Transition shim between structure for fastening a wing to a...

Aeronautics and astronautics – Aircraft structure – Details

Reexamination Certificate

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Details

C244S119000

Reexamination Certificate

active

07607614

ABSTRACT:
A shim adapted for positioning on the upper surface of at least one wing of an aircraft. The shim restores an aerodynamic profile of the wing at the position of a zone of transition between structure fastening the wing to the fuselage of the aircraft and the upper surface of the aircraft. The shim enables a seal to run from the fastening structure to the upper surface of the wing, in eliminating the zones at which the seal may break open. An aircraft provided with such a shim is also disclosed.

REFERENCES:
patent: 3499622 (1970-03-01), Surcin et al.
patent: 4885885 (1989-12-01), Gottschling
patent: 6581877 (2003-06-01), Pauly
patent: 6655635 (2003-12-01), Maury et al.
patent: 2 827 029 (2003-01-01), None
patent: 1 225 511 (1971-03-01), None

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