Turbine ring assembly that can be set while cold

A turbine ring assembly comprising:

• both a plurality of ring sectors made of ceramic matrix composite material together forming a turbine ring and also a ring support structure including first and second annular flanges, the ring support structure being made of a material having a coefficient of thermal expansion that is greater than the coefficient of thermal expansion of the ceramic matrix composite material of the ring sectors, each ring sector presenting in section on a plane defined by an axial direction (Da) and a radial direction (Dr) of the turbine ring a K-shape having a portion forming an annular base with, in the radial direction (Dr) of the turbine ring, an inside face defining the inside face of the turbine ring and an outside face from which there extend first and second S-shaped tabs, the tabs of each ring sector being held between the two annular flanges of the ring support structure;
• wherein the face of the first tab of each ring sector that faces inwards in the radial direction of the turbine ring rests on first and second holder elements secured to the first annular flange, the face of said first tab of each ring sector that faces outwards in the radial direction of the turbine ring being in contact with first and second clamping elements secured to the ring support structure, the first and second clamping elements respectively facing the first and second holder elements in the radial direction (Dr) of the turbine ring;
• and
• wherein the face of the second tab of each ring sector that faces inwards in the radial direction of the turbine ring rests on a third holder element secured to the second annular flange, the face of said second tab of each ring sector that faces outwards in the radial direction of the turbine ring being in contact with a third clamping element secured to the ring support structure, the third clamping element facing the third holder element in the radial direction (Dr) of the turbine ring.