FR2557203B1 - Turbomoteur a gaz et methode de fonctionnement - Google Patents

Turbomoteur a gaz et methode de fonctionnement

Info

Publication number
FR2557203B1
FR2557203B1 FR848419766A FR8419766A FR2557203B1 FR 2557203 B1 FR2557203 B1 FR 2557203B1 FR 848419766 A FR848419766 A FR 848419766A FR 8419766 A FR8419766 A FR 8419766A FR 2557203 B1 FR2557203 B1 FR 2557203B1
Authority
FR
France
Prior art keywords
turbomotor
gas
operating method
operating
gas turbomotor
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 - Fee Related
Application number
FR848419766A
Other languages
English (en)
Other versions
FR2557203A1 (fr
Inventor
Edward J Hovan
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 FR2557203A1 publication Critical patent/FR2557203A1/fr
Application granted granted Critical
Publication of FR2557203B1 publication Critical patent/FR2557203B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F01D25/08—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
    • F01D25/183—Sealing means
    • 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
    • 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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR848419766A 1983-12-23 1984-12-24 Turbomoteur a gaz et methode de fonctionnement Expired - Fee Related FR2557203B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/564,996 US4561246A (en) 1983-12-23 1983-12-23 Bearing compartment for a gas turbine engine

Publications (2)

Publication Number Publication Date
FR2557203A1 FR2557203A1 (fr) 1985-06-28
FR2557203B1 true FR2557203B1 (fr) 1991-09-06

Family

ID=24256772

Family Applications (1)

Application Number Title Priority Date Filing Date
FR848419766A Expired - Fee Related FR2557203B1 (fr) 1983-12-23 1984-12-24 Turbomoteur a gaz et methode de fonctionnement

Country Status (5)

Country Link
US (1) US4561246A (fr)
JP (1) JPS60142022A (fr)
DE (1) DE3447740C2 (fr)
FR (1) FR2557203B1 (fr)
GB (1) GB2152148B (fr)

