Flexible closing device for a wing leading edge

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

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244130, B64C 350

Patent

active

050445804

ABSTRACT:
An aircraft wing leading arrangement includes a forward slat (10) movable between a stowed position and a deployed position in which a slot (13) is revealed. To prevent undesirable flow disturbances in the slot (13), a shutter device is provided for the aperture (22) in the leading edge through which the slat actuator mechanism (14) protrudes in the deployed position. This shutter device consists of a sprung (38) panel (30) of flexible material pivotally movable between aperture-blocking and aperture-unblocking positions.

REFERENCES:
patent: 2400322 (1946-05-01), Wheeler
patent: 4640477 (1987-02-01), Pace
patent: 4838502 (1989-06-01), Pinson
patent: 4848707 (1989-07-01), Britton
patent: 4951727 (1990-08-01), Bybee

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