TURBOFAN ENGINE WITH CORE EXHAUST AND BYPASS FLOW MIXING
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United States of America Patent
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Aug 26, 2021
app pub date -
Feb 20, 2020
filing date -
Feb 20, 2020
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Abstract
A gas turbine engine, the engine including a core turbine engine forming a core flowpath, a rotatable first stage blade assembly in which a bypass airflow passage is formed downstream of the first stage blade assembly, and a shroud positioned at the bypass airflow passage radially outward of the core turbine engine, wherein a first flowpath is formed outward of the shroud at which a first portion of air is flowed, and wherein the shroud and the core turbine engine form a second flowpath therebetween, the core flowpath in fluid communication with the second flowpath to flow a mixture of a second portion of air and combustion gases in the second flowpath.
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