EP0224764B1 - Dispositif compensateur de force axiale pour pompes à fluide - Google Patents
Dispositif compensateur de force axiale pour pompes à fluide Download PDFInfo
- Publication number
- EP0224764B1 EP0224764B1 EP86115684A EP86115684A EP0224764B1 EP 0224764 B1 EP0224764 B1 EP 0224764B1 EP 86115684 A EP86115684 A EP 86115684A EP 86115684 A EP86115684 A EP 86115684A EP 0224764 B1 EP0224764 B1 EP 0224764B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- sleeve
- bores
- gap
- equalizer
- equalizer according
- 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
- 239000012530 fluid Substances 0.000 title description 15
- 239000007788 liquid Substances 0.000 claims abstract description 20
- 230000002093 peripheral effect Effects 0.000 claims description 2
- 230000035515 penetration Effects 0.000 description 2
- 241001295925 Gegenes Species 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 230000003472 neutralizing effect Effects 0.000 description 1
- 230000010355 oscillation Effects 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
Images
Classifications
-
- 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
- F01D25/04—Antivibration arrangements
-
- 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
- F01D3/00—Machines or engines with axial-thrust balancing effected by working-fluid
- F01D3/04—Machines or engines with axial-thrust balancing effected by working-fluid axial thrust being compensated by thrust-balancing dummy piston or the like
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/04—Shafts or bearings, or assemblies thereof
- F04D29/041—Axial thrust balancing
- F04D29/0416—Axial thrust balancing balancing pistons
Definitions
- the invention relates to an axial thrust compensation device for a liquid pump, which essentially consists of a fixed sleeve and a relief piston rotating in this sleeve and firmly connected to the impeller shaft, and to the use of such an axial thrust compensation device.
- Such devices are used in liquid pumps, in particular in multi-stage high-performance radial pumps, and have the purpose and the task of neutralizing or reducing large axial thrust forces.
- the patent specification DE-C 611 232 describes a device for axle thrust relief, in which the working fluid flowing through the gap between the relief piston and the bushing is discharged via drain openings in the bushing and relief holes.
- the published patent application DE-A 1 940 555 describes an encapsulated centrifugal pump in which an intermediate wall is arranged on both sides of the rotor in the rotor space of the housing.
- the partition wall and the housing wall form a second channel for the working fluid.
- the rotor each has a groove which, when the rotor is displaced in the axial direction, changes the flow in the rotor space in such a way that the centering forces acting on the rotor are increased.
- the construction is self-centering.
- French patent FR-A 1 276 208 describes a centrifugal pump in which the actual pump wheel lies between unevenly sized pressure surfaces of the axial thrust compensation device.
- An axial thrust compensation device consists of a rotating pressure compensation or relief piston which is firmly connected to the pump impeller and which runs in a fixed sleeve without contact.
- the sleeve can be designed as a separate part that is firmly connected to the housing.
- the relief piston itself can be designed as part of the pump rotor shaft or can be rigidly connected to the rotor shaft as a separate part.
- the axial thrust compensation device is arranged downstream of the last stage in the direction of the following pump stages.
- the pressure conditions in the area of the axial thrust compensating device in the liquid are such that, in the operating state, working liquid constantly flows from the impeller side space to and through the gap between the bushing and the relief piston.
- This liquid is set in rotation in the impeller side space, the intensity of which increases with the flow rate through the gap.
- the working medium therefore enters the gap with a peripheral component. This rotation of the working fluid can interfere with the maximum performance of the pump by increasing the tendency of the rotor to natural vibrations.
- the object of the invention is to completely prevent the penetration of liquid on the pump wheel side with pre-rotation into the gap and to supply liquid without pre-rotation to the gap without complex additional devices.
- the invention as characterized in the claims, solves this problem with the aid of the flowing partial flow from the gap into the impeller side space. Since only pre-rotation-free liquid is fed into the gap via the channels, the rotational movement of the liquid through the gap into the gap space facing away from the pump wheel is reduced, which in turn reduces the tendency of the pump rotor to natural vibrations in the limit load range and thus permits higher pump outputs with the same dimensions of the pump rotor shaft .
- a device according to the invention has particular advantages for multi-stage, high-speed high-pressure radial pumps such as Boiler feed pumps.
- the figure shows schematically in section a part of the last two stages of a radial pump with an axial thrust compensation device.
