Method of Helicopter Turboshaft Engines’ Protection During Surge in Starting Mode

This article proposes a mathematical model for protecting helicopter turboshaft engines from surges, starting with fuel metering supply and maintaining stable compressor operation. The model includes several stages: first, fuel is supplied according to a specified program; second, an unstable compre...

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Autors principals:	Denys Baranovskyi, Serhii Vladov, Maryna Bulakh, Victoria Vysotska, Viktor Vasylenko, Jan Czyżewski
Format:	Artigo
Idioma:	Inglês
Publicat:	MDPI AG 2025-01-01
Col·lecció:	Energies
Matèries:	helicopter turboshaft engines surge gas temperature in front of the compressor turbine gas generator rotor speed compressor operation neural network
Accés en línia:	https://www.mdpi.com/1996-1073/18/1/168
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