Abstract: A metallic coating on a part made from a ceramic composite is obtained from a powder obtained by mixing two powders: namely,a base powder A comprising 2 to 5% of a reactive element Ti or Zr, at least one melting element B or Si in proportions ensuring a liquidus temperature between 1000.degree. C. and 1300.degree. C. and additional metallic elements including at least 50% Ni or Ni+Co;a powder B in a weight ratio of 5 to 30%, the elements of which are chosen to impart to the part particularly desired surface properties such as anti-wear, anti-oxidation and/or anti-corrosion, and to ensure a liquidus temperature of powder B greater than that of powder A.

Abstract: A hollow blade for a turboshaft engine, such as a fan rotor blade of large chord, is manufactured by a method in which primary components including two outer metal sheets and at least one intermediate sheet are hot formed so that the components are curved and twisted to a desired shape, diffusion barriers are formed at selected positions on the intermediate sheet, the shaped components are assembled and located on suitable process tooling, the assembled components are diffusion welded together, the welded assembly is internally pressurized by gas to inflate and superplastically deform selected areas to form a hollow in said assembly, and performing finishing operations on the hollow assembly to obtain the hollow blade.