Dynamic response modification and stress reduction in dovetail a

Fluid reaction surfaces (i.e. – impellers) – Specific working member mount – Blade received in well or slot

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

416219R, 416500, F01D 532

Patent

active

044809573

ABSTRACT:
A dovetail of a rotor blade is preferentially remove to thereby modify the support given to the root of a rotor blade. The modified support changes the vibrational characteristics of the rotor blade for reducing the tendency toward crack initiation. In one embodiment of the invention, one or more damping masses are fitted into the dovetail slot within the removed portion of the dovetail. The damping masses are loaded outward against the base of the rotor blade by centrifugal force and frictionally damp some of the vibrational energy of the rotor blade.

REFERENCES:
patent: 1229490 (1917-06-01), London
patent: 1699747 (1929-01-01), McKay
patent: 2686655 (1954-08-01), Schorner
patent: 2942843 (1960-06-01), Sampson
patent: 3292900 (1966-12-01), Pettersen
patent: 3385512 (1968-05-01), Bandukwalla
patent: 3689177 (1972-09-01), Klassen
patent: 3720480 (1973-03-01), Plowman et al.
patent: 3887298 (1975-06-01), Hess 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

Dynamic response modification and stress reduction in dovetail a does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Dynamic response modification and stress reduction in dovetail a, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Dynamic response modification and stress reduction in dovetail a will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-1040272

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