IT8522684A0 - Segmento di tenuta raffreddabile per una macchina rotativa. - Google Patents

Segmento di tenuta raffreddabile per una macchina rotativa.

Info

Publication number
IT8522684A0
IT8522684A0 IT8522684A IT2268485A IT8522684A0 IT 8522684 A0 IT8522684 A0 IT 8522684A0 IT 8522684 A IT8522684 A IT 8522684A IT 2268485 A IT2268485 A IT 2268485A IT 8522684 A0 IT8522684 A0 IT 8522684A0
Authority
IT
Italy
Prior art keywords
coolable
rotary machine
seal segment
segment
seal
Prior art date
Application number
IT8522684A
Other languages
English (en)
Other versions
IT1186037B (it
Inventor
Robert 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 IT8522684A0 publication Critical patent/IT8522684A0/it
Application granted granted Critical
Publication of IT1186037B publication Critical patent/IT1186037B/it

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
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246—Fastening of diaphragms or stator-rings
    • 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
    • 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
    • F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
    • F01D11/122—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with erodable or abradable material
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/201—Heat transfer, e.g. cooling by impingement of a fluid
    • 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)
IT8522684A 1984-12-21 1985-10-31 Segmento di tenuta raffreddabile per una macchina rotativa IT1186037B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/684,657 US4650395A (en) 1984-12-21 1984-12-21 Coolable seal segment for a rotary machine

Publications (2)

Publication Number Publication Date
IT8522684A0 true IT8522684A0 (it) 1985-10-31
IT1186037B IT1186037B (it) 1987-11-18

Family

ID=24748997

Family Applications (1)

Application Number Title Priority Date Filing Date
IT8522684A IT1186037B (it) 1984-12-21 1985-10-31 Segmento di tenuta raffreddabile per una macchina rotativa

Country Status (10)

Country Link
US (1) US4650395A (it)
JP (1) JPH0689654B2 (it)
CA (1) CA1235070A (it)
CH (1) CH669976A5 (it)
DE (1) DE3537044C2 (it)
FR (1) FR2575224B1 (it)
GB (1) GB2169037B (it)
IL (1) IL76660A (it)
IT (1) IT1186037B (it)
SE (1) SE458624B (it)

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FR2723144B1 (fr) * 1984-11-29 1996-12-13 Snecma Distributeur de turbine
FR2603947B1 (fr) * 1986-09-17 1990-11-30 Snecma Dispositif de maintien d'un joint d'etancheite sur un bout d'arbre et turbomachine le comportant
JPH0158807U (it) * 1987-10-07 1989-04-13
GB8921003D0 (en) * 1989-09-15 1989-11-01 Rolls Royce Plc Improvements in or relating to shroud rings
GB2239678B (en) * 1989-12-08 1993-03-03 Rolls Royce Plc Gas turbine engine blade shroud assembly
US5071313A (en) * 1990-01-16 1991-12-10 General Electric Company Rotor blade shroud segment
EP0447886B1 (de) * 1990-03-23 1994-07-13 Asea Brown Boveri Ag Axialdurchströmte Gasturbine
GB2245316B (en) * 1990-06-21 1993-12-15 Rolls Royce Plc Improvements in shroud assemblies for turbine rotors
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
JPH07503298A (ja) * 1992-11-24 1995-04-06 ユナイテッド　テクノロジーズ　コーポレイション タービン用の冷却可能なアウタエアシール装置
US5333992A (en) * 1993-02-05 1994-08-02 United Technologies Corporation Coolable outer air seal assembly for a gas turbine engine
US5486090A (en) * 1994-03-30 1996-01-23 United Technologies Corporation Turbine shroud segment with serpentine cooling channels
US5439348A (en) * 1994-03-30 1995-08-08 United Technologies Corporation Turbine shroud segment including a coating layer having varying thickness
US5423659A (en) * 1994-04-28 1995-06-13 United Technologies Corporation Shroud segment having a cut-back retaining hook
US5538393A (en) * 1995-01-31 1996-07-23 United Technologies Corporation Turbine shroud segment with serpentine cooling channels having a bend passage
WO2001066914A1 (fr) * 2000-03-07 2001-09-13 Mitsubishi Heavy Industries, Ltd. Anneau fendu de turbine a gaz
FR2857406B1 (fr) * 2003-07-10 2005-09-30 Snecma Moteurs Refroidissement des anneaux de turbine
DE10334698A1 (de) * 2003-07-25 2005-02-10 Rolls-Royce Deutschland Ltd & Co Kg Deckbandsegment für eine Strömungsmaschine
US7546683B2 (en) * 2003-12-29 2009-06-16 General Electric Company Touch-up of layer paint oxides for gas turbine disks and seals
US7771160B2 (en) * 2006-08-10 2010-08-10 United Technologies Corporation Ceramic shroud assembly
US7665960B2 (en) 2006-08-10 2010-02-23 United Technologies Corporation Turbine shroud thermal distortion control
US7871244B2 (en) * 2007-02-15 2011-01-18 Siemens Energy, Inc. Ring seal for a turbine engine
GB0703827D0 (en) 2007-02-28 2007-04-11 Rolls Royce Plc Rotor seal segment
US8206092B2 (en) * 2007-12-05 2012-06-26 United Technologies Corp. Gas turbine engines and related systems involving blade outer air seals
US8177492B2 (en) * 2008-03-04 2012-05-15 United Technologies Corporation Passage obstruction for improved inlet coolant filling
US20110044803A1 (en) * 2009-08-18 2011-02-24 Pratt & Whitney Canada Corp. Blade outer air seal anti-rotation
US8167546B2 (en) * 2009-09-01 2012-05-01 United Technologies Corporation Ceramic turbine shroud support
US8303245B2 (en) * 2009-10-09 2012-11-06 General Electric Company Shroud assembly with discourager
US8439636B1 (en) * 2009-10-20 2013-05-14 Florida Turbine Technologies, Inc. Turbine blade outer air seal
JP5920856B2 (ja) * 2012-01-26 2016-05-18 ゼネラル エレクトリック テクノロジー ゲゼルシャフト ミット ベシュレンクテル ハフツングＧｅｎｅｒａｌ Ｅｌｅｃｔｒｉｃ Ｔｅｃｈｎｏｌｏｇｙ ＧｍｂＨ ターボ機械用のセグメント化された内環を備えるステータ構成部材
US9316109B2 (en) * 2012-04-10 2016-04-19 General Electric Company Turbine shroud assembly and method of forming
US9617866B2 (en) 2012-07-27 2017-04-11 United Technologies Corporation Blade outer air seal for a gas turbine engine
US10577963B2 (en) * 2014-01-20 2020-03-03 United Technologies Corporation Retention clip for a blade outer air seal
US10458264B2 (en) * 2015-05-05 2019-10-29 United Technologies Corporation Seal arrangement for turbine engine component
FR3036432B1 (fr) * 2015-05-22 2019-04-19 Safran Ceramics Ensemble d'anneau de turbine avec maintien axial
US10132184B2 (en) * 2016-03-16 2018-11-20 United Technologies Corporation Boas spring loaded rail shield
US10161258B2 (en) * 2016-03-16 2018-12-25 United Technologies Corporation Boas rail shield
US10329941B2 (en) 2016-05-06 2019-06-25 United Technologies Corporation Impingement manifold
US10544683B2 (en) 2016-08-30 2020-01-28 Rolls-Royce Corporation Air-film cooled component for a gas turbine engine
FR3058755B1 (fr) * 2016-11-15 2020-09-25 Safran Aircraft Engines Turbine pour turbomachine

