GB201704204D0 - Method, system, and apparatus for reducing a turbine clearance - Google Patents

Method, system, and apparatus for reducing a turbine clearance

Info

Publication number
GB201704204D0
GB201704204D0 GBGB1704204.5A GB201704204A GB201704204D0 GB 201704204 D0 GB201704204 D0 GB 201704204D0 GB 201704204 A GB201704204 A GB 201704204A GB 201704204 D0 GB201704204 D0 GB 201704204D0
Authority
GB
United Kingdom
Prior art keywords
reducing
turbine clearance
turbine
clearance
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.)
Withdrawn
Application number
GBGB1704204.5A
Other versions
GB2552048A (en
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.)
General Electric Co
Original Assignee
General Electric Co
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
Priority claimed from US15/077,731 external-priority patent/US9758252B2/en
Application filed by General Electric Co filed Critical General Electric Co
Publication of GB201704204D0 publication Critical patent/GB201704204D0/en
Publication of GB2552048A publication Critical patent/GB2552048A/en
Withdrawn legal-status Critical Current

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
    • 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
    • F01D11/22Actively adjusting tip-clearance by mechanically actuating the stator or rotor components, e.g. moving shroud sections relative to the rotor
    • 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
    • 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
    • F05D2240/11Shroud seal segments
    • 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
    • F05D2270/00Control
    • F05D2270/30Control parameters, e.g. input parameters
    • F05D2270/301Pressure
    • 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
    • F05D2270/00Control
    • F05D2270/30Control parameters, e.g. input parameters
    • F05D2270/304Spool rotational speed
    • 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
    • F05D2270/00Control
    • F05D2270/40Type of control system
    • F05D2270/44Type of control system active, predictive, or anticipative

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
GB1704204.5A 2016-03-22 2017-03-16 Method, system, and apparatus for reducing a turbine clearance Withdrawn GB2552048A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US15/077,731 US9758252B2 (en) 2012-08-23 2016-03-22 Method, system, and apparatus for reducing a turbine clearance

Publications (2)

Publication Number Publication Date
GB201704204D0 true GB201704204D0 (en) 2017-05-03
GB2552048A GB2552048A (en) 2018-01-10

Family

ID=58688352

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1704204.5A Withdrawn GB2552048A (en) 2016-03-22 2017-03-16 Method, system, and apparatus for reducing a turbine clearance

Country Status (1)

Country Link
GB (1) GB2552048A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11339678B2 (en) * 2018-07-19 2022-05-24 Raytheon Technologies Corporation Systems and methods for controlling blade tip clearances
FR3098845B1 (en) 2019-07-19 2021-12-24 Safran Aircraft Engines Method for controlling a clearance control valve during a stepped climb in the cruising phase

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4856272A (en) * 1988-05-02 1989-08-15 United Technologies Corporation Method for maintaining blade tip clearance
US5088885A (en) * 1989-10-12 1992-02-18 United Technologies Corporation Method for protecting gas turbine engine seals
US7596954B2 (en) * 2004-07-09 2009-10-06 United Technologies Corporation Blade clearance control
WO2015153171A1 (en) * 2014-03-31 2015-10-08 United Technologies Corporation Active clearance control for gas turbine engine
DE102014214915B3 (en) * 2014-07-30 2015-12-10 MTU Aero Engines AG Housing for a gas turbine, aircraft engine and a method for operating a gas turbine
GB201518641D0 (en) * 2015-10-21 2015-12-02 Rolls Royce Plc A system and method

Also Published As

Publication number Publication date
GB2552048A (en) 2018-01-10

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)