Turbine blade platform seal

Seal for a joint or juncture – Seal between relatively movable parts – Close proximity seal

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Details

416193A, 416248, 416500, F16J 1502, F01D 1102

Patent

active

059246995

ABSTRACT:
A seal for a turbine blade in a gas turbine engine has a sealing portion with two subportions, where the subportions are longitudinally offset from one another, so that the seal may provide sealing for adjacent turbine blades having longitudinally offset inner platform surfaces. The offset between the sealing subportions should correspond generally to the offset between the platform surfaces.

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