A leading edge structure for an aerofoil

Details A leading edge structure for an aerofoil A leading edge structure for an aerofoil

B - Operations, Transporting

64

C

B64C 3/50 (2006.01)

Patent

CA 2675127

A leading edge structure is disclosed for an aircraft wing in which a droop nose is articulated by a double hinge, in particular said leading edge structure comprising: a fixed leading edge structure (201); a movable leading edge structure (202) comprising a trailing edge, said movable leading edge structure being attached to said fixed leading edge structure by a first and second set of hinge arms (204,205); an actuator (210) arranged to act on said movable leading edge structure so as to move said movable leading edge structure betwen a deployed position and a stowed position relative to said fixed leading edge structure, wherein the stowed movable part provides the leading edge surface for the aerofoil, and said first and second hinge arms are arranged to hold said trailing edge of said movable leading edge structure adjacent said aerofoil surface of said fixed leading edge structure in said deployed and stowed positions and to maintain said trailing edge away from said aerofoil surface for a substantial part of said movement of said movable leading edge structure between said deployed and stowed positions.

L'invention concerne une structure de bord d'attaque pour une aile d'avion, dans laquelle structure un nez basculant est articulé par une double charnière.

Affiliated with

Also associated with

Rating

A leading edge structure for an aerofoil does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with A leading edge structure for an aerofoil, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and A leading edge structure for an aerofoil will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFCA-PAI-O-2044325