Patent ID: 11885234
Assignee: HONEYWELL INTERNATIONAL INC.
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F  B  Y | IPC F

Claim 17:
18. The method of claim 16, wherein the receiving, by the processor, the shape and location further comprises:
receiving, by the processor, a location of the first local vortex generator array on the shroud as between 0% chord to −10% chord in the chordwise direction at 100% span and up to 20% of a distance defined on the shroud from the pressure side of the at least one airfoil to an adjacent airfoil of the plurality of airfoils; and
receiving, by the processor, a location of the second local vortex generator array on the hub as between 0% chord to −10% chord in the chordwise direction at 0% span and up to 20% of a second distance defined on the hub from the pressure side of the at least one airfoil to the adjacent airfoil of the plurality of airfoils.