Clearance control assembly

A clearance control assembly for a gas turbine engine that defines an axial direction and a radial direction and includes a stage of rotor blades and a shroud hanger. The assembly includes a case configured to be positioned outward along the radial direction from the stage of rotor blades when insta...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Packer, Travis J, Wallace, Thomas Ryan, Jendrix, Richard William, Hile, Michael Alan, Grooms, James Hamilton, Tracey, Bradford Alan, Fasig, David, Schimmels, Scott Alan
Format: Patent
Sprache:eng
Schlagworte:
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