公开(公告)号：US12241377B2

公开(公告)日：2025-03-04

申请号：US17800067

申请日：2021-02-17

Applicant: SAFRAN AIRCRAFT ENGINES

Inventor： Christophe Lima

IPC: F01D17/14 ,  B64C11/32 ,  B64D27/10 ,  F01D9/04 ,  F01D17/16

Abstract: A turbomachine module with a longitudinal axis comprising an unducted propeller rotated about the longitudinal axis and at least one straightener. The module includes a plurality of unducted variable-pitch stator blades extending along a radial axis, perpendicular to the longitudinal axis, from a fixed casing. The module includes a first stator blade pitch-changing system. The pitch-changing system includes at least one first control that includes a first fixed body connected to the fixed casing and a first body which is axially mobile in relation to the first fixed body and at least one first joining mechanism joining each stator blade to the first mobile body of the first control. The first joining mechanism includes: a joining ring centered on the longitudinal axis, joined to the feet of each stator blade and at least one lever joined, on one hand, to the joining ring and, on the other hand, to the first mobile body of the first control.

公开(公告)号：US20230079110A1

公开(公告)日：2023-03-16

申请号：US17800067

申请日：2021-02-17

Applicant: SAFRAN AIRCRAFT ENGINES

Inventor： Christophe Lima

IPC: F01D17/14 ,  F01D9/04 ,  B64C11/32 ,  B64D27/10

Abstract: A turbomachine module with a longitudinal axis comprising an unducted propeller rotated about the longitudinal axis and at least one straightener. The module includes a plurality of unducted variable-pitch stator blades extending along a radial axis, perpendicular to the longitudinal axis, from a fixed casing. The module includes a first stator blade pitch-changing system. The pitch-changing system includes at least one first control that includes a first fixed body connected to the fixed casing and a first body which is axially mobile in relation to the first fixed body and at least one first joining mechanism joining each stator blade to the first mobile body of the first control. The first joining mechanism includes: a joining ring centered on the longitudinal axis, joined to the feet of each stator blade and at least one lever joined, on one hand, to the joining ring and, on the other hand, to the first mobile body of the first control.

公开(公告)号：US11585237B2

公开(公告)日：2023-02-21

申请号：US17275133

申请日：2019-09-03

Applicant: SAFRAN AIRCRAFT ENGINES

Inventor： Christophe Lima ,  Boucif Bensalah ,  Alain Dominique Gendraud ,  Alberto Martin Matos ,  Valentin Olivier Jean-Jacques Quesnel

IPC: F01D25/16 ,  F16C27/04 ,  F16C33/58 ,  F16C35/077 ,  F16C17/20

Abstract: A system for the axial retention of a holding ring for a bearing for guiding in rotation a rotary shaft of a turbomachine is disclosed. The system includes an annular bearing support and a bearing holding ring that is borne by the annular bearing support. The bearing holder ring includes an upstream ring configured to be brought into contact with the bearing support and a downstream ring that is elastically deformable. The bearing support has a first axial retention element, and the bearing holding ring has a second axial retention element. The first and second axial retention elements are configured to cooperate with one another to axially retain the bearing holding ring in the event of damage to the downstream ring.

公开(公告)号：US20220034237A1

公开(公告)日：2022-02-03

申请号：US17275133

申请日：2019-09-03

Applicant: SAFRAN AIRCRAFT ENGINES

Inventor： Christophe Lima ,  Boucif Bensalah ,  Alain Dominique Gendraud ,  Alberto Martin Matos ,  Valentin Olivier Jean-Jacques Quesnel

IPC: F01D25/16 ,  F16C19/52 ,  F16C27/04 ,  F16C33/58 ,  F16C35/077 ,  F16C17/20 ,  F16C19/22 ,  F16C27/02 ,  F16C35/02 ,  F16C39/02

Abstract: A system for the axial retention of a holding ring for a bearing for guiding in rotation a rotary shaft of a turbomachine is disclosed. The system includes an annular bearing support and a bearing holding ring that is borne by the annular bearing support. The bearing holder ring includes an upstream ring configured to be brought into contact with the bearing support and a downstream ring that is elastically deformable. The bearing support has a first axial retention element, and the bearing holding ring has a second axial retention element. The first and second axial retention elements are configured to cooperate with one another to axially retain the bearing holding ring in the event of damage to the downstream ring.