Optimized Core for a Structural Assembly

摘要

The present application relates a core member for a core-stiffened structural assembly. The core member includes a plurality of cell members oriented a direction to provide a tailored stiffness in a certain direction. The core member can further include one or more planar members that can aid in shear transfer between cell members. The cell members can be made from bonding a plurality of corrugated layers together. The core-stiffened structure can be a rotor blade for an aircraft. In such an embodiment, the torsional stiffness of the rotor blade can be tailored in at least one of the chordwise and spanwise directions to provide tailor a torsional stiffness at any give location in the rotor blade.

主权项

1. A core-stiffened panel, the panel comprising:
a first face sheet; a second face sheet; a core configured provide stiffness to the panel, the core having a plurality of cell members, the core comprising a plurality of rows of cell members, including:
a first row of cell members, each cell in the first row of cell members being positioned at a first angle relative to a vertical direction;a second row of cell members adjacent to the first row of cell members, each cell in the second row of cell members being positioned at a second angle relative to a vertical direction, the second angle being symmetrical to the first angle;a third row of cell members separated from the second row of cell members by plural rows of cell members, each cell in the third row of cell members being positioned at a third angle relative to a vertical direction, the third angle being different from the first and second angles; anda fourth row of cell members, each cell in the fourth row of cell members being positioned at a fourth angle relative to a vertical direction, the fourth angle being symmetrical to the third angle.