Lift augmentation system for aircraft

Aeronautics and astronautics – Aircraft – heavier-than-air – Airplane and fluid sustained

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

244 124, 244667, 244 23B, B64C 2900

Patent

active

052441679

ABSTRACT:
A lift augmentation system for aircraft which comprises a plurality of propellers parallel to an aircraft wing and inset parallel to and at the trailing edge of the wing. The propellers function to both directly produce vertical lift in the manner of helicopter blades and to augment air circulation over the wing to enhance lift produced by the wing. The propellers are set into the trailing edge of the wing along the length of the wing, with the inboard propellers preferably closely spaced to the fuselage to force air flow over the reducing taper of the fuselage. Each propeller is tiltable in all directions about a vertical axis through the propeller hub and the assembly of engine and propeller is hinged to the wing for pivoting in a plane substantially parallel to the aircraft axis.

REFERENCES:
patent: 1766844 (1930-06-01), Springer
patent: 1868832 (1932-07-01), Henter et al.
patent: 1987788 (1935-01-01), Morton
patent: 2415710 (1947-02-01), Smith
patent: 2963245 (1960-12-01), Bolton
patent: 3179354 (1965-04-01), Alvaresz-Calderon
patent: 3260477 (1966-07-01), Grahame
patent: 3284027 (1966-11-01), Mesniere
patent: 3372891 (1968-03-01), Malvestuto, Jr.
patent: 4828203 (1989-05-01), Clifton 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

Lift augmentation system for aircraft does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Lift augmentation system for aircraft, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Lift augmentation system for aircraft will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-2021653

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