초록 ▼

Axial flow fan propellers are provided with a roughened portion along the trailing edge of the fan blades on the pressure side of the blade to minimize tonal acoustic emissions generated by laminar boundary layer vortex shedding. The roughened portion may be provided by trip surfaces formed in the b

Axial flow fan propellers are provided with a roughened portion along the trailing edge of the fan blades on the pressure side of the blade to minimize tonal acoustic emissions generated by laminar boundary layer vortex shedding. The roughened portion may be provided by trip surfaces formed in the blades, by strips of abrasive material adhered to the blades along the trailing edges, respectively, by parallel or cross-hatched serrations in the blades or by upturned or offset trailing edges of the blades. The height of the roughened portion should be about equal to the boundary layer thickness of air flowing over the blade surfaces during operation of the fan. The fan propellers are particularly advantageous in heat exchanger applications, such as residential air conditioning system condenser units.

대표청구항 ▼

What is claimed is: 1. An air moving fan propeller having a hub and plural circumferentially spaced blades, each of said blades having a leading edge, a peripheral rim or tip and a trailing edge with respect to the direction of rotation, at least selected ones of said blades including a portion for

What is claimed is: 1. An air moving fan propeller having a hub and plural circumferentially spaced blades, each of said blades having a leading edge, a peripheral rim or tip and a trailing edge with respect to the direction of rotation, at least selected ones of said blades including a portion formed on a pressure side surface thereof, respectively, disposed adjacent said trailing edge of said selected ones of said blades, respectively, and extending generally from said peripheral tip inwardly toward said hub along said trailing edge and including projections extending into a boundary layer of air flowing over said surface of said blades, respectively, said projections extending over a major portion of said trailing edge of said blades, respectively, and from said trailing edge of said blades over at least 3% of the chordwise length of said blades, respectively, said projections being formed by plural, generally parallel alternate grooves and corresponding upturned sharp edges having a height above said surface at least equal to the thickness of said boundary layer, said thickness of said boundary layer being definable as (1.721��X)/Re1/2 wherein Re is the Reynolds number and X is the chordwise position on said blade from said leading edge, and said grooves and said sharp edges are formed by skiving said blades, respectively, and said grooves and said sharp edges extend along and substantially parallel to said trailing edge.