Gas turbine engine
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United States of America Patent
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-
Dec 26, 2023
Grant Date -
N/A
app pub date -
May 18, 2023
filing date -
May 20, 2022
priority date (Note) -
In Force
status (Latency Note)
Importance
Abstract
A gas turbine engine includes a core engine casing, a bypass duct and a core engine duct. The gas turbine engine further includes a plurality of flaps pivotally coupled to the core engine casing and arranged circumferentially around a principal rotational axis. Each flap extends from a first casing end and is configured to pivotally rotate relative to core engine casing about a pivot axis between a first position and a second position. In the first position, each flap is disposed in a circumferential direction and is radially disposed between a plurality of outlet guide vanes and a plurality of stator vanes. In the second position, each flap is inclined to the first position and extends at least partially into the bypass duct and the core engine duct.
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