Gas turbine engine with secondary air flow circuit
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United States of America Patent
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Jan 5, 2016
Grant Date -
Jul 5, 2012
app pub date -
Dec 28, 2011
filing date -
Dec 30, 2010
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Abstract
One embodiment of the present invention is a unique gas turbine engine. Another embodiment of the present invention is a gas turbine engine having a unique secondary air flow circuit. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for gas turbine engines and secondary air flow circuits. Further embodiments, forms, features, aspects, benefits, and advantages of the present application will become apparent from the description and figures provided herewith.
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