GAS TURBINE FAN FAIRING PLATFORM AND METHOD OF FAIRING A ROOT LEADING EDGE OF A FAN BLADE OF A GAS TURBINE ENGINE

摘要

A gas turbine fan fairing platform (10) includes at least one body (14; 18) defining a surface (22) and having an opening (50) receptive to a blade (30), a protrusion (34) extending outwardly from the surface in a direction that will position the protrusion along a leading edge (38) near a root (42) of the blade.