Bladed aircraft rotor with flexible blade mountings

Details Bladed aircraft rotor with flexible blade mountings Bladed aircraft rotor with flexible blade mountings

1987-03-27

1988-07-26

Powell, Jr., Everette A.

Fluid reaction surfaces (i.e., impellers)

Having positive means for impeller adjustment

Tiltable carrier

416102, 416134A, 416141, B64C 2740

Patent

active

047596899

ABSTRACT:
A two-bladed aircraft rotor is disclosed having blades mounted for freedom of blade motions, at least in the flapping sense and in the pitch-change sense, with the blades driven by flexible bellows.

REFERENCES:
patent: 2163893 (1939-06-01), Schairer
patent: 2961051 (1960-11-01), Wilford et al.
patent: 3080002 (1963-03-01), DuPont
patent: 3082826 (1963-03-01), Doman et al.
patent: 4203709 (1980-05-01), Watson
patent: 4266912 (1981-05-01), Roman
patent: 4297078 (1981-10-01), Martin
patent: 4323332 (1982-04-01), Fradenburgh
patent: 4326834 (1982-04-01), Ostrowski
patent: 4477225 (1984-10-01), Burkam
patent: 4502840 (1985-03-01), Roman
patent: 4566856 (1986-01-01), Miller
patent: 4575358 (1986-03-01), Ferris

Affiliated with

Also associated with

Rating

Bladed aircraft rotor with flexible blade mountings does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Bladed aircraft rotor with flexible blade mountings, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Bladed aircraft rotor with flexible blade mountings will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-255851