Method of lost-wax manufacture of an annular bladed turbomachine assembly, metal mould and wax model for implementing such a method

1. A method of manufacture of a wax model of an annular bladed turbomachine stator assembly for manufacture of a mould of this bladed assembly, the model including two coaxial shrouds, respectively radially internal and radially external, which shrouds are connected to one another by multiple blades, at least one of which includes an internal cavity, the method comprising:

using a metal mould having roughly a shape to be given to the model of an annular bladed assembly;

positioning of a core, intended to form an impression of the cavity, in a portion of the metal mould which defines the blade including the cavity, the core including a generally lengthened shape with a radially external end assembled on the metal mould;

injecting a wax in the metal mould fitted with the core; and

after the wax has cooled, removing the resulting wax model, fitted with the core, from the mould,

wherein the core is manufactured in metal, and is positioned such that its radially internal end is housed in the portion of the mould defining the blade including the cavity, not contacting the radially internal shroud portion of the mould.

2. The method according to claim 1 , wherein the metal core has a transverse section which tapers in the direction of its radially internal end.

3. A method of manufacture of an annular bladed turbomachine stator assembly including two coaxial shrouds, which are respectively radially internal and radially external, connected to one another by multiple blades at least one of which includes an internal cavity, the method comprising:

manufacturing a wax model of the bladed annular assembly, by the method according to claim 1 ;

manufacturing a mould in a refractory material by duplicate moulding of the wax model, followed by elimination of the wax;

casting a molten metal alloy in the mould made from a refractory material fitted with the core to form the bladed annular assembly;

after the metal alloy has cooled, removing the bladed annular assembly and eliminating the core.

4. The method according to claim 3 , further comprising:

before the manufacturing the mould in the refractory material, extracting the metal core out of the wax model, followed by positioning in the impression formed in the wax by the metal core of a core of the same shape manufactured in a ceramic material.

5. The method according to claim 4 , wherein the refractory material is a cement.

6. A metal mould for manufacture, by a method according to claim 1 , of a wax model of an annular bladed turbomachine stator assembly including two coaxial shrouds, respectively radially internal and radially external, the shrouds being connected to one another by multiple blades, at least one of which includes an internal cavity, the mould comprising:

a core of a generally lengthened shape having a radially external end assembled on the metal mould to form an impression of the cavity,

wherein the core is manufactured in metal, and is positioned such that its radially internal end is housed in a portion of the mould defining the blade including the cavity, not contacting a radially internal shroud portion of the mould.

7. A wax model for manufacture, by a method according to claim 3 , of an annular bladed turbomachine stator assembly including two coaxial shrouds, respectively radially internal and radially external, the shrouds being connected to one another by multiple blades, at least one of which includes an internal cavity, the model comprising:

a core of a generally lengthened shape having a radially external end protruding from the model, to form an impression of the cavity,

wherein the core is manufactured in metal, and is positioned such that its radially internal end is housed in a portion of the model defining the blade including the cavity, not contacting a radially internal shroud portion of the model.