Soft inplane helicopter rotor

Details Soft inplane helicopter rotor Soft inplane helicopter rotor

B - Operations, Transporting

64

C

244/15

B64C 27/48 (2006.01) B64C 27/35 (2006.01) B64C 27/43 (2006.01)

Patent

CA 1102772

SOFT INPLANE HELICOPTER ROTOR Abstract of the Disclosure The present invention relates to a helicopter rotor hub assembly in which a blade grip extends inboard of a yoke and transfers centrifugal forces to the yoke through a spherical elastomeric bearing. Pitch change of the grip and blade is accommodated by the spherical elastomeric bearing which also acts as the pivot point for lead-lag motion of the blade and grip. A lead-lag damper is located inboard of the elastomeric bearing and is connected between one end of the grip spaced away from the lead-lag pivot and the yoke for damping the lead-lag motion between the grip and yoke.

334233

Affiliated with

Also associated with

Rating

Soft inplane helicopter rotor does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-74810