CA2441514C - Apparatus and method for damping vibrations between a compressor stator vane and a casing of a gas turbine engine - Google Patents

Apparatus and method for damping vibrations between a compressor stator vane and a casing of a gas turbine engine Download PDF

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Publication number
CA2441514C
CA2441514C CA2441514A CA2441514A CA2441514C CA 2441514 C CA2441514 C CA 2441514C CA 2441514 A CA2441514 A CA 2441514A CA 2441514 A CA2441514 A CA 2441514A CA 2441514 C CA2441514 C CA 2441514C
Authority
CA
Canada
Prior art keywords
casing
stator vane
platform
damping member
outer platform
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
CA2441514A
Other languages
English (en)
French (fr)
Other versions
CA2441514A1 (en
Inventor
Carl Grant
David Curr Douglas
Stephen Rex Payling
James Vota
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
Application filed by General Electric Co filed Critical General Electric Co
Publication of CA2441514A1 publication Critical patent/CA2441514A1/en
Application granted granted Critical
Publication of CA2441514C publication Critical patent/CA2441514C/en
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • 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
    • 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
    • F01D5/26—Antivibration means not restricted to blade form or construction or to blade-to-blade connections or to the use of particular materials
    • 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
    • F05D2300/431—Rubber

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CA2441514A 2002-09-30 2003-09-18 Apparatus and method for damping vibrations between a compressor stator vane and a casing of a gas turbine engine Expired - Fee Related CA2441514C (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/260,633 2002-09-30
US10/260,633 US6969239B2 (en) 2002-09-30 2002-09-30 Apparatus and method for damping vibrations between a compressor stator vane and a casing of a gas turbine engine

Publications (2)

Publication Number Publication Date
CA2441514A1 CA2441514A1 (en) 2004-03-30
CA2441514C true CA2441514C (en) 2010-12-14

Family

ID=32029737

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2441514A Expired - Fee Related CA2441514C (en) 2002-09-30 2003-09-18 Apparatus and method for damping vibrations between a compressor stator vane and a casing of a gas turbine engine

Country Status (3)

Country Link
US (1) US6969239B2 (enExample)
JP (1) JP3914909B2 (enExample)
CA (1) CA2441514C (enExample)

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US7406864B1 (en) 2007-02-28 2008-08-05 Nuovo Pignone Holdings, S.P.A. Method for prevention/detection of mechanical overload in a reciprocating gas compressor
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US8834097B2 (en) * 2010-06-09 2014-09-16 Hamilton Sundstrand Corporation Compressor diffuser vane damper
FR2961553B1 (fr) * 2010-06-18 2012-08-31 Snecma Secteur angulaire de redresseur pour compresseur de turbomachine, redresseur de turbomachine et turbomachine comprenant un tel secteur
FR2961554B1 (fr) * 2010-06-18 2012-07-20 Snecma Secteur angulaire de redresseur pour compresseur de turbomachine, redresseur de turbomachine et turbomachine comprenant un tel secteur
US8632300B2 (en) * 2010-07-22 2014-01-21 Siemens Energy, Inc. Energy absorbing apparatus in a gas turbine engine
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US8920112B2 (en) * 2012-01-05 2014-12-30 United Technologies Corporation Stator vane spring damper
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EP2943657B1 (en) * 2013-01-14 2019-08-14 United Technologies Corporation Organic matrix composite structural inlet guide vane for a turbine engine
US9506361B2 (en) 2013-03-08 2016-11-29 Pratt & Whitney Canada Corp. Low profile vane retention
FR3008639B1 (fr) * 2013-07-18 2015-08-07 Snecma Procede d'assemblage de pieces de turbomachine et ensemble mis en œuvre lors d'un tel procede
US9206700B2 (en) * 2013-10-25 2015-12-08 Siemens Aktiengesellschaft Outer vane support ring including a strong back plate in a compressor section of a gas turbine engine
US8939717B1 (en) * 2013-10-25 2015-01-27 Siemens Aktiengesellschaft Vane outer support ring with no forward hook in a compressor section of a gas turbine engine
EP3123002B1 (en) * 2014-03-27 2019-01-09 Siemens Aktiengesellschaft Stator vane support system within a gas turbine engine
US9816387B2 (en) 2014-09-09 2017-11-14 United Technologies Corporation Attachment faces for clamped turbine stator of a gas turbine engine
WO2016068859A1 (en) * 2014-10-28 2016-05-06 Siemens Energy, Inc. Modular turbine vane
US10378371B2 (en) 2014-12-18 2019-08-13 United Technologies Corporation Anti-rotation vane
EP3075961A1 (de) * 2015-04-02 2016-10-05 Siemens Aktiengesellschaft Leitschaufelanordnung
US10260527B2 (en) 2016-05-17 2019-04-16 General Electric Company Method and system for mitigating rotor bow
CN107747563B (zh) * 2017-09-30 2020-04-10 中国航发沈阳发动机研究所 带阻尼的风扇机匣
US11073033B2 (en) 2018-10-18 2021-07-27 Honeywell International Inc. Stator attachment system for gas turbine engine
JP7465374B2 (ja) 2021-02-05 2024-04-10 三菱重工業株式会社 静翼環、及び回転機械
KR102572871B1 (ko) * 2021-09-17 2023-08-30 두산에너빌리티 주식회사 압축기 베인 슈라우드 조립구조 및 이를 포함하는 압축기, 가스터빈, 압축기 베인 슈라우드 조립방법
JP7588064B2 (ja) * 2021-12-27 2024-11-21 本田技研工業株式会社 流体機械の静翼の振動減衰装置

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Also Published As

Publication number Publication date
US20040062652A1 (en) 2004-04-01
JP2004124941A (ja) 2004-04-22
JP3914909B2 (ja) 2007-05-16
CA2441514A1 (en) 2004-03-30
US6969239B2 (en) 2005-11-29

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Effective date: 20190918