Patent ID: 8544789

Claim:
A fixed wing aircraft, comprising: a fuselage having a longitudinal axis (X), a transverse axis (Y) and a vertical axis (Z); an airfoil comprising two fixed wings and a central casing; at least one laminated elastic link through which the airfoil is fastened to the fuselage, wherein the at least one laminated elastic link has a longitudinal axis (A), and the at least one laminated elastic link secures the airfoil to the fuselage in a configuration in which the longitudinal axis (A) of the at least one laminated elastic link extends along the transverse axis (Y) of the fuselage and provides translational movement between the airfoil and fuselage in the direction of the transverse axis (Y) of the fuselage; and wherein the at least one laminated elastic link is comprised of precompressed elastomer between two concentric tubes.