A deburring method for a casting sand core 40 for removing burrs from a deburring target part 41 in the casting sand core 40 including the deburring target part 41, the deburring target part 41 being at least one of an opening and a cut-out part. The deburring method includes: inserting a bag 13 into the deburring target part 41 of the casting sand core 40; and inflating the bag 13 inserted into the deburring target part 41, and thereby pressing and breaking off burrs 42 formed on a peripheral surface of the deburring target part 41 by the inflated bag 13.

A mold surface repairing process, the process flow of which is as follows: first sand blastingdefect identificationrepairing weldingcoarse grindingsemi-finishing grindingfinishing grindingsecondary sand blastingmold heatingspray paint. The disclosure provides a combination of automatic equipment, special grinding tools and finishing grinding process, which ensures the quality and efficiency of the mold repair and reduces the labor force.

The use of a cementitious composition is described, as a coating for disposable foundry cores, said cementitious composition comprising at least one binder or hydraulic cement in a quantity ranging from 40% to 99.9% by weight with respect to the total weight of the cementitious composition; possibly one or more fillers in a quantity ranging from 0.1% to 60% by weight, with respect to the total weight of the cementitious composition, said filler preferably having a D99<100 m; at least one rheology modifying agent selected from cellulose, derivatives of cellulose such as methylhydroxyethylcellulose, vinyl acetate/versatate copolymers, polycarboxylate ether polymer, or a mixture thereof, in a quantity ranging from 0.1% to 5% by weight with respect to the total weight of the cementitious composition. A disposable foundry core is also described, having at least one coating layer based on said cementitious composition.

The use of a cementitious composition is described, as a coating for disposable foundry cores, said cementitious composition comprising at least one binder or hydraulic cement in a quantity ranging from 40% to 99.9% by weight with respect to the total weight of the cementitious composition; possibly one or more fillers in a quantity ranging from 0.1% to 60% by weight, with respect to the total weight of the cementitious composition, said filler preferably having a D99<100 m; at least one rheology modifying agent selected from cellulose, derivatives of cellulose such as methylhydroxyethylcellulose, vinyl acetate/versatate copolymers, polycarboxylate ether polymer, or a mixture thereof, in a quantity ranging from 0.1% to 5% by weight with respect to the total weight of the cementitious composition. A disposable foundry core is also described, having at least one coating layer based on said cementitious composition.

A deburring method for a casting sand core 40 for removing burrs from a deburring target part 41 in the casting sand core 40 including the deburring target part 41, the deburring target part 41 being at least one of an opening and a cut-out part. The deburring method includes: inserting a bag 13 into the deburring target part 41 of the casting sand core 40; and inflating the bag 13 inserted into the deburring target part 41, and thereby pressing and breaking off burrs 42 formed on a peripheral surface of the deburring target part 41 by the inflated bag 13.

A deburring method for a casting sand core 40 for removing burrs from a deburring target part 41 in the casting sand core 40 including the deburring target part 41, the deburring target part 41 being at least one of an opening and a cut-out part. The deburring method includes: inserting a bag 13 into the deburring target part 41 of the casting sand core 40; and inflating the bag 13 inserted into the deburring target part 41, and thereby pressing and breaking off burrs 42 formed on a peripheral surface of the deburring target part 41 by the inflated bag 13.

A core for use in casting an internal cooling circuit within a gas turbine engine component, the core including a core body with an outer skin in which a core body additively manufacturing binder is locally eliminated. A method of manufacturing a core for casting a component, including casting a core body for at least partially forming an internal passage architecture of a component; and forming an outer skin on the core body in which a core body binder is locally eliminated.

A core for use in casting an internal cooling circuit within a gas turbine engine component, the core including a core body with an outer skin in which a core body additively manufacturing binder is locally eliminated. A method of manufacturing a core for casting a component, including casting a core body for at least partially forming an internal passage architecture of a component; and forming an outer skin on the core body in which a core body binder is locally eliminated.

A method includes coating of one or more zones of the refractory alloy part, using a treatment composition including one or more types of preceramic polymer, a solvent and one or more active fillers, and heat treating the coated refractory alloy part, the heat treatment allowing to partially convert the preceramic polymer to form a ceramic layer, the active filler forming on a surface of the refractory alloy part, one or more ternary alloys and forming a continuous layer between the surface of the refractory alloy part and the ceramic layer obtained by conversion. The heat treatment forms a continuous layer of the ternary alloy. The treatment composition includes, relative to the total weight of the treatment composition, a weight proportion of between 40% and 66% of the one or more active fillers, and an active filler/preceramic polymer weight ratio is greater than or equal to 2.

A method for the manufacture of a component comprises the following steps, in sequence using an additive layer manufacturing process to build a three-dimensional net shape of the component; performing a first abrasive blasting operation on a region of a surface of the component; and performing a second abrasive blasting operation on the region. The angle of incidence of the abrasive on the surface in the first abrasive blasting operation is less than the angle of incidence of the abrasive on the surface in the second abrasive blasting operation.