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
- Авторлар: Ivanov A.V.1, Danilikhin A.M.2, Baranov V.V.2
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Мекемелер:
- Moscow Aviation Institute (National Research University)
- OAO Aerosila, Research and Production Enterprise
- Шығарылым: Том 61, № 1 (2018)
- Беттер: 138-144
- Бөлім: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230451
- DOI: https://doi.org/10.3103/S1068799818010221
- ID: 230451
Дәйексөз келтіру
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.
Негізгі сөздер
Авторлар туралы
A. Ivanov
Moscow Aviation Institute (National Research University)
Email: vint@aerosila.ru
Ресей, Volokolamskoe sh. 4, Moscow, 125993
A. Danilikhin
OAO Aerosila, Research and Production Enterprise
Email: vint@aerosila.ru
Ресей, ul. Zhdanova 6, Stupino, Moskovskaya oblast, 142800
V. Baranov
OAO Aerosila, Research and Production Enterprise
Хат алмасуға жауапты Автор.
Email: vint@aerosila.ru
Ресей, ul. Zhdanova 6, Stupino, Moskovskaya oblast, 142800
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