Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Radial flow devices
Patent
1977-11-11
1979-03-06
Powell, Jr., Everette A.
Fluid reaction surfaces (i.e., impellers)
Specific blade structure
Radial flow devices
416226, 416228, B64C 2746
Patent
active
041428374
ABSTRACT:
A helicopter blade of improved airfoil shape which reduces or eliminates retreating blade stall by reducing the magnitude of the upper airfoil blade surface peak pressure and distributes it over a greater chord section of the blade to thereby reduce flow separation and drag.
REFERENCES:
patent: 3728045 (1973-04-01), Balch
patent: 3822105 (1974-07-01), Jepson
patent: 3999888 (1976-12-01), Zincone
Hauschild Vernon F.
Powell Jr. Everette A.
United Technologies Corporation
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