Fiber-optical pressure transducer for the UA engine control system

G. I. Leonovich; Леонович Г. И.; S. A. Matyunin; Матюнин С. А.; A. I. Glushkov; Глушков А. И.; N. A. Livochkina; Ливочкина Н. А.; V. I. Solovyov; Соловьёв В. И.

doi:10.18287/2541-7533-2011-0-5(29)-145-150

Fiber-optical pressure transducer for the UA engine control system

Authors: Leonovich G.I.¹, Matyunin S.A.¹, Glushkov A.I.¹, Livochkina N.A.², Solovyov V.I.¹
Affiliations:
1. Samara State Aerospace University
2. SRPSRC “TsSKB-Progress”, Samara
Issue: Vol 10, No 5 (2011)
Pages: 145-150
Section: ISSUE WITHOUT SECTION
URL: https://journals.ssau.ru/vestnik/article/view/2753
DOI: https://doi.org/10.18287/2541-7533-2011-0-5(29)-145-150
ID: 2753

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Abstract

The difficulties of power plant optimization and airborne equipment complexing are related to UA dimensions and functional complexity of its accessories. They are exhibited to the greatest extent in aircraft with small dimensions. At the same time, up-to-date technologies make it possible to produce powerful miniature processors, superlight fiber-optical transducers and onboard networks on their basis. The use of sensor conduction coatings substantially increases the sensitivity of fiber-optical transducers and expands their dynamic range. In particular, this is true of pressure transducers for power plant control systems.