The Boeing Company
Vortex reduction apparatus for use with airfoils
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Abstract:
Vortex reduction apparatus for use with airfoils are disclosed. An example vortex reduction apparatus includes a housing to couple to a tip of an airfoil. The housing defines a volute fluid flow passageway between an inlet and an outlet. The volute fluid flow passageway is structured to induce a rotational fluid flow in a first rotational direction opposite a second rotational direction of a shed vortex induced at the tip of the airfoil during flight.
Status:
Grant
Type:
Utility
Filling date:
8 May 2019
Issue date:
26 Jul 2022