GAS TURBINE ENGINE WITH COMPOSITE AIRFOIL AND PREFORM CORE
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United States of America
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Feb 13, 2025
app pub date -
Aug 10, 2023
filing date -
Aug 10, 2023
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Abstract
A gas turbine engine includes a fan section, a compressor section, combustion section, and turbine section in serial flow arrangement, that defining an engine centerline extending between a forward direction and an aft direction. A composite component, such as an airfoil, extends between a root and a tip, defining a span-wise direction therebetween, and between a leading edge and a trailing edge, defining a chord-wise direction therebetween. The composite component includes a preform core including a first set of fibers as a first set of warp fibers and a first set of weft fibers.
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