FR3056656B1 - Enceinte lubrifiee pour turbomachine d'aeronef, limitant la retention de lubrifiant lors du tangage - Google Patents

Enceinte lubrifiee pour turbomachine d'aeronef, limitant la retention de lubrifiant lors du tangage Download PDF

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Publication number
FR3056656B1
FR3056656B1 FR1659350A FR1659350A FR3056656B1 FR 3056656 B1 FR3056656 B1 FR 3056656B1 FR 1659350 A FR1659350 A FR 1659350A FR 1659350 A FR1659350 A FR 1659350A FR 3056656 B1 FR3056656 B1 FR 3056656B1
Authority
FR
France
Prior art keywords
tanging
lubricated
speaker
retention during
aircraft turbomachine
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.)
Active
Application number
FR1659350A
Other languages
English (en)
Other versions
FR3056656A1 (fr
Inventor
Rene Morreale Serge
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
Safran Aircraft Engines 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 Safran Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1659350A priority Critical patent/FR3056656B1/fr
Priority to PCT/FR2017/052599 priority patent/WO2018060595A1/fr
Priority to US16/336,263 priority patent/US11441439B2/en
Priority to GB1904358.7A priority patent/GB2569066B/en
Publication of FR3056656A1 publication Critical patent/FR3056656A1/fr
Application granted granted Critical
Publication of FR3056656B1 publication Critical patent/FR3056656B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F01D9/00—Stators
    • F01D9/06—Fluid supply conduits to nozzles or the like
    • F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
    • 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
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/30—Parts of ball or roller bearings
    • F16C33/66—Special parts or details in view of lubrication
    • F16C33/6637—Special parts or details in view of lubrication with liquid lubricant
    • F16C33/6685—Details of collecting or draining, e.g. returning the liquid to a sump
    • 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
    • F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/06—Arrangements of bearings; Lubricating
    • 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
    • F16N—LUBRICATING
    • F16N31/00—Means for collecting, retaining, or draining-off lubricant in or on machines or apparatus
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • 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
    • F05D2260/601—Fluid transfer using an ejector or a jet pump
    • 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
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2326/00—Articles relating to transporting
    • F16C2326/43—Aeroplanes; Helicopters
    • 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
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2360/00—Engines or pumps
    • F16C2360/23—Gas turbine engines
    • 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
    • F16N—LUBRICATING
    • F16N2210/00—Applications
    • F16N2210/02—Turbines
    • 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)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Rolling Contact Bearings (AREA)
FR1659350A 2016-09-29 2016-09-29 Enceinte lubrifiee pour turbomachine d'aeronef, limitant la retention de lubrifiant lors du tangage Active FR3056656B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR1659350A FR3056656B1 (fr) 2016-09-29 2016-09-29 Enceinte lubrifiee pour turbomachine d'aeronef, limitant la retention de lubrifiant lors du tangage
PCT/FR2017/052599 WO2018060595A1 (fr) 2016-09-29 2017-09-27 Enceinte lubrifiee pour turbomachine d'aeronef, limitant la retention de lubrifiant lors du tangage
US16/336,263 US11441439B2 (en) 2016-09-29 2017-09-27 Lubricated enclosure for an aircraft turbine engine, limiting the retention of lubricant during pitching
GB1904358.7A GB2569066B (en) 2016-09-29 2017-09-27 Lubricated enclosure for an aircraft turbine engine, limiting the retention of lubricant during pitching

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1659350 2016-09-29
FR1659350A FR3056656B1 (fr) 2016-09-29 2016-09-29 Enceinte lubrifiee pour turbomachine d'aeronef, limitant la retention de lubrifiant lors du tangage

Publications (2)

Publication Number Publication Date
FR3056656A1 FR3056656A1 (fr) 2018-03-30
FR3056656B1 true FR3056656B1 (fr) 2018-12-07

Family

ID=57539449

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1659350A Active FR3056656B1 (fr) 2016-09-29 2016-09-29 Enceinte lubrifiee pour turbomachine d'aeronef, limitant la retention de lubrifiant lors du tangage

Country Status (4)

Country Link
US (1) US11441439B2 (fr)
FR (1) FR3056656B1 (fr)
GB (1) GB2569066B (fr)
WO (1) WO2018060595A1 (fr)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3056656B1 (fr) * 2016-09-29 2018-12-07 Safran Aircraft Engines Enceinte lubrifiee pour turbomachine d'aeronef, limitant la retention de lubrifiant lors du tangage
FR3079265B1 (fr) * 2018-03-23 2020-04-17 Safran Aircraft Engines Support de palier de turboreacteur obtenu par fabrication additive
US10753400B2 (en) 2018-09-21 2020-08-25 Raytheon Technologies Corporation Ball bearing with lubricant drain
FR3100843B1 (fr) * 2019-09-13 2023-04-28 Safran Aircraft Engines Support de palier de turbomachine à récupération d’huile améliorée
FR3104655B1 (fr) * 2019-12-16 2021-12-24 Safran Helicopter Engines Roulement à trois points de contact avec drain amélioré
US11668247B2 (en) * 2021-04-16 2023-06-06 Raytheon Technologies Corporation Geared gas turbine with oil scavenge ejector pump assist
FR3132939B1 (fr) * 2022-02-21 2024-02-09 Safran Aircraft Engines Système d’étanchéité et de drainage de fuites d’huile pour enceinte de palier de turbomachine

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2043799B (en) * 1979-03-05 1983-03-16 Rolls Royce Draining oil from bearing
FR2740187B1 (fr) * 1995-10-18 1997-11-21 Snecma Roulement avec drainage dynamique alimente en lubrifiant
JP2005106108A (ja) * 2003-09-29 2005-04-21 Nsk Ltd 転がり軸受装置
US6996968B2 (en) * 2003-12-17 2006-02-14 United Technologies Corporation Bifurcated oil scavenge system for a gas turbine engine
US7377110B2 (en) * 2004-03-31 2008-05-27 United Technologies Corporation Deoiler for a lubrication system
FR2880930B1 (fr) * 2005-01-17 2007-03-02 Snecma Moteurs Sa Ensemble a roulement comprenant une double injection de liquide lubrifiant, et engin aeronautique comportant au moins un tel ensemble
US7878303B2 (en) * 2006-11-14 2011-02-01 Rolls-Royce Corporation Lubrication scavenge system
US8210316B2 (en) * 2006-12-12 2012-07-03 United Technologies Corporation Oil scavenge system for a gas turbine engine
FR3056656B1 (fr) * 2016-09-29 2018-12-07 Safran Aircraft Engines Enceinte lubrifiee pour turbomachine d'aeronef, limitant la retention de lubrifiant lors du tangage

Also Published As

Publication number Publication date
FR3056656A1 (fr) 2018-03-30
GB2569066A (en) 2019-06-05
GB2569066B (en) 2022-01-05
GB201904358D0 (en) 2019-05-15
WO2018060595A1 (fr) 2018-04-05
US20190211875A1 (en) 2019-07-11
US11441439B2 (en) 2022-09-13

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