Development of airframe design elements control technique under operational conditions

Authors

  • O. L. Pusyryov National Aviation University
  • V. O. Volkogon National Aviation University
  • O. M. Alekseev National Aviation University
  • V. V. Ushakov National Aviation University

DOI:

https://doi.org/10.18372/1990-5548.50.11386

Keywords:

Diagnostics, composite materials, infrared radiation, inspection

Abstract

The paper proposes to use a method of infrared pulse-echo inspection to control airframe designelements, made of polymeric composite materials under operators` conditions. The following is described:skeleton operation diagram of the given method, device structure and results of the preliminary researchesconfirming operation capacity of the method offered

Author Biographies

O. L. Pusyryov, National Aviation University

Candidate of Science (Engineering). Associate Professor. Aviation Technical Department, Flight Academy

V. O. Volkogon, National Aviation University

Post-graduate student. Educational and Research Institute of Air Navigation

O. M. Alekseev, National Aviation University

Postdoctoral student. Candidate of Science (Engineering). Associate Professor. Educational and Research Institute of Air Navigation

V. V. Ushakov, National Aviation University

Assistant Professor.Aviation Technical Department, Flight Academy

References

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Klyuev Eds. vols. 1–7; book 2, Moscow: Mashinostroenie, 2004.

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How to Cite

Pusyryov, O. L., Volkogon, V. O., Alekseev, O. M., & Ushakov, V. V. (2016). Development of airframe design elements control technique under operational conditions. Electronics and Control Systems, 4(50), 46–50. https://doi.org/10.18372/1990-5548.50.11386

Issue

Vol. 4 No. 50 (2016)

Section

AUTOMATIC CONTROL SYSTEMS

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