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...

Full description

Saved in:
Bibliographic Details
Main Authors Schwarz, Frederick M, Snape, Nathan
Format Patent
LanguageEnglish
Published 05.03.2024
Subjects
Online AccessGet full text

Cover

Loading…