Determination of vibration characteristics of blades of gas turbine engines contactless method

Authors

  • О.Г. Кучер НАУ, кафедра авіаційних двигунів
  • В.В. Харитон НАУ, кафедра авіаційних двигунів

DOI:

https://doi.org/10.18372/2306-1472.31.1452

Abstract

 Non-contact method simulation for blade real-time dynamic behavior determination is presented. This method uses eddy-current, capacitance or optical probes for blade tip deflections measurements which are related with time of blade tip passing trough the probe.

Author Biographies

О.Г. Кучер, НАУ, кафедра авіаційних двигунів

д-р техн. наук, проф.

В.В. Харитон, НАУ, кафедра авіаційних двигунів

асп.

References

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How to Cite

Кучер, О., & Харитон, В. (2007). Determination of vibration characteristics of blades of gas turbine engines contactless method. Proceedings of National Aviation University, 31(1), 134–138. https://doi.org/10.18372/2306-1472.31.1452

Issue

Section

MODERN AVIATION AND SPACE TEHNOLOGY