| 摘要 |
<p>The pylon (12) has an upstream part (24) and a downstream part (26) that are connected with each other by an articulation, where the part (26) is fixed under an aircraft wing (14) and the part (24) is fixed at a hood of an engine (10) i.e. turbofan engine. A motorized unit e.g. hydraulic/ electric actuator (44), connects two parts and permits in-flight modification of position in height of the engine between a cruise position and a takeoff/landing position. The unit has a cylinder (46) articulated on the part (24), and a piston rod (48) is articulated on the part (26).</p> |
