Rigid wing with variable sustentation due to deployment of a...

B - Operations – Transporting – 64 – C

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

B64C 3/54 (2006.01) B64C 31/028 (2006.01)

Patent

CA 2534404

The invention relates to a wing with variable sustentation for small aeroplanes or ULM planes, said wing being characterised in that it has a flexible wing system (3) that can be continuously deployed in the extension of the rigid wing (4) by means of at least one articulated system (5), and in that said flexible wing system (3) and said articulated system (5) are completely incorporated into the rear part of the rigid wing (4) in the configuration of a cruising flight.

La présente invention concerne une aile de portance variable pour petits avions ou ULM, caractérisée par le fait qu'elle comporte une voilure souple (3) déployable de manière continue dans le prolongement de l'aile rigide (4) au moyen d'au moins un système articulé (5) et par le fait que ladite voilure souple (3) et ledit système articulé (5) sont complètement incorporés dans la partie arrière de l'aile rigide (4) en configuration de vol de croisière.

LandOfFree

Say what you really think

Search LandOfFree.com for Canadian inventors and patents. Rate them and share your experience with other people.

Rating

Rigid wing with variable sustentation due to deployment of 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 Rigid wing with variable sustentation due to deployment of a..., we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Rigid wing with variable sustentation due to deployment of a... will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFCA-PAI-O-2050831

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