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
Electronic product design
Method for repairing or replacing damaged tissue
Memory device program window adjustment
Software execution management apparatus, method, and computer-readable medium thereof
Laser receiver for detecting a relative position
Maize variety hybrid X13A495
Auto-provisioning of network services over an Ethernet access link
  Randomly Featured Patents
Electric wiring system of a motor vehicle with replaceable cryptographic key and/or certificate
Occlusion apparatus, system, and method
Method and structure for nitride based laser diode arrays on an insulating substrate
Method for organizing the execution of electronically controlled switching processes
Superabrasive grain setting method
Article of protective clothing
Handle structure with a swingable curved grip element particularly for luggage containment means
Shift lever apparatus
Golf cleat