FR3026135B1 - Dispositif de lubrification pour palier de turbomachine - Google Patents

Dispositif de lubrification pour palier de turbomachine Download PDF

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Publication number
FR3026135B1
FR3026135B1 FR1458905A FR1458905A FR3026135B1 FR 3026135 B1 FR3026135 B1 FR 3026135B1 FR 1458905 A FR1458905 A FR 1458905A FR 1458905 A FR1458905 A FR 1458905A FR 3026135 B1 FR3026135 B1 FR 3026135B1
Authority
FR
France
Prior art keywords
main body
lubrication device
cavity
bearing lubrication
turbomachine bearing
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
FR1458905A
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English (en)
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FR3026135A1 (fr
Inventor
Christophe Lima
Dimitri Marquie
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
Priority to FR1458905A priority Critical patent/FR3026135B1/fr
Publication of FR3026135A1 publication Critical patent/FR3026135A1/fr
Application granted granted Critical
Publication of FR3026135B1 publication Critical patent/FR3026135B1/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
    • 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
    • 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
    • F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
    • 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
    • F05D2260/98—Lubrication
    • 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)
  • Rolling Contact Bearings (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

L'objet principal de l'invention est un dispositif (1) de lubrification pour palier de turbomachine, comportant un corps principal (12) pourvu d'une cavité interne (9) pour l'écoulement d'un fluide de lubrification, le corps principal (12) comportant, au niveau de son extrémité interne (12a), au moins une buse d'éjection (4a, 4b), en communication fluidique avec la cavité interne (9), pour l'éjection du fluide de lubrification en direction d'au moins le palier, caractérisé en ce que la dimension axiale (Da, Db) de la cavité interne (9) du corps principal (12) est plus faible dans au moins une première portion de cavité (9a) s'étendant depuis ladite au moins une buse d'éjection (4a, 4b) au niveau de l'extrémité interne (12a) du corps principal (12) que dans au moins une deuxième portion de cavité (9b) s'étendant depuis l'extrémité externe (12b) du corps principal (12).
FR1458905A 2014-09-22 2014-09-22 Dispositif de lubrification pour palier de turbomachine Active FR3026135B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1458905A FR3026135B1 (fr) 2014-09-22 2014-09-22 Dispositif de lubrification pour palier de turbomachine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1458905A FR3026135B1 (fr) 2014-09-22 2014-09-22 Dispositif de lubrification pour palier de turbomachine

Publications (2)

Publication Number Publication Date
FR3026135A1 FR3026135A1 (fr) 2016-03-25
FR3026135B1 true FR3026135B1 (fr) 2020-08-14

Family

ID=52474003

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1458905A Active FR3026135B1 (fr) 2014-09-22 2014-09-22 Dispositif de lubrification pour palier de turbomachine

Country Status (1)

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FR (1) FR3026135B1 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20180087404A1 (en) * 2016-09-23 2018-03-29 Rolls-Royce Corporation Oil distributor
FR3080650B1 (fr) 2018-04-26 2020-04-03 Safran Aircraft Engines Ensemble de lubrification pour une turbomachine
CN109543304B (zh) * 2018-11-23 2022-12-09 中南大学 一种航空螺旋锥齿轮喷油润滑喷嘴布局优化设计方法
FR3091903B1 (fr) * 2019-01-23 2020-12-25 Safran Aircraft Engines Gicleur de liquide lubrifiant à débit limité
FR3094403B1 (fr) 2019-04-01 2021-06-25 Safran Trans Systems Gicleur pour turbomachine comprenant une tête d’éjection à face oblique

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7278516B2 (en) * 2004-03-09 2007-10-09 Honeywell International, Inc. Apparatus and method for bearing lubrication in turbine engines
US20120011824A1 (en) * 2010-07-16 2012-01-19 United Technologies Corporation Integral lubrication tube and nozzle combination
FR2977636B1 (fr) * 2011-07-06 2013-08-09 Snecma Dispositif de lubrification d'un palier a roulement inter-arbres de turbopropulseur a double helice

Also Published As

Publication number Publication date
FR3026135A1 (fr) 2016-03-25

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