KR20020051819A - 터빈 버킷 조정 방법과 터빈 버킷 - Google Patents

터빈 버킷 조정 방법과 터빈 버킷 Download PDF

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Publication number
KR20020051819A
KR20020051819A KR1020010064765A KR20010064765A KR20020051819A KR 20020051819 A KR20020051819 A KR 20020051819A KR 1020010064765 A KR1020010064765 A KR 1020010064765A KR 20010064765 A KR20010064765 A KR 20010064765A KR 20020051819 A KR20020051819 A KR 20020051819A
Authority
KR
South Korea
Prior art keywords
turbine bucket
bucket
ribs
turbine
adjust
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
KR1020010064765A
Other languages
English (en)
Korean (ko)
Inventor
왕존지퀴앙
노턴폴프란시스
바브케빈조셉
자칼라아리엘시저-프레페나
Original Assignee
제이 엘. 차스킨, 버나드 스나이더, 아더엠. 킹
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 제이 엘. 차스킨, 버나드 스나이더, 아더엠. 킹, 제너럴 일렉트릭 캄파니 filed Critical 제이 엘. 차스킨, 버나드 스나이더, 아더엠. 킹
Publication of KR20020051819A publication Critical patent/KR20020051819A/ko
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
    • 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
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on 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
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/21—Manufacture essentially without removing material by casting
    • 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
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49764—Method of mechanical manufacture with testing or indicating

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
KR1020010064765A 2000-12-22 2001-10-19 터빈 버킷 조정 방법과 터빈 버킷 Ceased KR20020051819A (ko)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/741,892 US6481972B2 (en) 2000-12-22 2000-12-22 Turbine bucket natural frequency tuning rib
US09/741,892 2000-12-22

Publications (1)

Publication Number Publication Date
KR20020051819A true KR20020051819A (ko) 2002-06-29

Family

ID=24982631

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1020010064765A Ceased KR20020051819A (ko) 2000-12-22 2001-10-19 터빈 버킷 조정 방법과 터빈 버킷

Country Status (5)

Country Link
US (1) US6481972B2 (enExample)
EP (1) EP1217171A3 (enExample)
JP (1) JP2002201904A (enExample)
KR (1) KR20020051819A (enExample)
CZ (1) CZ20013657A3 (enExample)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6776583B1 (en) 2003-02-27 2004-08-17 General Electric Company Turbine bucket damper pin
DE50309922D1 (de) * 2003-07-29 2008-07-10 Siemens Ag Gekühlte Turbinenschaufel
US7001150B2 (en) * 2003-10-16 2006-02-21 Pratt & Whitney Canada Corp. Hollow turbine blade stiffening
US7008179B2 (en) * 2003-12-16 2006-03-07 General Electric Co. Turbine blade frequency tuned pin bank
US20060219268A1 (en) * 2005-03-30 2006-10-05 Gunilla Jacobson Neutralization of systemic poisoning in wafer processing
US20080089789A1 (en) * 2006-10-17 2008-04-17 Thomas Joseph Farineau Airfoils for use with turbine assemblies and methods of assembling the same
GB2450937B (en) * 2007-07-13 2009-06-03 Rolls Royce Plc Component with tuned frequency response
US20090155082A1 (en) * 2007-12-18 2009-06-18 Loc Duong Method to maximize resonance-free running range for a turbine blade
EP2161411A1 (de) * 2008-09-05 2010-03-10 Siemens Aktiengesellschaft Turbinenschaufel mit angepasster Eigenfrequenz mittels eines Einsatzes
US8172511B2 (en) * 2009-05-04 2012-05-08 Hamilton Sunstrand Corporation Radial compressor with blades decoupled and tuned at anti-nodes
US8172510B2 (en) * 2009-05-04 2012-05-08 Hamilton Sundstrand Corporation Radial compressor of asymmetric cyclic sector with coupled blades tuned at anti-nodes
US9447691B2 (en) * 2011-08-22 2016-09-20 General Electric Company Bucket assembly treating apparatus and method for treating bucket assembly
US9091175B2 (en) * 2011-08-24 2015-07-28 Pratt & Whitney Canada Corp. Hollow core airfoil stiffener rib
US10156146B2 (en) 2016-04-25 2018-12-18 General Electric Company Airfoil with variable slot decoupling
FR3052182B1 (fr) * 2016-06-06 2018-06-15 Safran Roue aubagee de turbomachine a comportement vibratoire ameliore
US10641098B2 (en) 2017-07-14 2020-05-05 United Technologies Corporation Gas turbine engine hollow fan blade rib orientation
JP7064076B2 (ja) 2018-03-27 2022-05-10 三菱重工業株式会社 タービン翼及びタービン並びにタービン翼の固有振動数のチューニング方法
WO2020263396A1 (en) * 2019-06-28 2020-12-30 Siemens Aktiengesellschaft Turbine airfoil incorporating modal frequency response tuning
KR102361585B1 (ko) * 2020-11-23 2022-02-14 한전케이피에스 주식회사 리브의 설계방법
CN115492642B (zh) * 2022-08-26 2025-02-25 中国科学院工程热物理研究所 一种冷却结构可调的涡轮叶片及航空发动机

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4108573A (en) * 1977-01-26 1978-08-22 Westinghouse Electric Corp. Vibratory tuning of rotatable blades for elastic fluid machines
US5253824A (en) * 1991-04-16 1993-10-19 General Electric Company Hollow core airfoil
US5413463A (en) * 1991-12-30 1995-05-09 General Electric Company Turbulated cooling passages in gas turbine buckets
US5472316A (en) * 1994-09-19 1995-12-05 General Electric Company Enhanced cooling apparatus for gas turbine engine airfoils
US5536143A (en) 1995-03-31 1996-07-16 General Electric Co. Closed circuit steam cooled bucket
US5797726A (en) * 1997-01-03 1998-08-25 General Electric Company Turbulator configuration for cooling passages or rotor blade in a gas turbine engine
US5988982A (en) * 1997-09-09 1999-11-23 Lsp Technologies, Inc. Altering vibration frequencies of workpieces, such as gas turbine engine blades
US5947688A (en) * 1997-12-22 1999-09-07 General Electric Company Frequency tuned hybrid blade
US6273682B1 (en) * 1999-08-23 2001-08-14 General Electric Company Turbine blade with preferentially-cooled trailing edge pressure wall

Also Published As

Publication number Publication date
US20020081206A1 (en) 2002-06-27
CZ20013657A3 (cs) 2002-08-14
EP1217171A2 (en) 2002-06-26
EP1217171A3 (en) 2003-12-10
JP2002201904A (ja) 2002-07-19
US6481972B2 (en) 2002-11-19

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