FR3010728B1 - Ecrou de serrage et d'evacuation d'huile, et turbomachine - Google Patents

Ecrou de serrage et d'evacuation d'huile, et turbomachine

Info

Publication number
FR3010728B1
FR3010728B1 FR1358982A FR1358982A FR3010728B1 FR 3010728 B1 FR3010728 B1 FR 3010728B1 FR 1358982 A FR1358982 A FR 1358982A FR 1358982 A FR1358982 A FR 1358982A FR 3010728 B1 FR3010728 B1 FR 3010728B1
Authority
FR
France
Prior art keywords
turbomachine
tightening
nut
oil drain
drain
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
FR1358982A
Other languages
English (en)
Other versions
FR3010728A1 (fr
Inventor
Olivier Belmonte
Emmanuel Pierre Dimitri Patsouris
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 FR1358982A priority Critical patent/FR3010728B1/fr
Priority to US14/489,635 priority patent/US9944382B2/en
Priority to GB1416529.4A priority patent/GB2520394B/en
Publication of FR3010728A1 publication Critical patent/FR3010728A1/fr
Application granted granted Critical
Publication of FR3010728B1 publication Critical patent/FR3010728B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/02—Hub construction
    • B64C11/04—Blade mountings
    • B64C11/06—Blade mountings for variable-pitch blades
    • 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
    • F01D7/00—Rotors with blades adjustable in operation; Control thereof
    • 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
    • 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
    • F16C33/72—Sealings
    • F16C33/76—Sealings of ball or roller bearings
    • F16C33/78—Sealings of ball or roller bearings with a diaphragm, disc, or ring, with or without resilient members
    • 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
    • F16C35/00—Rigid support of bearing units; Housings, e.g. caps, covers
    • F16C35/04—Rigid support of bearing units; Housings, e.g. caps, covers in the case of ball or roller bearings
    • F16C35/06—Mounting or dismounting of ball or roller bearings; Fixing them onto shaft or in housing
    • F16C35/063—Fixing them on the shaft
    • 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
    • F16N31/02—Oil catchers; Oil wipers
    • F16N2031/025—Oil-slinger
FR1358982A 2013-09-18 2013-09-18 Ecrou de serrage et d'evacuation d'huile, et turbomachine Active FR3010728B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1358982A FR3010728B1 (fr) 2013-09-18 2013-09-18 Ecrou de serrage et d'evacuation d'huile, et turbomachine
US14/489,635 US9944382B2 (en) 2013-09-18 2014-09-18 Tightening and oil discharging nut, and a turbine engine
GB1416529.4A GB2520394B (en) 2013-09-18 2014-09-18 A device for controlling the pitch of a blade of a rotor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1358982A FR3010728B1 (fr) 2013-09-18 2013-09-18 Ecrou de serrage et d'evacuation d'huile, et turbomachine

Publications (2)

Publication Number Publication Date
FR3010728A1 FR3010728A1 (fr) 2015-03-20
FR3010728B1 true FR3010728B1 (fr) 2018-02-16

Family

ID=49484368

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1358982A Active FR3010728B1 (fr) 2013-09-18 2013-09-18 Ecrou de serrage et d'evacuation d'huile, et turbomachine

Country Status (3)

Country Link
US (1) US9944382B2 (fr)
FR (1) FR3010728B1 (fr)
GB (1) GB2520394B (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3055310B1 (fr) * 2016-08-26 2018-08-17 Safran Aircraft Engines Turbomachine a dispositif de guidage d'huile et procede de demontage de la turbomachine
FR3057910B1 (fr) * 2016-10-24 2019-06-28 Safran Aircraft Engines Turbomachine d'aeronef comprenant des moyens d'etancheite
CN106498637B (zh) * 2017-01-05 2022-03-04 无锡市兴达缝纫机配件有限公司 一种缝纫机用油盒
CN107339323A (zh) * 2017-08-30 2017-11-10 重庆市丰蕙达金属锻造有限公司 防泄漏轴承座
FR3124839B1 (fr) * 2021-06-30 2023-07-28 Safran Aircraft Engines Agencement d’etancheite d’un roulement soumis a des forces centrifuges

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB564928A (en) * 1943-04-06 1944-10-19 Leonard Gaskell Fairhurst Improvements in and relating to variable-pitch screw-propellers
GB1486150A (en) * 1975-06-26 1977-09-21 Mitsubishi Heavy Ind Ltd Rotors for axial-flow machines for example fans
JP2002349278A (ja) * 2001-04-26 2002-12-04 Mtu Friedrichshafen Gmbh 排気ガスターボ過給器のための噴射円板
JP4797299B2 (ja) * 2001-08-14 2011-10-19 株式会社Ｉｈｉ ガスタービンエンジン
EP2192272B1 (fr) * 2008-11-28 2011-01-12 ABB Turbo Systems AG Dispositif pour étanchéifier un boîtier de palier de turbocompresseur
FR2944557B1 (fr) * 2009-04-16 2011-05-27 Snecma Systeme d'anti-rotation d'un tourillon d'une turbine haute pression dans une turbomachine

Also Published As

Publication number Publication date
GB2520394A (en) 2015-05-20
US20150078899A1 (en) 2015-03-19
GB2520394B (en) 2018-04-04
US9944382B2 (en) 2018-04-17
GB201416529D0 (en) 2014-11-05
FR3010728A1 (fr) 2015-03-20

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