Gas turbine engine assembly and methods of assembling same
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United States of America Patent
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Mar 30, 2010
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app pub date -
Oct 19, 2005
filing date -
Oct 19, 2005
priority date (Note) -
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Abstract
A method for assembling a gas turbine engine includes providing a core gas turbine engine including a high-pressure compressor, a combustor, and a turbine, and coupling a counter-rotating fan assembly to the core gas turbine engine such that air discharged from the counter-rotating fan assembly is channeled directly into an inlet of the gas turbine engine compressor.
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