Rolls-royce Corporation

Peter A Evans

Geoffrey M Dailey

Andrew J Deighton

Pierre-Antoine J Sis

Richard A B McCall

A bladed rotor includes rotor disc having a peripheral region, and a plurality of rotor blades attached to and extending radially outwardly from peripheral region. Each rotor blade has a root portion which is located in a correspondingly shaped axially-extending slot provided in the peripheral region of rotor disc, and the root portion of each blade is axially retained in its respective slot by a plate located axially adjacent the root portion and rotor disc, and which extends circumferentially across respective slot. Retention plate is held in position by seal member having a first surface which engages radially-inwardly directed surface of rotor disc, and second surface which is located radially-outwardly of first surface and engages the retention plate. Seal member has a curved profile in radial cross-section so as to define a concavity located radially between first and second engaging surfaces and which is directed axially towards the rotor disc.

Bladed rotor for a gas turbine engine

A hollow cooled aerofoil blade (,) is provided with a central, lengthways extending plenum (,) and has pressure and suction flanks (,). The suction flank (,) has lengthways extending passages (,) therein that direct cooling air from the root region (,) into the central plenum (,). From the central plenum, the cooling air flows through a first set of apertures (,) into lengthways extending passages (,) in the pressure flank (,). The cooling air then flows through a second set of apertures (,) in the pressure flank to provide film cooling of the pressure flank (,) external surface.

Growing community of inventors

Derby, United Kingdom

Peter A Evans