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Automated system for testing specimens of helicopter blades

  • Mechanical Measurements
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Measurement Techniques Aims and scope

Abstract

A description is presented of an automated system for testing specimens of helicopter blades. Features of monitoring and testing operations are also described along with stages of the testing process.

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References

  1. Z. A. Bashirov and S. R. Kaminsky, Fatigue Test Control System. Fourth International Congress on Sound and Vibration, St. Petersburg, Russia, June 24–27 (1996), Vol. 2, p. 1101.

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  2. V. V. Stashin, A. V. Urusov, and O. F. Mologontseva, Designing Digital Devices on Single-Crystal Microcontrollers [in Russian], Energoizdat, Moscow (1990).

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Authors
  1. Z. A. Bashirov
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  2. S. R. Kaminskii
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  3. S. S. Kaminskii
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Additional information

Translated from Izmeritel'naya Tekhnika, No. 7, pp. 37–39, July, 1997.

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Bashirov, Z.A., Kaminskii, S.R. & Kaminskii, S.S. Automated system for testing specimens of helicopter blades. Meas Tech 40, 663–665 (1997). https://doi.org/10.1007/BF02504183

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  • DOI: https://doi.org/10.1007/BF02504183

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