Bicambered™ helicopter
rotor blade design features very high
angle of attack capabilities and
much higher lift coefficients with less
separation and blade stall than standard
rotor blade design and will revolutionize helicopter
transportation.
Helicopter
blade stall and rotor blade noise are significant
factors in helicopter operation. Recirculation
of air outside the rotor disk causes loss of
lift. All of these factors can be mitigated
with Bicambered™ blade
rotors.
Contact us today and
let us show you how our patented technology can
be implemented into the design of your helicopter
blade rotor application. Give us a call at 1-800-776-7357 or
complete our Contact Form for
more information. |
