-
公开(公告)号:US10794189B2
公开(公告)日:2020-10-06
申请号:US16321263
申请日:2017-07-27
Applicant: SAFRAN AIRCRAFT ENGINES
Abstract: The invention relates to an assembly for a turbine engine extending about a longitudinal axis, comprising: a nose cone (20) comprising a conical body (22) extending about the longitudinal axis and a flange (23) comprising a first contact surface (24) forming an extension of an inner surface (25) of the conical body (22); a front shroud (21) comprising an overall annular body (26) extending about the longitudinal axis and a flange (27) comprising a first contact surface (28) forming an extension of an outer surface (29) of the annular body (26), the first contact surface (24) of the nose cone (20) being in contact with the first contact surface (28) of the front shroud (21), the first contact surfaces (24, 28) of the nose cone (20) and the front shroud (21) being tilted in the downstream direction towards the longitudinal axis, so that the flange (23) of the nose cone (20) is secured to the flange (27) of the front shroud (21); and attachment elements (30) configured to clamp the first contact surface (24) of the flange (23) of the nose cone (20) against the first contact surface (28) of the flange (27) of the front shroud (21).
-
公开(公告)号:US10156152B2
公开(公告)日:2018-12-18
申请号:US15549354
申请日:2016-02-09
Applicant: SAFRAN AIRCRAFT ENGINES
Inventor: Arnaud Michel Marie Accary , Alexandre Michel Henri Hasquenoph , Frédéric David Stéphane Rogues , Régis Eugène Henri Servant
Abstract: A nut for a turbine engine, in particular for axially locking a bearing race. The nut comprises a thread for screwing onto a part of the turbine engine, and a lock for ensuring the nut cannot rotate relative to the engine part. The nut further comprises at least one dynamic seal.
-
公开(公告)号:US20180016929A1
公开(公告)日:2018-01-18
申请号:US15549354
申请日:2016-02-09
Applicant: SAFRAN AIRCRAFT ENGINES
Inventor: Arnaud Michel Marie Accary , Alexandre Michel Henri Hasquenoph , Frédéric David Stéphane Rogues , Régis Eugène Henri Servant
CPC classification number: F01D11/02 , F01D25/00 , F01D25/162 , F01D25/183 , F02C7/00 , F05D2250/75 , F05D2260/31 , F16B33/004 , F16B39/10
Abstract: A nut for a turbine engine, in particular for axially locking a bearing race. The nut comprises a thread for screwing onto a part of the turbine engine, and a lock for ensuring the nut cannot rotate relative to the engine part. The nut further comprises at least one dynamic seal.
-
-