Heat exchanger for gas turbine engine mounted in intermediate case
A gas turbine engine has a compressor section including a lower pressure compressor and a higher pressure compressor, and a turbine section. A core engine housing surrounds the compressor section and the turbine section. An outer intermediate housing wall defines an internal chamber between the core...
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Main Authors | , |
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Format | Patent |
Language | English |
Published |
20.04.2021
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Subjects | |
Online Access | Get full text |
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