Vane for a rotor arrangement for a gas turbine engine

摘要

A Vane for a Rotor Arrangement of a Gas Turbine engine A vane (20) for a rotor arrangement (14) of a gas turbine engine (10) comprises an aerofoil member (34) and a mounting member (23) from which the aerofoil member (34) extends. The mounting member (23) includes a sloped region (46, 62) to guide gas flowing over the mounting member (23) into a bleed arrangement (30). A vane assembly (19) and a rotor arrangement (14) comprising such vanes (20) are also disclosed.