FR2557207B1 - Systeme de refroidissement pour fournir un tampon d'air a un compartiment de palier - Google Patents

Systeme de refroidissement pour fournir un tampon d'air a un compartiment de palier

Info

Publication number
FR2557207B1
FR2557207B1 FR848419768A FR8419768A FR2557207B1 FR 2557207 B1 FR2557207 B1 FR 2557207B1 FR 848419768 A FR848419768 A FR 848419768A FR 8419768 A FR8419768 A FR 8419768A FR 2557207 B1 FR2557207 B1 FR 2557207B1
Authority
FR
France
Prior art keywords
providing
cooling system
air buffer
bearing compartment
compartment
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 - Lifetime
Application number
FR848419768A
Other languages
English (en)
Other versions
FR2557207A1 (fr
Inventor
Edward J Hovan
Joseph P Zimonis
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of FR2557207A1 publication Critical patent/FR2557207A1/fr
Application granted granted Critical
Publication of FR2557207B1 publication Critical patent/FR2557207B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/18—Lubricating arrangements
    • F01D25/183—Sealing means
    • 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
    • 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
    • F02C7/12—Cooling of plants
    • F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • 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
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • F02C7/185—Cooling means for reducing the temperature of the cooling air or gas
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S165/00—Heat exchange
    • Y10S165/908—Fluid jets

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR848419768A 1983-12-23 1984-12-24 Systeme de refroidissement pour fournir un tampon d'air a un compartiment de palier Expired - Lifetime FR2557207B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/564,995 US4542623A (en) 1983-12-23 1983-12-23 Air cooler for providing buffer air to a bearing compartment

Publications (2)

Publication Number Publication Date
FR2557207A1 FR2557207A1 (fr) 1985-06-28
FR2557207B1 true FR2557207B1 (fr) 1991-09-06

Family

ID=24256768

Family Applications (1)

Application Number Title Priority Date Filing Date
FR848419768A Expired - Lifetime FR2557207B1 (fr) 1983-12-23 1984-12-24 Systeme de refroidissement pour fournir un tampon d'air a un compartiment de palier

Country Status (5)

Country Link
US (1) US4542623A (fr)
JP (1) JPS60142021A (fr)
DE (1) DE3447717C2 (fr)
FR (1) FR2557207B1 (fr)
GB (1) GB2152589B (fr)

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US8997500B2 (en) * 2010-02-19 2015-04-07 United Technologies Corporation Gas turbine engine oil buffering
US20120011824A1 (en) * 2010-07-16 2012-01-19 United Technologies Corporation Integral lubrication tube and nozzle combination
US8845282B2 (en) * 2011-09-28 2014-09-30 United Technologies Corporation Seal plate with cooling passage
US20130192240A1 (en) * 2012-01-31 2013-08-01 Peter M. Munsell Buffer system for a gas turbine engine
WO2014051691A1 (fr) * 2012-09-27 2014-04-03 United Technologies Corporation Écoulement d'air formant tampon vers un compartiment de palier
US9617916B2 (en) * 2012-11-28 2017-04-11 Pratt & Whitney Canada Corp. Gas turbine engine with bearing buffer air flow and method
WO2014159505A1 (fr) 2013-03-14 2014-10-02 United Technologies Corporation Collecteur d'échangeur de chaleur de moteur à turbine à gaz
WO2015088635A2 (fr) 2013-12-13 2015-06-18 United Technologies Corporation Déflecteur d'huile à refroidissement par convection de surface radiale
FR3016661B1 (fr) * 2014-01-23 2019-05-03 Safran Aircraft Engines Enceinte de palier d'une turbomachine
US11808210B2 (en) * 2015-02-12 2023-11-07 Rtx Corporation Intercooled cooling air with heat exchanger packaging
US10196932B2 (en) * 2015-12-08 2019-02-05 General Electric Company OGV heat exchangers networked in parallel and serial flow
US11125160B2 (en) * 2015-12-28 2021-09-21 General Electric Company Method and system for combination heat exchanger
US20170211417A1 (en) * 2016-01-21 2017-07-27 United Technologies Corporation Systems and methods for cooling a bearing
US10823061B2 (en) 2016-07-15 2020-11-03 General Electric Company Engine air inlet having a double-panel heated wall
US10422246B2 (en) 2016-10-24 2019-09-24 General Electric Company Bearing housing with impingement cooling system
US10830448B2 (en) * 2016-10-26 2020-11-10 Raytheon Technologies Corporation Combustor liner panel with a multiple of heat transfer augmentors for a gas turbine engine combustor
US9840938B1 (en) * 2016-12-07 2017-12-12 Pratt & Whitney Canada Corp. Housing for bearing cavity in a gas turbine engine
EP3450722B1 (fr) * 2017-08-31 2024-02-14 General Electric Company Système de distribution d'air pour moteur à turbine à gaz
US10781709B2 (en) 2018-01-09 2020-09-22 General Electric Company Turbine engine with a seal
RU181987U1 (ru) * 2018-02-01 2018-07-31 Ао "Вникти" Система для охлаждения опоры подшипников газотурбинного двигателя при его аварийной остановке
RU2679573C1 (ru) * 2018-02-16 2019-02-11 Валерий Николаевич Сиротин Система охлаждения подшипников турбин газотурбинного двигателя
FR3078367B1 (fr) * 2018-02-23 2021-09-03 Safran Aircraft Engines Turbomachine comportant un echangeur de chaleur dans la veine secondaire
US11199103B2 (en) 2018-09-06 2021-12-14 General Electric Company Seal assembly for a turbomachine
US10648510B1 (en) * 2018-10-17 2020-05-12 Pratt & Whitney Canada Corp. Baffle for installation inside a bearing chamber of a gas turbine engine
US11692479B2 (en) * 2019-10-03 2023-07-04 General Electric Company Heat exchanger with active buffer layer
US11560843B2 (en) 2020-02-25 2023-01-24 General Electric Company Frame for a heat engine
US11255264B2 (en) 2020-02-25 2022-02-22 General Electric Company Frame for a heat engine
US11326519B2 (en) 2020-02-25 2022-05-10 General Electric Company Frame for a heat engine
US11459909B2 (en) * 2020-09-15 2022-10-04 Pratt & Whitney Canada Corp. Rotating heat exchanger
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US11834992B2 (en) 2022-04-27 2023-12-05 General Electric Company Heat exchanger capacity for one or more heat exchangers associated with an accessory gearbox of a turbofan engine
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Also Published As

Publication number Publication date
FR2557207A1 (fr) 1985-06-28
JPH0474532B2 (fr) 1992-11-26
GB2152589A (en) 1985-08-07
DE3447717A1 (de) 1985-07-04
US4542623A (en) 1985-09-24
GB2152589B (en) 1987-10-14
DE3447717C2 (de) 1998-02-12
GB8431264D0 (en) 1985-01-23
JPS60142021A (ja) 1985-07-27

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