| 摘要 |
<p>In order to carry out mounting of a turbine engine (10) on an aircraft structure such as a wing (12), a central, non-rotating forward body of the turbine engine is used, which is linked by a ball-and-socket joint (16) to a thrust transmission member such as an air intake (14), which is itself linked to the wing (12) by a thrust transmission system (18). In this way, the thrust (X) of the turbine engine is transmitted to the air intake (14) along the longitudinal axis of the turbine engine, before being transmitted to the aircraft structure by the system (18). The casings and the shaft lines of the turbine engine are thus not subjected to any bending moment, which makes it possible to optimise the performance of this turbine engine. Moreover, the deformation of the wing (12) remains possible, without risk of surge in the turbine engine. <IMAGE></p> |
