Bleed diffuser for gas turbine engine
A gas turbine engine includes a compressor section, a combustion section communicating with and disposed downstream of the compressor section relative to a direction of airflow, and a gas turbine section communicating with and disposed downstream of the combustion section relative to a direction of...
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Main Authors | , , |
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Format | Patent |
Language | English |
Published |
14.10.2008
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Subjects | |
Online Access | Get full text |
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