Rotor blade internal damper

Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Formed with main spar

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

416145, 416229R, 416500, B64C 2746

Patent

active

041881710

ABSTRACT:
A load absorbing elastic member or members is incorporated in the design of a rotor blade to assist in reducing flapwise and chordwise bending moments, torsional loading, and to reduce or eliminate the control system loads induced by rotor blade moment stall. In all its embodiments, the load absorbing elastic member has operatively associated therewith a constraining member which serves as a strain amplifier permitting the load absorbing elastic member to achieve its purpose effectively.

REFERENCES:
patent: 2568230 (1951-09-01), Gluhareff
patent: 2950766 (1960-08-01), Huber
patent: 2951542 (1960-09-01), Stulen et al.
patent: 2961053 (1960-11-01), Prewitt et al.
patent: 3168144 (1965-02-01), Capowich et al.
patent: 3217807 (1965-11-01), Underhill et al.
patent: 3484174 (1969-12-01), McCoubrey
patent: 3586460 (1971-06-01), Toner
patent: 3603701 (1971-09-01), Tarczynski
patent: 3645481 (1972-02-01), Purdy
patent: 3782856 (1974-01-01), Salkind 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

Rotor blade internal damper does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Rotor blade internal damper, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Rotor blade internal damper will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-1853306

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