ATE333614T1 - Pufferdichtungsanordnung für ölwanne - Google Patents
Pufferdichtungsanordnung für ölwanneInfo
- Publication number
- ATE333614T1 ATE333614T1 AT00992000T AT00992000T ATE333614T1 AT E333614 T1 ATE333614 T1 AT E333614T1 AT 00992000 T AT00992000 T AT 00992000T AT 00992000 T AT00992000 T AT 00992000T AT E333614 T1 ATE333614 T1 AT E333614T1
- Authority
- AT
- Austria
- Prior art keywords
- buffer
- section
- sections
- buffer seal
- oil
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/44—Free-space packings
- F16J15/443—Free-space packings provided with discharge channels
-
- 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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
- F01D11/04—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type using sealing fluid, e.g. steam
-
- 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
- F01D25/18—Lubricating arrangements
- F01D25/183—Sealing means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/16—Sealings between relatively-moving surfaces
- F16J15/40—Sealings between relatively-moving surfaces by means of fluid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/60—Fluid transfer
- F05D2260/602—Drainage
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Sealing With Elastic Sealing Lips (AREA)
- Gasket Seals (AREA)
- Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/428,092 US6330790B1 (en) | 1999-10-27 | 1999-10-27 | Oil sump buffer seal |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE333614T1 true ATE333614T1 (de) | 2006-08-15 |
Family
ID=23697521
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT00992000T ATE333614T1 (de) | 1999-10-27 | 2000-10-19 | Pufferdichtungsanordnung für ölwanne |
Country Status (6)
Country | Link |
---|---|
US (1) | US6330790B1 (de) |
EP (1) | EP1307672B1 (de) |
AT (1) | ATE333614T1 (de) |
CA (1) | CA2389357C (de) |
DE (1) | DE60029487T2 (de) |
WO (1) | WO2001031235A2 (de) |
Families Citing this family (48)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6623238B2 (en) | 1998-08-21 | 2003-09-23 | Honeywell International, Inc. | Air turbine starter with seal assembly |
US6619430B2 (en) * | 2001-10-12 | 2003-09-16 | Carrier Corporation | Refrigerant gas buffered seal system |
US20030097872A1 (en) * | 2001-11-29 | 2003-05-29 | Granitz Charles Robert | System for reducing oil consumption in gas turbine engines |
US6976679B2 (en) * | 2003-11-07 | 2005-12-20 | The Boeing Company | Inter-fluid seal assembly and method therefor |
US6991235B2 (en) * | 2003-11-07 | 2006-01-31 | The Boeing Company | Gas-buffered seal assembly and method therefor |
US6996968B2 (en) * | 2003-12-17 | 2006-02-14 | United Technologies Corporation | Bifurcated oil scavenge system for a gas turbine engine |
US7093418B2 (en) * | 2004-04-21 | 2006-08-22 | Honeywell International, Inc. | Gas turbine engine including a low pressure sump seal buffer source and thermally isolated sump |
JP4776249B2 (ja) * | 2005-02-25 | 2011-09-21 | 株式会社東芝 | 液体の軸封装置とその軸封装置を用いた回転電機 |
DE102005015212A1 (de) * | 2005-04-02 | 2006-10-05 | Leybold Vacuum Gmbh | Wellendichtung |
EP1712816A1 (de) * | 2005-04-14 | 2006-10-18 | Siemens Aktiengesellschaft | Dichtungssystem zur Abdichtung eines Prozessgasraumes gegen einen Dichtraum |
JP2006301289A (ja) * | 2005-04-20 | 2006-11-02 | Tokyo Ohka Kogyo Co Ltd | ネガ型レジスト組成物およびレジストパターン形成方法 |
