FR2164215A5 - - Google Patents

Info

Publication number
FR2164215A5
FR2164215A5 FR7242682A FR7242682A FR2164215A5 FR 2164215 A5 FR2164215 A5 FR 2164215A5 FR 7242682 A FR7242682 A FR 7242682A FR 7242682 A FR7242682 A FR 7242682A FR 2164215 A5 FR2164215 A5 FR 2164215A5
Authority
FR
France
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
Application number
FR7242682A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Application granted granted Critical
Publication of FR2164215A5 publication Critical patent/FR2164215A5/fr
Expired 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
    • 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
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/16—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means
    • F01D11/18—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means using stator or rotor components with predetermined thermal response, e.g. selective insulation, thermal inertia, differential expansion
FR7242682A 1971-12-01 1972-11-30 Expired FR2164215A5 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB5566571A GB1363897A (en) 1971-12-01 1971-12-01 Composite elongate member having a predetermined effective coeffi cient of linear expansion

Publications (1)

Publication Number Publication Date
FR2164215A5 true FR2164215A5 (fr) 1973-07-27

Family

ID=10474529

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7242682A Expired FR2164215A5 (fr) 1971-12-01 1972-11-30

Country Status (12)

Country Link
US (1) US3854843A (fr)
JP (1) JPS5138371B2 (fr)
AU (1) AU463454B2 (fr)
BE (1) BE792224A (fr)
CA (1) CA989312A (fr)
CH (1) CH561354A5 (fr)
DE (1) DE2258480A1 (fr)
FR (1) FR2164215A5 (fr)
GB (1) GB1363897A (fr)
IT (1) IT975912B (fr)
NL (1) NL7216110A (fr)
SE (1) SE385941B (fr)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2307965A1 (fr) * 1975-04-14 1976-11-12 Gen Electric Turbomachine a reglage du jeu radial entre des pieces tournantes et des pieces fixes
FR2371575A1 (fr) * 1976-11-22 1978-06-16 Gen Electric Structure de virole de turbine a gaz
EP0192512A1 (fr) * 1985-01-24 1986-08-27 Societe Europeenne De Propulsion (S.E.P.) S.A. Anneaux de turbine abradable et turbines ainsi obtenues
US4646810A (en) * 1984-10-30 1987-03-03 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Method for the manufacture of a ceramic turbine ring integral with a metallic annular carrier
EP0192556B1 (fr) * 1985-02-13 1989-05-24 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Carter de turbomachine associé à un dispositif pour ajuster le jeu entre aubes mobiles et carter
FR2662741A1 (fr) * 1990-05-31 1991-12-06 Gen Electric Stator pour turbine a gaz auquel est applique selectivement un revetement ayant une certaine conductivite thermique.
EP0616113A1 (fr) * 1993-03-01 1994-09-21 General Electric Company Support découplé pour garniture d'étanchéité

