Engine assembly i.e. turbofan assembly, for aircraft, has connection units ensuring passage of efforts along effort resumption directions defining effort resumption plane, where resumption plane and rod plane intercept along straight line

摘要

The assembly has a mounting system including a front engine mount (16) provided with fixing units e.g. locks (58), secured to an intermediate casing (23). The engine mount comprises connection units e.g. rod (54), connecting the fixing units to a main body (30) of the engine mount. The connection units ensure passage of efforts along effort resumption directions defining an effort resumption plane (P2), where the effort resumption plane and a connecting rod plane (P1) intercept along a straight line (60) secant to a longitudinal axis (5) of an engine.