High-lift system for an aircraft with a main wing and an...

Details High-lift system for an aircraft with a main wing and an... High-lift system for an aircraft with a main wing and an...

B - Operations, Transporting

64

C

B64C 9/24 (2006.01) B64C 3/50 (2006.01)

Patent

CA 2710169

The invention relates to a lift system for an aircraft, comprising a main wing and a slat that can be adjusted in relation to said main wing, into various adjustable states, by means of an adjusting device thus forming a gap (5) between the rear side of the slat (1b) that faces the main wing and the main wing (2), the size of said gap being dependent on the adjusted state of the slat (1) in relation to the main wing (2). An air duct (11) comprising at least one inlet (20) and one outlet is formed inside the slat, said inlet (20) being arranged on the rear side (1b) facing the main wing, in order to influence the flow in the gap (5).

Système hypersustentateur pour un avion doté d'une aile principale et d'un volet de bord d'attaque réglable par rapport à cette aile dans différentes positions de réglage au moyen d'un dispositif de réglage, sachant qu'on obtient, entre l'aile principale (2) et le côté arrière (1b) dudit volet qui est tourné vers l'aile principale, un interstice (5) dont la taille est fonction de la position de réglage du volet de bord d'attaque (1) par rapport à l'aile principale (2). Un conduit de guidage d'air (11) doté d'au moins une admission (20) et d'une évacuation est formé à l'intérieur du volet de bord d'attaque. L'admission (20) est disposée sur le côté arrière (1b) tourné vers l'aile principale, afin d'influer sur l'écoulement dans l'interstice (5).

Affiliated with

Also associated with

Rating

High-lift system for an aircraft with a main wing and an... does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-1676640