Patent ID: 11913468
Assignee: COLLINS ENGINE NOZZLES, INC.
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F  Y | IPC F

Claim 0:
1. A method of making an impeller comprising:
additively manufacturing the impeller that includes:
a hub defining a rotational axis;
a shroud spaced apart from the hub along the rotational axis; and
a plurality of blades extending axially between the hub and the shroud;
wherein additively manufacturing the impeller includes building the impeller in a layer by layer process in a build direction along the rotational axis starting from a base of the hub, wherein the plurality of blades includes a plurality of perforated blades that support the shroud during additively manufacturing the impeller, wherein each of the perforated blades defines a perforated blade length and defines a plurality of columns spaced apart from one another along the perforated blade length, wherein each column includes a capital that tapers wide in a direction extending away from the respective base of the column, wherein each capital of each column of the plurality of perforated blades, together with primary blades, support the shroud such that a majority of a ceiling surface of the shroud that is opposite from the hub across the primary blades is defined by each capital of the plurality of columns and where the primary blades contact the shroud.