Patent ID: 7887009
Filing Date: 2011-02-15
Classification: B64C

Abstract:
1. An aircraft comprising: a fuselage having a right side portion opposite a left side portion; a wing having a right wing portion extending outwardly from the right side portion of the fuselage and a left wing portion extending outwardly from the left side portion of the fuselage, wherein the right wing portion is fixedly attached to the left wing portion by a wing center section extending through at least a portion of the fuselage; a first pivotable link structurally attaching an upper portion of the wing center section to the right side portion of the fuselage; a second pivotable link structurally attaching the upper portion of the wing center section to the left side portion of the fuselage; and a third pivotable link structurally attaching a bottom portion of the wing center section to a longitudinal keel member of the fuselage.