Efficient trailing edge system for an aircraft wing

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

244215, 244216, B64C 920, B64C 2108

Patent

active

041204700

ABSTRACT:
A trailing edge system including spoilers and flaps in which the spoilers serve as both spoilers and as fairing surfaces which 1) maintain smooth upper wing surface contours for all flap positions and 2) enable relatively small, lighter weight flaps to have the effects of larger, heavier ones.

REFERENCES:
patent: 1422616 (1922-07-01), Page
patent: 2635837 (1953-04-01), Grant
patent: 3837601 (1974-09-01), Cole
patent: 3977630 (1976-08-01), Lewis et al.
patent: 3987983 (1976-10-01), Cole

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

Efficient trailing edge system for an aircraft wing does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

     

Profile ID: LFUS-PAI-O-372235

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