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DE4435322B4 (de) * 1994-10-01 2005-05-04 Alstom Verfahren und Vorrichtung zur Wellendichtung und zur Kühlung auf der Abgasseite einer axialdurchströmten Gasturbine
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JP4153446B2 (ja) * 2004-02-19 2008-09-24 株式会社日立製作所 ガスタービン
FR2877036B1 (fr) * 2004-10-27 2006-12-22 Snecma Moteurs Sa Dispositif de lubrification d'un composant dans une turbomachine
US7458202B2 (en) * 2004-10-29 2008-12-02 General Electric Company Lubrication system for a counter-rotating turbine engine and method of assembling same
US7287384B2 (en) * 2004-12-13 2007-10-30 Pratt & Whitney Canada Corp. Bearing chamber pressurization system
ITMI20061086A1 (it) * 2006-06-01 2007-12-02 Nuovo Pignone Spa Dispositivo per ottimizzare il raffreddamento nelle turbine a gas
US7828513B2 (en) * 2006-10-05 2010-11-09 Pratt & Whitney Canada Corp. Air seal arrangement for a gas turbine engine
US7748209B1 (en) 2006-12-08 2010-07-06 Florida Turbine Technologies, Inc. Small single use gas turbine engine with oil-less bearing arrangement
US8215895B2 (en) * 2008-03-03 2012-07-10 Rolls-Royce Corporation Vapor phase lubrication system
US8240974B2 (en) 2008-03-21 2012-08-14 United Technologies Corporation Cold air buffer supply tube
US8192151B2 (en) 2009-04-29 2012-06-05 General Electric Company Turbine engine having cooling gland
US8561411B2 (en) * 2009-09-02 2013-10-22 United Technologies Corporation Air particle separator for a gas turbine engine
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JP5539131B2 (ja) * 2010-09-14 2014-07-02 株式会社日立製作所 ２軸式ガスタービンの内周抽気構造
US9506402B2 (en) * 2011-07-29 2016-11-29 United Technologies Corporation Three spool engine bearing configuration
US9260191B2 (en) * 2011-08-26 2016-02-16 Hs Marston Aerospace Ltd. Heat exhanger apparatus including heat transfer surfaces
US8967944B2 (en) 2011-08-29 2015-03-03 United Technologies Corporation Accessory gearbox buffer cooling air pump system
US9200569B2 (en) 2011-10-21 2015-12-01 United Technologies Corporation Compartment cooling for a gas turbine engine
US20130192240A1 (en) 2012-01-31 2013-08-01 Peter M. Munsell Buffer system for a gas turbine engine
US8769962B2 (en) 2012-01-31 2014-07-08 United Technologies Corporation Multi-circuit buffer system for a gas turbine engine
US9435259B2 (en) 2012-02-27 2016-09-06 United Technologies Corporation Gas turbine engine cooling system
US9347374B2 (en) 2012-02-27 2016-05-24 United Technologies Corporation Gas turbine engine buffer cooling system
US9157325B2 (en) 2012-02-27 2015-10-13 United Technologies Corporation Buffer cooling system providing gas turbine engine architecture cooling
US9038398B2 (en) * 2012-02-27 2015-05-26 United Technologies Corporation Gas turbine engine buffer cooling system
US9353647B2 (en) 2012-04-27 2016-05-31 General Electric Company Wide discourager tooth
US9567908B2 (en) * 2012-04-27 2017-02-14 General Electric Company Mitigating vortex pumping effect upstream of oil seal
US9599410B2 (en) 2012-07-27 2017-03-21 General Electric Company Plate-like air-cooled engine surface cooler with fluid channel and varying fin geometry
US9234439B2 (en) 2012-11-01 2016-01-12 United Technologies Corporation Gas turbine engine with bearing compartment wall cooling
US9316153B2 (en) 2013-01-22 2016-04-19 Siemens Energy, Inc. Purge and cooling air for an exhaust section of a gas turbine assembly
EP2971688B1 (fr) * 2013-03-14 2018-11-28 United Technologies Corporation Turbine à gaz avec une protection thermique et procédé de montage d'un telle protection
DE102013213520A1 (de) * 2013-07-10 2015-01-15 Rolls-Royce Deutschland Ltd & Co Kg Vorrichtung und Verfahren zum Ableiten von Sperrluft in einem Turbofan-Triebwerk
JP2016528436A (ja) * 2013-08-16 2016-09-15 ゼネラル・エレクトリック・カンパニイ 流れ渦スポイラ
US10677161B2 (en) * 2013-08-28 2020-06-09 Raytheon Technologies Corporation Gas turbine engine diffuser cooling and mixing arrangement
US9926797B2 (en) * 2015-01-22 2018-03-27 United Technologies Corporation Flange trapped seal configuration
US10215098B2 (en) 2015-01-22 2019-02-26 United Technologies Corporation Bearing compartment seal
US10161256B2 (en) 2015-01-22 2018-12-25 Untied Technologies Corporation Seal with backup seal