- the schematic section through the housing and rotor of the last two stages of a radial pump shows the one-part or multi-part, fixed pump housing 1 and the two pump wheels 2, 3, which are rigidly connected to the pump wheel shaft 4.
- the direction of flow of the liquid in the channels 22, 23 of the pump wheels 2, 3, in the pump wheel adjoining rooms 12, 21, 31 and in the main flow channels 11 is indicated by arrows.
- the axial thrust compensation device consists of the bush 5, which is fixedly connected to the housing, and the relief piston 6, which is rigidly connected to the rotor shaft 4 and rotates in the bush 5.
- the sleeve 5 has bores 51, only one of which is shown, which open into an internal groove 52, which in turn opens into the gap 56 between the sleeve 5 and the relief piston 6.
- the bores in the recess 15 are connected to the wheel side space 31 on the outside of the bush 5.
- the outer and inner diameter (D 2 , Di) of the sleeve 5 and the outer diameter (Ds) of the relief piston 6 are the flows conditions in this area as shown by the arrows.
- the embodiment of the invention suitable for a particular type of pump can be determined by a pump specialist without any problems.
- the groove 52 has the task of uniformly supplying the working fluid to the gap 56 over the circumference of the compensating piston 6 and thus, seen over the circumference, to create pressure conditions which are as balanced as possible. However, it is also conceivable that the groove 52 is completely absent and the bores 51 open directly into the gap 56.
- the working fluid is supplied to the bores 51 via the recess 15.
- the recess 15 is missing and the bores 51 are connected directly to the pump wheel side space 31 through lateral bores in the bushing 5 (not shown here) or inclined bores in the housing 1.
- the rotation of the pump wheel 3 generates a rotating flow of the working fluid in the wheel side space 31 and thus an outward radial pressure gradient.
- the ratios must now be selected so that in the operating state the radial pressure difference in the side space 31 between the sleeve outer and inner diameter (D 2 , D 1 ) is greater than the pressure loss in the bores 51 and groove 52 with a flow rate (Qi) alone, ie that part of the flow (Q) which flows in the gap 56 towards the end of the gap 56 facing the pump wheel. If this condition is met, a ram flow (Q 2 ) flows from the mouth to the end of the pump impeller end into the impeller side space 31, which at the same time completely prevents the penetration of working fluid with pre-rotation into the gap 56.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Non-Positive-Displacement Pumps (AREA)
- Rotary Pumps (AREA)
Claims (10)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH5066/85 | 1985-11-27 | ||
CH5066/85A CH669241A5 (de) | 1985-11-27 | 1985-11-27 | Axialschub-ausgleichsvorrichtung fuer fluessigkeitspumpe. |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0224764A1 EP0224764A1 (fr) | 1987-06-10 |
EP0224764B1 true EP0224764B1 (fr) | 1989-05-03 |
Family
ID=4287365
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP86115684A Expired EP0224764B1 (fr) | 1985-11-27 | 1986-11-12 | Dispositif compensateur de force axiale pour pompes à fluide |
Country Status (5)
Country | Link |
---|---|
US (1) | US4892459A (fr) |
EP (1) | EP0224764B1 (fr) |
CH (1) | CH669241A5 (fr) |
DE (1) | DE3663165D1 (fr) |
FI (1) | FI93259C (fr) |
Families Citing this family (36)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5104284A (en) * | 1990-12-17 | 1992-04-14 | Dresser-Rand Company | Thrust compensating apparatus |
FR2687429B1 (fr) * | 1992-02-17 | 1994-04-01 | Gec Alsthom Sa | Procede et dispositif pour supprimer l'instabilite d'une turbine a vapeur. |
