ТУРБОРЕАКТИВНЫЙ ДВИГАТЕЛЬ ДЛЯ КРЕПЛЕНИЯ НА ХВОСТОВОЙ ЧАСТИ ФЮЗЕЛЯЖА ЛЕТАТЕЛЬНОГО АППАРАТА В ВЕРХНЕМПОЛОЖЕНИИ

摘要

The engine has accessories (22-25) that are arranged at the periphery of a crank case (12). The crank case has fixation points (31-33) for fixing hall stands (28, 28). The fixing points are arranged so as to permit assembling of a jet engine (10) from either one of sides of a fuselage (1). The accessories are arranged on the crank case such that they are accessible from the exterior of the fuselage. An independent claim is also included for a flight having a fuselage.