Articulated helicopter rotor with an improved blade-to-hub...

Details Articulated helicopter rotor with an improved blade-to-hub... Articulated helicopter rotor with an improved blade-to-hub...

B - Operations, Transporting

64

C

B64C 27/35 (2006.01) B64C 27/33 (2006.01)

Patent

CA 2056190

Abstract of the Disclosure An articulated helicopter rotor with an improved blade-to-hub connection. An articulated helicopter rotor wherein the blade-to-hub connection consists of a spherical elastomeric bearing connected to the hub and a composite yoke connected thereto in series and consisting of a plurality of unidirectional high strength fibers bonded together to form a continuous strap which passes through a central opening in the elastomeric bearing and is pin-wrap connected to the hub at a single station and to the blade at two spaced stations so is to produce a construction which is light in weight, easy to manufacture, ballistically tolerant, redundant, and readily visually inspectable for structural integrity. S-4100 - 21 -

Affiliated with

Also associated with

Rating

Articulated helicopter rotor with an improved blade-to-hub... does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1713660