FR1291350A - Ensemble de palier - Google Patents

Ensemble de palier

Info

Publication number
FR1291350A
FR1291350A FR864072A FR864072A FR1291350A FR 1291350 A FR1291350 A FR 1291350A FR 864072 A FR864072 A FR 864072A FR 864072 A FR864072 A FR 864072A FR 1291350 A FR1291350 A FR 1291350A
Authority
FR
France
Prior art keywords
bearing assembly
bearing
assembly
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.)
Expired
Application number
FR864072A
Other languages
English (en)
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of FR1291350A publication Critical patent/FR1291350A/fr
Expired legal-status Critical Current

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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
    • F01D11/04—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type using sealing fluid, e.g. steam
    • 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
    • F01D25/18—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
    • F02C7/06—Arrangements of bearings; Lubricating
    • 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
    • F16C19/00—Bearings with rolling contact, for exclusively rotary movement
    • F16C19/22—Bearings with rolling contact, for exclusively rotary movement with bearing rollers essentially of the same size in one or more circular rows, e.g. needle bearings
    • F16C19/24—Bearings with rolling contact, for exclusively rotary movement with bearing rollers essentially of the same size in one or more circular rows, e.g. needle bearings for radial load mainly
    • F16C19/26—Bearings with rolling contact, for exclusively rotary movement with bearing rollers essentially of the same size in one or more circular rows, e.g. needle bearings for radial load mainly with a single row of rollers
    • 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
    • F16C37/00—Cooling of bearings
    • F16C37/007—Cooling of bearings of rolling bearings
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Sealing Of Bearings (AREA)
  • Mounting Of Bearings Or Others (AREA)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
FR864072A 1960-06-07 1961-06-06 Ensemble de palier Expired FR1291350A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB19992/60A GB912331A (en) 1960-06-07 1960-06-07 Bearing assembly

Publications (1)

Publication Number Publication Date
FR1291350A true FR1291350A (fr) 1962-04-20

Family

ID=10138534

Family Applications (1)

Application Number Title Priority Date Filing Date
FR864072A Expired FR1291350A (fr) 1960-06-07 1961-06-06 Ensemble de palier

Country Status (4)

Country Link
US (1) US3057542A (fr)
DE (1) DE1210626B (fr)
FR (1) FR1291350A (fr)
GB (1) GB912331A (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1108858A2 (fr) * 1999-12-15 2001-06-20 General Electric Company Cône de support à double paroi
WO2005116407A2 (fr) * 2004-04-21 2005-12-08 Honeywell International Inc. Moteur a turbine a gaz comportant une source tampon de joint de carter basse pression et carter thermiquement isole
EP2867496A4 (fr) * 2012-07-02 2015-07-29 United Technologies Corp Appareil de refroidissement pour châssis intermédiaire de turbine

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3129983A (en) * 1962-07-06 1964-04-21 United Aircraft Corp Oil divider
US3135562A (en) * 1963-01-07 1964-06-02 Rolls Royce Bearings
GB961522A (en) * 1963-01-09 1964-06-24 Rolls Royce Bearing assembly
GB1013140A (en) * 1964-09-04 1965-12-15 Rolls Royce Bearing assembly
US3451653A (en) * 1967-03-22 1969-06-24 Gen Electric Turbomachinery rotors
US4321007A (en) * 1979-12-21 1982-03-23 United Technologies Corporation Outer case cooling for a turbine intermediate case
US4369016A (en) * 1979-12-21 1983-01-18 United Technologies Corporation Turbine intermediate case
US5212940A (en) * 1991-04-16 1993-05-25 General Electric Company Tip clearance control apparatus and method
US5450719A (en) * 1993-11-17 1995-09-19 Alliedsignal, Inc. Gas turbine engine rear magnetic or foil bearing cooling using exhaust eductor
DE4412314A1 (de) * 1994-04-11 1995-10-12 Abb Management Ag Ölablaufleitung einer thermischen Turbomaschine
US6582187B1 (en) * 2000-03-10 2003-06-24 General Electric Company Methods and apparatus for isolating gas turbine engine bearings
US8371812B2 (en) * 2008-11-29 2013-02-12 General Electric Company Turbine frame assembly and method for a gas turbine engine
US9051878B2 (en) * 2011-06-22 2015-06-09 Hamilton Sundstrand Corporation Engine bearing compartment
US10233762B2 (en) * 2013-02-27 2019-03-19 United Technologies Corporation Cooled seal assembly for arranging between a stator and a rotor
US9644495B2 (en) * 2013-08-20 2017-05-09 Honeywell International Inc. Thermal isolating service tubes and assemblies thereof for gas turbine engines
US9598981B2 (en) * 2013-11-22 2017-03-21 Siemens Energy, Inc. Industrial gas turbine exhaust system diffuser inlet lip
FR3013766B1 (fr) * 2013-11-25 2017-11-10 Snecma Turbomachine comprenant un fourreau d'arbre et tube de fourreau associe
ITUB20160240A1 (it) * 2016-01-20 2017-07-20 Turboden Srl Metodo e dispositivo per ridurre le perdite di trafilamento in una turbina

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE536397C (de) * 1931-10-22 Anton Piller Lager
GB578765A (en) * 1942-09-09 1946-07-11 Frank Bernard Halford Improvements in or relating to shaft bearings
GB630792A (en) * 1946-11-20 1949-10-21 Havilland Engine Co Ltd Improvements in or relating to the cooling of the bearings of turbo-machinery as used in aircraft
US2584973A (en) * 1947-04-10 1952-02-12 Luwa S A Cooling and sealing means for disk atomizer shafts

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1108858A2 (fr) * 1999-12-15 2001-06-20 General Electric Company Cône de support à double paroi
EP1108858A3 (fr) * 1999-12-15 2003-01-15 General Electric Company Cône de support à double paroi
WO2005116407A2 (fr) * 2004-04-21 2005-12-08 Honeywell International Inc. Moteur a turbine a gaz comportant une source tampon de joint de carter basse pression et carter thermiquement isole
WO2005116407A3 (fr) * 2004-04-21 2006-04-20 Honeywell Int Inc Moteur a turbine a gaz comportant une source tampon de joint de carter basse pression et carter thermiquement isole
US7093418B2 (en) 2004-04-21 2006-08-22 Honeywell International, Inc. Gas turbine engine including a low pressure sump seal buffer source and thermally isolated sump
EP2867496A4 (fr) * 2012-07-02 2015-07-29 United Technologies Corp Appareil de refroidissement pour châssis intermédiaire de turbine

Also Published As

Publication number Publication date
US3057542A (en) 1962-10-09
DE1210626B (de) 1966-02-10
GB912331A (en) 1962-12-05

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