| 摘要 |
The invention relates to a thrust reverser for a turbojet pod, including cowls (6) that move backwards to open said reverser, wherein each cowl comprises a main axial guide rail, that mainly bears the load of said cowl, and a secondary rail guiding an outer portion of said cowl. Said thrust reverser is characterized in that a rear end stop (14, 16) of the cowl (6) is arranged on the main rail. |
