CH707754A2 - Strömungshülse zur thermischen Steuerung eines doppelwandigen Turbinengehäuses und zugehöriges Verfahren. - Google Patents

Strömungshülse zur thermischen Steuerung eines doppelwandigen Turbinengehäuses und zugehöriges Verfahren. Download PDF

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Publication number
CH707754A2
CH707754A2 CH00324/14A CH3242014A CH707754A2 CH 707754 A2 CH707754 A2 CH 707754A2 CH 00324/14 A CH00324/14 A CH 00324/14A CH 3242014 A CH3242014 A CH 3242014A CH 707754 A2 CH707754 A2 CH 707754A2
Authority
CH
Switzerland
Prior art keywords
flow
base
air
flow sleeve
sleeve
Prior art date
Application number
CH00324/14A
Other languages
German (de)
English (en)
Inventor
Radu Ioan Danescu
David Martin Johnson
Kenneth Damon Black
Christopher Paul Cox
Ozgur Bozkurt
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of CH707754A2 publication Critical patent/CH707754A2/de

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08Cooling; Heating; Heat-insulation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/20Actively adjusting tip-clearance
    • F01D11/24Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D19/00Starting of machines or engines; Regulating, controlling, or safety means in connection therewith
    • F01D19/02Starting of machines or engines; Regulating, controlling, or safety means in connection therewith dependent on temperature of component parts, e.g. of turbine-casing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/26Double casings; Measures against temperature strain in casings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/32Application in turbines in gas turbines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/10Stators
    • F05D2240/12Fluid guiding means, e.g. vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/10Stators
    • F05D2240/14Casings or housings protecting or supporting assemblies within
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/20Heat transfer, e.g. cooling

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CH00324/14A 2013-03-11 2014-03-05 Strömungshülse zur thermischen Steuerung eines doppelwandigen Turbinengehäuses und zugehöriges Verfahren. CH707754A2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US13/794,136 US9453429B2 (en) 2013-03-11 2013-03-11 Flow sleeve for thermal control of a double-wall turbine shell and related method

Publications (1)

Publication Number Publication Date
CH707754A2 true CH707754A2 (de) 2014-09-15

Family

ID=51385700

Family Applications (1)

Application Number Title Priority Date Filing Date
CH00324/14A CH707754A2 (de) 2013-03-11 2014-03-05 Strömungshülse zur thermischen Steuerung eines doppelwandigen Turbinengehäuses und zugehöriges Verfahren.

Country Status (4)

Country Link
US (2) US9453429B2 (enExample)
JP (1) JP6411754B2 (enExample)
CH (1) CH707754A2 (enExample)
DE (1) DE102014102778B4 (enExample)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10513944B2 (en) * 2015-12-21 2019-12-24 General Electric Company Manifold for use in a clearance control system and method of manufacturing
US10830102B2 (en) * 2018-03-01 2020-11-10 General Electric Company Casing with tunable lattice structure
FR3086691B1 (fr) * 2018-09-28 2020-12-11 Safran Aircraft Engines Ensemble annulaire pour turbomachine
US11255264B2 (en) 2020-02-25 2022-02-22 General Electric Company Frame for a heat engine
US11560843B2 (en) 2020-02-25 2023-01-24 General Electric Company Frame for a heat engine
US11326519B2 (en) 2020-02-25 2022-05-10 General Electric Company Frame for a heat engine

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3600890A (en) 1968-11-29 1971-08-24 United Aircraft Corp Turbine cooling construction
US3879940A (en) 1973-07-30 1975-04-29 Gen Electric Gas turbine engine fuel delivery tube assembly
US4522559A (en) 1982-02-19 1985-06-11 General Electric Company Compressor casing
FR2614073B1 (fr) 1987-04-15 1992-02-14 Snecma Dispositif d'ajustement en temps reel du jeu radial entre un rotor et un stator de turbomachine
US5012420A (en) 1988-03-31 1991-04-30 General Electric Company Active clearance control for gas turbine engine
US5115636A (en) 1990-09-12 1992-05-26 General Electric Company Borescope plug
US5685693A (en) 1995-03-31 1997-11-11 General Electric Co. Removable inner turbine shell with bucket tip clearance control
GB2310255B (en) * 1996-02-13 1999-06-16 Rolls Royce Plc A turbomachine
JP3631898B2 (ja) * 1998-03-03 2005-03-23 三菱重工業株式会社 ガスタービンにおける分割環の冷却構造
FR2832178B1 (fr) 2001-11-15 2004-07-09 Snecma Moteurs Dispositif de refroidissement pour anneaux de turbine a gaz
DE10202783A1 (de) 2002-01-25 2003-07-31 Alstom Switzerland Ltd Gekühltes Bauteil für eine thermische Maschine, insbesondere eine Gasturbine
US7008183B2 (en) * 2003-12-26 2006-03-07 General Electric Company Deflector embedded impingement baffle
JP2006037855A (ja) * 2004-07-28 2006-02-09 Mitsubishi Heavy Ind Ltd 車室ケーシング及びガスタービン
GB2417762B (en) 2004-09-04 2006-10-04 Rolls Royce Plc Turbine case cooling
US8152446B2 (en) 2007-08-23 2012-04-10 General Electric Company Apparatus and method for reducing eccentricity and out-of-roundness in turbines
US8079804B2 (en) 2008-09-18 2011-12-20 Siemens Energy, Inc. Cooling structure for outer surface of a gas turbine case
JP5470662B2 (ja) * 2011-01-27 2014-04-16 株式会社日立製作所 ガスタービン燃焼器

Also Published As

Publication number Publication date
US9453429B2 (en) 2016-09-27
US10024189B2 (en) 2018-07-17
US20160348534A1 (en) 2016-12-01
US20140341702A1 (en) 2014-11-20
JP6411754B2 (ja) 2018-10-24
DE102014102778B4 (de) 2023-12-07
JP2014173597A (ja) 2014-09-22
DE102014102778A1 (de) 2014-09-11

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Legal Events

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Representative=s name: GENERAL ELECTRIC TECHNOLOGY GMBH GLOBAL PATENT, CH

AZW Rejection (application)