| 摘要 |
<p>The invention concerns a pod (1) for an aircraft comprising a cowling (5), an engine (6) housed in the inner volume of the cowling, an annular channel (9) circulating a secondary thrust flow arranged between the engine and the cowling, and at least one thrust reverser (2) for forming a reverse flow from the secondary thrust flow circulating in the annular channel. The thrust reverser comprising a plurality of doors (10) provided in the rear part (7) of the cowling, so as to form a trailing edge of the cowling. The thrust reverser can comprise means for actuating the doors such that at least one actuating means actuates two adjacent doors and at least one door is actuated by two actuating means.</p> |
