公开(公告)号：US11725822B2

公开(公告)日：2023-08-15

申请号：US16423953

申请日：2019-05-28

Applicant: SAFRAN AIRCRAFT ENGINES

Inventor： Romain Nicolas Lunel ,  Damien Bonnefoi ,  Christophe Pieussergues ,  Luc Namer ,  Dominique Raulin ,  Dan Ranjiv Joory ,  Benjamin Frantz Karl Villenave

IPC: F23R3/60 ,  F02C3/06 ,  F02C7/20 ,  F02C7/22 ,  F02C9/16 ,  F23R3/26 ,  F23R3/28

CPC classification number: F23R3/60 ,  F02C3/06 ,  F02C7/20 ,  F02C7/22 ,  F02C9/16 ,  F23R3/26 ,  F23R3/28 ,  F05D2220/323 ,  F05D2260/30

Abstract: The invention concerns a turbo engine comprising a combustion chamber (110) arranged inside the outer housing (112) and comprising an internal revolution wall (118) and an external revolution wall (116). First stop parts (54) and second stop parts (56) fixed respectively to the outer housing and to the combustion chamber are provided, the first and second stop parts being adapted to come to a substantially axial stop two by two by forming stop pairs (58).