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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Bibliographic Details
Main Authors WALTHER RONALD S, SMITH PETER G, GUKEISEN ROBERT
Format Patent
LanguageEnglish
Published 14.10.2008
Subjects
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