PROCEDURE ESTABLISHING ANGULAR POSITIONS OF BLADES OF TURBOMACHINES ( VARIANTS ) Russian patent published in 2003 - IPC

Abstract RU 2215986 C1

FIELD: measurement technology. SUBSTANCE: procedure can be employed for contact-free test of radial clearances between butts of blades and jacket of fan and of angular positions of blades in process of operation of fan during tests and operation. In compliance with first variant dependence of length of path S in which blade interacts with eddy-current converter on angular position α. of blade is established first. Inverse relationship α = f(S) is constructed by obtained dependence, eddy- current converter is placed on frame of turbo-machine. In process of operation of turbo-machine eddy- current converter is excited in zone of clearance measurement with alternating magnetic field and values of signals measured in passage of blades through sensitive zone of eddy-current converter are recorded. Length ttp of pulse during which blade interacts with eddy-current converter is measured, linear velocity of motion of peripheral section of blade V is measured too. Length of path S in which blade interacts with eddy-current converter is calculated by multiplication of length ttp of pulse by linear velocity of motion of peripheral section of blade V by which angular position of blade is established with use of relationship α = f(S) obtained earlier. In correspondence with second variant dependence of length of path S during which blade interacts with eddy-current converter on angular position α, of blade is found beforehand. Obtained dependence is used to construct inverse relationship α = f(S). In process of operation of turbo- machine pulse repetition period T is measured, length ttp of pulse during which blade interacts with eddy-current converter is measured. Relative pulse duration is computed as relation of pulse repetition period T to length ttp of pulse during which blade interacts with eddy-current converter. Length S of path in which blade interacts with eddy-current converter is computed by division of value of spacing between blades into pulse repetition period Q and angular position of blade is established by substitution of obtained value of length S of path into relationship α = f(S) obtained before. EFFECT: reduced number of pickups required for establishment of angular positions of blades. 4 cl, 1 dwg

Similar patents RU2215986C1

Title Year Author Number
METHOD FOR EVALUATING ANGULAR POSITIONS OF TURBINE PERIPHERAL BLADE SECTIONS 2003
  • Mednikov V.A.
  • Shchegolev V.V.
RU2238520C1
METHOD DETERMINING DEFORMATION OF BLADES OF ROTATING WHEEL OF TURBO-MACHINE AND GEAR FOR ITS IMPLEMENTATION 1998
  • Danilin A.I.
  • Surkov V.V.
  • Chernjavskij A.Zh.
RU2152590C1
METHOD FOR METERING VIBRATION AMPLITUDES OF TURBOMACHINE BLADES 2003
  • Shchegolev V.V.
RU2244272C1
DEVICE WARNING OF PREEMERGENCY DEFORMATION OF BLADES OF TURBO-MACHINE 2000
  • Danilin A.I.
  • Chernjavskij A.Zh.
RU2177145C1
METHOD ESTABLISHING PARAMETERS OF VIBRATIONS OF BLADES OF TURBOMACHINES 2002
  • Mednikov V.A.
  • Shchegolev V.V.
RU2229104C1
METHOD FOR DETERMINING AMPLITUDE OF OSCILLATIONS OF TURBOMACHINE BLADE 2002
  • Mednikov V.A.
  • Shchegolev V.V.
RU2207524C1
GAS TURBINE BLADE 2000
  • Ermolaev G.V.
  • Aronov B.M.
RU2178086C2
METHOD FOR SPIN AND SPIN COMPONENT AMPLITUDE MEASUREMENT FOR ROTODYNAMIC MACHINE BLADE OSCILLATION, AND DEVICE FOR IMPLEMENTATION OF METHOD 2007
  • Danilin Aleksandr Ivanovich
  • Lofitskij Igor' Vadimovich
  • Danilin Sergej Aleksandrovich
  • Chernjavskij Arkadij Zhorzhevich
  • Serpokrylov Mikhail Ivanovich
  • Aref'Eva Ol'Ga Viktorovna
RU2337330C1
METHOD FOR DETERMINING PARAMETERS OF OSCILLATIONS OF BLADES OF ROTATING IMPELLER OF TURBOMACHINE AND APPARATUS FOR PERFORMING THE SAME 2001
  • Danilin A.I.
  • Chernjavskij A.Zh.
RU2207523C1
GEAR FOR ELECTRIC DISCHARGE TREATMENT OF AIR IN SMALL-SIZED CLOSED VOLUMES 1999
  • Zhuravlev O.A.
  • Ivchenko A.V.
RU2173666C2

RU 2 215 986 C1

Authors

Mednikov V.A.

Shchegolev V.V.

Dates

2003-11-10Published

2002-03-11Filed