RU2358132C2 - Смазочное устройство для смазки элементов турбомашины и турбореактивный двигатель - Google Patents

Смазочное устройство для смазки элементов турбомашины и турбореактивный двигатель Download PDF

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Publication number
RU2358132C2
RU2358132C2 RU2005133004/06A RU2005133004A RU2358132C2 RU 2358132 C2 RU2358132 C2 RU 2358132C2 RU 2005133004/06 A RU2005133004/06 A RU 2005133004/06A RU 2005133004 A RU2005133004 A RU 2005133004A RU 2358132 C2 RU2358132 C2 RU 2358132C2
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RU
Russia
Prior art keywords
annular
gasket
lubricating
supporting part
cavity
Prior art date
Application number
RU2005133004/06A
Other languages
English (en)
Russian (ru)
Other versions
RU2005133004A (ru
Inventor
Себастьен ПРЕСТЕЛЬ (FR)
Себастьен Престель
Оливье РЕНОН (FR)
Оливье РЕНОН
Жан-Люк СУПИЗОН (FR)
Жан-Люк СУПИЗОН
Original Assignee
Снекма
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Снекма filed Critical Снекма
Publication of RU2005133004A publication Critical patent/RU2005133004A/ru
Application granted granted Critical
Publication of RU2358132C2 publication Critical patent/RU2358132C2/ru

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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
    • F01D25/08—Cooling; Heating; Heat-insulation
    • 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
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/12—Cooling
    • F01D25/125—Cooling of bearings
    • 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
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
  • Rolling Contact Bearings (AREA)
RU2005133004/06A 2004-10-27 2005-10-26 Смазочное устройство для смазки элементов турбомашины и турбореактивный двигатель RU2358132C2 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0411435A FR2877036B1 (fr) 2004-10-27 2004-10-27 Dispositif de lubrification d'un composant dans une turbomachine
FR0411435 2004-10-27

Publications (2)

Publication Number Publication Date
RU2005133004A RU2005133004A (ru) 2007-05-10
RU2358132C2 true RU2358132C2 (ru) 2009-06-10

Family

ID=34952821

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2005133004/06A RU2358132C2 (ru) 2004-10-27 2005-10-26 Смазочное устройство для смазки элементов турбомашины и турбореактивный двигатель

Country Status (9)

Country Link
US (1) US7252476B2 (enExample)
EP (1) EP1653052B1 (enExample)
JP (1) JP4751172B2 (enExample)
CN (1) CN100529361C (enExample)
CA (1) CA2524594C (enExample)
DE (1) DE602005013731D1 (enExample)
FR (1) FR2877036B1 (enExample)
RU (1) RU2358132C2 (enExample)
UA (1) UA86585C2 (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2657105C2 (ru) * 2013-06-12 2018-06-08 Снекма Цапфа для турбины высокого давления и турбореактивный двигатель, включающий в себя такую цапфу

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0720628D0 (en) * 2007-10-20 2007-11-28 Rolls Royce Plc Bearing arrangement
FR2960612B1 (fr) * 2010-05-25 2012-06-22 Snecma Boite d'engrenages dans une turbomachine
DE102012223462B3 (de) * 2012-12-17 2013-08-08 Siemens Aktiengesellschaft Backup Dichtung in Kompaktbauweise bei einem Gehäuse einer Strömungsmaschine
EP2971688B1 (en) * 2013-03-14 2018-11-28 United Technologies Corporation Gas turbine engine disclosing a heat shield and method of mounting this heat shield
EP2873810B2 (fr) * 2013-11-18 2020-07-01 Safran Aero Boosters SA Couvercle annulaire de délimitation d'enceinte de lubrification de turbomachine
FR3013387B1 (fr) * 2013-11-20 2015-11-20 Snecma Support de palier presentant une geometrie facilitant l'evacuation des noyaux de fonderie
FR3016043B1 (fr) * 2013-12-26 2015-12-25 Snecma Procede de validation d'un systeme de detection de particules pour une turbomachine
FR3027637B1 (fr) * 2014-10-27 2017-04-28 Snecma Tige pour assemblage d'un couvercle, d'une piece de support de palier, et d'un joint d'etancheite
FR3039211B1 (fr) * 2015-07-21 2019-07-26 Safran Aircraft Engines Dispositif de compression pour ameliorer l'etancheite entre un couvercle de turbomachine et une piece de support de palier
FR3039618B1 (fr) * 2015-07-28 2017-08-18 Snecma Systeme d'etancheite pour turbomachine, joint d'etancheite et couvercle d'arrivee d'huile associes
FR3055372B1 (fr) * 2016-08-25 2021-10-01 Safran Aircraft Engines Dispositif de compression pour ameliorer l'etancheite entre un couvercle de turbomachine et une piece de support de palier
FR3061738B1 (fr) * 2017-01-12 2019-05-31 Safran Aircraft Engines Ensemble d'anneau de turbine
DE102017223112A1 (de) * 2017-12-18 2019-06-19 MTU Aero Engines AG Gehäuseanordnung für eine Strömungsmaschine sowie Strömungsmaschinenanordnung mit einer solchen Gehäuseanordnung und Verfahren zum Herstellen der Gehäuseanordnung
CN110332023B (zh) * 2019-07-16 2021-12-28 中国航发沈阳发动机研究所 一种具有冷却功能的端面密封结构
FR3107310B1 (fr) * 2020-02-17 2022-01-14 Safran Aircraft Engines Dispositif de distribution d’huile d’un palier a roulement de turbomachine d’aeronef

