A variable-pitch vane including a plurality of propeller blades (2). Each blade has a variable pitch according to a blade rotational axis (A1) and a root (201). A plurality of rotor connecting shafts (6), each shaft having a foot (602) and a head (601). The root (201) of each blade is mounted on the head (601) of a rotor connecting shaft via a pivot (8) in such a way as to allow each blade (2) to rotate according to the blade rotational axis (A1), in which each blade (2) has a blade pitch, such that the blade rotational axis (A1) is inclined relative to a radial axis (A2) passing through the foot (602) of the corresponding shaft.
ЛОПАСТНАЯ СИСТЕМА С РЕГУЛИРУЕМЫМ УГЛОМ УСТАНОВКИ
2017-04-06
Patent
Electronic Resource
Russian
IPC: | B64C AEROPLANES , Flugzeuge |
ВЫПУСКНАЯ СИСТЕМА ОТОПИТЕЛЬНО-ВЕНТИЛЯЦИОННОЙ УСТАНОВКИ КУЗОВНЫХ ОБЪЕКТОВ
European Patent Office | 2017
СИСТЕМА И СПОСОБ ДЛЯ ФОРСИРОВАНИЯ ГЛАВНОЙ СИЛОВОЙ УСТАНОВКИ
European Patent Office | 2019
СИСТЕМА УСТАНОВКИ ДИСПЛЕЯ ДЛЯ СНИЖЕНИЯ КРИТЕРИЯ ТРАВМИРОВАНИЯ ГОЛОВЫ
European Patent Office | 2017