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
- 作者: Ivanov A.V.1, Danilikhin A.M.2, Baranov V.V.2
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隶属关系:
- Moscow Aviation Institute (National Research University)
- OAO Aerosila, Research and Production Enterprise
- 期: 卷 61, 编号 1 (2018)
- 页面: 138-144
- 栏目: 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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详细
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.
作者简介
A. Ivanov
Moscow Aviation Institute (National Research University)
Email: vint@aerosila.ru
俄罗斯联邦, Volokolamskoe sh. 4, Moscow, 125993
A. Danilikhin
OAO Aerosila, Research and Production Enterprise
Email: vint@aerosila.ru
俄罗斯联邦, ul. Zhdanova 6, Stupino, Moskovskaya oblast, 142800
V. Baranov
OAO Aerosila, Research and Production Enterprise
编辑信件的主要联系方式.
Email: vint@aerosila.ru
俄罗斯联邦, ul. Zhdanova 6, Stupino, Moskovskaya oblast, 142800
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