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Summary:A separate inter-blade platform 1 for a bladed rotor disc of a turbo-machine comprises a first part 2 in the form of a generally trapezoidal shaped frame made of a laminated material, and having ends 5, 6 for location on the upstream and downstream sides respectively of the rotor disc, and two lateral sides 7, 8 for location between successive blades of the rotor, and a second part 3 made of a relatively flexible and self-adhesive material of the polyurethane type attached to the first part, the second part 3 defining a plate 4, a portion enclosing the two lateral sides 7, 8 of the frame and a plurality of reinforcing ribs 11 which are integral with said enclosing portion and the underside of the plate 4.
Bibliography:Application Number: GB19920012467