LOCAL STIFFENING FOR GAS TURBINE ENGINE CASING
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United States of America
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Issued Date -
Jan 9, 2025
app pub date -
Aug 9, 2024
filing date -
Aug 9, 2024
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Abstract
A gas turbine engine under this disclosure could be said to include a compressor section, a combustor and a turbine section. At least one casing surrounds at least one of the compressor and turbine section. The at least one casing is formed of sheet metal, and has at least one potential peak displacement point due to vibration across a speed range of the at least one of the compressor and turbine section. A stiffening element is fixed to a wall of the casing at the at least one potential peak displacement point. A method is also disclosed.
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