COOLING AIR FOR GAS TURBINE ENGINE WITH THERMALLY ISOLATED COOLING AIR DELIVERY

A gas turbine engine includes a plurality of rotating components housed within a compressor section and a turbine section. A first tap is connected to the compressor section and configured to deliver air at a first pressure. A heat exchanger is connected downstream of the first tap. A flowpath is de...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Schwarz, Frederick M, Snape, Nathan
Format: Patent
Sprache:eng
Schlagworte:
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