DE4313455A1 (de) * | 1993-04-24 | 1994-10-27 | Klein Schanzlin & Becker Ag | Radialer Spalt, beispielsweise einer Strömungsmaschine |
DE29500744U1 (de) * | 1995-01-18 | 1996-05-15 | Sihi Ind Consult Gmbh | Strömungsmaschine mit Entlastungskolben |
JPH09324791A (ja) * | 1996-06-07 | 1997-12-16 | Ebara Corp | サブマージドモータポンプ |
US6012898A (en) * | 1996-06-07 | 2000-01-11 | Ebara Corporation | Submerged motor pump |
US6129507A (en) | 1999-04-30 | 2000-10-10 | Technology Commercialization Corporation | Method and device for reducing axial thrust in rotary machines and a centrifugal pump using same |
JP4281614B2 (ja) * | 2004-05-10 | 2009-06-17 | 株式会社日立プラントテクノロジー | ポンプ装置 |
US7794199B2 (en) * | 2005-05-24 | 2010-09-14 | Franklin Electric Co., Inc. | Bypass system for purging air from a submersible pump |
US20090004032A1 (en) * | 2007-03-29 | 2009-01-01 | Ebara International Corporation | Deswirl mechanisms and roller bearings in an axial thrust equalization mechanism for liquid cryogenic turbomachinery |
EP2154332A1 (fr) * | 2008-08-14 | 2010-02-17 | Siemens Aktiengesellschaft | Réduction de la charge thermique d'un boîtier extérieur pour une turbomachine |
US9014791B2 (en) | 2009-04-17 | 2015-04-21 | Echogen Power Systems, Llc | System and method for managing thermal issues in gas turbine engines |
MX2012000059A (es) | 2009-06-22 | 2012-06-01 | Echogen Power Systems Inc | Sistema y metodo para manejar problemas termicos en uno o mas procesos industriales. |
WO2011017476A1 (fr) | 2009-08-04 | 2011-02-10 | Echogen Power Systems Inc. | Pompe à chaleur avec collecteur solaire intégré |
US8813497B2 (en) | 2009-09-17 | 2014-08-26 | Echogen Power Systems, Llc | Automated mass management control |
US8613195B2 (en) | 2009-09-17 | 2013-12-24 | Echogen Power Systems, Llc | Heat engine and heat to electricity systems and methods with working fluid mass management control |
US8794002B2 (en) | 2009-09-17 | 2014-08-05 | Echogen Power Systems | Thermal energy conversion method |
US8869531B2 (en) | 2009-09-17 | 2014-10-28 | Echogen Power Systems, Llc | Heat engines with cascade cycles |
RU2451920C1 (ru) * | 2010-11-23 | 2012-05-27 | Открытое акционерное общество Научно-производственное объединение "Искра" | Экспериментальная установка для исследования модельных ступеней центробежных компрессоров |
US8857186B2 (en) | 2010-11-29 | 2014-10-14 | Echogen Power Systems, L.L.C. | Heat engine cycles for high ambient conditions |
US8616001B2 (en) | 2010-11-29 | 2013-12-31 | Echogen Power Systems, Llc | Driven starter pump and start sequence |
WO2013055391A1 (fr) | 2011-10-03 | 2013-04-18 | Echogen Power Systems, Llc | Cycle de réfrigération du dioxyde de carbone |
WO2014031526A1 (fr) | 2012-08-20 | 2014-02-27 | Echogen Power Systems, L.L.C. | Circuit de fluide de travail super critique comprenant une turbopompe et une pompe de démarrage en une configuration en série |
US9341084B2 (en) | 2012-10-12 | 2016-05-17 | Echogen Power Systems, Llc | Supercritical carbon dioxide power cycle for waste heat recovery |
US9118226B2 (en) | 2012-10-12 | 2015-08-25 | Echogen Power Systems, Llc | Heat engine system with a supercritical working fluid and processes thereof |
US9638065B2 (en) | 2013-01-28 | 2017-05-02 | Echogen Power Systems, Llc | Methods for reducing wear on components of a heat engine system at startup |
CA2899163C (fr) | 2013-01-28 | 2021-08-10 | Echogen Power Systems, L.L.C. | Procede de commande d'un robinet de debit d'une turbine de travail au cours d'un cycle de rankine supercritique au dioxyde de carbone |
AU2014225990B2 (en) | 2013-03-04 | 2018-07-26 | Echogen Power Systems, L.L.C. | Heat engine systems with high net power supercritical carbon dioxide circuits |
