SE8505155D0 - Kylbart statoraggregat for en roterande maskin - Google Patents

Kylbart statoraggregat for en roterande maskin

Info

Publication number
SE8505155D0
SE8505155D0 SE8505155A SE8505155A SE8505155D0 SE 8505155 D0 SE8505155 D0 SE 8505155D0 SE 8505155 A SE8505155 A SE 8505155A SE 8505155 A SE8505155 A SE 8505155A SE 8505155 D0 SE8505155 D0 SE 8505155D0
Authority
SE
Sweden
Prior art keywords
outer air
air seal
cooling
support
rotating machine
Prior art date
Application number
SE8505155A
Other languages
English (en)
Other versions
SE8505155L (sv
SE458545B (sv
Inventor
R H Weidner
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 SE8505155D0 publication Critical patent/SE8505155D0/sv
Publication of SE8505155L publication Critical patent/SE8505155L/sv
Publication of SE458545B publication Critical patent/SE458545B/sv

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
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • 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
    • F01D25/14—Casings modified therefor
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
SE8505155A 1984-12-05 1985-10-31 Saett att kyla ett statoraggregat samt kylbart statoraggregat SE458545B (sv)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/678,518 US4642024A (en) 1984-12-05 1984-12-05 Coolable stator assembly for a rotary machine

Publications (3)

Publication Number Publication Date
SE8505155D0 true SE8505155D0 (sv) 1985-10-31
SE8505155L SE8505155L (sv) 1986-06-06
SE458545B SE458545B (sv) 1989-04-10

Family

ID=24723129

Family Applications (1)

Application Number Title Priority Date Filing Date
SE8505155A SE458545B (sv) 1984-12-05 1985-10-31 Saett att kyla ett statoraggregat samt kylbart statoraggregat

Country Status (10)

Country Link
US (1) US4642024A (sv)
JP (1) JPH0756202B2 (sv)
CA (1) CA1212047A (sv)
CH (1) CH681243A5 (sv)
DE (1) DE3537043C2 (sv)
FR (1) FR2574115B1 (sv)
GB (1) GB2168110B (sv)
IL (1) IL76659A (sv)
IT (1) IT1186038B (sv)
SE (1) SE458545B (sv)