US7175388B2 (en) * | 2005-04-21 | 2007-02-13 | Pratt & Whitney Canada Corp. | Integrated labyrinth and carbon seal |
US7435052B2 (en) * | 2005-05-20 | 2008-10-14 | Honeywell International Inc. | Shaft oil purge system |
US7410341B2 (en) * | 2005-06-22 | 2008-08-12 | Honeywell International, Inc. | Internally-cooled seal housing for turbine engine |
DE102005041003A1 (de) * | 2005-08-29 | 2007-03-01 | Man Turbo Ag | Wellendichtung für einen Getriebeexpander oder -kompressor |
US7544039B1 (en) | 2006-06-14 | 2009-06-09 | Florida Turbine Technologies, Inc. | Dual spool shaft with intershaft seal |
US7591631B2 (en) * | 2006-06-30 | 2009-09-22 | United Technologies Corporation | Flow delivery system for seals |
US8167534B2 (en) * | 2006-09-14 | 2012-05-01 | Solar Turbines Inc. | Seal for a turbine engine |
US7967560B2 (en) * | 2006-11-07 | 2011-06-28 | United Technologies Corporation | Radially energized oil capture device for a geared turbofan |
US7878303B2 (en) * | 2006-11-14 | 2011-02-01 | Rolls-Royce Corporation | Lubrication scavenge system |
US7789200B2 (en) | 2006-11-14 | 2010-09-07 | Rolls-Royce Corporation | Sump housing |
US7784395B2 (en) * | 2007-03-28 | 2010-08-31 | Clyde Union Inc. | Zero emissions reciprocating pump |
US8511219B2 (en) * | 2007-03-28 | 2013-08-20 | Clyde Union Inc. | Zero emissions reciprocating pump |
US8167091B2 (en) | 2007-03-28 | 2012-05-01 | Pratt & Whitney Canada Corp. | Oil scavenge system having churning damper for gas turbine engines |
DE102008008886A1 (de) * | 2008-02-13 | 2009-08-20 | Man Turbo Ag | Eintrittsstutzen für einen Axialverdichter |
FR2929325B1 (fr) * | 2008-03-26 | 2012-09-28 | Snecma | Dispositif et procede d'equilibrage de pression dans une enceinte palier de turboreacteur |
US7730939B2 (en) * | 2008-03-27 | 2010-06-08 | Oil Flow Usa, Inc. | Safety clamp for walking beam compressor |
US20090246049A1 (en) * | 2008-03-27 | 2009-10-01 | Oil Flow Usa, Inc. | Coated cylinder for walking beam compressor |
US8047820B2 (en) * | 2008-03-27 | 2011-11-01 | Oil Flow Usa, Inc. | Stuffing box for walking beam compressor |
WO2010083427A1 (en) * | 2009-01-15 | 2010-07-22 | Dresser-Rand Company | Shaft sealing with convergent nozzle |
US8561411B2 (en) * | 2009-09-02 | 2013-10-22 | United Technologies Corporation | Air particle separator for a gas turbine engine |
EP2458158B1 (de) * | 2010-11-24 | 2013-08-21 | Techspace Aero S.A. | Schmieranordnung für Turbotriebwerk |
US20120156005A1 (en) * | 2010-12-16 | 2012-06-21 | Caterpillar Inc. | Buffer air for a labyrinth seal |
US8944749B2 (en) | 2012-01-24 | 2015-02-03 | Pratt & Whitney Canada Corp. | Oil purge system for a mid turbine frame |
US9217336B2 (en) * | 2012-02-16 | 2015-12-22 | Solar Turbines Incorporated | Gas turbine engine lubrication fluid barrier |
US9567908B2 (en) | 2012-04-27 | 2017-02-14 | General Electric Company | Mitigating vortex pumping effect upstream of oil seal |
ITCO20120020A1 (it) * | 2012-04-27 | 2013-10-28 | Nuovo Pignone Srl | Compressore, alimentazione del gas di tenuta e metodo |
US9353647B2 (en) * | 2012-04-27 | 2016-05-31 | General Electric Company | Wide discourager tooth |
US20140144121A1 (en) * | 2012-11-28 | 2014-05-29 | Pratt & Whitney Canada Corp. | Gas turbine engine with bearing oil leak recuperation system |
