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FR2991386B1 - Turbomachine comportant des moyens de fixation amont d'un tube de deshuilage - Google Patents

Turbomachine comportant des moyens de fixation amont d'un tube de deshuilage

Info

Publication number
FR2991386B1
FR2991386B1 FR1255230A FR1255230A FR2991386B1 FR 2991386 B1 FR2991386 B1 FR 2991386B1 FR 1255230 A FR1255230 A FR 1255230A FR 1255230 A FR1255230 A FR 1255230A FR 2991386 B1 FR2991386 B1 FR 2991386B1
Authority
FR
France
Prior art keywords
dehuiling
turbomachine
tube
fastening means
means before
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
FR1255230A
Other languages
English (en)
Other versions
FR2991386A1 (fr
Inventor
Michel Gilbert Roland Brault
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 FR1255230A priority Critical patent/FR2991386B1/fr
Priority to PCT/FR2013/051239 priority patent/WO2013182790A1/fr
Priority to GB1421713.7A priority patent/GB2517860B/en
Priority to US14/401,911 priority patent/US9784130B2/en
Priority to PCT/FR2013/051253 priority patent/WO2013182797A1/fr
Publication of FR2991386A1 publication Critical patent/FR2991386A1/fr
Application granted granted Critical
Publication of FR2991386B1 publication Critical patent/FR2991386B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • 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
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Lubrication Of Internal Combustion Engines (AREA)
  • Mechanical Operated Clutches (AREA)
FR1255230A 2012-06-05 2012-06-05 Turbomachine comportant des moyens de fixation amont d'un tube de deshuilage Active FR2991386B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR1255230A FR2991386B1 (fr) 2012-06-05 2012-06-05 Turbomachine comportant des moyens de fixation amont d'un tube de deshuilage
PCT/FR2013/051239 WO2013182790A1 (fr) 2012-06-05 2013-05-31 Dispositif de déshuilage pour une turbomachine
GB1421713.7A GB2517860B (en) 2012-06-05 2013-06-03 Turbine engine comprising an upstream attachment means for a de-oiling pipe
US14/401,911 US9784130B2 (en) 2012-06-05 2013-06-03 Turbine engine comprising an upstream attachment means for a de-oiling pipe
PCT/FR2013/051253 WO2013182797A1 (fr) 2012-06-05 2013-06-03 Turbomachine comportant des moyens de fixation amont d'un tube de deshuilage

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1255230A FR2991386B1 (fr) 2012-06-05 2012-06-05 Turbomachine comportant des moyens de fixation amont d'un tube de deshuilage

Publications (2)

Publication Number Publication Date
FR2991386A1 FR2991386A1 (fr) 2013-12-06
FR2991386B1 true FR2991386B1 (fr) 2014-07-18

Family

ID=46889207

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1255230A Active FR2991386B1 (fr) 2012-06-05 2012-06-05 Turbomachine comportant des moyens de fixation amont d'un tube de deshuilage

Country Status (4)

Country Link
US (1) US9784130B2 (fr)
FR (1) FR2991386B1 (fr)
GB (1) GB2517860B (fr)
WO (1) WO2013182797A1 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3028781B1 (fr) * 2014-11-25 2016-12-30 Snecma Piece pour rotor de turbomachine d'aeronef comprenant une protuberance annulaire usinable pourvue d'un orifice de deshuilage et procede de preparation de celle-ci
FR3075868B1 (fr) * 2017-12-22 2019-11-15 Safran Aircraft Engines Tube de degazage pour une turbomachine d'aeronef a reducteur
FR3087224B1 (fr) * 2018-10-10 2021-05-21 Safran Aircraft Engines Systeme de fixation d'un arbre d'une turbine contrarotative pour une turbomachine d'aeronef
US11415015B2 (en) 2019-10-23 2022-08-16 Pratt & Whitney Canada Corp. Sleeve for oil service tubes
FR3107717B1 (fr) * 2020-02-27 2022-09-09 Safran Aircraft Engines Tube de dégazage pour une turbomachine
US11268442B2 (en) * 2020-07-01 2022-03-08 Raytheon Technologies Corporation Mid mount sleeve arrangement

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5257903A (en) * 1991-10-30 1993-11-02 General Electric Company Low pressure drop radial inflow air-oil separating arrangement and separator employed therein
US6325381B1 (en) * 1999-05-04 2001-12-04 System Seals, Inc. High-pressure rotary seal
FR2896827B1 (fr) * 2006-01-27 2008-04-25 Snecma Sa Assemblage a encombrement radial reduit entre un arbre de turbine et un tourillon d'arbre de compresseur de turbomachine
US7704029B2 (en) * 2007-11-19 2010-04-27 Pratt & Whitney Canada Corp. Arrangement for releasably holding a component in a fixed position on a shaft
US8292034B2 (en) 2007-11-28 2012-10-23 General Electric Company Air-oil separator
FR2926604B1 (fr) * 2008-01-23 2010-03-26 Snecma Centrage d'une piece a l'interieur d'un arbre de rotor dans une turbomachine
FR2928566B1 (fr) * 2008-03-12 2010-04-16 Snecma Deshuileur centrifuge a section de passage variable
US8092132B2 (en) * 2008-12-05 2012-01-10 American Axle & Manufacturing, Inc. Fastener with anti-rotation clip
US8459954B2 (en) * 2010-01-19 2013-06-11 United Technologies Corporation Torsional flexing energy absorbing blade lock
US8875378B2 (en) * 2011-11-07 2014-11-04 United Technologies Corporation Tie bolt employing differential thread

Also Published As

Publication number Publication date
GB2517860B (en) 2020-02-19
US20150167495A1 (en) 2015-06-18
US9784130B2 (en) 2017-10-10
WO2013182797A1 (fr) 2013-12-12
GB201421713D0 (en) 2015-01-21
GB2517860A (en) 2015-03-04
FR2991386A1 (fr) 2013-12-06

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