Families Citing this family (66)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4916906A (en) * 1988-03-25 1990-04-17 General Electric Company Breach-cooled structure
US4826397A (en) * 1988-06-29 1989-05-02 United Technologies Corporation Stator assembly for a gas turbine engine
US5039278A (en) * 1989-04-11 1991-08-13 General Electric Company Power turbine ventilation system
GB8921003D0 (en) * 1989-09-15 1989-11-01 Rolls Royce Plc Improvements in or relating to shroud rings
US5092735A (en) * 1990-07-02 1992-03-03 The United States Of America As Represented By The Secretary Of The Air Force Blade outer air seal cooling system
US5116199A (en) * 1990-12-20 1992-05-26 General Electric Company Blade tip clearance control apparatus using shroud segment annular support ring thermal expansion
US5080557A (en) * 1991-01-14 1992-01-14 General Motors Corporation Turbine blade shroud assembly
US5165847A (en) * 1991-05-20 1992-11-24 General Electric Company Tapered enlargement metering inlet channel for a shroud cooling assembly of gas turbine engines
US5176495A (en) * 1991-07-09 1993-01-05 General Electric Company Thermal shielding apparatus or radiositor for a gas turbine engine
US5188506A (en) * 1991-08-28 1993-02-23 General Electric Company Apparatus and method for preventing leakage of cooling air in a shroud assembly of a gas turbine engine
US5205708A (en) * 1992-02-07 1993-04-27 General Electric Company High pressure turbine component interference fit up
US5273396A (en) * 1992-06-22 1993-12-28 General Electric Company Arrangement for defining improved cooling airflow supply path through clearance control ring and shroud
US5249920A (en) * 1992-07-09 1993-10-05 General Electric Company Turbine nozzle seal arrangement
US5380150A (en) * 1993-11-08 1995-01-10 United Technologies Corporation Turbine shroud segment
US5374161A (en) * 1993-12-13 1994-12-20 United Technologies Corporation Blade outer air seal cooling enhanced with inter-segment film slot
US5584651A (en) * 1994-10-31 1996-12-17 General Electric Company Cooled shroud
GB9709086D0 (en) * 1997-05-07 1997-06-25 Rolls Royce Plc Gas turbine engine cooling apparatus
US6315519B1 (en) 1998-09-28 2001-11-13 General Electric Company Turbine inner shroud and turbine assembly containing such inner shroud
US6113349A (en) * 1998-09-28 2000-09-05 General Electric Company Turbine assembly containing an inner shroud
DE19855130A1 (de) * 1998-11-30 2000-05-31 Abb Alstom Power Ch Ag Kühlbarer Mantel einer Gasturbine oder dergleichen
DE50004728D1 (de) 1999-03-30 2004-01-22 Siemens Ag Strömungsmaschine mit einer kühlbaren anordnung von wandelementen und verfahren zur kühlung einer anordnung von wandelementen
DE19919654A1 (de) * 1999-04-29 2000-11-02 Abb Alstom Power Ch Ag Hitzeschild für eine Gasturbine
WO2001009553A1 (de) 1999-08-03 2001-02-08 Siemens Aktiengesellschaft Prallkühlvorrichtung
DE19938274A1 (de) 1999-08-12 2001-02-15 Asea Brown Boveri Vorrichtung und Verfahren zur geziehlten Spalteinstellung zwischen Stator- und Rotoranordnung einer Strömungsmaschine
JP4622074B2 (ja) * 2000-09-28 2011-02-02 株式会社Ｉｈｉ タービンシュラウド冷却構造
GB0029337D0 (en) 2000-12-01 2001-01-17 Rolls Royce Plc A seal segment for a turbine
DE10122695A1 (de) * 2001-05-10 2002-11-21 Siemens Ag Verfahren zur Kühlung einer Gasturbine und Gasturbinenanlage
US6877952B2 (en) * 2002-09-09 2005-04-12 Florida Turbine Technologies, Inc Passive clearance control
US8919781B2 (en) 2003-05-01 2014-12-30 Advanced Technologies Group, Inc. Self-adjusting non-contact seal
US8641045B2 (en) * 2003-05-01 2014-02-04 Advanced Technologies Group, Inc. Seal with stacked sealing elements
US7896352B2 (en) * 2003-05-01 2011-03-01 Justak John F Seal with stacked sealing elements
FR2869944B1 (fr) * 2004-05-04 2006-08-11 Snecma Moteurs Sa Dispositif de refroidissement pour anneau fixe de turbine a gaz
US20070020088A1 (en) * 2005-07-20 2007-01-25 Pratt & Whitney Canada Corp. Turbine shroud segment impingement cooling on vane outer shroud
US7520715B2 (en) * 2005-07-19 2009-04-21 Pratt & Whitney Canada Corp. Turbine shroud segment transpiration cooling with individual cast inlet and outlet cavities
US7374395B2 (en) * 2005-07-19 2008-05-20 Pratt & Whitney Canada Corp. Turbine shroud segment feather seal located in radial shroud legs
FR2891300A1 (fr) * 2005-09-23 2007-03-30 Snecma Sa Dispositif de controle de jeu dans une turbine a gaz
US8439629B2 (en) * 2007-03-01 2013-05-14 United Technologies Corporation Blade outer air seal
US8123466B2 (en) * 2007-03-01 2012-02-28 United Technologies Corporation Blade outer air seal
US8240980B1 (en) 2007-10-19 2012-08-14 Florida Turbine Technologies, Inc. Turbine inter-stage gap cooling and sealing arrangement
FR2922589B1 (fr) * 2007-10-22 2009-12-04 Snecma Controle du jeu en sommet d'aubes dans une turbine haute-pression de turbomachine
US8177492B2 (en) * 2008-03-04 2012-05-15 United Technologies Corporation Passage obstruction for improved inlet coolant filling
US8038399B1 (en) * 2008-11-22 2011-10-18 Florida Turbine Technologies, Inc. Turbine rim cavity sealing
US20110044803A1 (en) * 2009-08-18 2011-02-24 Pratt & Whitney Canada Corp. Blade outer air seal anti-rotation
FR2972483B1 (fr) * 2011-03-07 2013-04-19 Snecma Carter de turbine comportant des moyens de fixation de secteurs d'anneau
US8826668B2 (en) * 2011-08-02 2014-09-09 Siemens Energy, Inc. Two stage serial impingement cooling for isogrid structures
US8920116B2 (en) * 2011-10-07 2014-12-30 Siemens Energy, Inc. Wear prevention system for securing compressor airfoils within a turbine engine
US9103225B2 (en) * 2012-06-04 2015-08-11 United Technologies Corporation Blade outer air seal with cored passages
US9803491B2 (en) 2012-12-31 2017-10-31 United Technologies Corporation Blade outer air seal having shiplap structure
US10100737B2 (en) * 2013-05-16 2018-10-16 Siemens Energy, Inc. Impingement cooling arrangement having a snap-in plate
EP3102794B1 (en) * 2014-01-27 2019-12-18 United Technologies Corporation Blade outer air seal mount
US10662792B2 (en) * 2014-02-03 2020-05-26 Raytheon Technologies Corporation Gas turbine engine cooling fluid composite tube
US10145308B2 (en) * 2014-02-10 2018-12-04 United Technologies Corporation Gas turbine engine ring seal
US10590785B2 (en) * 2014-09-09 2020-03-17 United Technologies Corporation Beveled coverplate
US10301956B2 (en) 2014-09-25 2019-05-28 United Technologies Corporation Seal assembly for sealing an axial gap between components
CA2916710A1 (en) * 2015-01-29 2016-07-29 Rolls-Royce Corporation Seals for gas turbine engines
US10385718B2 (en) 2015-06-29 2019-08-20 Rolls-Royce North American Technologies, Inc. Turbine shroud segment with side perimeter seal
US10047624B2 (en) * 2015-06-29 2018-08-14 Rolls-Royce North American Technologies Inc. Turbine shroud segment with flange-facing perimeter seal
US10094234B2 (en) 2015-06-29 2018-10-09 Rolls-Royce North America Technologies Inc. Turbine shroud segment with buffer air seal system
US10196919B2 (en) 2015-06-29 2019-02-05 Rolls-Royce North American Technologies Inc. Turbine shroud segment with load distribution springs
US10767863B2 (en) * 2015-07-22 2020-09-08 Rolls-Royce North American Technologies, Inc. Combustor tile with monolithic inserts
JP6546481B2 (ja) * 2015-08-31 2019-07-17 川崎重工業株式会社 排気ディフューザ
EP3141702A1 (en) * 2015-09-14 2017-03-15 Siemens Aktiengesellschaft Gas turbine guide vane segment and method of manufacturing
US10329941B2 (en) 2016-05-06 2019-06-25 United Technologies Corporation Impingement manifold
DE102016217320A1 (de) * 2016-09-12 2018-03-15 Siemens Aktiengesellschaft Gasturbine mit getrennter Kühlung für Turbine und Abgasgehäuse
US10533446B2 (en) * 2017-05-15 2020-01-14 United Technologies Corporation Alternative W-seal groove arrangement
US11903101B2 (en) 2019-12-13 2024-02-13 Goodrich Corporation Internal heating trace assembly

