PL385983A1 - Measuring method of torsional vibrations of turbine blade and blades' disk in flow turbomachine, using an induction sensor - Google Patents

Measuring method of torsional vibrations of turbine blade and blades' disk in flow turbomachine, using an induction sensor

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Publication number
PL385983A1
PL385983A1 PL385983A PL38598308A PL385983A1 PL 385983 A1 PL385983 A1 PL 385983A1 PL 385983 A PL385983 A PL 385983A PL 38598308 A PL38598308 A PL 38598308A PL 385983 A1 PL385983 A1 PL 385983A1
Authority
PL
Poland
Prior art keywords
sensor
torsional vibrations
blade
blades
disk
Prior art date
Application number
PL385983A
Other languages
Polish (pl)
Other versions
PL210354B1 (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 PL385983A priority Critical patent/PL210354B1/en
Publication of PL385983A1 publication Critical patent/PL385983A1/en
Publication of PL210354B1 publication Critical patent/PL210354B1/en

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  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)

Abstract

Wynalazek rozwiązuje zagadnienie pomiaru drgań skrętnych łopatki wirnika i drgań tarczy wieńca łopatek wirnikowej maszyny przepływowej za pomocą czujnika indukcyjnego. Sygnały powstałe w czujniku odbiera się przez układ dwóch prostopadłych względem siebie cewek indukcyjnych, których uzwojenie ma kierunek równoległy do linii sił pola magnetycznego wytwarzanego przez magnes. Stosunek wartości tych sygnałów określa kąt skręcenia łopatki względem wyznaczonej osi czujnika. Czas przejścia łopatki przez pole magnetyczne czujnika jest określany przez przejście sygnału jednej z cewek przez wartość zerową. Wynalazek znajduje zastosowanie w diagnostyce turbinowych maszyn przepływowych.The invention solves the problem of measuring the torsional vibrations of the rotor blade and the vibrations of the blade ring disc of a turbomachine rotor using an inductive sensor. The signals generated in the sensor are received by a system of two perpendicular induction coils, the winding of which has a direction parallel to the lines of force of the magnetic field generated by the magnet. The ratio of the values of these signals determines the angle of rotation of the blade relative to the designated sensor axis. The time the blade passes through the sensor's magnetic field is determined by the passage of the signal of one of the coils through the zero value. The invention is used in the diagnostics of turbine turbomachines.

PL385983A 2008-06-30 2008-06-30 Measuring method of torsional vibrations of turbine blade and blades' disk in flow turbomachine, using an induction sensor PL210354B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL385983A PL210354B1 (en) 2008-06-30 2008-06-30 Measuring method of torsional vibrations of turbine blade and blades' disk in flow turbomachine, using an induction sensor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PL385983A PL210354B1 (en) 2008-06-30 2008-06-30 Measuring method of torsional vibrations of turbine blade and blades' disk in flow turbomachine, using an induction sensor

Publications (2)

Publication Number Publication Date
PL385983A1 true PL385983A1 (en) 2010-01-04
PL210354B1 PL210354B1 (en) 2012-01-31

Family

ID=43012055

Family Applications (1)

Application Number Title Priority Date Filing Date
PL385983A PL210354B1 (en) 2008-06-30 2008-06-30 Measuring method of torsional vibrations of turbine blade and blades' disk in flow turbomachine, using an induction sensor

Country Status (1)

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PL (1) PL210354B1 (en)

Also Published As

Publication number Publication date
PL210354B1 (en) 2012-01-31

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