The adjustment of the mathematical model accuracy of the gas-hydraulic flight control actuator power circuit of an aircraft
- Авторлар: Ermakov S.1, Lalabekov V.1, Samsonovich S.1
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Мекемелер:
- Moscow Aviation Institute (National Research University)
- Шығарылым: Том 60, № 3 (2017)
- Беттер: 412-420
- Бөлім: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230200
- DOI: https://doi.org/10.3103/S1068799817030138
- ID: 230200
Дәйексөз келтіру
Аннотация
The methodology is proposed and the mathematical model is developed for the purpose of numerical simulation of the power circuit of the gas-hydraulic actuator with displacing power source for the gimbaled nozzle control. It provides the highest power efficiency factor of the actuator as a part of aircraft by means of pulling together the profiles of available and required power.
Авторлар туралы
S. Ermakov
Moscow Aviation Institute (National Research University)
Email: lalabekov.valentin@yandex.ru
Ресей, Volokolamskoe shosse 4, Moscow, 125993
V. Lalabekov
Moscow Aviation Institute (National Research University)
Хат алмасуға жауапты Автор.
Email: lalabekov.valentin@yandex.ru
Ресей, Volokolamskoe shosse 4, Moscow, 125993
S. Samsonovich
Moscow Aviation Institute (National Research University)
Email: lalabekov.valentin@yandex.ru
Ресей, Volokolamskoe shosse 4, Moscow, 125993