Family Cites Families (39)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR957575A (sv) * 1946-10-02 1950-02-23
GB702931A (en) * 1951-04-18 1954-01-27 Bristol Aeroplane Co Ltd Improvements in or relating to rotary machines comprising fluid compressing means
BE514728A (sv) * 1951-10-10
GB753224A (en) * 1953-04-13 1956-07-18 Rolls Royce Improvements in or relating to blading for turbines or compressors
US2787440A (en) * 1953-05-21 1957-04-02 Westinghouse Electric Corp Turbine apparatus
US2859934A (en) * 1953-07-29 1958-11-11 Havilland Engine Co Ltd Gas turbines
US2977090A (en) * 1956-06-12 1961-03-28 Daniel J Mccarty Heat responsive means for blade cooling
US3365172A (en) * 1966-11-02 1968-01-23 Gen Electric Air cooled shroud seal
US3391904A (en) * 1966-11-02 1968-07-09 United Aircraft Corp Optimum response tip seal
US3411794A (en) * 1966-12-12 1968-11-19 Gen Motors Corp Cooled seal ring
GB1266505A (sv) * 1968-09-17 1972-03-08
US3736069A (en) * 1968-10-28 1973-05-29 Gen Motors Corp Turbine stator cooling control
US3814313A (en) * 1968-10-28 1974-06-04 Gen Motors Corp Turbine cooling control valve
US3575528A (en) * 1968-10-28 1971-04-20 Gen Motors Corp Turbine rotor cooling
BE756582A (fr) * 1969-10-02 1971-03-01 Gen Electric Ecran circulaire et support d'ecran avec dispositif de reglage de la temperature pour turbomachine
US3603599A (en) * 1970-05-06 1971-09-07 Gen Motors Corp Cooled seal
US3742705A (en) * 1970-12-28 1973-07-03 United Aircraft Corp Thermal response shroud for rotating body
US3825364A (en) * 1972-06-09 1974-07-23 Gen Electric Porous abradable turbine shroud
US3836279A (en) * 1973-02-23 1974-09-17 United Aircraft Corp Seal means for blade and shroud
US3864056A (en) * 1973-07-27 1975-02-04 Westinghouse Electric Corp Cooled turbine blade ring assembly
US3965066A (en) * 1974-03-15 1976-06-22 General Electric Company Combustor-turbine nozzle interconnection
US4023919A (en) * 1974-12-19 1977-05-17 General Electric Company Thermal actuated valve for clearance control
US3966356A (en) * 1975-09-22 1976-06-29 General Motors Corporation Blade tip seal mount
GB1484288A (en) * 1975-12-03 1977-09-01 Rolls Royce Gas turbine engines
JPS5284351A (en) * 1975-12-30 1977-07-13 Hitachi Ltd Axial sealer for rotor
US4127357A (en) * 1977-06-24 1978-11-28 General Electric Company Variable shroud for a turbomachine
US4177004A (en) * 1977-10-31 1979-12-04 General Electric Company Combined turbine shroud and vane support structure
US4157232A (en) * 1977-10-31 1979-06-05 General Electric Company Turbine shroud support
FR2416345A1 (fr) * 1978-01-31 1979-08-31 Snecma Dispositif de refroidissement par impact des segments d'etancheite de turbine d'un turboreacteur
US4251185A (en) * 1978-05-01 1981-02-17 Caterpillar Tractor Co. Expansion control ring for a turbine shroud assembly
US4247248A (en) * 1978-12-20 1981-01-27 United Technologies Corporation Outer air seal support structure for gas turbine engine
GB2047354B (en) * 1979-04-26 1983-03-30 Rolls Royce Gas turbine engines
US4337016A (en) * 1979-12-13 1982-06-29 United Technologies Corporation Dual wall seal means
GB2076071B (en) * 1980-05-16 1983-11-02 United Technologies Corp Flow directing assembly for a gas turbine engine
GB2081817B (en) * 1980-08-08 1984-02-15 Rolls Royce Turbine blade shrouding
US4526226A (en) * 1981-08-31 1985-07-02 General Electric Company Multiple-impingement cooled structure
GB2117843B (en) * 1982-04-01 1985-11-06 Rolls Royce Compressor shrouds
FR2540937B1 (fr) * 1983-02-10 1987-05-22 Snecma Anneau pour un rotor de turbine d'une turbomachine
US4541775A (en) * 1983-03-30 1985-09-17 United Technologies Corporation Clearance control in turbine seals

