Module, useful in a mold for molding a part of an aircraft turbomachine or part for manufacture of turbomachine, comprises a module body defining a portion of a molding surface and a supporting device comprising orifices and two assemblies

摘要

The module comprises a module body (14) defining a portion (16a) of a molding surface (16) of the module, and a device (20) for supporting inserts to be integrated with a part of a turbomachine. The supporting device comprises orifices for the accommodation of the inserts in each of which one end of one of the inserts is designed to be introduced, and two assemblies having imprinted surfaces defining a portion of the orifices. The orifices are opened on a surface of the support device for forming an integral part of the molding surface. The module comprises a module body (14) defining a portion (16a) of a molding surface (16) of the module, and a device (20) for supporting inserts to be integrated with a part of a turbomachine. The supporting device comprises orifices for the accommodation of the inserts in each of which one end of one of the inserts is designed to be introduced, and two assemblies having imprinted surfaces defining a portion of the orifices. The orifices are opened on a surface of the support device for forming an integral part of the molding surface. The two assemblies are designed such that the assemblies are movable relative to each other in a closed position in which the imprinted surface forms the two portions of the orifices and in a release position. The supporting device is designed so as to be movable relative to each other when the assemblies occupy their closed position, and is rotatably mounted on the module body according to a first rotational axis (34). The two assemblies are rotatably mounted to each other according to a second rotation axis (38), and comprise a unit for blocking the inserts in the orifices. The first and second rotation axes are orthogonal, and are arranged in horizontal planes. The blocking unit is present in the form of a pressure member projecting into the orifices. The pressure member is coupled to an elastic return unit by forcing it to occupy a blocking position. The module further comprises a first locking unit for maintaining the module body and the support device in the molding position, and a second locking unit for maintaining the two assemblies in the closed position. An independent claim is included for a process for fabricating a part of an aircraft turbomachine or a part for the manufacture of the aircraft turbomachine by molding.