US11808210B2 (en) 2015-02-12 2023-11-07 Rtx Corporation Intercooled cooling air with heat exchanger packaging
US10731560B2 (en) 2015-02-12 2020-08-04 Raytheon Technologies Corporation Intercooled cooling air
US10371055B2 (en) 2015-02-12 2019-08-06 United Technologies Corporation Intercooled cooling air using cooling compressor as starter
US10480419B2 (en) 2015-04-24 2019-11-19 United Technologies Corporation Intercooled cooling air with plural heat exchangers
US10830148B2 (en) 2015-04-24 2020-11-10 Raytheon Technologies Corporation Intercooled cooling air with dual pass heat exchanger
US10221862B2 (en) 2015-04-24 2019-03-05 United Technologies Corporation Intercooled cooling air tapped from plural locations
US10100739B2 (en) 2015-05-18 2018-10-16 United Technologies Corporation Cooled cooling air system for a gas turbine engine
EP3109438B1 (fr) * 2015-06-22 2019-09-18 United Technologies Corporation Air de refroidissement refroidi avec une pluralité d'échangeurs de chaleur
US10794288B2 (en) 2015-07-07 2020-10-06 Raytheon Technologies Corporation Cooled cooling air system for a turbofan engine
US10443508B2 (en) 2015-12-14 2019-10-15 United Technologies Corporation Intercooled cooling air with auxiliary compressor control
US10669940B2 (en) 2016-09-19 2020-06-02 Raytheon Technologies Corporation Gas turbine engine with intercooled cooling air and turbine drive
US10422246B2 (en) 2016-10-24 2019-09-24 General Electric Company Bearing housing with impingement cooling system
US10550768B2 (en) 2016-11-08 2020-02-04 United Technologies Corporation Intercooled cooled cooling integrated air cycle machine
US10794290B2 (en) 2016-11-08 2020-10-06 Raytheon Technologies Corporation Intercooled cooled cooling integrated air cycle machine
US10961911B2 (en) 2017-01-17 2021-03-30 Raytheon Technologies Corporation Injection cooled cooling air system for a gas turbine engine
US10995673B2 (en) 2017-01-19 2021-05-04 Raytheon Technologies Corporation Gas turbine engine with intercooled cooling air and dual towershaft accessory gearbox
US10577964B2 (en) 2017-03-31 2020-03-03 United Technologies Corporation Cooled cooling air for blade air seal through outer chamber
US10711640B2 (en) 2017-04-11 2020-07-14 Raytheon Technologies Corporation Cooled cooling air to blade outer air seal passing through a static vane
EP3450722B1 (fr) * 2017-08-31 2024-02-14 General Electric Company Système de distribution d'air pour moteur à turbine à gaz
US10738703B2 (en) 2018-03-22 2020-08-11 Raytheon Technologies Corporation Intercooled cooling air with combined features
US10808619B2 (en) 2018-04-19 2020-10-20 Raytheon Technologies Corporation Intercooled cooling air with advanced cooling system
US10830145B2 (en) 2018-04-19 2020-11-10 Raytheon Technologies Corporation Intercooled cooling air fleet management system
US10718233B2 (en) 2018-06-19 2020-07-21 Raytheon Technologies Corporation Intercooled cooling air with low temperature bearing compartment air
US11255268B2 (en) 2018-07-31 2022-02-22 Raytheon Technologies Corporation Intercooled cooling air with selective pressure dump
US10697370B2 (en) 2018-08-30 2020-06-30 Rolls-Royce North American Technologies Inc. Oil supply assembly for gas turbine engine
US10837318B2 (en) * 2019-01-08 2020-11-17 Raytheon Technologies Corporation Buffer system for gas turbine engine
GB201911980D0 (en) * 2019-08-21 2019-10-02 Rolls Royce Plc Gas turbine engine
EP4023870A4 (fr) * 2019-08-30 2023-09-27 Kawasaki Jukogyo Kabushiki Kaisha Moteur à turbine à gaz
RU203516U1 (ru) * 2020-11-02 2021-04-08 Акционерное общество «Копейский машиностроительный завод» Подшипниковая опора зубчатого колеса горного комбайна
CN114810354B (zh) * 2021-01-29 2023-12-22 中国航发商用航空发动机有限责任公司 航空发动机
CN114542205B (zh) * 2022-02-11 2022-11-22 中国航发沈阳发动机研究所 一种高马赫航空发动机耐高温高压轴承腔结构

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Also Published As

Publication number Publication date
DE3447740A1 (de) 1985-07-04
JPS60142022A (ja) 1985-07-27
GB2152148B (en) 1987-08-26
GB8431276D0 (en) 1985-01-23
US4561246A (en) 1985-12-31
FR2557203A1 (fr) 1985-06-28
JPH0474533B2 (fr) 1992-11-26
DE3447740C2 (de) 1998-01-29
GB2152148A (en) 1985-07-31

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Legal Events

Date Code Title Description
ST Notification of lapse