Adjustable-length connecting rod for an aircraft turbomachine, connecting rod having a generally elongate shape and having first and second longitudinal opposite ends for attachment to elements to be connected. The first longitudinal end is connected to a first threaded shaft screwed into a first tubular portion of an adjustment sleeve. The second longitudinal end is connected to a second threaded shaft screwed into a second tubular portion of the adjustment sleeve. The connecting rod further includes a housing in which at least a portion of the first shaft is configured to slide.
ТЯГА С РЕГУЛИРУЕМОЙ ДЛИНОЙ ДЛЯ ГАЗОТУРБИННОГО ДВИГАТЕЛЯ
2020-10-08
Patent
Electronic Resource
Russian
ГИБКАЯ ПОДДЕРЖИВАЮЩАЯ КОНСТРУКЦИЯ ДЛЯ ЗУБЧАТОЙ ТРАНСМИССИИ ГАЗОТУРБИННОГО ДВИГАТЕЛЯ
European Patent Office | 2015
СПОСОБ И УСТРОЙСТВО ОБНАРУЖЕНИЯ ОБЛЕДЕНЕНИЯ ВОЗДУХОЗАБОРНИКА ГАЗОТУРБИННОГО ДВИГАТЕЛЯ
European Patent Office | 2017
European Patent Office | 2017