Flap interconnect for deflection control
AssigneeThe Boeing Company
InventorsKevin R. Tsai, Kyle A. Johnson
Life of this patent
Estimating the term…
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AssigneeThe Boeing Company
InventorsKevin R. Tsai, Kyle A. Johnson
Estimating the term…
An aircraft wing has a flap arrangement with an inboard flap configured to move in a chordwise extension direction relative to the wing, the inboard flap having an outboard side, and an outboard flap adjacent to the inboard flap and configured to move in the chordwise extension direction relative to the wing, the outboard flap including an inboard side. A flap interconnect between the inboard flap and outboard flap has a roller mounted to a pin extending from the outboard side of the inboard flap and a guide track extending from the inboard side of the outboard flap. The guide track engages the roller on the inboard flap to limit deflection of the outboard flap relative to the inboard flap during movement of the inboard flap in the chordwise extension direction and movement of the outboard flap in the chordwise extension direction, to provide relative alignment of the inboard flap and outboard flap.
An aircraft wing having a flap arrangement comprising:
A flap interconnect between an inboard flap and an outboard flap, comprising:
A flap configuration for a wing comprising:
A method for engagement between an inboard flap and an outboard flap, said method comprising:
Dependencies are inferred from the claim text.