US 12,188,432 B2
Device for attaching a connecting rod small end for a thrust reversal cascade flap
Xavier Cazuc, Moissy-Cramayel (FR); and Jean-Phillipe Joret, Moissy-Cramayel (FR)
Assigned to SAFRAN NACELLES, Gonfreville-l'Orcher (FR)
Appl. No. 17/797,528
Filed by SAFRAN NACELLES, Gonfreville-l'Orcher (FR)
PCT Filed Feb. 5, 2021, PCT No. PCT/EP2021/052868
§ 371(c)(1), (2) Date Aug. 4, 2022,
PCT Pub. No. WO2021/156477, PCT Pub. Date Aug. 12, 2021.
Claims priority of application No. 2001198 (FR), filed on Feb. 6, 2020.
Prior Publication US 2023/0059782 A1, Feb. 23, 2023
Int. Cl. F02K 1/72 (2006.01)
CPC F02K 1/72 (2013.01) [F05D 2260/31 (2013.01); F05D 2260/36 (2013.01); F05D 2260/38 (2013.01); F05D 2260/50 (2013.01)] 13 Claims
OG exemplary drawing
 
1. A device for attaching a connecting rod small end of a thrust reversal cascade flap onto an inner fixed structure of a turbojet engine nacelle, comprising a fitting configured to be fixed to said inner fixed structure and a connection interface forming a joint between the connecting rod small end and the fitting, and a removable locking means configured to cooperate with the connection interface so as to rotationally lock the connection means interface, the locking means and the connection interface being arranged inside the fitting.