KR20060050297A - 스팀 터빈 블레이드와 스팀 터빈 로터 휠 및 그 상의블레이드 열의 공력 탄성적 반응을 억제하는 방법 - Google Patents

스팀 터빈 블레이드와 스팀 터빈 로터 휠 및 그 상의블레이드 열의 공력 탄성적 반응을 억제하는 방법 Download PDF

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Publication number
KR20060050297A
KR20060050297A KR1020050072168A KR20050072168A KR20060050297A KR 20060050297 A KR20060050297 A KR 20060050297A KR 1020050072168 A KR1020050072168 A KR 1020050072168A KR 20050072168 A KR20050072168 A KR 20050072168A KR 20060050297 A KR20060050297 A KR 20060050297A
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KR
South Korea
Prior art keywords
blades
steam turbine
blade
filled
group
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
KR1020050072168A
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English (en)
Korean (ko)
Inventor
스티븐 세바스찬 버드긱
가이 더블유 드레오나르도
웬디 더블유 린
케빈 조셉 바브
Original Assignee
제너럴 일렉트릭 캄파니
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 제너럴 일렉트릭 캄파니 filed Critical 제너럴 일렉트릭 캄파니
Publication of KR20060050297A publication Critical patent/KR20060050297A/ko
Ceased legal-status Critical Current

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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
    • 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
    • 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
    • F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
    • 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
    • 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
    • F01D5/16—Form or construction for counteracting blade vibration
    • 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
    • F05D2260/00—Function
    • F05D2260/96—Preventing, counteracting or reducing vibration or noise
    • F05D2260/961—Preventing, counteracting or reducing vibration or noise by mistuning rotor blades or stator vanes with irregular interblade spacing, airfoil shape
    • 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
    • F05D2300/40—Organic materials
    • F05D2300/43—Synthetic polymers, e.g. plastics; Rubber
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S416/00—Fluid reaction surfaces, i.e. impellers
    • Y10S416/50—Vibration damping features

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
KR1020050072168A 2004-08-09 2005-08-08 스팀 터빈 블레이드와 스팀 터빈 로터 휠 및 그 상의블레이드 열의 공력 탄성적 반응을 억제하는 방법 Ceased KR20060050297A (ko)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/913,407 2004-08-09
US10/913,407 US7147437B2 (en) 2004-08-09 2004-08-09 Mixed tuned hybrid blade related method

Publications (1)

Publication Number Publication Date
KR20060050297A true KR20060050297A (ko) 2006-05-19

Family

ID=34941842

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1020050072168A Ceased KR20060050297A (ko) 2004-08-09 2005-08-08 스팀 터빈 블레이드와 스팀 터빈 로터 휠 및 그 상의블레이드 열의 공력 탄성적 반응을 억제하는 방법

Country Status (6)

Country Link
US (1) US7147437B2 (https=)
EP (1) EP1626161B1 (https=)
JP (1) JP2006052732A (https=)
KR (1) KR20060050297A (https=)
CN (1) CN1734062B (https=)
DE (1) DE602005006483D1 (https=)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10215029B2 (en) 2016-01-27 2019-02-26 Hanwha Power Systems Co., Ltd. Blade assembly
KR20220025033A (ko) * 2019-06-28 2022-03-03 지멘스 에너지 글로벌 게엠베하 운트 코. 카게 모달 주파수 응답 튜닝을 포함하는 터빈 에어포일

