JPH11141307A - ガスタービンエンジンのロータ段の振動を制御する装置 - Google Patents

ガスタービンエンジンのロータ段の振動を制御する装置

Info

Publication number
JPH11141307A
JPH11141307A JP10260997A JP26099798A JPH11141307A JP H11141307 A JPH11141307 A JP H11141307A JP 10260997 A JP10260997 A JP 10260997A JP 26099798 A JP26099798 A JP 26099798A JP H11141307 A JPH11141307 A JP H11141307A
Authority
JP
Japan
Prior art keywords
high pressure
pressure gas
rotor stage
stage
holes
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.)
Pending
Application number
JP10260997A
Other languages
English (en)
Japanese (ja)
Other versions
JPH11141307A5 (enExample
Inventor
Yehia M El-Aini
エヒア・エム・エル−アイニ
Barry K Benedict
バリー・ケー・ベネディクト
Samy Baghdadi
サミー・バグダディ
A Paul Matheny
エー・ポール・マセニー
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.)
RTX Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of JPH11141307A publication Critical patent/JPH11141307A/ja
Publication of JPH11141307A5 publication Critical patent/JPH11141307A5/ja
Pending legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/667—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps by influencing the flow pattern, e.g. suppression of turbulence
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/04—Antivibration arrangements
    • F01D25/06—Antivibration arrangements for preventing 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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/10—Anti- vibration means
    • 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
    • F01D5/141—Shape, i.e. outer, aerodynamic form
    • F01D5/145—Means for influencing boundary layers or secondary circulations
    • 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
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/68—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers
    • F04D29/681—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
JP10260997A 1997-08-29 1998-08-31 ガスタービンエンジンのロータ段の振動を制御する装置 Pending JPH11141307A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/920,493 1997-08-29
US08/920,493 US6055805A (en) 1997-08-29 1997-08-29 Active rotor stage vibration control

Publications (2)

Publication Number Publication Date
JPH11141307A true JPH11141307A (ja) 1999-05-25
JPH11141307A5 JPH11141307A5 (enExample) 2005-10-27

Family

ID=25443842

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10260997A Pending JPH11141307A (ja) 1997-08-29 1998-08-31 ガスタービンエンジンのロータ段の振動を制御する装置

Country Status (5)

Country Link
US (2) US6055805A (enExample)
EP (2) EP1353039B1 (enExample)
JP (1) JPH11141307A (enExample)
KR (1) KR100539037B1 (enExample)
DE (2) DE69836154T2 (enExample)

Cited By (1)

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JP2008163947A (ja) * 2006-12-28 2008-07-17 General Electric Co <Ge> 流れ再循環を備えた圧縮システムの操作線制御

