Auxiliary helicopter rotor

Fluid reaction surfaces (i.e. – impellers) – Articulated – resiliently mounted or self-shifting impeller... – Plural articulation

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

416123, 416138, B64C 2738

Patent

active

048284580

ABSTRACT:
An auxiliary helicopter rotor on which at least two blades extend radially from a hub, each of which blades presents a root connecting it to the hub, and a beam having two wings extending respectively along the back and face of the blade; the wings of the beam diverging along the root in such a manner as to form a fork engaged both by a center plate on the hub, to which the fork is connected via a spherical joint, and by a flexible leaf extending from the center plate inside the fork and connected to the beam of the blade by means of an axial joint.

REFERENCES:
patent: 2949967 (1960-08-01), Jovanovich
patent: 3942910 (1976-03-01), Snyder et al.
patent: 4129403 (1978-12-01), Watson
patent: 4135856 (1979-01-01), McGuire
patent: 4257739 (1981-03-01), Covington et al.
patent: 4342540 (1982-08-01), Lovera et al.

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

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

Rate now

     

Profile ID: LFUS-PAI-O-86475

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.