Acoustically swept rotor

Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Tined or irregular periphery

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416238, 415119, B64C 2746

Patent

active

041689399

ABSTRACT:
Impulsive noise reduction is provided in a rotor blade by "acoustically sweeping" the chord line from root to tip so that the acoustic radiation resulting from the summation of potential singularities used to model the flow about the blade tend to cancel for all times at an observation point in the acoustic far field.

REFERENCES:
patent: 1801216 (1931-04-01), Anderson
patent: 2043736 (1936-06-01), Charavay
patent: 2451106 (1948-10-01), Martin
patent: 2962260 (1960-11-01), Foley
patent: 3065933 (1962-11-01), Williams
patent: 3399731 (1968-09-01), Giles
patent: 3989406 (1976-11-01), Bliss
Aero Digest, vol. 63, No. 1, Jul. 1951, pp. 99-107.

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