Rolls-Royce Corporation

Rolls-Royce Deutschland Ltd & Co. Kg

Nicholas Robert Atkins

Knut Lehmann

Howard P Hodson

John Coull

Li He

Qiang Zhang

Manuel Herm

Adrian James White

Andrew P Wheeler

A turbine blade has a root portion, a platform and an aerofoil, the aerofoil is mounted on the platform and is formed by a pressure side wall and a suction side wall and has an outer surface, the pressure side wall and the suction side wall meet at a leading edge and a trailing edge, the aerofoil has an axial chord length, the suction side wall defines part of the radially outward surface of the aerofoil, the suction side wall defines an overhang, the overhang has a maximum overhang length that is between 5% and 20% of the axial chord length of the blade and is located between 5% and 50% of the suction surface length from the leading edge.

Turbine blade with tip overhang along suction side

An aerofoil structure for a rotating blade-row in a casing. The aerofoil structure includes a suction side, a pressure side and a tip therebetween. At least a portion of the tip includes a shaped feature provided on a surface of the tip. The shaped feature has a convergent portion orientated to reduce a gap between the tip and the casing in a direction from the pressure side to the suction side of the aerofoil structure.

Aerofoil structure

Growing community of inventors

Cambridge, United Kingdom

Nicholas Robert Atkins