Aircraft wing construction

Claim 1

AN AIRCRAFT WING COMPRISING A LONGITUDINALLY EXTENDING OUTER SHELL OF TRANSVERSE AIRFOIL CONFIGURATION INCLUDING UPPER AND LOWER WALLS, A PLURALITY OF TRANSVERSELY SPACED LONGITUDINALLY EXTENDING TRIANGULAR PRISMATIC INNER SHELLS DISPOSED IN SAID OUTER SHELL AND HAVING TRANSVERSELY SPACED SIDE WALLS, THE APICES OF DIFFERENT OF SAID PRISMATIC SHELLS BEING ALTERNATELY DIRECTED TOWARD SAID UPPER AND LOWER WALLS RESPECTIVELY AND THE BASES OF RESPECTIVE THEREOF BEING SPACED FROM AND CONFRONTING THE OPPOSITE OF SAID UPPER AND LOWER WALLS, AND A COHESIVE RIGID LIGHTWEIGHT CELLULAR CORE SUBSTANTIALLY FILLING THE SPACES DELINEATED BY THE OUTER FACES OF SAID PRISMATIC SHELLS AND THE INNER FACES OF SAID OUTER SHELL AND ADHERING THERETO TO DEFINE A TRUSS STRUCTURE FORMED OF TRIANGULAR SECTIONS CONSTITUTED OF SUBSTANTIALLY LINEAR ELEMENTS INCLUDING RESPECTIVE PAIRS OF SAID CONFRONTING WALLS AND BASE AND CORRESPONDINGLY SANDWICHED CELLULAR CORE SECTIONS.