HOUSING FOR A GAS TURBINE, AIRCRAFT ENGINE, AND A PROCESS FOR OPERATING A GAS TURBINE

A housing for a gas turbine is disclosed. At least one wall element is housed on the housing so as to move, which limits a flow channel of the housing in the radial direction from a rotational axis of a rotor of the gas turbine toward the exterior. The housing includes at least one variably adjustab...

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Hauptverfasser: MALZACHER FRANZ, BOECK ALEXANDER
Format: Patent
Sprache:eng
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