Patent ID: 11946391
Assignee: GENERAL ELECTRIC COMPANY
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC F  B | IPC B  F

Claim 8:
9. The airfoil of claim 1, wherein the composite core defines a pressure sidewall camber distance and a suction sidewall camber distance, the pressure sidewall camber distance spans between the core leading edge and the core trailing edge along the pressure sidewall of the composite core and the suction sidewall camber distance spans between the core leading edge and the core trailing edge along the suction sidewall of the composite core, and
wherein the trailing wrap is wrapped around the core leading edge of the composite core such that trailing wrap extends from the core leading edge at least twenty percent of the pressure sidewall camber distance and from the core leading edge at least twenty percent of the suction sidewall camber distance.