Families Citing this family (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5242906U (fr) * 1975-09-22 1977-03-26
JPS52127105U (fr) * 1976-03-25 1977-09-27
JPS52143312A (en) * 1976-05-24 1977-11-29 Hitachi Ltd Steam seal ring
US4411594A (en) * 1979-06-30 1983-10-25 Rolls-Royce Limited Support member and a component supported thereby
US4522559A (en) * 1982-02-19 1985-06-11 General Electric Company Compressor casing
US4485630A (en) * 1982-12-08 1984-12-04 General Electric Company Combustor liner
GB2165590B (en) * 1984-10-09 1988-05-05 Rolls Royce Improvements in or relating to rotor tip clearance control devices
US4768924A (en) * 1986-07-22 1988-09-06 Pratt & Whitney Canada Inc. Ceramic stator vane assembly
GB8921003D0 (en) * 1989-09-15 1989-11-01 Rolls Royce Plc Improvements in or relating to shroud rings
DE4309199A1 (de) * 1993-03-22 1994-09-29 Abb Management Ag Vorrichtung zur Befestigung von Wärmestausegmenten und Leitschaufeln in axialdurchströmten Turbinen
US5388959A (en) * 1993-08-23 1995-02-14 General Electric Company Seal including a non-metallic abradable material
FR2794816B1 (fr) * 1999-06-10 2001-07-06 Snecma Stator de compresseur a haute pression
US6382905B1 (en) * 2000-04-28 2002-05-07 General Electric Company Fan casing liner support
GB0015207D0 (en) * 2000-06-21 2000-08-09 Neyrfor Weir Ltd A turbine
US6896483B2 (en) * 2001-07-02 2005-05-24 Allison Advanced Development Company Blade track assembly
US6733235B2 (en) * 2002-03-28 2004-05-11 General Electric Company Shroud segment and assembly for a turbine engine
US7013718B2 (en) * 2003-04-28 2006-03-21 Watson Cogeneration Company Method for monitoring the performance of a turbine
CA2566359A1 (fr) * 2004-05-17 2006-05-04 L. James Cardarella, Jr. Renforcement de carter de turbine dans un moteur propulseur a turbine a gaz
GB2416194B (en) * 2004-07-15 2006-08-16 Rolls Royce Plc A spacer arrangement
US8191254B2 (en) * 2004-09-23 2012-06-05 Carlton Forge Works Method and apparatus for improving fan case containment and heat resistance in a gas turbine jet engine
US7484927B2 (en) * 2006-04-14 2009-02-03 General Electric Company Steam turbine variable clearance packing
US7686569B2 (en) * 2006-12-04 2010-03-30 Siemens Energy, Inc. Blade clearance system for a turbine engine
US8231338B2 (en) 2009-05-05 2012-07-31 General Electric Company Turbine shell with pin support
WO2013110792A1 (fr) * 2012-01-26 2013-08-01 Alstom Technology Ltd Élément formant stator pourvu d'une bague intérieure segmentée pour une turbomachine
WO2014130159A1 (fr) * 2013-02-23 2014-08-28 Ottow Nathan W Régulation du jeu entre des pales pour moteur à turbine à gaz
DE102013210876B4 (de) * 2013-06-11 2015-02-26 MTU Aero Engines AG Verbundbauteil zur thermischen Spaltsteuerung in einer Strömungsmaschine sowie dieses enthaltende Strömungsmaschine
DE102013212741A1 (de) * 2013-06-28 2014-12-31 Siemens Aktiengesellschaft Gasturbine und Hitzeschild für eine Gasturbine
FR3011608B1 (fr) * 2013-10-09 2016-05-27 Snecma Joint a labyrinthe et machine tournante comprenant un tel joint
US10696906B2 (en) 2017-09-29 2020-06-30 Marathon Petroleum Company Lp Tower bottoms coke catching device
US10815816B2 (en) * 2018-09-24 2020-10-27 General Electric Company Containment case active clearance control structure
US11008882B2 (en) * 2019-04-18 2021-05-18 Rolls-Royce North American Technologies Inc. Blade tip clearance assembly
US11384301B2 (en) 2020-02-19 2022-07-12 Marathon Petroleum Company Lp Low sulfur fuel oil blends for stability enhancement and associated methods
US11898109B2 (en) 2021-02-25 2024-02-13 Marathon Petroleum Company Lp Assemblies and methods for enhancing control of hydrotreating and fluid catalytic cracking (FCC) processes using spectroscopic analyzers
US11905468B2 (en) 2021-02-25 2024-02-20 Marathon Petroleum Company Lp Assemblies and methods for enhancing control of fluid catalytic cracking (FCC) processes using spectroscopic analyzers
US20220268694A1 (en) 2021-02-25 2022-08-25 Marathon Petroleum Company Lp Methods and assemblies for determining and using standardized spectral responses for calibration of spectroscopic analyzers
US11802257B2 (en) 2022-01-31 2023-10-31 Marathon Petroleum Company Lp Systems and methods for reducing rendered fats pour point

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2555256A (en) * 1948-04-14 1951-05-29 Nat Tube Co Pipe-line pipe
NL202529A (fr) * 1954-12-16
US2962256A (en) * 1956-03-28 1960-11-29 Napier & Son Ltd Turbine blade shroud rings
FR1247283A (fr) * 1959-02-09 1960-11-25 Westinghouse Electric Corp Appareillage de turbine
US3085398A (en) * 1961-01-10 1963-04-16 Gen Electric Variable-clearance shroud structure for gas turbine engines
US3430898A (en) * 1967-05-01 1969-03-04 Us Navy Leading edge for hypersonic vehicle

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2307965A1 (fr) * 1975-04-14 1976-11-12 Gen Electric Turbomachine a reglage du jeu radial entre des pieces tournantes et des pieces fixes
FR2371575A1 (fr) * 1976-11-22 1978-06-16 Gen Electric Structure de virole de turbine a gaz
US4646810A (en) * 1984-10-30 1987-03-03 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Method for the manufacture of a ceramic turbine ring integral with a metallic annular carrier
EP0192512A1 (fr) * 1985-01-24 1986-08-27 Societe Europeenne De Propulsion (S.E.P.) S.A. Anneaux de turbine abradable et turbines ainsi obtenues
EP0192556B1 (fr) * 1985-02-13 1989-05-24 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Carter de turbomachine associé à un dispositif pour ajuster le jeu entre aubes mobiles et carter
FR2662741A1 (fr) * 1990-05-31 1991-12-06 Gen Electric Stator pour turbine a gaz auquel est applique selectivement un revetement ayant une certaine conductivite thermique.
EP0616113A1 (fr) * 1993-03-01 1994-09-21 General Electric Company Support découplé pour garniture d'étanchéité

Also Published As

Publication number Publication date
SE385941B (sv) 1976-07-26
CA989312A (en) 1976-05-18
BE792224A (fr) 1973-03-30
DE2258480A1 (de) 1973-06-07
US3854843A (en) 1974-12-17
AU4931272A (en) 1974-06-06
GB1363897A (en) 1974-08-21
AU463454B2 (en) 1975-07-24
JPS4863111A (fr) 1973-09-03
IT975912B (it) 1974-08-10
CH561354A5 (fr) 1975-04-30
JPS5138371B2 (fr) 1976-10-21
NL7216110A (fr) 1973-06-05

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Legal Events

Date Code Title Description
ST Notification of lapse