US9617916B2 (en) * | 2012-11-28 | 2017-04-11 | Pratt & Whitney Canada Corp. | Gas turbine engine with bearing buffer air flow and method |
US10247036B2 (en) * | 2012-12-14 | 2019-04-02 | General Electric Company | Pressure fed oil drain for gas turbine engine sump |
FR3011035B1 (fr) * | 2013-09-25 | 2015-10-09 | Snecma | Carter d'echappement comprenant un dispositif d'evacuation de fluide, et turbomachine |
US10196986B2 (en) | 2015-09-04 | 2019-02-05 | General Electric Company | Hydrodynamic seals in bearing compartments of gas turbine engines |
US10344869B2 (en) * | 2016-05-31 | 2019-07-09 | Rolls-Royce Corporation | Labyrinth seal with lubricant directing projection |
FR3075252B1 (fr) * | 2017-12-14 | 2020-06-26 | Safran Aircraft Engines | Ensemble d'etancheite |
US10767560B2 (en) * | 2018-09-11 | 2020-09-08 | Raytheon Technologies Corporation | Bearing compartment oil auto-ignition mitigation |
US11306614B2 (en) | 2018-10-04 | 2022-04-19 | Rolls-Royce Corporation | Sump auxiliary vent system |
US11365682B1 (en) * | 2021-03-04 | 2022-06-21 | Rolls-Royce North American Technologies Inc. | Gas turbine engine cooled sump buffer air system |
Family Cites Families (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1773067A (en) | 1928-01-27 | 1930-08-12 | Gen Electric | Method of sealing shaft packings |
US1878731A (en) | 1930-08-28 | 1932-09-20 | Thompson Paul Wheeler | Method of and means for sealing the shaft packings of turbines |
DE1106567B (de) * | 1956-03-15 | 1961-05-10 | Siemens Ag | Labyrinth-Wellendichtung mit Sperrgaszufuhr zur Abdichtung oelnebelhaltiger Raeume |
GB954788A (en) | 1962-09-05 | 1964-04-08 | Stal Laval Turbin Ab | Method of sealing a turbine or compressor shaft |
GB1021410A (en) | 1964-03-31 | 1966-03-02 | Stal Laval Turbin Ab | Method of sealing a turbine or compressor shaft |
CH418363A (de) * | 1964-06-26 | 1966-08-15 | Escher Wyss Ag | Wellendichtung für eine thermische Maschine |
CH464625A (de) * | 1966-10-12 | 1968-10-31 | Sulzer Ag | Wellendichtung für ein Gebläse, insbesondere für das Umwälzgebläse einer gasgekühlten Kernreaktoranlage |
DE2625551A1 (de) | 1976-06-05 | 1977-12-15 | Motoren Turbinen Union | Einrichtung zur abdichtung der lagerkammer einer turbomaschine, insbesondere eines gasturbinentriebwerks |
US4156342A (en) | 1976-06-11 | 1979-05-29 | Westinghouse Canada Limited | Cooling apparatus for a bearing in a gas turbine |
US4189156A (en) | 1978-06-08 | 1980-02-19 | Carrier Corporation | Seal system for a turbomachine employing working fluid in its liquid phase as the sealing fluid |
US4257617A (en) | 1978-11-06 | 1981-03-24 | Carrier Corporation | Shaft seal assembly |
US4193603A (en) | 1978-12-21 | 1980-03-18 | Carrier Corporation | Sealing system for a turbomachine |
US4373858A (en) * | 1980-12-10 | 1983-02-15 | The Bendix Corporation | Flow regulating shaft seal for an air motor |
US5042963A (en) | 1989-03-31 | 1991-08-27 | Allied-Signal Inc. | Dual range air turbine starter |
US5160005A (en) | 1990-11-27 | 1992-11-03 | Allied-Signal Inc. | Pawl and ratchet clutch with torsion shaft |
CH686525A5 (de) | 1992-07-02 | 1996-04-15 | Escher Wyss Ag | Turbomaschine . |
EP0577908B1 (de) | 1992-07-10 | 1995-09-06 | Ansaldo Energia S.P.A. | Verfahren zur Abdichtung des Rotors einer geothermischen Nassdampfturbine |
