INTER BLADE PLATFORM OF SIDE DEFLECTION TYPE FOR SUPPORTING BLADE OF TURBO JET ENGINE

摘要

PPROBLEM TO BE SOLVED: To provide an inter blade platform of a side deflection type for supporting blades of a turbo jet engine. PSOLUTION: The inter blade platform 3 for a blade supporting disc 1 of the turbo jet engine comprises a central portion 5 connected to the supporting disc 1 between two adjacent blades and two side portions 6, 7 extending from two side edges 6, 7 of the central portion 5 and so constructed that each of them is deflected by the impact of the blades 2 facing each other. PCOPYRIGHT: (C)2005,JPO&NCIPI