Torsionally compliant helicopter rotor blade with improved...

Details Torsionally compliant helicopter rotor blade with improved... Torsionally compliant helicopter rotor blade with improved...

B - Operations, Transporting

64

C

244/120

B64C 27/35 (2006.01) B64C 27/46 (2006.01)

Patent

CA 1078357

TORSIONALLY COMPLIANT HELICOPTER ROTOR BLADE WITH IMPROVED STABILITY AND PERFORMANCE CHARACTERISTICS ABSTRACT OF THE DISCLOSURE A torsionally compliant helicopter rotor blade with maximum blade torsional flexibility at the blade tip portion and so shaped at the blade root portion that the locus of shear centers and the locus of centers of lift are sub- stantially coincident, and so shaped at the tip portion so that the locus of shear centers is selectively forward of the locus of centers of lift to establish an aerodynamic restoring moment in response to blade tip torsional excursions, thereby improving blade torsional stability. - 1 -

270512

Affiliated with

Also associated with

Rating

Torsionally compliant helicopter rotor blade with improved... does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Torsionally compliant helicopter rotor blade with improved..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Torsionally compliant helicopter rotor blade with improved... will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-551560