Rotor blade shaft integrity monitoring system

Fluid reaction surfaces (i.e. – impellers) – With measuring – testing – signalling or inspection means

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

416134A, 416226, B64C 2748

Patent

active

044391064

ABSTRACT:
A helicopter rotor blade to hub arm attachment configured to react centrifugal loads from the blade through a blade cuff, spindle, and elastomeric bearings utilizes a bolt in the bore of the spindle for secondary load path operation and a spindle integrity monitoring indicator to provide a visual showing of a deviation from the normal load path.

REFERENCES:
patent: 3547555 (1970-12-01), Jensen
patent: 3667862 (1972-06-01), Parr
patent: 3691820 (1972-09-01), Fiore
patent: 3942910 (1976-03-01), Snyder et al.
patent: 4203708 (1980-05-01), Rybicki
patent: 4264277 (1981-04-01), McCafferty
patent: 4373862 (1983-02-01), Ferris 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 shaft integrity monitoring system 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 shaft integrity monitoring system, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Rotor blade shaft integrity monitoring system will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-1752812

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