| 摘要 |
Aspects of the disclosure are directed to a system for a thrust reverser of an aircraft comprising: a primary sleeve 202, and a secondary sleeve 232, wherein a first stroke 202' associated with the primary sleeve 202 is different from a second stroke 232' associated with the secondary sleeve 232, and wherein the primary sleeve 202 traverses a first distance associated with the first stroke 202' at the outset of a deployment of the thrust reverser and a second distance associated with the first stroke at a later stage of the deployment. |