Also Published As

Publication number Publication date
DE3537043A1 (de) 1986-06-05
IL76659A0 (en) 1986-02-28
IT1186038B (it) 1987-11-18
DE3537043C2 (de) 1997-06-19
GB8524590D0 (en) 1985-11-06
US4642024A (en) 1987-02-10
GB2168110B (en) 1988-06-08
IT8522685A0 (it) 1985-10-31
JPS61135904A (ja) 1986-06-23
CH681243A5 (sv) 1993-02-15
CA1212047A (en) 1986-09-30
FR2574115A1 (fr) 1986-06-06
FR2574115B1 (fr) 1992-04-24
SE8505155L (sv) 1986-06-06
JPH0756202B2 (ja) 1995-06-14
GB2168110A (en) 1986-06-11
IL76659A (en) 1994-11-28
SE458545B (sv) 1989-04-10

Similar Documents

Publication Publication Date Title
SE8505155L (sv) Kylbart statoraggregat for en roterande maskin
US5649806A (en) Enhanced film cooling slot for turbine blade outer air seals
US5092735A (en) Blade outer air seal cooling system
US4820116A (en) Turbine cooling for gas turbine engine
US4348157A (en) Air cooled turbine for a gas turbine engine
US5660523A (en) Turbine blade squealer tip peripheral end wall with cooling passage arrangement
US4526226A (en) Multiple-impingement cooled structure
US4650394A (en) Coolable seal assembly for a gas turbine engine
US5927942A (en) Mounting and sealing arrangement for a turbine shroud segment
US5609469A (en) Rotor assembly shroud
US4688988A (en) Coolable stator assembly for a gas turbine engine
US7104751B2 (en) Hot gas path assembly
CA2229883A1 (en) Gas turbine shroud and platform seal system
GB1601422A (en) Tip cooling for turbomachinery blades
US5706646A (en) Gas turbine gas duct arrangement
GB1298643A (en) Labyrinth seals for high temperature machines
ATE280896T1 (de) Ventilatorverkleidung
SE8803527D0 (sv) Gasturbinmotorfoerstaerkare
GB825967A (en) Improvements in turbines and in particular gas turbines
SE8502035D0 (sv) Roterande tetning
GB2239679A (en) Self-cooling joint connection for abutting segments in a gas turbine engine
KR920006617A (ko) 가스 터어빈 베인 구조체의 차등적인 열팽창을 최소화시키기 위한 장치 및 방법
GB1177410A (en) Improvements in Gas Turbine Engine Turbine Rotor Shrouds
GB2253012A (en) Blade tip clearance control apparatus
CA2151761A1 (en) Expansion Turbine for Cryogenic Rectification System

Legal Events

Date Code Title Description
NAL Patent in force

Ref document number: 8505155-5

Format of ref document f/p: F

NUG Patent has lapsed