Cross beam rotor

Fluid reaction surfaces (i.e. – impellers) – Articulated – resiliently mounted or self-shifting impeller... – Nonmetallic resilient mounting

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

416141, B64C 2738

Patent

active

042995388

ABSTRACT:
A helicopter rotor having an even number of articulated blades wherein opposing blades are interconnected by a common spar passing across the rotor axis. Pitch change is introduced to the blade at the spar-blade attachment joint through a torque member connected at its outboard end to the blade joint and including a control horn at its inner end to receive pitch inputs. Drive for the rotor and support for each blade is provided by a spherical bearing directly connecting the torque member to the blade associated hub arm.

REFERENCES:
patent: 3231222 (1966-01-01), Scheutzow
patent: 3885887 (1975-05-01), Desjardins
patent: 4053258 (1977-10-01), Mouille
patent: 4087203 (1978-05-01), Ferris
patent: 4093400 (1978-06-01), Rybicki
patent: 4104003 (1978-08-01), Mouille

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

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

Rate now

     

Profile ID: LFUS-PAI-O-2360566

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