WO2008019657A3 - Anordnung zur laufspaltoptimierung für turbomaschinen - Google Patents

Anordnung zur laufspaltoptimierung für turbomaschinen Download PDF

Info

Publication number
WO2008019657A3
WO2008019657A3 PCT/DE2007/001416 DE2007001416W WO2008019657A3 WO 2008019657 A3 WO2008019657 A3 WO 2008019657A3 DE 2007001416 W DE2007001416 W DE 2007001416W WO 2008019657 A3 WO2008019657 A3 WO 2008019657A3
Authority
WO
WIPO (PCT)
Prior art keywords
running clearance
arrangement
ring
optimising
relation
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.)
Ceased
Application number
PCT/DE2007/001416
Other languages
English (en)
French (fr)
Other versions
WO2008019657A2 (de
Inventor
Alexander Boeck
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.)
MTU Aero Engines AG
Original Assignee
MTU Aero Engines GmbH
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 MTU Aero Engines GmbH filed Critical MTU Aero Engines GmbH
Priority to EP07817418.2A priority Critical patent/EP2052133B1/de
Priority to CA002660368A priority patent/CA2660368A1/en
Priority to US12/376,398 priority patent/US8608427B2/en
Publication of WO2008019657A2 publication Critical patent/WO2008019657A2/de
Publication of WO2008019657A3 publication Critical patent/WO2008019657A3/de
Anticipated expiration legal-status Critical
Ceased 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
    • F01D11/20—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
    • 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
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/11—Shroud seal segments
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/50—Intrinsic material properties or characteristics
    • F05D2300/501—Elasticity

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Anordnung zur Laufspaltoptimierung für Turbomaschinen in Axialbauart durch Steuerung bzw. Regelung des laufspaltrelevanten Innendurchmessers mindestens einer einen Laufschaufelkranz umschließenden Statorstruktur. Die Statorstruktur weist einen geschlossenen Innenring, einen zu diesem konzentrischen und radial beabstandeten Außenring sowie mehrere, den Innenring mit dem Außenring integral verbindende, relativ zur Radialrichtung in Umfangsrichtung geneigte Stege auf. Die Anordnung umfasst eine Verstelleinrichtung zur Verdrehung des Innenrings relativ zum Außenring unter elastischer Veränderung des laufspaltrelevanten Innendurchmessers.
PCT/DE2007/001416 2006-08-17 2007-08-08 Anordnung zur laufspaltoptimierung für turbomaschinen Ceased WO2008019657A2 (de)

Priority Applications (3)

Application Number Priority Date Filing Date Title
EP07817418.2A EP2052133B1 (de) 2006-08-17 2007-08-08 Anordnung zur laufspaltoptimierung für turbomaschinen
CA002660368A CA2660368A1 (en) 2006-08-17 2007-08-08 Arrangement for optimizing the running clearance for turbomachines
US12/376,398 US8608427B2 (en) 2006-08-17 2007-08-08 Arrangement for optimising the running clearance for turbomachines

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102006038753A DE102006038753A1 (de) 2006-08-17 2006-08-17 Anordnung zur Laufspaltoptimierung für Turbomaschinen
DE102006038753.8 2006-08-17

Publications (2)

Publication Number Publication Date
WO2008019657A2 WO2008019657A2 (de) 2008-02-21
WO2008019657A3 true WO2008019657A3 (de) 2008-04-17

Family

ID=39044234

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/DE2007/001416 Ceased WO2008019657A2 (de) 2006-08-17 2007-08-08 Anordnung zur laufspaltoptimierung für turbomaschinen

Country Status (5)

