| 摘要 |
Sealing arrangement between a stator assembly and a rotor (12) of a gas turbine engine, the rotor (12) being rotatable about an engine axis, the stator assembly comprising vanes (22) provided at their radially inner ends with a vane support structure (28) which comprises an annular platform (30) supporting the vanes and a radial flange (32) which extends radially inwardly from the platform, the sealing arrangement comprising an array of leaves (36) which extend inwardly from the radially inner periphery of the flange (32), towards a circumferential sealing surface (13) of the rotor (12).
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