FR1291350A - Ensemble de palier - Google Patents
Ensemble de palierInfo
- 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
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 Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
- Sealing Of Bearings (AREA)
- Mounting Of Bearings Or Others (AREA)
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)
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)
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 |
US4369016A (en) * | 1979-12-21 | 1983-01-18 | United Technologies Corporation | Turbine intermediate case |
US4321007A (en) * | 1979-12-21 | 1982-03-23 | United Technologies Corporation | Outer case cooling for a 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)
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 |
-
1960
- 1960-06-07 GB GB19992/60A patent/GB912331A/en not_active Expired
-
1961
- 1961-06-05 US US114975A patent/US3057542A/en not_active Expired - Lifetime
- 1961-06-06 FR FR864072A patent/FR1291350A/fr not_active Expired
- 1961-06-06 DE DER30472A patent/DE1210626B/de active Pending
Cited By (6)
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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