Joint for use in aircraft construction

Aeronautics and astronautics – Aircraft structure – Details

Reexamination Certificate

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Details

C244S131000, C244S123100

Reexamination Certificate

active

07909290

ABSTRACT:
A joint for use in aircraft construction, for example a wing, comprises: a cover skin having an interior surface, an exterior surface and a distal portion, said distal portion having an exterior-facing surface; and a butt-strap having a first portion for connection to the skin, said first portion having an interior surface, an exterior surface and a distal end. The first portion of the butt-strap is connected to the distal portion of the skin such that a junction is formed between the exterior surface of the skin and the exterior surface of the first portion of the butt-strap. The exterior-facing surface of the distal portion of the skin is of a shape complementary to the shape of the interior surface of the first portion of the butt-strap. The first portion of the butt-strap tapers towards its distal end such that, at said junction, the exterior surface of the skin and the exterior surface of the first portion of the butt-strap form a substantially continuous exterior surface.

REFERENCES:
patent: 4507011 (1985-03-01), Brown
patent: 5803406 (1998-09-01), Kolodziej et al.
patent: 6375120 (2002-04-01), Wolnek
patent: 7021856 (2006-04-01), Assler et al.
patent: 7296656 (2007-11-01), Sanicki et al.
patent: 2006/0032982 (2006-02-01), Stephens
patent: 2006/0251496 (2006-11-01), Wood et al.
patent: 2008/0164376 (2008-07-01), Kato et al.
patent: 2010/0006702 (2010-01-01), Fogarty et al.
patent: 2010/0065688 (2010-03-01), Wood
patent: 2010/0077690 (2010-04-01), Durand
patent: 704327 (1941-03-01), None
patent: 1022131 (1966-03-01), None
patent: 82/00313 (1982-02-01), None
GB Search Report for GB0525896.7 dated Apr. 5, 2006.
ISR for PCT/GB2006/004439 dated Mar. 16, 2007.

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