Aircraft structure

Aeronautics and astronautics – Aircraft structure – Airfoil construction

Reexamination Certificate

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C244S123140, C244S132000

Reexamination Certificate

active

08070100

ABSTRACT:
An aircraft structure comprising: a spar; a primary cover attached to the spar and extending on a first side of the spar; and a secondary cover positioned on a second side of the spar and partially overlapping an internal surface of the primary cover. A bracket is attached to the spar, and a spacer is provided between the secondary cover and the bracket. The spacer is sized so that the primary and secondary covers together form a substantially continuous external aerodynamic surface. The structure provides an alternative to conventional butt-strap arrangements.

REFERENCES:
patent: 2164531 (1939-07-01), Lee
patent: 2334975 (1943-11-01), Williams
patent: 2742247 (1956-04-01), Lachmann
patent: 2774555 (1956-12-01), Crawford et al.
patent: 3716209 (1973-02-01), Pierce
patent: 4053124 (1977-10-01), Cole
patent: 4351502 (1982-09-01), Statkus
patent: 7770846 (2010-08-01), Perez Rodriguez et al.
patent: 7909290 (2011-03-01), Cooper
patent: 7992822 (2011-08-01), Kato et al.
patent: 2010/0077690 (2010-04-01), Durand
UK Search Report for Great Britain Application No. 0805963.6, dated Jul. 23, 2008.

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