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...
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Main Authors | , |
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Format | Patent |
Language | English |
Published |
05.03.2024
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Subjects | |
Online Access | Get full text |
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