B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
244/120
B64C 27/46 (2006.01) B64C 27/467 (2006.01)
Patent
CA 1092581
IMPROVED HELICOPTER BLADE ABSTRACT OF THE DISCLOSURE 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. -1-
316033
Swabey Ogilvy Renault
United Technologies Corporation
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