WO2016073252A1 (fr) | 2014-11-03 | 2016-05-12 | Echogen Power Systems, L.L.C. | Gestion de poussée active d'une turbopompe à l'intérieur d'un circuit de circulation de fluide de travail supercritique dans un système de moteur thermique |
EP3121450B1 (fr) * | 2015-07-23 | 2020-09-02 | Sulzer Management AG | Pompe de transport d'un fluide présentant une viscosité variable |
US10883388B2 (en) | 2018-06-27 | 2021-01-05 | Echogen Power Systems Llc | Systems and methods for generating electricity via a pumped thermal energy storage system |
CN113227583B (zh) * | 2018-09-27 | 2023-08-08 | Ksb股份有限公司 | 具有轴向推力优化的多级泵 |
EP3896288A1 (fr) * | 2020-04-16 | 2021-10-20 | Sulzer Management AG | Pompe centrifuge pour transporter un fluide |
US11435120B2 (en) | 2020-05-05 | 2022-09-06 | Echogen Power Systems (Delaware), Inc. | Split expansion heat pump cycle |
WO2022125816A1 (fr) | 2020-12-09 | 2022-06-16 | Supercritical Storage Company, Inc. | Système de stockage d'énergie thermique électrique à trois réservoirs |
KR102567992B1 (ko) * | 2021-08-09 | 2023-08-18 | 터보윈 주식회사 | 베어링마모요인추력저감보정부가 적용된 공기 압축 수단 |
Family Cites Families (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE611232C (de) * | 1935-03-25 | Klein | Einrichtung zur Achsschubentlastung an Kreiselpumpen | |
DE539225C (de) * | 1931-11-26 | Georg Weyland | Axialschubentlastung mittels stufenfoermiger Entlastungsscheiben | |
DE390366C (de) * | 1924-02-18 | Paul Joseph Charles Marechal | Entlastungsvorrichtung an Turbomaschinen | |
DE407077C (de) * | 1920-11-06 | 1924-12-10 | Paul Joseph Charles Marechal | Entlastungsvorrichtung fuer Turbinen |
US2410769A (en) * | 1941-05-07 | 1946-11-05 | Vickers Electrical Co Ltd | Turbine, turbine type compressor, and the like rotating machine |
DE922807C (de) * | 1945-03-06 | 1955-01-24 | Aeg | Einrichtung zum Ausgleich des Axialschubes mehrstufiger Kreiselpumpen |
DE1147120B (de) * | 1959-10-28 | 1963-04-11 | Siemens Ag | Einrichtung zum Ausgleich des Axialschubes bei einer unter Fluessigkeit arbeitenden Kreiselpumpe |
FR1276208A (fr) * | 1960-12-14 | 1961-11-17 | Pompe sans bourrage ni presse-étoupe avec passage du liquide par une section intérieure du palier d'entrée | |
US3280750A (en) * | 1964-09-17 | 1966-10-25 | Crane Co | Motor driven pump |
US3393947A (en) * | 1966-04-13 | 1968-07-23 | United Aircraft Corp | Two-directional axial thrust balancer |
US3565543A (en) * | 1969-04-02 | 1971-02-23 | United Aircraft Corp | Pressure balanced starter rotor |
DE1940555C3 (de) * | 1969-08-08 | 1975-11-27 | Spezialnoje Konstruktorskoje Bjuro Po Projektirowaniju Germetitscheskich Elektronasosow I Elektrodwigateljej, Kisinew (Sowjetunion) | Stopfbuchslose Zentrifugalpumpe |
US3614255A (en) * | 1969-11-13 | 1971-10-19 | Gen Electric | Thrust balancing arrangement for steam turbine |
US3671137A (en) * | 1970-06-22 | 1972-06-20 | Borg Warner | Centrifugal pump with hydrostatic bearing |
DE2413655C3 (de) * | 1974-03-21 | 1978-05-03 | Maschinenfabrik Augsburg-Nuernberg Ag, 8500 Nuernberg | Einrichtung zum dynamischen Stabilisieren des Läufers einer Gas- oder Dampfturbine |
US4121839A (en) * | 1976-08-18 | 1978-10-24 | Mitsui Toatsu Chemicals, Inc. | Sealing system for use in composite multi-stage pump |
US4170435A (en) * | 1977-10-14 | 1979-10-09 | Swearingen Judson S | Thrust controlled rotary apparatus |
DE2757952C2 (de) * | 1977-12-24 | 1983-02-24 | Sihi Gmbh & Co Kg, 2210 Itzehoe | Selbstansaugende Kreiselpumpe |
JPS5872693A (ja) * | 1981-10-28 | 1983-04-30 | Hitachi Ltd | 軸推力平衡装置 |
-
1985
- 1985-11-27 CH CH5066/85A patent/CH669241A5/de not_active IP Right Cessation
-
1986
- 1986-10-28 FI FI864381A patent/FI93259C/fi not_active IP Right Cessation
- 1986-11-12 EP EP86115684A patent/EP0224764B1/fr not_active Expired
- 1986-11-12 DE DE8686115684T patent/DE3663165D1/de not_active Expired
-
1988
