Method and control unit for controlling the play of a high-pressure turbine

A method for controlling the clearance between the blade tips of a high-pressure turbine of a gas turbine aircraft engine and a turbine shroud, including the controlling of a valve delivering a stream of air to the turbine shroud, this method further including the following steps: the detection of a...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Fraisse, Patrice, Lecordix, Jean-Loïc Hervé, Brusq, Tangi Rumon
Format: Patent
Sprache:eng
Schlagworte:
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