Invention Grant
US08740554B2 Cover plate with interstage seal for a gas turbine engine 有权
用于燃气轮机的间隔板盖板

Cover plate with interstage seal for a gas turbine engine
Abstract:
An air seal assembly for a gas turbine engine includes a first cover plate with a radially extending knife edge seal defined about and axis of rotation. The first cover plate is mountable to a first rotor disk for rotation therewith, the first radially extending knife edge seal interfaces with a vane structure. A second cover plate with a second radially extending knife edge seal defined about the axis of rotation, the second cover plate mountable to the second rotor disk for rotation therewith. The second radially extending knife edge seal interfaces with the vane structure.
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