Fiber preform for a turbine ring sector, and its method of fabrication
View Patent ↗A fiber preform for a turbine ring sector obtained by three-dimensional weaving and including a base-forming first portion, two tab-forming L-shaped portions each presenting two branches, two ends of the first portion being extended by respective ones of the first branches, and a second portion connecting together the two tabs, first and second strips woven together forming the first branches, a first fraction of the thicknesses of the second branches, and the first portion, there being a non-linked zone between them that is situated in the first branches and in the first portion, and a third woven strip forming the second portion and a second fraction of the thickness of the second branches of each of the tabs.
1. A fiber preform for a turbine ring sector, the preform being obtained by three-dimensional weaving and comprising:
a base-forming first portion;
two tab-forming L-shaped portions forming tabs each presenting a first branch and a second branch, two ends of the first portion being extended by respective ones of the first branches, and a second portion connecting together the two tabs by a first connection formed between the second portion and one of the two tabs and a second connection formed between the second portion and the other of the two tabs, the second portion co-operating with the tabs and the first portion to define a cavity; and
first and second strips that are woven together forming the first branches, a first fraction of the thicknesses of the second branches, and the first portion, there being a non-interlinked zone between the first and second strips, the non-interlinked zone being situated in the first branches and in the first portion, and a third woven strip forming the second portion and a second fraction of the thickness of the second branches of each of the tabs,
wherein, in the non-interlinked zone, the first strip and the second strip are woven with independent weft yarns for each of the first and second strips.
2. A fiber preform according to claim 1 , wherein at least one of the first and second connections formed between the second portion and the two tabs is situated substantially between the corresponding first branch and second branch.
3. A fiber preform according to claim 1 , wherein at least one of the first and second connections formed between the second portion and the two tabs is a result of an assembly formed by the first and second strips and the third strip.
4. A fiber preform according to claim 1 , wherein at least one of the first and second connections formed between the second portion and the two tabs is formed by stitching.
5. A fiber preform according to claim 1 , wherein the second branch of each tab is formed by superposing a fraction of the assembly formed by the first and second strips and a fraction of the third strip.
6. A single-piece turbine ring sector made of ceramic matrix composite material formed by a preform according to claim 1 and metal strips arranged in the non-interlinked zone situated between the first strip and the second strip in the locations of the first portion and the first branches of the tabs.
7. A turbine ring assembly comprising:
a plurality of ring sectors according to claim 6 ; and
a ring support structure,
wherein the first fiber preform portions constitute an annular inner wall, the second fiber preform portions constitute an annular outer wall, and the ends of the second branches of the two tabs are engaged in respective housings of the ring support structure.
8. A single-piece turbine ring sector made of ceramic matrix composite material comprising a preform according to claim 1 .