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公开(公告)号：US12188432B2
公开(公告)日：2025-01-07
申请号：US17797528
申请日：2021-02-05
Applicant: SAFRAN NACELLES
Inventor： Xavier Cazuc , Jean-Phillipe Joret
IPC: F02K1/72
Abstract: A device for attaching a connecting rod small end for a thrust reversal cascade flap onto a fixed internal structure of a turbojet engine nacelle includes a fitting configured to be fixed to the internal structure and a connection interface forming a joint between the connecting rod small end and the fitting. The device further includes a removable fork configured to cooperate with the connection interface, wherein the fork and the connection interface are arranged inside the fitting.
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