Turbine ring assembly
A turbine ring assembly includes both a plurality of ring sectors made of ceramic matrix composite material forming a turbine ring, and also a ring support structure. Each ring sector includes a portion forming an annular base with an inner face defining the inside space of the turbine ring and an outer face from which an attachment portion of the ring sector extends for attaching it to the ring support structure. The ring support structure includes two annular flanges between which the attachment portion of each ring sector is held. Each annular flange of the ring support structure presents at least one sloping portion bearing against the attachment portions of the ring sectors, the sloping portion, when observed in meridian section, forming a non-zero angle relative to the radial direction and relative to the axial direction.
1. A turbine ring assembly comprising:
a plurality of ring sectors made of ceramic matrix composite material forming a turbine ring; and
a ring support structure, each of the plurality of ring sectors having a portion forming an annular base with an inner face defining an inside space of the turbine ring and an outer face from which an attachment portion of each of the plurality of ring sectors extends for attaching each of the plurality of ring sectors to the ring support structure,
wherein the ring support structure comprises two annular flanges between which the attachment portion of each of the plurality of ring sectors is held, each of the two annular flanges of the ring support structure presenting a sloping portion bearing against the attachment portion of each of the plurality of ring sectors, said sloping portion, when observed in meridian section, forming a non-zero angle relative to a radial direction and relative to an axial direction, and
wherein the attachment portion of each of the plurality of ring sectors is held to the ring support structure by axial portions of the ring support structure each extending parallel to the axial direction, the axial portions being formed by a plurality of fitted elements engaged without clearance when cold through the two annular flanges.
2. The assembly according to claim 1 , wherein the attachment portion of each of the plurality of ring sectors is in a form of tabs extending radially.
3. The assembly according to claim 2 , wherein radially outer ends of the tabs do not come into contact and wherein the tabs of each of the plurality of ring sectors define therebetween an internal ventilation volume for each of the plurality of ring sectors.
4. The assembly according to claim 1 , wherein each of the plurality of ring sectors is of a section that is Ω-shaped or π-shaped.
5. A turbine engine including the turbine ring assembly according to claim 1 .
6. The assembly according to claim 1 , wherein one fitted element of the plurality of fitted elements include a peg passing through a first orifice provided in one of the two annular flanges and a second orifice provided in one ring sector of the plurality of sectors, the one of the two annular flanges being upstream of a second of the two annular flanges, and the first orifice being radially outward of the sloping portion of the one of the two annular flanges.