Injection mold for a wax model of a turbine blade having an isostatic core holder
AssigneeSnecma
InventorsPatrick Pourfilet, Daniel Quach, Jean-Louis Martial Verger
Life of this patent
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AssigneeSnecma
InventorsPatrick Pourfilet, Daniel Quach, Jean-Louis Martial Verger
Estimating the term…
An injection mold producing a model of a turbine engine blade, including: a top surface that folds onto a bottom surface, both surfaces including long rods for supporting a core generating cooling cavities inside the blade, wherein the long rods of the bottom surface are configured to contact a first surface of the airfoil at bearing points, and the long rods of the top surface are configured to contact a second surface of the airfoil at clamping points; at least one short rod extending from one of the surfaces of the mold and pointing towards a false point located on one of the surfaces of the airfoil, the length of the short rod being shorter than the distance between the surface of the mold and the surface of the blade at the false point, and the difference between the length and the distance being equal to tolerance in relation to positioning of the false point in event of deformation of the core.
An injection mold for producing a model of a turbine engine blade to be produced by a lost wax casting technique, comprising:
Dependencies are inferred from the claim text.