Virtual multi-stream gas turbine engine
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United States of America Patent
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May 1, 2018
Issued Date -
N/A
app pub date -
Jan 23, 2015
filing date -
Jan 24, 2014
priority date (Note) -
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Abstract
A gas turbine engine is provided that includes a core flow path to direct a core stream flow. A common flow path is outboard of the core flow path, where the common flow path directs both a second stream flow and a third stream flow. Another gas turbine engine is provided that includes an outer case structure around a central longitudinal engine axis. An intermediate case structure is inboard of the outer case structure, where the intermediate case structure and the outer case structure direct both a third stream flow and a second stream flow. An inner case structure is inboard of the intermediate case structure, where the inner case structure and the intermediate case structure direct a core stream flow.
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