CA2862644C - Commande de jeu d'extremite de turbine a gaz - Google Patents

Commande de jeu d'extremite de turbine a gaz Download PDF

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Publication number
CA2862644C
CA2862644C CA2862644A CA2862644A CA2862644C CA 2862644 C CA2862644 C CA 2862644C CA 2862644 A CA2862644 A CA 2862644A CA 2862644 A CA2862644 A CA 2862644A CA 2862644 C CA2862644 C CA 2862644C
Authority
CA
Canada
Prior art keywords
gas turbine
turbine engine
thermoelectric device
flow path
component
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.)
Expired - Fee Related
Application number
CA2862644A
Other languages
English (en)
Other versions
CA2862644A1 (fr
Inventor
Adam J. Morrison
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.)
Rolls Royce North American Technologies Inc
Original Assignee
Rolls Royce North American Technologies Inc
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 Rolls Royce North American Technologies Inc filed Critical Rolls Royce North American Technologies Inc
Publication of CA2862644A1 publication Critical patent/CA2862644A1/fr
Application granted granted Critical
Publication of CA2862644C publication Critical patent/CA2862644C/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F01D11/20—Actively adjusting tip-clearance
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • 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
    • F01D11/20—Actively adjusting tip-clearance
    • F01D11/22—Actively adjusting tip-clearance by mechanically actuating the stator or rotor components, e.g. moving shroud sections relative to the rotor
    • 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
    • F01D11/20—Actively adjusting tip-clearance
    • F01D11/24—Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
    • 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
    • F05D2270/00—Control
    • F05D2270/40—Type of control system
    • F05D2270/44—Type 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

La présente invention concerne une turbine à gaz comportant un dispositif thermoélectrique capable de changer un jeu d'extrémité dans un composant de turbomachine. Dans une forme non limitative, le composant de turbomachine est un compresseur. Le dispositif thermoélectrique peut être utilisé sous différentes formes pour récolter la puissance provenant de la chaleur perdue. Le système de commande de jeu d'extrémité peut comprendre un capteur servant à déterminer le jeu entre une extrémité et une paroi du composant de turbomachine.
CA2862644A 2011-12-30 2012-12-28 Commande de jeu d'extremite de turbine a gaz Expired - Fee Related CA2862644C (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201161581793P 2011-12-30 2011-12-30
US61/581,793 2011-12-30
PCT/US2012/072133 WO2013141937A1 (fr) 2011-12-30 2012-12-28 Commande de jeu d'extrémité de turbine à gaz

Publications (2)

Publication Number Publication Date
CA2862644A1 CA2862644A1 (fr) 2013-09-26
CA2862644C true CA2862644C (fr) 2019-08-27

Family

ID=49223148

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2862644A Expired - Fee Related CA2862644C (fr) 2011-12-30 2012-12-28 Commande de jeu d'extremite de turbine a gaz

Country Status (4)

Country Link
US (1) US20140314567A1 (fr)
EP (1) EP2805025B1 (fr)
CA (1) CA2862644C (fr)
WO (1) WO2013141937A1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
PL225446B1 (pl) * 2013-04-30 2017-04-28 Gen Electric Zespół sterowania cieplnego dla turbiny, zespół wytwarzania energii elektrycznej zawierający turbinę oraz turbina zawierająca zespół sterowania cieplnego
US10472986B2 (en) * 2014-01-24 2019-11-12 United Technologies Corporation Systems for thermoelectric cooling for jet aircraft propulsion systems
US10938328B2 (en) 2016-06-22 2021-03-02 General Electric Company Harvesting energy from composite aircraft engine components

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2994472A (en) 1958-12-29 1961-08-01 Gen Electric Tip clearance control system for turbomachines
US4326804A (en) * 1980-02-11 1982-04-27 General Electric Company Apparatus and method for optical clearance determination
GB2117450B (en) * 1981-03-20 1984-06-27 Rolls Royce Casing support for a gas turbine engine
US5216887A (en) * 1987-06-30 1993-06-08 Kabushiki Kaisha Komatsu Seisakusho Radiative-type air-conditioning unit
US5667358A (en) * 1995-11-30 1997-09-16 Westinghouse Electric Corporation Method for reducing steady state rotor blade tip clearance in a land-based gas turbine to improve efficiency
GB2388407B (en) * 2002-05-10 2005-10-26 Rolls Royce Plc Gas turbine blade tip clearance control structure
WO2006059982A1 (fr) * 2004-12-01 2006-06-08 United Technologies Corporation Regulateur a distance de carburant moteur et regulateur electronique moteur pour moteur a turbine
US20070277866A1 (en) * 2006-05-31 2007-12-06 General Electric Company Thermoelectric nanotube arrays
JP2008157340A (ja) * 2006-12-22 2008-07-10 Ntn Corp 転がり軸受
US9018512B2 (en) * 2007-12-21 2015-04-28 The Boeing Company Thermoelectric generation system
FR2942077B1 (fr) * 2009-02-06 2013-08-16 Turbomeca Generation thermoelectrique pour turbine a gaz
FR2943093B1 (fr) * 2009-03-16 2015-04-24 Snecma Dispositif de reglage de la position radiale et/ou axiale d'une virole de stator de turbomachine
FR2943717B1 (fr) * 2009-03-27 2016-02-19 Snecma Stator de compresseur ou turbine de turbomachine permettant un controle du jeu en sommet d'aubes d'un rotor en regard
US8578696B2 (en) * 2010-08-03 2013-11-12 General Electric Company Turbulated arrangement of thermoelectric elements for utilizing waste heat generated from turbine engine
US20120118345A1 (en) * 2010-11-15 2012-05-17 The Boeing Company Thermal integration of thermoelectronic device
US9151176B2 (en) * 2011-11-22 2015-10-06 General Electric Company Systems and methods for adjusting clearances in turbines
US9057282B2 (en) * 2011-11-22 2015-06-16 General Electric Company Systems and methods for adjusting clearances in turbines
US8776530B2 (en) * 2011-11-23 2014-07-15 General Electric Company Gas turbine engine lockout reduction
WO2013141938A1 (fr) * 2011-12-30 2013-09-26 Rolls-Royce North American Technologies, Inc. Commande de jeu d'extrémité de turbine à gaz
EP2664746A3 (fr) * 2012-05-16 2014-04-23 General Electric Company Systèmes et procédés permettant de régler des dégagements dans des turbines
PL225446B1 (pl) * 2013-04-30 2017-04-28 Gen Electric Zespół sterowania cieplnego dla turbiny, zespół wytwarzania energii elektrycznej zawierający turbinę oraz turbina zawierająca zespół sterowania cieplnego

Also Published As

Publication number Publication date
EP2805025A4 (fr) 2015-11-11
CA2862644A1 (fr) 2013-09-26
US20140314567A1 (en) 2014-10-23
WO2013141937A1 (fr) 2013-09-26
EP2805025A1 (fr) 2014-11-26
EP2805025B1 (fr) 2018-05-02

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Legal Events

Date Code Title Description
EEER Examination request

Effective date: 20171227

MKLA Lapsed

Effective date: 20201229