U JPH0248438Y2 (enrdf_load_stackoverflow) | 1984-09-27 | 1984-09-27 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0201602A1 EP0201602A1 (de) | 1986-11-20 |
EP0201602A4 EP0201602A4 (de) | 1987-01-20 |
EP0201602B1 true EP0201602B1 (de) | 1990-05-09 |
Family
ID=15419813
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP85904861A Expired - Lifetime EP0201602B1 (de) | 1984-09-27 | 1985-09-26 | Ring für spinnmaschinen |
Country Status (6)
Country | Link |
---|---|
US (1) | US4698958A (enrdf_load_stackoverflow) |
EP (1) | EP0201602B1 (enrdf_load_stackoverflow) |
JP (1) | JPH0248438Y2 (enrdf_load_stackoverflow) |
KR (1) | KR880700113A (enrdf_load_stackoverflow) |
DE (1) | DE3577583D1 (enrdf_load_stackoverflow) |
WO (1) | WO1986002113A1 (enrdf_load_stackoverflow) |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0643648B2 (ja) * | 1987-11-27 | 1994-06-08 | 金井重要工業株式会社 | 紡機用リング |
JPH0811848B2 (ja) * | 1987-12-28 | 1996-02-07 | 金井 宏之 | 紡機用リング |
JPH01321925A (ja) * | 1988-06-23 | 1989-12-27 | Kanai Jiyuuyou Kogyo Kk | 紡機用リング |
US5175988A (en) * | 1988-06-23 | 1993-01-05 | Kanai Juyo Kogyo Company Ltd. | Ring for spinning machinery |
US5160318A (en) * | 1989-02-23 | 1992-11-03 | Linvatec Corporation | Surgical cutting instrument with ceramic coating on an inner tubular member |
US5086615A (en) * | 1990-02-15 | 1992-02-11 | A. B. Carter, Inc. | Coated spinning rings and travelers |
DE4219197A1 (de) * | 1992-06-12 | 1993-12-16 | Zinser Textilmaschinen Gmbh | Ringe und Läufer von Spinn- und Zwirnmaschinen |
US5313773A (en) * | 1992-06-24 | 1994-05-24 | A. B. Carter, Inc. | Coatings for spinning applications and rings and travelers coated therewith |
DE4342148A1 (de) * | 1993-12-10 | 1995-06-14 | Cerasiv Gmbh | Ring-/Läufersystem für Spinn- und Zwirnmaschinen |
US5721055A (en) * | 1995-01-03 | 1998-02-24 | Surface Technology, Inc. | Lubricated textile spinning machinery parts |
EP0843034A3 (en) * | 1996-11-14 | 1999-02-17 | Howa Machinery, Ltd. | Rotary spinning ring structure |
US5829240A (en) * | 1997-03-17 | 1998-11-03 | A. B. Carter, Inc. | Spinning ring having improved traveler bearing surface |
US6360520B2 (en) | 2000-01-14 | 2002-03-26 | Ab Carter, Inc. | Spinning ring having amorphous chromium bearing surface |
US20060251910A1 (en) * | 2005-05-06 | 2006-11-09 | Lancsek Thomas S | Composite electroless plating |
US20090011136A1 (en) * | 2005-05-06 | 2009-01-08 | Thomas Steven Lancsek | Composite electroless plating |
US20070184271A1 (en) * | 2006-02-08 | 2007-08-09 | Feldstein Michael D | Coated textile machinery parts |
CH719102A1 (de) * | 2021-11-01 | 2023-05-15 | Braecker Ag | Spinn- oder Zwirnring sowie zugehöriger Ringläufer. |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US273090A (en) * | 1883-02-27 | Spinning-ring | ||
US1595858A (en) * | 1921-11-19 | 1926-08-10 | Crompton Randolph | Traveler ring and traveler for spinning or twister frames |
US1957041A (en) * | 1933-09-06 | 1934-05-01 | U S Ring Traveler Company | Ring holder and ring for travelers |
US2194930A (en) * | 1938-11-26 | 1940-03-26 | Edward F Feen | Glass spinning ring |
US2798357A (en) * | 1951-09-29 | 1957-07-09 | Rieter Joh Jacob & Cie Ag | Spinning ring |
US3118272A (en) * | 1962-06-08 | 1964-01-21 | Powdered metal bearings | |
US3421307A (en) * | 1964-12-24 | 1969-01-14 | Dana Corp | Bearing member having a composite coating |
-
1984
- 1984-09-27 JP JP1984146976U patent/JPH0248438Y2/ja not_active Expired
-
1985
- 1985-09-26 WO PCT/JP1985/000531 patent/WO1986002113A1/ja not_active Application Discontinuation
- 1985-09-26 US US06/848,380 patent/US4698958A/en not_active Expired - Fee Related
- 1985-09-26 EP EP85904861A patent/EP0201602B1/de not_active Expired - Lifetime
- 1985-09-26 DE DE8585904861T patent/DE3577583D1/de not_active Revoked
-
1986
- 1986-04-08 KR KR860700201A patent/KR880700113A/ko not_active Ceased
Also Published As
Publication number | Publication date |
---|---|
US4698958A (en) | 1987-10-13 |
EP0201602A1 (de) | 1986-11-20 |
JPS6164169U (enrdf_load_stackoverflow) | 1986-05-01 |
DE3577583D1 (de) | 1990-06-13 |
WO1986002113A1 (en) | 1986-04-10 |
EP0201602A4 (de) | 1987-01-20 |
KR880700113A (ko) | 1988-02-15 |
JPH0248438Y2 (enrdf_load_stackoverflow) | 1990-12-19 |
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