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3874676A (en) * 1974-03-21 1975-04-01 Carrier Corp Cooling apparatus for shaft seal
DE19648641A1 (de) * 1996-11-25 1998-05-28 Asea Brown Boveri Wärmeschutzvorrichtung für die Lagerung einer Turbine
WO1998039609A1 (en) * 1997-03-07 1998-09-11 Semitool, Inc. Semiconductor processing furnace
RU2132474C1 (ru) * 1994-05-17 1999-06-27 Прэтт энд Уитни Кэнэдэ, Инк. Узел кольцеобразный подшипниковой опоры (варианты)
RU2151896C1 (ru) * 1998-10-19 2000-06-27 Открытое акционерное общество "Авиадвигатель" Опора газотурбинного двигателя
RU2189475C2 (ru) * 2000-10-26 2002-09-20 Открытое акционерное общество "Авиадвигатель" Опора газотурбинного двигателя

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4709545A (en) * 1983-05-31 1987-12-01 United Technologies Corporation Bearing compartment protection system
EP0127562B1 (en) * 1983-05-31 1990-08-08 United Technologies Corporation Bearing compartment protection system
US4561246A (en) * 1983-12-23 1985-12-31 United Technologies Corporation Bearing compartment for a gas turbine engine
US5374161A (en) * 1993-12-13 1994-12-20 United Technologies Corporation Blade outer air seal cooling enhanced with inter-segment film slot
JP2003129803A (ja) * 2001-10-24 2003-05-08 Mitsubishi Heavy Ind Ltd ガスタービン

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3874676A (en) * 1974-03-21 1975-04-01 Carrier Corp Cooling apparatus for shaft seal
RU2132474C1 (ru) * 1994-05-17 1999-06-27 Прэтт энд Уитни Кэнэдэ, Инк. Узел кольцеобразный подшипниковой опоры (варианты)
DE19648641A1 (de) * 1996-11-25 1998-05-28 Asea Brown Boveri Wärmeschutzvorrichtung für die Lagerung einer Turbine
WO1998039609A1 (en) * 1997-03-07 1998-09-11 Semitool, Inc. Semiconductor processing furnace
RU2151896C1 (ru) * 1998-10-19 2000-06-27 Открытое акционерное общество "Авиадвигатель" Опора газотурбинного двигателя
RU2189475C2 (ru) * 2000-10-26 2002-09-20 Открытое акционерное общество "Авиадвигатель" Опора газотурбинного двигателя

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2657105C2 (ru) * 2013-06-12 2018-06-08 Снекма Цапфа для турбины высокого давления и турбореактивный двигатель, включающий в себя такую цапфу

Also Published As

Publication number Publication date
JP2006125398A (ja) 2006-05-18
CN1773092A (zh) 2006-05-17
US7252476B2 (en) 2007-08-07
US20060088408A1 (en) 2006-04-27
RU2005133004A (ru) 2007-05-10
DE602005013731D1 (de) 2009-05-20
CA2524594C (fr) 2012-12-11
FR2877036B1 (fr) 2006-12-22
CA2524594A1 (fr) 2006-04-27
EP1653052A1 (fr) 2006-05-03
UA86585C2 (uk) 2009-05-12
JP4751172B2 (ja) 2011-08-17
EP1653052B1 (fr) 2009-04-08
CN100529361C (zh) 2009-08-19
FR2877036A1 (fr) 2006-04-28

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MM4A The patent is invalid due to non-payment of fees

Effective date: 20191027