Back to results
US 5,848,765 AGranted
Reduced amplitude corrugated web spar
AssigneeThe Boeing Company
InventorTimothy E. Gillespie
Life of this patent
Estimating the term…
Abstract
A reduced amplitude corrugated web spar for use in airplane wings and the like is disclosed. The amplitude of the corrugation is determined based upon general stability requirements of the spar, and the fasteners are offset from the center line of the web corrugations. The resulting spar is easier to manufacture and still provides the structural integrity required of the wings.
Claims1
A corrugated web spar for use as a support structure in an airplane, comprising:
- a top flange;
- a bottom flange;
- a corrugated web extending between the top flange and the bottom flange, the corrugated web including corrugations having an amplitude which is substantially equivalent to a minimum amplitude required for a desired general stability for selected web spar depth, web thickness, and corrugation wave length, the corrugation wave length being determined by a desired fastener spacing for the corrugated web spar, and
- fasteners holes in the top and bottom flanges for attaching the skin of the airplane to the corrugated web spar, the fasteners holes being offset on the top and bottom flanges from the central plane of the corrugated web the minimum required distance so that the fasteners do not interfere with the web corrugations of the corrugated web spar and adjacent fasteners.
1 more element
Dependencies are inferred from the claim text.