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US6202403B1 (en) * 1998-12-22 2001-03-20 General Electric Company Core compartment valve cooling valve scheduling
FR2814197B1 (fr) * 2000-09-21 2003-01-10 Snecma Moteurs Procede et dispositif pour l'attenuation des sons d'interaction rotor/stator dans une turbomachine
US6409469B1 (en) * 2000-11-21 2002-06-25 Pratt & Whitney Canada Corp. Fan-stator interaction tone reduction
US7631483B2 (en) * 2003-09-22 2009-12-15 General Electric Company Method and system for reduction of jet engine noise
GB2407142B (en) * 2003-10-15 2006-03-01 Rolls Royce Plc An arrangement for bleeding the boundary layer from an aircraft engine
JP2005226584A (ja) * 2004-02-13 2005-08-25 Honda Motor Co Ltd コンプレッサ及びガスタービンエンジン
DE102004030597A1 (de) 2004-06-24 2006-01-26 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit Aussenradstrahlerzeugung am Stator
DE102004054752A1 (de) * 2004-11-12 2006-05-18 Rolls-Royce Deutschland Ltd & Co Kg Schaufel einer Strömungsarbeitsmaschine mit erweiterter Randprofiltiefe
DE102005052466A1 (de) * 2005-11-03 2007-05-10 Mtu Aero Engines Gmbh Mehrstufiger Verdichter für eine Gasturbine mit Abblasöffnungen und Einblasöffnungen zum Stabilisieren der Verdichterströmung
US7617670B2 (en) * 2006-03-31 2009-11-17 Lockheed Martin Corporation Flow control redistribution to mitigate high cycle fatigue
US20070245708A1 (en) * 2006-04-20 2007-10-25 United Technologies Corporation High cycle fatigue management for gas turbine engines
US7797944B2 (en) * 2006-10-20 2010-09-21 United Technologies Corporation Gas turbine engine having slim-line nacelle
US7870721B2 (en) * 2006-11-10 2011-01-18 United Technologies Corporation Gas turbine engine providing simulated boundary layer thickness increase
US8408491B2 (en) * 2007-04-24 2013-04-02 United Technologies Corporation Nacelle assembly having inlet airfoil for a gas turbine engine
DE102007026455A1 (de) * 2007-06-05 2008-12-11 Rolls-Royce Deutschland Ltd & Co Kg Strahltriebwerk mit Verdichterluftzirkulation und Verfahren zum Betreiben desselben
US8082726B2 (en) * 2007-06-26 2011-12-27 United Technologies Corporation Tangential anti-swirl air supply
US8402739B2 (en) * 2007-06-28 2013-03-26 United Technologies Corporation Variable shape inlet section for a nacelle assembly of a gas turbine engine
US8371806B2 (en) * 2007-10-03 2013-02-12 United Technologies Corporation Gas turbine engine having core auxiliary duct passage
US8240120B2 (en) * 2007-10-25 2012-08-14 United Technologies Corporation Vibration management for gas turbine engines
US9004399B2 (en) 2007-11-13 2015-04-14 United Technologies Corporation Nacelle flow assembly
US8186942B2 (en) * 2007-12-14 2012-05-29 United Technologies Corporation Nacelle assembly with turbulators
US8192147B2 (en) * 2007-12-14 2012-06-05 United Technologies Corporation Nacelle assembly having inlet bleed
DE102008016800A1 (de) * 2008-04-02 2009-10-08 Mtu Aero Engines Gmbh Gasturbinenverdichter
FR2931906B1 (fr) * 2008-05-30 2017-06-02 Snecma Compresseur de turbomachine avec un systeme d'injection d'air.
DE102008052409A1 (de) 2008-10-21 2010-04-22 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit saugseitennaher Randenergetisierung
US8591166B2 (en) * 2008-12-31 2013-11-26 Rolls-Royce North American Technologies, Inc. Axial compressor vane
DE102009032549A1 (de) * 2009-07-10 2011-01-13 Mtu Aero Engines Gmbh Verfahren zum Mindern von Schwingungsamplituden
US20110250046A1 (en) * 2010-04-07 2011-10-13 Honeywell International Inc. Turbofan engine performance recovery system and method
US8105039B1 (en) 2011-04-01 2012-01-31 United Technologies Corp. Airfoil tip shroud damper
WO2013102098A1 (en) * 2011-12-29 2013-07-04 Rolls-Royce North American Technologies, Inc. Vavle for gas turbine engine
US8640820B2 (en) * 2012-01-11 2014-02-04 Polytechnic Institute Of New York University High-speed jet noise reduction via fluidic injection
US10107191B2 (en) * 2012-02-29 2018-10-23 United Technologies Corporation Geared gas turbine engine with reduced fan noise
US9017033B2 (en) 2012-06-07 2015-04-28 United Technologies Corporation Fan blade platform
EP2904252B2 (en) * 2012-10-01 2020-11-25 United Technologies Corporation Static guide vane with internal hollow channels
US20160258440A1 (en) * 2015-03-02 2016-09-08 Rolls-Royce Corporation Gas turbine engine with airfoil dampening system
FR3034145B1 (fr) * 2015-03-26 2017-04-07 Snecma Etage de compresseur
EP3296573A1 (en) * 2016-09-20 2018-03-21 Siemens Aktiengesellschaft A technique for controlling rotating stall in compressor for a gas turbine engine
CN110268197B (zh) * 2017-02-08 2020-08-14 西门子股份公司 最小化在特定频率范围内作用在涡轮叶片上的力的方法
US10775269B2 (en) * 2017-02-08 2020-09-15 Raytheon Technologies Corporation Blade health inspection using an excitation actuator and vibration sensor
EP3477120A1 (en) * 2017-10-26 2019-05-01 Siemens Aktiengesellschaft Gas turbine engine control method and system
JP6916755B2 (ja) * 2018-03-09 2021-08-11 三菱重工業株式会社 回転機械
FR3079552B1 (fr) * 2018-03-29 2021-06-04 Safran Aircraft Engines Turbomachine comportant au moins une aube amont comportant une portion de soufflage pour limiter la resonance d'une aube aval
US20200072062A1 (en) * 2018-08-31 2020-03-05 General Electric Company System and Method for Airfoil Vibration Control
CA3073417A1 (en) 2019-04-18 2020-10-18 Pratt & Whitney Canada Corp. Fan blade ice protection using hot air
US11118457B2 (en) * 2019-10-21 2021-09-14 Pratt & Whitney Canada Corp. Method for fan blade heating using coanda effect
US11333079B2 (en) * 2020-04-28 2022-05-17 General Electric Company Methods and apparatus to detect air flow separation of an engine
US11828237B2 (en) 2020-04-28 2023-11-28 General Electric Company Methods and apparatus to control air flow separation of an engine
US11085303B1 (en) * 2020-06-16 2021-08-10 General Electric Company Pressurized damping fluid injection for damping turbine blade vibration

