公开(公告)号：US20230340883A1

公开(公告)日：2023-10-26

申请号：US18254071

申请日：2021-11-08

Applicant: SAFRAN CERAMICS

Inventor： Clément Marie Benoît ROUSSILLE ,  Matthieu Arnaud GIMAT ,  Julien André Roger MATEO

IPC: F01D5/28 ,  D03D25/00 ,  D03D1/00 ,  D03D15/242 ,  D03D15/275 ,  C04B35/80 ,  F01D5/18

CPC classification number: F01D5/282 ,  D03D25/005 ,  D03D1/00 ,  D03D15/242 ,  D03D15/275 ,  C04B35/80 ,  F01D5/18 ,  D10B2505/02 ,  D10B2101/16 ,  C04B2235/5256 ,  F05D2300/6033 ,  F05D2230/50 ,  F05D2260/20

Abstract: A woven fibrous preform of a hollow aerodynamic profile of a turbomachine vane or blade, has a non-interlinked trailing edge and a draping of two 3D woven fibrous textures.

公开(公告)号：US20250100183A1

公开(公告)日：2025-03-27

申请号：US18852931

申请日：2023-03-28

Applicant: SAFRAN CERAMICS

Inventor： Nicolas EBERLING-FUX ,  Clément Marie Benoît ROUSSILLE ,  Mélissa BAZERQUE ,  Paul CARMINATI

IPC: B28B1/26 ,  B28B23/00 ,  C04B35/565

Abstract: A method for densifying a fibrous texture made of ceramic material with a ceramic matrix used in injection equipment including a mold cavity defined between a mold and a counter-mold, the mold cavity defining an internal space, and a membrane comprising a stiffened zone, the membrane being intended to be placed between a fibrous texture present in the mold cavity and the counter-mold, and the stiffened zone of the membrane having a Young's modulus greater than 200 GPa, the method including placing a predensified fibrous texture in the mold cavity, the predensified fibrous texture having corrugations on the surface and placing the membrane on the predensified fibrous texture in such a way that the stiffened zone of the membrane is in contact with the peaks of the corrugations of the predensified fibrous texture; closing the injection equipment, and densifying.

公开(公告)号：US20230399265A1

公开(公告)日：2023-12-14

申请号：US18257029

申请日：2021-12-08

Applicant: SAFRAN CERAMICS

Inventor： Arnaud DELEHOUZE ,  Eric BOUILLON ,  Gildas GARNIER ,  Clément Marie Benoît ROUSSILLE

IPC: C04B35/657 ,  C04B35/628 ,  C04B35/80 ,  F01D5/28

CPC classification number: C04B35/657 ,  C04B35/62844 ,  C04B35/80 ,  F01D5/282 ,  F05D2300/6033 ,  F05D2230/22 ,  C04B2235/5256 ,  C04B2235/616

Abstract: A method for manufacturing a turbomachine blade made of ceramic matrix composite component includes at least a structural part and a functional part secured to the structural part, the method including obtaining an assembly including a first preform of the functional part that is mounted on a second preform of the structural part or on the structural part, the first preform including a fibrous reinforcement of short fibres, and the second preform or the structural part comprising a woven fibrous reinforcement, and densification of the first preform of the assembly by infiltration with a molten composition.

公开(公告)号：US20230407814A1

公开(公告)日：2023-12-21

申请号：US18251965

申请日：2021-11-04

Applicant: SAFRAN CERAMICS

Inventor： Thomas VANDELLOS ,  Benoit CARRERE ,  Eric CONETE ,  Jean-Philippe JORET ,  Vincent DEVANLAY ,  Clément Marie Benoît ROUSSILLE

IPC: F02K1/04 ,  F02K1/82

CPC classification number: F02K1/04 ,  F02K1/827

Abstract: An assembly for a turbomachine with a longitudinal axis having an exhaust cone with an outer annular wall for the flow of a primary airflow and an annular box arranged radially inside the outer annular wall, an exhaust casing arranged upstream of and connected to the exhaust cone. One end of the outer annular wall or one end of the annular box may be free to move relative to and have no mechanical connection with the exhaust cone or the exhaust casing.

公开(公告)号：US20230191746A1

公开(公告)日：2023-06-22

申请号：US18012149

申请日：2021-06-23

Applicant: SAFRAN CERAMICS

Inventor： Matthieu Arnaud GIMAT ,  Julien André Roger MATEO ,  Clément Marie Benoît ROUSSILLE

IPC: B32B7/04 ,  B32B3/06 ,  B32B5/02

CPC classification number: B32B7/04 ,  B32B3/06 ,  B32B5/024 ,  B32B37/0038

Abstract: A method for manufacturing a turbine nozzle vane made of ceramic matrix composite material, wherein the vane is manufactured using a first fibrous preform including a hollow central section intended to form a fibrous reinforcement of an airfoil of the vane to be obtained, and a pair of second fibrous preforms each having an opening with a shape of the airfoil of the vane to be obtained.