Rotor blades efficiency increase at the last stage of steam turbines

The results of the comparative researches of given and new profiles are offered. The new profile is received on the basis of inverse problem solving which allows to get aerodynamic loss minimization and necessary index of rotor blade’s resistance in the zone with serving wires. The results are exami...

Повний опис

Збережено в:
Бібліографічні деталі
Дата:2017
Автори: Левченко, Е. В., Субботович, В. П., Юдин, А. Ю., Бояршинов, А. Ю.
Формат: Стаття
Мова:Russian
Опубліковано: Інститут енергетичних машин і систем ім. А. М. Підгорного Національної академії наук України 2017
Теми:
Онлайн доступ:https://journals.uran.ua/jme/article/view/91628
Теги: Додати тег
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Назва журналу:Energy Technologies & Resource Saving

Репозитарії

Energy Technologies & Resource Saving
Опис
Резюме:The results of the comparative researches of given and new profiles are offered. The new profile is received on the basis of inverse problem solving which allows to get aerodynamic loss minimization and necessary index of rotor blade’s resistance in the zone with serving wires. The results are examined from the gas dynamics improvement of this zone of rotor blade in the area of transonic velocities point of view. It is shown that in this area new profile has a noticeably smaller loss profile coefficient than the given one which is used in real blade.