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US2958456A (en) * 1954-10-06 1960-11-01 Power Jets Res & Dev Ltd Multi-stage aerofoil-bladed compressors
US3572960A (en) * 1969-01-02 1971-03-30 Gen Electric Reduction of sound in gas turbine engines
BE755567A (fr) * 1969-12-01 1971-02-15 Gen Electric Structure d'aube fixe, pour moteur a turbines a gaz et arrangement de reglage de temperature associe
FR2370170A1 (fr) * 1976-11-05 1978-06-02 Snecma Procede et dispositif pour la diminution du bruit des turbomachines
FR2370171A1 (fr) * 1976-11-05 1978-06-02 Snecma Procede et dispositif pour la diminution du bruit des turbomachines
GB2125111B (en) * 1982-03-23 1985-06-05 Rolls Royce Shroud assembly for a gas turbine engine
US5082421A (en) * 1986-04-28 1992-01-21 Rolls-Royce Plc Active control of unsteady motion phenomena in turbomachinery
US5275528A (en) * 1990-08-28 1994-01-04 Rolls-Royce Plc Flow control method and means
WO1996003585A1 (en) * 1994-07-28 1996-02-08 The Boeing Company Active control of tone noise in engine ducts
US5584651A (en) * 1994-10-31 1996-12-17 General Electric Company Cooled shroud

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008163947A (ja) * 2006-12-28 2008-07-17 General Electric Co <Ge> 流れ再循環を備えた圧縮システムの操作線制御

Also Published As

Publication number Publication date
DE69836154D1 (de) 2006-11-23
US6125626A (en) 2000-10-03
KR100539037B1 (ko) 2006-02-28
DE69825825T2 (de) 2005-09-01
EP1353039A3 (en) 2004-05-06
US6055805A (en) 2000-05-02
EP0899427A2 (en) 1999-03-03
DE69825825D1 (de) 2004-09-30
EP0899427B1 (en) 2004-08-25
KR19990023997A (ko) 1999-03-25
EP1353039A2 (en) 2003-10-15
EP0899427A3 (en) 2000-07-05
EP1353039B1 (en) 2006-10-11
DE69836154T2 (de) 2007-02-01

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