- 1988-12-13 US US07/283,612 patent/US4892459A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
FI93259C (fi) | 1995-03-10 |
EP0224764A1 (fr) | 1987-06-10 |
DE3663165D1 (en) | 1989-06-08 |
FI864381A0 (fi) | 1986-10-28 |
FI93259B (fi) | 1994-11-30 |
CH669241A5 (de) | 1989-02-28 |
FI864381A (fi) | 1987-05-28 |
US4892459A (en) | 1990-01-09 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0224764B1 (fr) | Dispositif compensateur de force axiale pour pompes à fluide | |
DE69004975T2 (de) | Pumpenlaufrad. | |
EP0750720B1 (fr) | Turbomachine avec piston d'allegement | |
DE3231171C1 (de) | Sperrfluessigkeitsdichtung | |
DE6608771U (de) | Lager fuer schnell umlaufende maschinen, vorzugsweise turbolader. | |
EP0934466A1 (fr) | Pompe d'alimentation | |
EP1327802B1 (fr) | Dispositif de joint hydraulique | |
DE4200687A1 (de) | Radiallager | |
DE2533804B2 (de) | Lager fuer den rotor einer oe-spinnmaschine | |
DE69621868T2 (de) | Seitenkanalbrennstoffpumpe für Kraftfahrzeug | |
DE19850920A1 (de) | Radialkolbenpumpe | |
DE69716552T2 (de) | Dichtung/lagervorrichtung | |
EP1495227A2 (fr) | Groupe motopompe hydraulique | |
DE10238415B4 (de) | Gleitlager für eine Welle eines Abgasturboladers | |
DE2539425C2 (fr) | ||
DE102016124283A1 (de) | Hydrodynamische Kupplung | |
DE1703077A1 (de) | Hydraulische Zahnradpumpe oder Zahnradmotor | |
DE102009007696A1 (de) | Lageranordnung | |
DE1728310A1 (de) | Druckmitteluebertragungseinrichtung | |
EP0461131B1 (fr) | Dispositif d'equilibrage de poussees axiales | |
DE102017106942A1 (de) | Hydrodynamische Kupplung | |
DE2117766A1 (de) | Hochdruckkreiselpumpe | |
DE1528717B2 (de) | Vorrichtung zum ausgleich des axialschubes bei mehrstufigen kreiselpumpen | |
DE19621773A1 (de) | Außendruckluftlagerspindel | |
DE2633481A1 (de) | Radialgleitlager fuer die welle schnell laufender maschinen, insbesondere fuer abgasturbolader |
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): BE DE FR GB IT NL SE |
|
17P | Request for examination filed |
Effective date: 19870613 |
|
17Q | First examination report despatched |
Effective date: 19880315 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
ITF | It: translation for a ep patent filed | ||
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): BE DE FR GB IT NL SE |
|
GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) | ||
REF | Corresponds to: |
Ref document number: 3663165 Country of ref document: DE Date of ref document: 19890608 |
|
ET | Fr: translation filed | ||
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 | ||
ITTA | It: last paid annual fee | ||
EAL | Se: european patent in force in sweden |
Ref document number: 86115684.2 |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: IF02 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20051110 Year of fee payment: 20 Ref country code: DE Payment date: 20051110 Year of fee payment: 20 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: NL Payment date: 20051114 Year of fee payment: 20 Ref country code: SE Payment date: 20051114 Year of fee payment: 20 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20051121 Year of fee payment: 20 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: IT Payment date: 20051122 Year of fee payment: 20 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: BE Payment date: 20051216 Year of fee payment: 20 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION Effective date: 20061111 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION Effective date: 20061112 |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: PE20 |
|
NLV7 | Nl: ceased due to reaching the maximum lifetime of a patent |
Effective date: 20061112 |
|
EUG | Se: european patent has lapsed | ||
BE20 | Be: patent expired |
Owner name: *GEBRUDER SULZER A.G. Effective date: 20061112 |