公开(公告)号：US11649738B2

公开(公告)日：2023-05-16

申请号：US17273898

申请日：2019-09-04

Applicant: SAFRAN AIRCRAFT ENGINES

Inventor： Antonin Etienne Diego Tessiereau ,  Cyrille François Antoine Mathias ,  Wouter Balk

IPC: F01D25/28 ,  F01D25/00 ,  F01D25/24 ,  F01D9/02

CPC classification number: F01D25/28 ,  F01D9/02 ,  F01D25/005 ,  F01D25/24 ,  F05D2240/14 ,  F05D2250/231 ,  F05D2250/232 ,  F05D2260/31 ,  F05D2260/606 ,  F05D2300/603

Abstract: The invention relates to an assembly for a turbomachine with a longitudinal axis comprising a first annular wall (24), panels (38) being arranged around the longitudinal axis (A) and extending radially opposite said first annular wall (24) so as to form a flow surface for a flow of air, each panel (38) being secured to the first annular wall (24) by at least one fixing member (72) passing through an orifice in the panel (38) and secured to the first annular wall (24) by means of a sleeve and a stud forming a spacer.