EP0683338A1 (de) * | 1994-05-17 | 1995-11-22 | Siemens Aktiengesellschaft | Wellenabdichtungssystem |
US5489190A (en) | 1994-07-29 | 1996-02-06 | Alliedsignal Inc. | Dynamic oil scavenge system |
US5538258A (en) | 1995-02-22 | 1996-07-23 | Alliedsignal Inc. | Oil seal for a high speed rotating shaft |
US5619850A (en) | 1995-05-09 | 1997-04-15 | Alliedsignal Inc. | Gas turbine engine with bleed air buffer seal |
DE19524732A1 (de) * | 1995-07-07 | 1997-01-09 | Bmw Rolls Royce Gmbh | Lagerkammer-Anordnung für eine Gasturbinen-Welle |
-
1999
- 1999-10-27 US US09/428,092 patent/US6330790B1/en not_active Expired - Lifetime
-
2000
- 2000-10-19 WO PCT/US2000/028925 patent/WO2001031235A2/en active IP Right Grant
- 2000-10-19 CA CA002389357A patent/CA2389357C/en not_active Expired - Fee Related
- 2000-10-19 DE DE60029487T patent/DE60029487T2/de not_active Expired - Lifetime
- 2000-10-19 AT AT00992000T patent/ATE333614T1/de not_active IP Right Cessation
- 2000-10-19 EP EP00992000A patent/EP1307672B1/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
WO2001031235A3 (en) | 2002-02-21 |
CA2389357A1 (en) | 2001-05-03 |
DE60029487T2 (de) | 2007-02-01 |
WO2001031235A2 (en) | 2001-05-03 |
CA2389357C (en) | 2008-10-07 |
US6330790B1 (en) | 2001-12-18 |
DE60029487D1 (de) | 2006-08-31 |
EP1307672A2 (de) | 2003-05-07 |
EP1307672B1 (de) | 2006-07-19 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE60029487D1 (de) | Pufferdichtungsanordnung für ölwanne | |
DE69926203D1 (de) | Zwischenwellen-Dichtungsanordnung für ein Gasturbinentriebwerk | |
US5975537A (en) | Rotor and stator assembly configured as an aspirating face seal | |
US8152450B1 (en) | Floating air seal for a turbine | |
GB0108398D0 (en) | Seal element for sealing a gap and combustion turbine having a seal element | |
CN1776264B (zh) | 用于转子轴的特别是静止时润滑的轴承结构的密封装置 | |
SE8802792D0 (sv) | Aircraft engines-evendale | |
FR2439872A1 (fr) | Turbine refroidie par air pour moteur a turbine a gaz | |
IT1319409B1 (it) | Sistema di scarico per cuscini portanti di turbine a gas | |
CA2352021A1 (en) | Turbocharger shaft dual phase seal | |
DE69922567D1 (de) | Dichtungsanordnung für eine Gasturbine | |
GB982085A (en) | Improvements in oil sump sealing systems for a gas turbine engine | |
DE19781063T1 (de) | Verbrennungsgasdichtung für einen Verbrennungsmotor | |
RU2005133004A (ru) | Смазочное устройство для смазки элементов турбомашины и турбореактивный двигатель | |
BR0105575B1 (pt) | conjunto de segmentos de gaxeta retráteis para um aparelho que extrai trabalho da expansão de um fluido de trabalho gasoso. | |
EP1146204A3 (de) | Abreibbare Dichtung | |
ATE524637T1 (de) | Abdichtungsvorrichtung für dampfturbinenleitapparate | |
DE69812837D1 (de) | Doppelkreuzdichtung für Gasturbinenleitschaufeln | |
DE60142167D1 (de) | Gleitringdichtung für einen turbolader | |
US5480232A (en) | Oil seal for gas turbine | |
EP1323891A3 (de) | Ergänzungsdichtung für Verdichtung einer Sehnenscharnierbefestigung für Gasturbinen | |
DE50011374D1 (de) | Schaltwalze | |
DK1336807T3 (da) | Tætningshoved til at tilföre et varmebærende medium | |
CN201148906Y (zh) | 涡轮增压器的油封结构 | |
DE29622322U1 (de) | Wellenabdichtung für Yachtantriebe, ölgeschmiert mit Radialwellendichtringen und Stopfbuchse |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |