公开(公告)号：US12152552B2

公开(公告)日：2024-11-26

申请号：US17904572

申请日：2021-02-16

Applicant: SAFRAN NACELLES

Inventor： Xavier Cazuc ,  Vincent Jean-Francois Peyron ,  Jean-Philippe Joret ,  Sebastien Laurent Marie Pascal

IPC: F02K1/72

Abstract: The invention relates to an assembly (601) which comprises a front frame (602) of a thrust reverser structure of an aircraft nacelle and at least one cascade (603). The assembly is characterized in that, when the cascade is fixed to the frame, the axial distance (L) that separates the first blading (605) upstream of the cascade from a covering area (606) between the extension of the cascade and the front frame is greater than or equal to once the mean height (h) of the cascade.