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BE514728A (it) * 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 (it) * 1968-09-17 1972-03-08
US3575528A (en) * 1968-10-28 1971-04-20 Gen Motors Corp Turbine rotor cooling
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
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
US3817719A (en) * 1971-07-09 1974-06-18 United Aircraft Corp High temperature abradable material and method of preparing the same
US3879831A (en) * 1971-11-15 1975-04-29 United Aircraft Corp Nickle base high temperature abradable material
US3781125A (en) * 1972-04-07 1973-12-25 Westinghouse Electric Corp Gas turbine nozzle vane structure
US3836279A (en) * 1973-02-23 1974-09-17 United Aircraft Corp Seal means for blade and shroud
US4109003A (en) * 1974-03-12 1978-08-22 Smith Kline & French Laboratories Limited Pharmacologically active compounds
US3965066A (en) * 1974-03-15 1976-06-22 General Electric Company Combustor-turbine nozzle interconnection
US3918925A (en) * 1974-05-13 1975-11-11 United Technologies Corp Abradable seal
US3936656A (en) * 1974-12-16 1976-02-03 United Technologies Corporation Method of affixing an abradable metallic fiber material to a metal substrate
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
US4076451A (en) * 1976-03-05 1978-02-28 United Technologies Corporation Ceramic turbine stator
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
US4247248A (en) * 1978-12-20 1981-01-27 United Technologies Corporation Outer air seal support structure for gas turbine engine
US4273824A (en) * 1979-05-11 1981-06-16 United Technologies Corporation Ceramic faced structures and methods for manufacture thereof
US4289446A (en) * 1979-06-27 1981-09-15 United Technologies Corporation Ceramic faced outer air seal for gas turbine engines
US4337016A (en) * 1979-12-13 1982-06-29 United Technologies Corporation Dual wall seal means
IL62818A (en) * 1980-05-16 1985-08-30 United Technologies Corp Flow directing assembly for a gas turbine engine
US4431373A (en) * 1980-05-16 1984-02-14 United Technologies Corporation Flow directing assembly for a gas turbine engine
GB2081817B (en) * 1980-08-08 1984-02-15 Rolls Royce Turbine blade shrouding
GB2117843B (en) * 1982-04-01 1985-11-06 Rolls Royce Compressor shrouds
US4422648A (en) * 1982-06-17 1983-12-27 United Technologies Corporation Ceramic faced outer air seal for gas turbine engines
US4650394A (en) * 1984-11-13 1987-03-17 United Technologies Corporation Coolable seal assembly for a gas turbine engine

Also Published As

Publication number Publication date
CH669976A5 (it) 1989-04-28
IL76660A0 (en) 1986-02-28
FR2575224A1 (fr) 1986-06-27
CA1235070A (en) 1988-04-12
GB2169037A (en) 1986-07-02
GB2169037B (en) 1989-09-20
DE3537044A1 (de) 1986-06-26
DE3537044C2 (de) 1997-03-13
JPS61157704A (ja) 1986-07-17
IT1186037B (it) 1987-11-18
JPH0689654B2 (ja) 1994-11-09
SE458624B (sv) 1989-04-17
GB8524592D0 (en) 1985-11-06
US4650395A (en) 1987-03-17
SE8505156D0 (sv) 1985-10-31
IL76660A (en) 1992-03-29
SE8505156L (sv) 1986-06-22
FR2575224B1 (fr) 1993-10-15

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Legal Events

Date Code Title Description
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19950929