| 摘要 |
The nozzle has a control system for controlling movable flaps (12a, 12b, 13). The system has control levers composed of controlled levers (16a) directly actuated by jacks (18) and follower levers (16b) actuated by the levers (16a) through a transmission link (20). The flaps (12b) associated with the levers (16b) present a radial offset relative to the flaps (12a) associated with the levers (16a) during stopping of the nozzle. An independent claim is also included for a turbomachine comprising a variable section nozzle. |
