Resources Contact Us Home
Flap interconnection system for aircraft

Image Number 8 for United States Patent #7546984.

Described is an interconnection system, in particular for flaps which are located side-by-side, on an aircraft wing, for example landing flaps or high-lift flaps. The interconnection system is in particular characterised in that it comprises a correspondingly guided compensating profile for a gap between the flaps, which gap changes when the flaps are moved. Preferably, the interconnection system is combined with a failsafe device for adjacent flaps in the form of a longitudinally adjustable interconnection strut which is connected to the adjacent flaps by way of corresponding load introduction fittings. The interconnection system is in particular suitable for large aircraft in which the gap between adjacent flaps, due to the relatively large lateral movement of the flaps during retraction and extension, becomes relatively wide, and the forces acting on the flaps are relatively great.

  Recently Added Patents
Coordinated multi-point transmission in a cellular network
Touch-sensitive device and communication device
Configurations and methods for effluent gas treatment
Multiplanar image displays and media formatted to provide 3D imagery without 3D glasses
Tire for motorcycle
Method for manufacturing a turbine engine vane
SMS transport resource control
  Randomly Featured Patents
Softener composition
Changeable configuration puzzle game
Machine tool
Dynamic mixer
System for speech recognition and correction, correction device and method for creating a lexicon of alternatives
Synthetic articles having a cork-like appearance
Self-positioning cabinet rail for a drawer guide
Mercury reduction system and method in combustion flue gas using staging
Inserting device of artificial blood stent