ES2009880A6 - Metodo y aparato para determinar las resonancias de vibracion de los alabes de una turbomaquina. - Google Patents

Metodo y aparato para determinar las resonancias de vibracion de los alabes de una turbomaquina.

Info

Publication number
ES2009880A6
ES2009880A6 ES8800511A ES8800511A ES2009880A6 ES 2009880 A6 ES2009880 A6 ES 2009880A6 ES 8800511 A ES8800511 A ES 8800511A ES 8800511 A ES8800511 A ES 8800511A ES 2009880 A6 ES2009880 A6 ES 2009880A6
Authority
ES
Spain
Prior art keywords
frequencies
programmable
resonance
excitation system
albes
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
Application number
ES8800511A
Other languages
English (en)
Spanish (es)
Inventor
Serge Peter Barton
Paul Francis Rozelle
Michael Twerdochlip
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.)
Westinghouse Electric Corp
Original Assignee
Westinghouse Electric 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 Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Publication of ES2009880A6 publication Critical patent/ES2009880A6/es
Expired 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
    • F01D5/16—Form or construction for counteracting blade vibration
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01H—MEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC OR INFRASONIC WAVES
    • G01H1/00—Measuring characteristics of vibrations in solids by using direct conduction to the detector
    • G01H1/003—Measuring characteristics of vibrations in solids by using direct conduction to the detector of rotating machines
    • G01H1/006—Measuring characteristics of vibrations in solids by using direct conduction to the detector of rotating machines of the rotor of turbo machines

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Control Of Turbines (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
ES8800511A 1987-02-24 1988-02-23 Metodo y aparato para determinar las resonancias de vibracion de los alabes de una turbomaquina. Expired ES2009880A6 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/018,384 US4776216A (en) 1987-02-24 1987-02-24 Programmable jet blade excitation system

Publications (1)

Publication Number Publication Date
ES2009880A6 true ES2009880A6 (es) 1989-10-16

Family

ID=21787655

Family Applications (1)

Application Number Title Priority Date Filing Date
ES8800511A Expired ES2009880A6 (es) 1987-02-24 1988-02-23 Metodo y aparato para determinar las resonancias de vibracion de los alabes de una turbomaquina.

Country Status (6)

Country Link
US (1) US4776216A (enExample)
JP (1) JPS63229333A (enExample)
KR (1) KR880010212A (enExample)
CN (1) CN1013405B (enExample)
ES (1) ES2009880A6 (enExample)
IT (1) IT1215837B (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2038903A2 (es) * 1990-08-30 1993-08-01 Westinghouse Electric Corp "aparato y metodo para simular senales sensoriales de paso de alabe"

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9618096D0 (en) * 1996-08-29 1996-10-09 Rolls Royce Plc Identification of resonant frequencies of vibration of rotating blades
DE19738595C1 (de) * 1997-09-04 1999-02-11 Mtu Muenchen Gmbh Prüfvorrichtung für Dämpfungselemente von Laufschaufeln
US6679121B2 (en) 2000-07-07 2004-01-20 Test Devices, Inc. Blade vibration test apparatus and method
NL1018974C2 (nl) * 2001-09-18 2003-04-04 Kema Nv Werkwijze en inrichting voor het onderzoeken van de rek van langwerpige lichamen.
EP2165167B1 (en) * 2007-04-30 2016-03-16 Nuovo Pignone S.p.A. Method and system for turbine blade characterization
US7987725B2 (en) * 2007-09-21 2011-08-02 Siemens Energy, Inc. Method of matching sensors in a multi-probe turbine blade vibration monitor
US7654145B2 (en) * 2007-09-27 2010-02-02 Siemens Energy, Inc. Non-synchronous vibrational excitation of turbine blades using a rotating excitation structure
EP2103915B1 (en) * 2008-03-17 2016-11-16 Siemens Aktiengesellschaft Apparatus and method for determining a resonant frequency of a wind turbine tower
US8650970B2 (en) * 2008-06-30 2014-02-18 Vestas Wind Systems A/S Test rig for testing blades for a wind turbine
KR101293357B1 (ko) * 2011-09-26 2013-08-05 한양대학교 산학협력단 다중블레이드 회전체 진동해석방법
US9739167B2 (en) * 2012-07-25 2017-08-22 Siemens Energy, Inc. Method and system for monitoring rotating blade health
CN103630314A (zh) * 2013-11-25 2014-03-12 苏州东菱振动试验仪器有限公司 叶片高在线气流激励系统及测试方法
US10794387B2 (en) * 2016-09-02 2020-10-06 Raytheon Technologies Corporation Damping characteristic determination for turbomachine airfoils
US10598183B2 (en) * 2016-11-29 2020-03-24 United Technologies Corporation Aeromechanical identification systems and methods
US10775269B2 (en) * 2017-02-08 2020-09-15 Raytheon Technologies Corporation Blade health inspection using an excitation actuator and vibration sensor
CN106706322B (zh) * 2017-03-23 2018-11-02 河海大学 一种水轮机碰摩故障模拟实验装置及模拟方法
US11898498B2 (en) 2019-04-30 2024-02-13 Rolls-Royce Deutschland Ltd & Co Kg Method and system for reducing cross-shaft vibrations
US11085303B1 (en) 2020-06-16 2021-08-10 General Electric Company Pressurized damping fluid injection for damping turbine blade vibration
US11143036B1 (en) 2020-08-20 2021-10-12 General Electric Company Turbine blade with friction and impact vibration damping elements
CN114993590B (zh) * 2021-02-24 2023-10-13 中国航发商用航空发动机有限责任公司 激振系统以及用于测试航空发动机转子的试验设备
CN113984311A (zh) * 2021-10-26 2022-01-28 中国航发沈阳发动机研究所 一种全发动机阶次叶盘激振试验装置及发动机阶次定距尺

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2682167A (en) * 1951-12-29 1954-06-29 Gen Electric Fatigue testing apparatus
US2738671A (en) * 1953-11-17 1956-03-20 Gen Electric Pneumatic fatigue testing device
DE1120709B (de) * 1958-06-04 1961-12-28 Daimler Benz Ag Verfahren und Vorrichtungen zur Messung von Schaufelschwingungen, insbesondere bei Strahltriebwerken

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2038903A2 (es) * 1990-08-30 1993-08-01 Westinghouse Electric Corp "aparato y metodo para simular senales sensoriales de paso de alabe"

Also Published As

Publication number Publication date
CN1013405B (zh) 1991-07-31
CN88100992A (zh) 1988-09-07
KR880010212A (ko) 1988-10-07
IT1215837B (it) 1990-02-22
US4776216A (en) 1988-10-11
IT8819360A0 (it) 1988-02-10
JPH0512653B2 (enExample) 1993-02-18
JPS63229333A (ja) 1988-09-26

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Legal Events

Date Code Title Description
SA6 Expiration date (snapshot 920101)

Free format text: 2008-02-23

FD1A Patent lapsed

Effective date: 19991108