Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Tined or irregular periphery
Patent
1977-09-08
1979-09-25
Powell, Jr., Everette A.
Fluid reaction surfaces (i.e., impellers)
Specific blade structure
Tined or irregular periphery
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.
Boxwell Donald A.
Schmitz Fredric H.
Vause C. Rande
Brekke Darrell G.
Manning John R.
McMillan Armand
Powell Jr. Everette A.
The United States of America as represented by the Administrator
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