Use of a Nonlinear Mathematical Model of Turboprop Engine on a Semi-Full-Scale Simulation Test Bench for Testing Propellers in Conjunction with Their Automatic Control System
- Authors: Ivanov A.V.1, Danilikhin A.M.2, Baranov V.V.2
-
Affiliations:
- Moscow Aviation Institute (National Research University)
- OAO Aerosila, Research and Production Enterprise
- Issue: Vol 61, No 1 (2018)
- Pages: 138-144
- Section: Aircraft and Rocket Engine Theory
- URL: https://journal-vniispk.ru/1068-7998/article/view/230451
- DOI: https://doi.org/10.3103/S1068799818010221
- ID: 230451
Cite item
Abstract
This paper considers an issue of increasing reliability of turboprop engine simulation on a semi-full-scale simulation test bench. A detailed mathematical model (subassembly model) of a turboprop engine is used for improving simulation quality and optimizing the algorithms of turboprop automatic control system in the operation conditions being expected.
About the authors
A. V. Ivanov
Moscow Aviation Institute (National Research University)
Email: vint@aerosila.ru
Russian Federation, Volokolamskoe sh. 4, Moscow, 125993
A. M. Danilikhin
OAO Aerosila, Research and Production Enterprise
Email: vint@aerosila.ru
Russian Federation, ul. Zhdanova 6, Stupino, Moskovskaya oblast, 142800
V. V. Baranov
OAO Aerosila, Research and Production Enterprise
Author for correspondence.
Email: vint@aerosila.ru
Russian Federation, ul. Zhdanova 6, Stupino, Moskovskaya oblast, 142800
Supplementary files
