PL385627A1 - Sposób pomiaru drgań łopatki turbiny wirnikowej maszyny przepływowej za pomocą czujnika indukcyjnego w wysokiej temperaturze - Google Patents

Sposób pomiaru drgań łopatki turbiny wirnikowej maszyny przepływowej za pomocą czujnika indukcyjnego w wysokiej temperaturze

Info

Publication number
PL385627A1
PL385627A1 PL385627A PL38562708A PL385627A1 PL 385627 A1 PL385627 A1 PL 385627A1 PL 385627 A PL385627 A PL 385627A PL 38562708 A PL38562708 A PL 38562708A PL 385627 A1 PL385627 A1 PL 385627A1
Authority
PL
Poland
Prior art keywords
measurement
high temperature
fluid flow
inductive sensor
machine rotor
Prior art date
Application number
PL385627A
Other languages
English (en)
Inventor
Edward Rokicki
Jarosław Spychała
Ryszard Szczepanik
Paweł Majewski
Original Assignee
Instytut Techniczny Wojsk Lotniczych
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 Instytut Techniczny Wojsk Lotniczych filed Critical Instytut Techniczny Wojsk Lotniczych
Priority to PL385627A priority Critical patent/PL385627A1/pl
Priority to US12/477,472 priority patent/US8125215B2/en
Publication of PL385627A1 publication Critical patent/PL385627A1/pl

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01HMEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC OR INFRASONIC WAVES
    • G01H1/00Measuring characteristics of vibrations in solids by using direct conduction to the detector
    • G01H1/003Measuring characteristics of vibrations in solids by using direct conduction to the detector of rotating machines
    • G01H1/006Measuring 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)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
PL385627A 2008-06-09 2008-06-09 Sposób pomiaru drgań łopatki turbiny wirnikowej maszyny przepływowej za pomocą czujnika indukcyjnego w wysokiej temperaturze PL385627A1 (pl)

Priority Applications (2)

Application Number Priority Date Filing Date Title
PL385627A PL385627A1 (pl) 2008-06-09 2008-06-09 Sposób pomiaru drgań łopatki turbiny wirnikowej maszyny przepływowej za pomocą czujnika indukcyjnego w wysokiej temperaturze
US12/477,472 US8125215B2 (en) 2008-06-09 2009-06-03 Measuring vibrations of a turbo-machine rotor blade with the help of an induction sensor in high temperature

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL385627A PL385627A1 (pl) 2008-06-09 2008-06-09 Sposób pomiaru drgań łopatki turbiny wirnikowej maszyny przepływowej za pomocą czujnika indukcyjnego w wysokiej temperaturze

Publications (1)

Publication Number Publication Date
PL385627A1 true PL385627A1 (pl) 2009-12-21

Family

ID=41695751

Family Applications (1)

Application Number Title Priority Date Filing Date
PL385627A PL385627A1 (pl) 2008-06-09 2008-06-09 Sposób pomiaru drgań łopatki turbiny wirnikowej maszyny przepływowej za pomocą czujnika indukcyjnego w wysokiej temperaturze

Country Status (2)

Country Link
US (1) US8125215B2 (pl)
PL (1) PL385627A1 (pl)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
PL210672B1 (pl) * 2008-06-23 2012-02-29 Inst Tech Wojsk Lotniczych Czujnik indukcyjny do pomiaru drgań łopatki wirnika przepływowej maszyny wirnikowej
DE102013222276A1 (de) * 2013-11-01 2015-05-21 Rolls-Royce Deutschland Ltd & Co Kg Induktiver Sensor und Verfahren zum Herstellen eines induktiven Sensors
FR3015673B1 (fr) * 2013-12-23 2015-12-18 Turbomeca Ensemble pour turbomachine pour mesurer des vibrations subies par une pale en rotation
FR3015671B1 (fr) 2013-12-23 2020-03-20 Safran Helicopter Engines Ensemble pour turbomachine pour mesurer des vibrations subies par une pale en rotation
CN112730021B (zh) * 2020-11-30 2023-04-07 湘潭大学 一种振动热冲击耦合的服役工况加载***和方法

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7023205B1 (en) * 2000-08-01 2006-04-04 General Dynamics Advanced Information Systems, Inc. Eddy current sensor capable of sensing through a conductive barrier
US6661222B1 (en) * 2002-05-31 2003-12-09 Siemens Westinghouse Power Corporation Turbine blade clearance on-line measurement system
US7424823B2 (en) * 2004-10-19 2008-09-16 Techno-Sciences, Inc. Method of determining the operating status of a turbine engine utilizing an analytic representation of sensor data

Also Published As

Publication number Publication date
US8125215B2 (en) 2012-02-28
US20100045273A1 (en) 2010-02-25

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Legal Events

Date Code Title Description
DISC Decisions on discontinuance of the proceedings (taken after the publication of the particulars of the applications)