| 摘要 |
A nozzle (40) for use in a gas turbine engine (10) includes a nozzle door (54) having a first end (54a), a second end (54b) opposed from the first end (54a), and a pivot (56) between the first end (54a) and the second end (54b). A linkage (64) connects to the nozzle door (54) and to an actuator (42). The actuator (42) is selectively operative to move the linkage (64) to in turn move the nozzle door (54) about the pivot (56) between a plurality of positions, such as a stowed position, an intermediate position, and a thrust reverse position, to influence a bypass airflow through a fan bypass passage (30). |
