FR2993609B1 - Dispositif d'evacuation d'huile d'une turbomachine comportant un conduit d'aspiration - Google Patents

Dispositif d'evacuation d'huile d'une turbomachine comportant un conduit d'aspiration

Info

Publication number
FR2993609B1
FR2993609B1 FR1256992A FR1256992A FR2993609B1 FR 2993609 B1 FR2993609 B1 FR 2993609B1 FR 1256992 A FR1256992 A FR 1256992A FR 1256992 A FR1256992 A FR 1256992A FR 2993609 B1 FR2993609 B1 FR 2993609B1
Authority
FR
France
Prior art keywords
turbomachine
suction pipe
draining device
oil draining
oil
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
FR1256992A
Other languages
English (en)
Other versions
FR2993609A1 (fr
Inventor
Maxime Rotenberg
Yolaine Fourquie
Laurent Pate
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 FR1256992A priority Critical patent/FR2993609B1/fr
Publication of FR2993609A1 publication Critical patent/FR2993609A1/fr
Application granted granted Critical
Publication of FR2993609B1 publication Critical patent/FR2993609B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • 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
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • 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
    • F05D2260/602—Drainage
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
FR1256992A 2012-07-19 2012-07-19 Dispositif d'evacuation d'huile d'une turbomachine comportant un conduit d'aspiration Active FR2993609B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1256992A FR2993609B1 (fr) 2012-07-19 2012-07-19 Dispositif d'evacuation d'huile d'une turbomachine comportant un conduit d'aspiration

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1256992A FR2993609B1 (fr) 2012-07-19 2012-07-19 Dispositif d'evacuation d'huile d'une turbomachine comportant un conduit d'aspiration

Publications (2)

Publication Number Publication Date
FR2993609A1 FR2993609A1 (fr) 2014-01-24
FR2993609B1 true FR2993609B1 (fr) 2014-11-21

Family

ID=46852270

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1256992A Active FR2993609B1 (fr) 2012-07-19 2012-07-19 Dispositif d'evacuation d'huile d'une turbomachine comportant un conduit d'aspiration

Country Status (1)

Country Link
FR (1) FR2993609B1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10167741B2 (en) * 2015-11-03 2019-01-01 Rohr, Inc. Nacelle fluid drain
US11286859B2 (en) * 2018-08-09 2022-03-29 General Electric Company Acoustic panel and method for making the same

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5114446A (en) * 1991-02-15 1992-05-19 United Technologies Corporation Deoiler for jet engine
FR2902830B1 (fr) * 2006-06-27 2008-08-08 Airbus France Sas Turboreacteur pour aeronef
FR2926738B1 (fr) * 2008-01-29 2010-04-02 Snecma Dispositif de deshuilage et turbomachine comportant ce dispositif
DE102009060051A1 (de) * 2009-12-21 2011-06-22 Rolls-Royce Deutschland Ltd & Co KG, 15827 Anordnung zum Abblasen von aus dem Schmierölentlüftungssystem eines Gasturbinentriebwerks ab getrennter Abluft

Also Published As

Publication number Publication date
FR2993609A1 (fr) 2014-01-24

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