EXHAUST DUCT FOR GAS TURBINE ENGINE
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United States of America Patent
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Issued Date -
Aug 1, 2024
app pub date -
Mar 1, 2024
filing date -
Jan 31, 2023
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Abstract
An exhaust duct of an aircraft engine includes an annular inlet conduit having an inlet central axis, and at least two outlet conduits in flow communication with the inlet conduit. The at least two outlet conduits are located non-parallel to the inlet central axis. Each of the at least two outlet conduits include an outlet port defining a distal end of each of the two outlet conduits. At least one of the outlet ports is non-circular in cross-sectional shape.
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