Method for manufacturing a housing for a turbine engine and tools for the implementation thereof

A method for manufacturing a casing of an aircraft turbine engine, said casing comprising:

• an annular body extending around an axis (A) and made of a composite material comprising fibres woven and embedded in a resin, said body comprising an annular fastening flange extending radially outwards at each axial ends thereof, and
• an annular layer of abradable material arranged inside said body, and covering a first internal annular surface of an intermediate section of said body,
• the method comprising a step b) of bonding the layer to the first surface, during which the casing is heated and compressed by a system present at least partly inside the casing,
• the method further comprising, prior to the step b) of heating and compressing the casing, a step a) of mounting at least two shaping tools between the flanges, each of the tools being located in a circumferential area outside the body so as to exert bearing forces in opposite axial directions on these flanges.