Airplane wing structure

Aeronautics and astronautics – Aircraft structure – Airfoil construction

Reexamination Certificate

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C244S123800

Reexamination Certificate

active

08056859

ABSTRACT:
A rib of an airplane wing is prevented from deforming due to a machining load when machining a rivet hole in parts where the rib and a skin are joined. With regard to a rib that provides a connection between first and second spars of the airplane wing, the rib is formed with mounting flanges secured to a skin via a rivet, a stringer through hole for a stringer to be positioned through, and first and second cutouts facing parts where the first and second spars and the skin are connected. Since reinforcing beads are formed along the mounting flanges and reinforcing flanges are formed so as to extend in the span direction from the edges of the stringer through hole and the first and second cutouts and be connected integrally to the mounting flanges, the stiffness of the rib toward a load in the vertical direction when drilling a rivet hole can be enhanced.

REFERENCES:
patent: 2483134 (1949-09-01), Gitz et al.
patent: 7740202 (2010-06-01), Namaizawa et al.
patent: 2004/0056152 (2004-03-01), Yamashita et al.
patent: 2000-506816 (2000-06-01), None
patent: 2002-302097 (2002-10-01), None

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