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
- Авторы: Ivanov A.V.1, Danilikhin A.M.2, Baranov V.V.2
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Учреждения:
- Moscow Aviation Institute (National Research University)
- OAO Aerosila, Research and Production Enterprise
- Выпуск: Том 61, № 1 (2018)
- Страницы: 138-144
- Раздел: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230451
- DOI: https://doi.org/10.3103/S1068799818010221
- ID: 230451
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Аннотация
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.
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Об авторах
A. Ivanov
Moscow Aviation Institute (National Research University)
Email: vint@aerosila.ru
Россия, Volokolamskoe sh. 4, Moscow, 125993
A. Danilikhin
OAO Aerosila, Research and Production Enterprise
Email: vint@aerosila.ru
Россия, ul. Zhdanova 6, Stupino, Moskovskaya oblast, 142800
V. Baranov
OAO Aerosila, Research and Production Enterprise
Автор, ответственный за переписку.
Email: vint@aerosila.ru
Россия, ul. Zhdanova 6, Stupino, Moskovskaya oblast, 142800
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