Invention Grant
US07854586B2 Inlet guide vane inner air seal surge retaining mechanism 有权
进气导叶内空气密封浪涌保持机构

Inlet guide vane inner air seal surge retaining mechanism
Abstract:
An inner air seal carrier for use in a gas turbine engine having an inlet guide vane surge retainer comprises a body, a stationary sealing element and an outcropping. The body secures around an inlet guide vane inner diameter shroud. The stationary sealing element is disposed on a radially inward face of the body for engaging with a rotatable sealing element of a compressor rotor. The outcropping is positioned on the radially inward face of the body forward of the stationary sealing element for engaging with the surge retainer.
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