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US7507073B2 (en) * 2006-02-24 2009-03-24 General Electric Company Methods and apparatus for assembling a steam turbine bucket
US7766625B2 (en) * 2006-03-31 2010-08-03 General Electric Company Methods and apparatus for reducing stress in turbine buckets
US20070292265A1 (en) * 2006-06-14 2007-12-20 General Electric Company System design and cooling method for LP steam turbines using last stage hybrid bucket
US7429165B2 (en) * 2006-06-14 2008-09-30 General Electric Company Hybrid blade for a steam turbine
EP1985803A1 (de) * 2007-04-23 2008-10-29 Siemens Aktiengesellschaft Verfahren zum Herstellen von beschichteten Turbinenlaufschaufeln
US7887299B2 (en) * 2007-06-07 2011-02-15 Honeywell International Inc. Rotary body for turbo machinery with mistuned blades
GB2450936B (en) * 2007-07-13 2010-01-20 Rolls Royce Plc Bladed rotor balancing
GB2450937B (en) * 2007-07-13 2009-06-03 Rolls Royce Plc Component with tuned frequency response
US8100641B2 (en) * 2008-09-09 2012-01-24 General Electric Company Steam turbine having stage with buckets of different materials
US8043063B2 (en) * 2009-03-26 2011-10-25 Pratt & Whitney Canada Corp. Intentionally mistuned integrally bladed rotor
US8419370B2 (en) * 2009-06-25 2013-04-16 Rolls-Royce Corporation Retaining and sealing ring assembly
US8469670B2 (en) * 2009-08-27 2013-06-25 Rolls-Royce Corporation Fan assembly
US8435006B2 (en) * 2009-09-30 2013-05-07 Rolls-Royce Corporation Fan
FR2956875B1 (fr) * 2010-02-26 2012-09-21 Snecma Aube allegee pour turbomachine, carter comportant une pluralite d'une telle aube et turbomachine comportant au moins un tel carter
US8726725B2 (en) 2011-03-08 2014-05-20 Schlumberger Technology Corporation Apparatus, system and method for determining at least one downhole parameter of a wellsite
US9297277B2 (en) 2011-09-30 2016-03-29 General Electric Company Power plant
US8763360B2 (en) 2011-11-03 2014-07-01 United Technologies Corporation Hollow fan blade tuning using distinct filler materials
US9097125B2 (en) * 2012-08-17 2015-08-04 Mapna Group Intentionally frequency mistuned turbine blades
EP2900923B1 (en) * 2012-09-25 2019-12-25 United Technologies Corporation Airfoil array with vanes that differ in geometry according to geometry classes
ES2546992T3 (es) * 2012-10-24 2015-09-30 MTU Aero Engines AG Método para desintonizar los álabes de un motor de turbina de gas
EP2942481B1 (en) * 2014-05-07 2019-03-27 Rolls-Royce Corporation Rotor for a gas turbine engine
CN104675443A (zh) * 2014-12-15 2015-06-03 中国燃气涡轮研究院 一种涡轮整体叶盘固有频率调整方法
US10641281B2 (en) 2016-08-08 2020-05-05 United Technologies Corporation Mistuned laminate airfoil
US10837287B2 (en) * 2017-01-20 2020-11-17 Pratt & Whitney Canada Corp. Mistuned bladed rotor and associated manufacturing method
JP6745235B2 (ja) * 2017-03-10 2020-08-26 三菱日立パワーシステムズ株式会社 ロータ及びこのロータを備える回転機械
US10954804B2 (en) * 2017-07-05 2021-03-23 Raytheon Technologies Corporation Rotary machines including a hybrid rotor with hollow and solid rotor blade sets
WO2019087281A1 (ja) * 2017-10-31 2019-05-09 三菱重工エンジン＆ターボチャージャ株式会社 タービン動翼、ターボチャージャ及びタービン動翼の製造方法
US10731471B2 (en) * 2018-12-28 2020-08-04 General Electric Company Hybrid rotor blades for turbine engines
US11220913B2 (en) * 2019-10-23 2022-01-11 Rolls-Royce Corporation Gas turbine engine blades with airfoil plugs for selected tuning
US11255199B2 (en) 2020-05-20 2022-02-22 Rolls-Royce Corporation Airfoil with shaped mass reduction pocket
US11767765B2 (en) * 2021-09-28 2023-09-26 General Electric Company Glass viscous damper
US11746659B2 (en) 2021-12-23 2023-09-05 Rolls-Royce North American Technologies Inc. Fan blade with internal shear-thickening fluid damping
US11560801B1 (en) 2021-12-23 2023-01-24 Rolls-Royce North American Technologies Inc. Fan blade with internal magnetorheological fluid damping
US12043368B2 (en) * 2022-03-23 2024-07-23 General Electric Company Rotating airfoil assembly

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US5286168A (en) * 1992-01-31 1994-02-15 Westinghouse Electric Corp. Freestanding mixed tuned blade
FR2688264A1 (fr) * 1992-03-04 1993-09-10 Snecma Redresseur de turbomachine a aubes ayant une face alveolee chargee en materiau composite.
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US6364616B1 (en) 2000-05-05 2002-04-02 General Electric Company Submerged rib hybrid blade
US6471482B2 (en) * 2000-11-30 2002-10-29 United Technologies Corporation Frequency-mistuned light-weight turbomachinery blade rows for increased flutter stability
US6428278B1 (en) * 2000-12-04 2002-08-06 United Technologies Corporation Mistuned rotor blade array for passive flutter control
US6854959B2 (en) * 2003-04-16 2005-02-15 General Electric Company Mixed tuned hybrid bucket and related method

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10215029B2 (en) 2016-01-27 2019-02-26 Hanwha Power Systems Co., Ltd. Blade assembly
KR20220025033A (ko) * 2019-06-28 2022-03-03 지멘스 에너지 글로벌 게엠베하 운트 코. 카게 모달 주파수 응답 튜닝을 포함하는 터빈 에어포일

Also Published As

Publication number Publication date
CN1734062A (zh) 2006-02-15
CN1734062B (zh) 2010-09-08
EP1626161B1 (en) 2008-05-07
US7147437B2 (en) 2006-12-12
EP1626161A1 (en) 2006-02-15
DE602005006483D1 (de) 2008-06-19
JP2006052732A (ja) 2006-02-23
US20060029501A1 (en) 2006-02-09

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