FR3111164B1 - Système d’élimination de dépôt interne dans un tube central d’évacuation de turboréacteur - Google Patents

Système d’élimination de dépôt interne dans un tube central d’évacuation de turboréacteur Download PDF

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Publication number
FR3111164B1
FR3111164B1 FR2005882A FR2005882A FR3111164B1 FR 3111164 B1 FR3111164 B1 FR 3111164B1 FR 2005882 A FR2005882 A FR 2005882A FR 2005882 A FR2005882 A FR 2005882A FR 3111164 B1 FR3111164 B1 FR 3111164B1
Authority
FR
France
Prior art keywords
tube
central
removal system
exhaust tube
deposit removal
Prior art date
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Active
Application number
FR2005882A
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English (en)
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FR3111164A1 (fr
Inventor
Thibault Maxime Adrien Mallet
Michel Georges Hugues
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 FR2005882A priority Critical patent/FR3111164B1/fr
Publication of FR3111164A1 publication Critical patent/FR3111164A1/fr
Application granted granted Critical
Publication of FR3111164B1 publication Critical patent/FR3111164B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • 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
    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16—Control of working fluid flow
    • F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
    • 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
    • F05D2260/605—Venting into the ambient atmosphere or the like
    • 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
    • F05D2260/609—Deoiling or demisting

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)

Abstract

L’invention concerne un turboréacteur comportant un tube central rotatif (14) d’évacuation d’un flux d’air chargé de lubrifiant, ce tube central rotatif (14) étant porté par un support de tube aval fixe (17). Selon l’invention, le support de tube aval (17) est équipé d’un dispositif de coupe fixe (19) agencé pour longer une surface interne du tube central rotatif (14), afin de limiter la formation de dépôt à la surface interne de ce tube central rotatif (14) par effet de centrifugation de l’huile circulant dans le flux d’air et de cockéfaction de cette huile à la surface interne du tube. Figure pour l’abrégé : Figure 3
FR2005882A 2020-06-05 2020-06-05 Système d’élimination de dépôt interne dans un tube central d’évacuation de turboréacteur Active FR3111164B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR2005882A FR3111164B1 (fr) 2020-06-05 2020-06-05 Système d’élimination de dépôt interne dans un tube central d’évacuation de turboréacteur

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2005882A FR3111164B1 (fr) 2020-06-05 2020-06-05 Système d’élimination de dépôt interne dans un tube central d’évacuation de turboréacteur
FR2005882 2020-06-05

Publications (2)

Publication Number Publication Date
FR3111164A1 FR3111164A1 (fr) 2021-12-10
FR3111164B1 true FR3111164B1 (fr) 2022-05-13

Family

ID=72266536

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2005882A Active FR3111164B1 (fr) 2020-06-05 2020-06-05 Système d’élimination de dépôt interne dans un tube central d’évacuation de turboréacteur

Country Status (1)

Country Link
FR (1) FR3111164B1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3150253A1 (fr) 2023-06-26 2024-12-27 Safran Aircraft Engines Arbre creux comprennant un anneau de mousse
FR3160744B1 (fr) 2024-03-26 2026-03-20 Safran Aircraft Engines Système de refroidissement et de lubrification d’un palier de turbomachine d’aéronef et son procédé d’utilisation

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3528241A (en) * 1969-02-24 1970-09-15 Gen Electric Gas turbine engine lubricant sump vent and circulating system
FR2903450B1 (fr) * 2006-07-07 2013-03-01 Snecma Procede de traitement des rejets d'huile dans un moteur a turbine a gaz
EP2553222B1 (fr) * 2010-03-26 2019-03-20 Safran Aircraft Engines Tube de degazage d'un turboreacteur, procede de montage d'un tel tube et turboreacteur avec un tel tube
US10794203B2 (en) * 2017-03-22 2020-10-06 General Electric Company Scavenge tube for a gas turbine engine

Also Published As

Publication number Publication date
FR3111164A1 (fr) 2021-12-10

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