EXTERNAL CORE GAS TURBINE ENGINE ASSEMBLY
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United States of America Patent
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Issued Date -
Sep 3, 2015
app pub date -
Aug 13, 2014
filing date -
Aug 15, 2013
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Abstract
A gas turbine engine utilizes one or more gas generators having a core inlet flowpath and an exhaust outlet. Adjacently offset from the core gas generator, is a propulsor assembly. An exhaust outlet of the core gas generator is fluidly connected to the propulsor assembly and exhaust from the gas generator drives a fan drive turbine.
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