CN100529361C - 一种用于润滑涡轮机中构件的装置 - Google Patents

一种用于润滑涡轮机中构件的装置 Download PDF

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Publication number
CN100529361C
CN100529361C CNB2005101181467A CN200510118146A CN100529361C CN 100529361 C CN100529361 C CN 100529361C CN B2005101181467 A CNB2005101181467 A CN B2005101181467A CN 200510118146 A CN200510118146 A CN 200510118146A CN 100529361 C CN100529361 C CN 100529361C
Authority
CN
China
Prior art keywords
supporting part
chamber
annular
lubricating
pipeline
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 - Fee Related
Application number
CNB2005101181467A
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English (en)
Chinese (zh)
Other versions
CN1773092A (zh
Inventor
塞巴斯蒂安·普雷斯特尔
奥利维耶·勒农
让-吕克·苏皮宗
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Publication of CN1773092A publication Critical patent/CN1773092A/zh
Application granted granted Critical
Publication of CN100529361C publication Critical patent/CN100529361C/zh
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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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)
CNB2005101181467A 2004-10-27 2005-10-26 一种用于润滑涡轮机中构件的装置 Expired - Fee Related CN100529361C (zh)

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
CN1773092A CN1773092A (zh) 2006-05-17
CN100529361C true CN100529361C (zh) 2009-08-19

Family

ID=34952821

Family Applications (1)

Application Number Title Priority Date Filing Date
CNB2005101181467A Expired - Fee Related CN100529361C (zh) 2004-10-27 2005-10-26 一种用于润滑涡轮机中构件的装置

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)

Families Citing this family (16)

* 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
FR3007069B1 (fr) * 2013-06-12 2015-07-17 Snecma Tourillon pour turbine haute pression, et turboreacteur incluant un tel tourillon
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

Family Cites Families (11)

* 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
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
US5415478A (en) * 1994-05-17 1995-05-16 Pratt & Whitney Canada, Inc. Annular bearing compartment
DE19648641A1 (de) * 1996-11-25 1998-05-28 Asea Brown Boveri Wärmeschutzvorrichtung für die Lagerung einer Turbine
JP2001517363A (ja) * 1997-03-07 2001-10-02 セミトゥール・インコーポレイテッド サブアッセンブリを加熱する半導体処理炉
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
JP2003129803A (ja) * 2001-10-24 2003-05-08 Mitsubishi Heavy Ind Ltd ガスタービン

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
RU2358132C2 (ru) 2009-06-10
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
FR2877036A1 (fr) 2006-04-28

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C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20090819

Termination date: 20191026

CF01 Termination of patent right due to non-payment of annual fee