Country Link
US (1) US8608427B2 (de)
EP (1) EP2052133B1 (de)
CA (1) CA2660368A1 (de)
DE (1) DE102006038753A1 (de)
WO (1) WO2008019657A2 (de)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009006029A1 (de) * 2009-01-24 2010-07-29 Mtu Aero Engines Gmbh Turbomaschine
US9228447B2 (en) 2012-02-14 2016-01-05 United Technologies Corporation Adjustable blade outer air seal apparatus
US9683453B2 (en) * 2013-09-11 2017-06-20 General Electric Company Turbine casing clearance management system
US9695705B2 (en) 2014-10-29 2017-07-04 General Electric Company Systems and methods for controlling rotor to stator clearances in a steam turbine
US10458429B2 (en) 2016-05-26 2019-10-29 Rolls-Royce Corporation Impeller shroud with slidable coupling for clearance control in a centrifugal compressor
US10851712B2 (en) 2017-06-27 2020-12-01 General Electric Company Clearance control device
IT201900005266A1 (it) * 2019-04-05 2020-10-05 Nuovo Pignone Tecnologie Srl Turbina a vapore con pale statoriche girevoli
CN110725722B (zh) * 2019-08-27 2022-04-19 中国科学院工程热物理研究所 一种适用于叶轮机械的动叶叶顶间隙动态连续可调结构
CN113107615B (zh) * 2021-04-08 2022-08-26 沈阳航空航天大学 基于偏心阻尼作用的主动间隙控制篦齿密封结构
US12006829B1 (en) 2023-02-16 2024-06-11 General Electric Company Seal member support system for a gas turbine engine
US12486779B2 (en) 2023-03-08 2025-12-02 General Electric Company Seal support assembly for a turbine engine
US12416243B2 (en) 2023-03-24 2025-09-16 General Electric Company Seal support assembly for a turbine engine
US12116896B1 (en) 2023-03-24 2024-10-15 General Electric Company Seal support assembly for a turbine engine
US12595745B2 (en) 2023-03-24 2026-04-07 General Electric Company Seal support assembly for a turbine engine
US12421861B2 (en) 2023-03-24 2025-09-23 General Electric Company Seal support assembly for a turbine engine
US12215587B2 (en) 2023-03-24 2025-02-04 General Electric Company Seal support assembly for a turbine engine
US12241375B2 (en) 2023-03-24 2025-03-04 General Electric Company Seal support assembly for a turbine engine
US12372002B2 (en) 2023-03-24 2025-07-29 General Electric Company Seal support assembly for a turbine engine
US12215588B2 (en) 2023-03-27 2025-02-04 General Electric Company Seal assembly for a gas turbine engine
US12326089B2 (en) 2023-04-24 2025-06-10 General Electric Company Seal assembly for a gas turbine engine
US12345163B2 (en) 2023-11-17 2025-07-01 Rolls-Royce Corporation Travel stop for a tip clearance control system
US12345162B2 (en) 2023-11-17 2025-07-01 Rolls-Royce Corporation Adjustable position impeller shroud for centrifugal compressors
CN119593817A (zh) * 2024-11-26 2025-03-11 西安西热节能技术有限公司 一种自适应调节间隙的轮缘密封结构、透平及汽轮机
CN120556986B (zh) * 2025-08-01 2025-10-28 浙江农林大学 基于主动气囊驱动的柱面间隙形状智能调控系统及方法

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2458676A1 (fr) * 1979-06-06 1981-01-02 Mtu Muenchen Gmbh Dispositif d'etancheite pour l'intervalle peripherique d'une turbomachine a flux axial
GB2108591A (en) * 1981-11-03 1983-05-18 Rolls Royce Casing of a gas turbine engine rotor
DE10233881A1 (de) * 2002-07-25 2004-02-12 Rolls-Royce Deutschland Ltd & Co Kg Durch thermische Effekte radial veränderbares Ringelement

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3227418A (en) * 1963-11-04 1966-01-04 Gen Electric Variable clearance seal
DE3509192A1 (de) * 1985-03-14 1986-09-25 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Stroemungsmaschine mit mitteln zur kontrolle des radialspaltes
GB2313414B (en) * 1996-05-24 2000-05-17 Rolls Royce Plc Gas turbine engine blade tip clearance control
US6454529B1 (en) * 2001-03-23 2002-09-24 General Electric Company Methods and apparatus for maintaining rotor assembly tip clearances
US7686569B2 (en) * 2006-12-04 2010-03-30 Siemens Energy, Inc. Blade clearance system for a turbine engine

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2458676A1 (fr) * 1979-06-06 1981-01-02 Mtu Muenchen Gmbh Dispositif d'etancheite pour l'intervalle peripherique d'une turbomachine a flux axial
GB2108591A (en) * 1981-11-03 1983-05-18 Rolls Royce Casing of a gas turbine engine rotor
DE10233881A1 (de) * 2002-07-25 2004-02-12 Rolls-Royce Deutschland Ltd & Co Kg Durch thermische Effekte radial veränderbares Ringelement

Also Published As

Publication number Publication date
DE102006038753A1 (de) 2008-03-13
EP2052133B1 (de) 2014-01-15
US8608427B2 (en) 2013-12-17
CA2660368A1 (en) 2008-02-21
EP2052133A2 (de) 2009-04-29
US20100232942A1 (en) 2010-09-16
WO2008019657A2 (de) 2008-02-21

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