公开(公告)号：US09835113B2

公开(公告)日：2017-12-05

申请号：US15076907

申请日：2016-03-22

Applicant: AIRCELLE

Inventor： Alexis Loncle

IPC: F02K1/78 ,  F02K1/76 ,  F02K1/72 ,  B64D29/06 ,  E05B63/18 ,  F02K1/80

CPC classification number: F02K1/766 ,  B64D29/06 ,  E05B63/18 ,  E05B63/185 ,  F02K1/72 ,  F02K1/763 ,  F02K1/80 ,  Y02T50/671

Abstract: The present disclosure relates to a thrust reverser for a turbojet engine nacelle, including cowls that move backwards to open the thrust reverser. Each cowl includes a primary axial guide rail that receives most of the loads of the cowl, and secondary rails guiding an outer portion of each cowl. The thrust reverser includes a rear end stop for each cowl is arranged on the primary axial guide rails.