Turboprofan jet modeling and equivalent specific fuel consumption optimization subsystem construction on the seminatural modelling stand

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Abstract

There was shown offered method’s of linear interpolation propfan’s multidimensional characteristic results using for modeling turboprofan jet in a total range of flight conditions and approach to equivalent specific fuel consumption optimization subsystem construction in automatic control system structure for reduction of environmental tests and maintenance costs. The offered methods considers requirements to mathematical models for the seminatural modeling stand - simplicity, ensuring of sufficient accuracy of result, work and functioning engine’s mathematical model in a mode of real time.

About the authors

G. I. Pogorelov

Open joint-stock company ufa's research-and-production enterprise «Molniya»

Author for correspondence.
Email: pogorelov@molniya-ufa.ru

candidate of technical sciences
general director deputy

Russian Federation

I. A. Krivosheev

Ufa's state aircraft technical university

Email: krivosh@sci.ugatu.ac.ru

doctor of technical sciences, professor

Russian Federation

A. G. Godovanyuk

Ufa's state aircraft technical university

Email: algen82@mail.ru

junior researcher

Russian Federation

O. E. Danilin

Ufa's state aircraft technical university

Email: odanilin@mail.ru

candidate of technical sciences, associate professor

Russian Federation

B. I. Badamshin

Ufa's state aircraft technical university

Email: badbul_auto@inbox.ru

post-graduate student

Russian Federation

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